easa/jaa quick reference handbook
TRANSCRIPT
EMERGENCY EVACUATION
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In connection with the use of this document, Embraer does not provide any express or implied warranties and expressly disclaims any warranty of merchantability or fitness for a particular purpose.
Copyright © 2007 by Embraer S.A.. All rights reserved.
EASA/JAA
QUICK REFERENCE HANDBOOK THIS PUBLICATION CANCELS AND SUPERSEDES THE QRH–135/1569 DATED JUNE 25, 2002; REVISION 6 DATED MARCH 31, 2005.
QRH–135/1569-02 JULY 16, 2007
REVISION 10 – FEBRUARY 10, 2014
LIST OF EFFECTIVE PAGES
THE PORTION OF THE TEXT AFFECTED BY THE CHANGE IS INDICATED BY A VERTICAL LINE IN THE OUTER MARGIN OF THE PAGE.
ORIGINAL...................... 0.................. JUL 16, 2007 REVISION...................... 1.................AUG 31, 2007 REVISION...................... 2.................MAR 28, 2008 REVISION...................... 3.................AUG 29, 2008 REVISION...................... 4..................JUN 30, 2009 REVISION...................... 5................. DEC 23, 2009 REVISION...................... 6.................MAR 29, 2010 REVISION...................... 7................. OCT 10, 2010 REVISION...................... 8................. DEC 23, 2010 REVISION...................... 9..................JUN 10, 2011 REVISION..................... 10.................FEB 10, 2014
TOTAL NUMBER OF PAGES IN THIS PUBLICATION IS 244 CONSISTING OF THE FOLLOWING:
PAGE N° CHANGE N° PAGE N° CHANGE N°
* Asterisk indicates pages changed, added, or deleted by the current revision.
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* Title ..................................10 * A ......................................10 * B ......................................10 * C ......................................10 I ........................................7 EAP INTRO-1 ....................0 EAP INTRO-2 ....................1 EAP INTRO-3 ....................9 EAP INTRO-4 ....................9 S-1 ...................................0 S-2 ...................................0 S-3 ...................................7 S-4 ...................................4 S-4A ..................................4 S-4B ..................................4 S-5 ...................................0 S-6 ...................................0 S-7 ...................................0 S-8 ...................................0 S-9 ...................................0 S-10 ..................................0 S-11 ..................................0 S-12 ..................................0 NAP-1 ...............................8 NAP-2 ...............................8 * NAP-3 ..............................10 NAP-4 ...............................0 * NAP-5 ..............................10 NAP-6 ...............................8 NAP-7 ...............................4 * NAP-8 ..............................10 NAP-9 ...............................7 NAP-10 ..............................3 NAP-11 ..............................4 * NAP-12 .............................10 NAP-13 ..............................9 NAP-14 ..............................0 * NAP-15 .............................10
NAP-16 ..............................0 NAP-17 ..............................0 NAP-18 ..............................4 NAP-19 ..............................0 NAP-20 ..............................8 NAP-21 ..............................8 NAP-22 ..............................8 NAP-23 ..............................4 NAP-24 ..............................4 NAP-25 ..............................4 NAP-26 ..............................8 NAP-26A ............................5 NAP-26B ............................5 NAP-27 ..............................0 NAP-28 ..............................0 NAP-29 ..............................0 NAP-30 ..............................0 NAP-31 ..............................0 NAP-32 ..............................0 NAP-33 ..............................0 NAP-34 ..............................0 NAP-35 ..............................0 NAP-36 ..............................8 NAP-37 ..............................0 * NAP-38 .............................10 NAP-39 ..............................7 NAP-40 ..............................0 NAP-41 ..............................0 NAP-42 ..............................3 NAP-43 ..............................3 NAP-44 ..............................8 EAP0-1 ..............................9 EAP0-2 ..............................9 EAP0-3 ..............................9 EAP0-4 ..............................9 EAP0-5 ..............................9 EAP0-6 ..............................9 * EAP0-7 .............................10 * EAP0-8 .............................10 EAP1-1 ..............................0 EAP1-2 ..............................0
LIST OF EFFECTIVE PAGES
THE PORTION OF THE TEXT AFFECTED BY THE CHANGE IS INDICATED BY A VERTICAL LINE IN THE OUTER MARGIN OF THE PAGE. PAGE N° CHANGE N° PAGE N° CHANGE N°
* Asterisk indicates pages changed, added, or deleted by the current revision.
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EAP1-3 .............................. 0 EAP1-4 .............................. 0 EAP1-5 .............................. 0 EAP1-6 .............................. 9 EAP1-7 .............................. 0 EAP1-8 .............................. 0 * EAP1-9 ............................. 10 * EAP1-10........................... 10 EAP1-11............................ 5 EAP1-12............................ 5 EAP1-13............................ 5 EAP1-14............................ 4 EAP2-1 .............................. 0 EAP2-2 .............................. 0 EAP2-3 .............................. 8 EAP2-4 .............................. 0 EAP2-5 .............................. 0 EAP2-6 .............................. 0 EAP2-7 .............................. 4 * EAP2-8 ............................. 10 * EAP2-9 ............................. 10 EAP2-10............................ 0 EAP2-11............................ 0 EAP2-12............................ 0 EAP2-13............................ 2 EAP2-14............................ 0 EAP3-1 .............................. 0 EAP3-2 .............................. 0 EAP3-3 .............................. 0 EAP3-4 .............................. 0 EAP3-5 .............................. 0 EAP3-6 .............................. 0 EAP4-1 .............................. 0 EAP4-2 .............................. 0 * EAP4-3 ............................. 10 EAP4-4 .............................. 0 EAP4-5 .............................. 0 EAP4-6 .............................. 0 EAP5-1 .............................. 0 EAP5-2 .............................. 0 EAP5-3 .............................. 9 EAP5-4 .............................. 0 EAP5-5 .............................. 8 EAP5-6 .............................. 0 EAP5-7 .............................. 4 * EAP5-8 ............................. 10 * EAP5-9 ............................. 10 EAP5-10............................ 4 EAP5-11............................ 4 EAP5-12............................ 0 EAP5-13............................ 9 EAP5-14............................ 9 EAP5-15............................ 9 EAP5-16............................ 9 EAP6-1 .............................. 9 EAP6-2 .............................. 9 EAP6-3 .............................. 9 EAP6-4 .............................. 9
* EAP6-5 ............................. 10 EAP6-6 .............................. 9 * EAP6-7 ............................. 10 * EAP6-8 ............................. 10 EAP6-9 .............................. 9 EAP6-10 ............................ 9 EAP6-11 ............................ 9 EAP6-12 ............................ 9 EAP6-13 ............................ 9 EAP6-14 ............................ 9 EAP7-1 .............................. 0 EAP7-2 .............................. 0 EAP7-3 .............................. 0 EAP7-4 .............................. 0 EAP7-5 .............................. 0 EAP7-6 .............................. 0 EAP8-1 .............................. 0 EAP8-2 .............................. 0 EAP8-3 .............................. 0 EAP8-4 .............................. 0 EAP8-5 .............................. 0 EAP8-6 .............................. 8 * EAP8-7 ............................. 10 EAP8-8 .............................. 0 EAP8-9 .............................. 0 EAP8-10 ............................ 0 EAP8-11 ............................ 0 EAP8-12 ............................ 0 EAP9-1 .............................. 9 EAP9-2 .............................. 9 EAP9-3 .............................. 9 EAP9-4 .............................. 9 EAP9-5 .............................. 9 * EAP9-6 ............................. 10 EAP9-7 .............................. 9 EAP9-8 .............................. 9 EAP9-9 .............................. 9 EAP9-10 ............................ 9 EAP9-11 ............................ 9 EAP9-12 ............................ 9 EAP9-13 ............................ 9 EAP9-14 ............................ 9 EAP9-15 ............................ 9 EAP9-16 ............................ 9 EAP10-1 ............................ 0 EAP10-2 ............................ 0 * EAP10-3 ........................... 10 EAP10-4 ............................ 4 EAP10-5 ............................ 0 EAP10-6 ............................ 0 EAP10-7 ............................ 0 EAP10-8 ............................ 9 EAP10-9 ............................ 0 EAP10-10 .......................... 0 EAP11-1 ............................ 0 EAP11-2 ............................ 0 EAP11-3 ............................ 0 EAP11-4 ............................ 4
LIST OF EFFECTIVE PAGES
THE PORTION OF THE TEXT AFFECTED BY THE CHANGE IS INDICATED BY A VERTICAL LINE IN THE OUTER MARGIN OF THE PAGE. PAGE N° CHANGE N° PAGE N° CHANGE N°
* Asterisk indicates pages changed, added, or deleted by the current revision.
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EAP11-5.............................0 EAP11-6.............................0 * EAP11-7............................10 EAP11-8.............................4 EAP12-1.............................0 EAP12-2.............................0 EAP12-3.............................4 EAP12-4.............................0 EAP12-5.............................0 EAP12-6.............................0 EAP12-7.............................0 EAP12-8.............................4 * EAP12-9............................10 EAP12-10...........................0 EAP13-1.............................0 EAP13-2.............................0 EAP13-3.............................0 EAP13-4.............................0 EAP14-1.............................9 EAP14-2.............................4 EAP14-3.............................4 * EAP14-4............................10 EAP14-5.............................4 * EAP14-6............................10 EAP14-7.............................4 EAP14-8.............................4 PD-1 .................................5 PD-2 .................................7 PD-2A ................................5 PD-2B ................................5 PD-3 .................................0 PD-4 .................................0 PD-5 .................................0 PD-6 .................................0 PD-7 .................................0 PD-8 .................................0 PD-9 .................................0 PD-10 ...............................0 PD-11 ...............................7 PD-12 ...............................7 PD-13 ...............................7 PD-14 ...............................7 PD-15 ...............................7 PD-16 ...............................7 APP-1 ...............................0 APP-2 ...............................4
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APPLICABILITY
This handbook is applicable to the Legacy 600 model.
NOTE: The Legacy 600 model has the certification designation of EMB-135 BJ.
The procedures contained in this handbook have been developed by the manufacturer for use during the operation of the Legacy 600. These procedures are provided as guidance and should not be construed as prohibiting the development of equivalent procedures.
The use of the on board checklist is based on the assumption that both pilots have been properly trained on the type of airplane and, therefore, have a thorough knowledge of the airplane’s systems and procedures.
It further assumes that they know the consequences of not performing the right actions at the right time.
In case of conflicting information between this handbook and the AFM-135/1541, the AFM must prevail.
EMERGENCY/ABNORMAL PROCEDURES
ORIGINAL EAP INTRO-1
INTRODUCTION The Emergency/Abnormal Procedures published in the Quick Reference Handbook (QRH) are provided to pilots as quick guide to minimize the consequences of emergency and abnormal situations that might occur during the airplane operation.
In case a discrepancy is found between the QRH and the approved Airplane Flight Manual (AFM), the AFM shall prevail.
Using the QRH requires proper training on the execution of all operational, emergency and abnormal procedures set forth in the AFM and a thorough knowledge of airplane systems.
The procedures set forth herein also require situational awareness for identification of emergency or abnormal situations and pilot skills to guarantee safety. The Emergency Evacuation procedure accomplishment may be necessary in many situations and its need is at pilot’s discretion.
It is EMBRAER recommendation that any unusual situation encountered should be reported as quickly as possible to Flight Operations and Maintenance Personnel.
Three blocks of procedures are contained in this manual:
Smoke Procedures: address all annunciated and non annunciated smoke related procedures.
Non Annunciated Procedures: procedures that are not related to an EICAS message but rather to a condition present in the airplane. The Checklists are arranged in alphabetical order with Emergency Checklists (black label) first, followed by Abnormal Checklists (gray label).
Annunciated Procedures: procedures related to an EICAS message. These procedures are grouped by system and the system tabs are in alphabetical order. Each title procedure is followed by the corresponding EICAS message identification. The message provided for each procedure represents the root cause of the failure. The Checklists for each System Tab are first arranged with the Procedures that are related to Warning messages (red label) followed by the Procedures related to Caution messages (amber label) and then followed by the Procedures related to Advisory messages (blue label), therefore arranged in Procedure’s title alphabetical order.
EMERGENCY/ABNORMAL PROCEDURES
EAP INTRO-2 REVISION 1
The emergency evacuation procedure is repeated in the last page of QRH, after Performance Data helping pilots to quickly get to this procedure.
Some procedures can either be annunciated or non annunciated. In this case, the procedures are presented in the Annunciated block but are referenced in the Non Annunciated index.
In each Annunciated System Tab Index, the related non annunciated procedures are presented with a cross-reference to the Non Annunciated Tab page. The Non Annunciated procedures index is classified into Emergency and Abnormal procedures, while both the Annunciated procedures index and EICAS Messages List are classified into Warning, Caution and Advisory.
Some EICAS messages do not have an associated QRH procedure. In these cases, “Crew Awareness” identifies the EICAS message as noted in the Index Table. If a Crew Awareness message is displayed on the EICAS, takeoff is prohibited, unless at least one of the following conditions is met:
- The message is an expected result of an intentional operation;
- Flight crew action is taken to clear the message; - Maintenance personnel take action to clear the
message; - The airplane is dispatched in accordance with
all approved company MEL provisions.
If one of the following Crew Awareness messages is presented after gate departure, the flight may continue only to the intended destination without further action:
- AHRS BASIC MODE, - DU 1 (2, 3, 4) FAN FAIL, - E1 (2) OIL IMP BYP, - ENG A/ICEOVERPRES, - IC 1 (2) FAN FAIL or - GEN 1 (2, 3, 4) BRG FAIL.
Some procedures include a characterization below the title if a relevant emergency/abnormal condition is present. Aural warnings, lights, EICAS indications, flight instrument flags or airplane condition can, itself or associated among themselves, characterize an emergency/abnormal situation.
The actions inside bold rectangular borderlines are recall items. They must be performed expeditiously, by memory.
EMERGENCY/ABNORMAL PROCEDURES
REVISION 9 EAP INTRO-3
Flying the airplane is always the priority in any emergency/abnormal situation. Checklists should be called after the flight path is under control, critical phases of flight (such as takeoff and landing) have ended and all recall items have been accomplished.
Some emergency and abnormal situations require landing at the nearest suitable airport. This statement will be listed at the beginning of a task checklist to give the crew proper time to plan the landing. Also, as an aid for planning the diversion airport, the landing distance correction factor will be presented together with the “Land at nearest suitable airport” statement.
Some procedures contain “Lists of Relevant Inoperative Items” for that particular condition. Those lists presents only the most relevant items and for the full list, the AOM should be consulted. As SMOKE events are very time critical, on those procedures the lists contain only items that significantly affect airplane performance and/or controllability. For the entire list of relevant inoperative items on those conditions, the pilot can refer to the procedures associated with the electrical busses off.
Throughout this manual, a text followed by “()” means that either condition applies. A text followed by “-” means that both conditions apply simultaneously.
Some procedures require cabin depressurization. This will require either dumping the cabin air or the using manual control to accomplish this task. In this situation, manual control depressurization is the recommended method to be used for passenger comfort and should be done by setting the pressurization mode selector to MAN position and smoothly setting the controller to FULL UP position. When a specific method for cabin depressurization is required, the procedure will clearly state it.
The procedures contained herein assume that:
Airplane systems were operating normally prior to the failure.
All emergency/abnormal actions are performed in the order they are listed in the procedure.
Normal procedures have been properly performed.
Aural warnings are silenced as necessary. Master Warning/Caution lights are reset as soon as the failure is recognized.
EMERGENCY/ABNORMAL PROCEDURES
EAP INTRO-4 REVISION 9
All procedures are self-contained. All other messages that may be generated by a single failure do not require that the procedures associated to those messages are accomplished in addition to the procedure addressing the root cause.
Circuit breakers must not be pushed in if they pop up.
All assigned tasks in the procedures have the indication END at the completion of each assigned task. No task is over until ……… has been reached. Upon completion of the checklist the reading pilot should state: “(Procedure Title) Checklist Complete”. In the event of multiple failures (excluding cascade failures) with different landing configuration and/or landing distance correction factors, the crew should use good judgment to determine the safest action.
According to the QRH philosophy, Rejected Takeoff (at or below V1) procedure is not considered in this manual. Indeed, should the flight crew decide to reject the takeoff; they will do it by memory, not by referring to the QRH. Consequently, Rejected Takeoff (at or below V1) procedure is a matter of flight crew training and is considered within the Standard Operating Procedures Manual, which contains the complete guidance to accomplish it.
END
EMERGENCY/ABNORMAL PROCEDURES
Smoke
ORIGINAL S-1
TABLE OF CONTENTS
BAGGAGE SMOKE................... S-3
LAVATORY SMOKE.................. S-3
AIR CONDITIONING SMOKE.... S-4
CABIN FIRE OR SMOKE .......... S-5
ELECTRICAL SYSTEM FIRE OR SMOKE....................... S-6
SMOKE EVACUATION.............. S-11
EMERGENCY/ABNORMAL PROCEDURES
Smoke
S-2 ORIGINAL
LIST OF EICAS MESSAGES
BAGG SMOKE...........................S-3
LAV SMOKE ..............................S-3
EMERGENCY/ABNORMAL PROCEDURES
Smoke
REVISION 7 S-3
BAGGAGE SMOKE
EICAS Warning: BAGG SMOKE
EICAS Caution BAGG ACCESS OPN......NOT DISPLAYED
Fire Extg Bagg Button (if installed) .........PUSH IN
LAND AT THE NEAREST SUITABLE AIRPORT. Altitude ..............................MAINTAIN
Delay the descent as long as possible.
NOTE: Advise Ground Crew of possible Halon vapors approximately 75 minutes after discharging fire extinguishing bottle.
LAVATORY SMOKE
EICAS Warning: LAV SMOKE (may be presented).
Lavatory Light CB (Located in Line E) ........... PULL
Lavatory Flush CB's (Located in Line E or Cabin Entertainment Panel)... PULL
CABIN FIRE OR SMOKE Procedure (S-5)......... AS REQUIRED
END
END
EMERGENCY/ABNORMAL PROCEDURES
Smoke
S-4 REVISION 4
AIR CONDITIONING SMOKE Condition: Smoke or odor inside the
cabin and/or cockpit.
Crew Oxygen Masks ....DON, 100% Smoke Goggles............DON Recirculation Fan.........PUSH OUT Crew Communication ..ESTABLISH
LAND AT THE NEAREST SUITABLE AIRPORT. XBleed...........................OPEN Suspected Bleed(s)......PUSH OUT Altitude..........................MAX 25’000 FT
MIN MEA No
Yes Suspected Pack .......... PUSH OUT Suspected Bleed ......... PUSH IN No
Yes Suspected Pack .......... PUSH IN Opposite Bleed............ PUSH OUT
No
Yes Opposite Bleed............ PUSH IN Opposite Pack ............. PUSH OUT
CONTINUES ON NEXT PAGE
SMOKE PERSISTS?
SMOKE PERSISTS?
SMOKE PERSISTS?
EMERGENCY/ABNORMAL PROCEDURES
Smoke
REVISION 4 S-4A
CONTINUED FROM PREVIOUS PAGE
No
Yes Altitude ........................ MEA OR
15’000 FT, WHICHEVER IS HIGHER
If it is not possible to descend below 15’000 ft, anti-ice system failure messages may be presented. In this case, exit icing conditions.
SMOKE EVACUATION Procedure (S-11) ........AS REQUIRED
ICING CONDITIONS?
END
EMERGENCY/ABNORMAL PROCEDURES
Smoke
ORIGINAL S-5
CABIN FIRE OR SMOKE
Condition: Smoke or odor inside the cabin and/or cockpit.
Crew Oxygen Masks......DON, 100% Smoke Goggles
or PBE..........................DON Recirculation Fan...........PUSH OUT Crew Communication....ESTABLISH
LAND AT THE NEAREST SUITABLE AIRPORT.
No
Yes
AIR CONDITIONING SMOKE (S-4) and/or ELECTRICAL SYSTEM FIRE OR SMOKE (S-6) Procedures................ AS REQUIRED
SMOKE EVACUATION Procedure (S-11)....... AS REQUIRED
END
END
TROUBLESHOOTING CONSIDERED?
EMERGENCY/ABNORMAL PROCEDURES
Smoke
S-6 ORIGINAL
ELECTRICAL SYSTEM FIRE OR SMOKE
Condition: Smoke confirmed from electrical source.
Crew Oxygen Masks .....DON, 100% Smoke Goggles.............DON Crew Communication ...ESTABLISH Recirculation Fan..........PUSH OUT
LAND AT THE NEAREST SUITABLE AIRPORT.
No
Yes Electrical Power to
Affected Equipment..OFF SMOKE EVACUATION
Procedure (S-11) ........ AS REQUIRED
Shed Buses ..................OFF No
Yes Relevant Inoperative Items: TAXI AND NOSE LANDING LIGHTS FLASHLIGHT RECHARGE SYSTEM SELCAL SYSTEM WINDSHIELD HEATING 2
SMOKE EVACUATION Procedure (S-11) ...... AS REQUIRED
Bus Ties ...................... OFF APU Generator ........... PUSH OUT
CONTINUES ON NEXT PAGE
SMOKE ORIGIN IDENTIFIED?
END
SMOKE DISSIPATES?
END
EMERGENCY/ABNORMAL PROCEDURES
Smoke
ORIGINAL S-7
CONTINUED FROM PREVIOUS PAGE Battery 2 ......................OFF
Central Bus deenergized. No
Yes Relevant Inoperative Items: TAXI AND NOSE LANDING LIGHTS FLASHLIGHT RECHARGE SYSTEM SELCAL SYSTEM WINDSHIELD HEATING 2
SMOKE EVACUATION Procedure (S-11) ......AS REQUIRED
Fuel Pumps .................1B AND
2A OR 2C Battery 2 ......................AUTO Battery 1 ......................OFF Generators 1 and 3 .....PUSH OUT
DC Bus 1 and Essential Bus 1 deenergized.
No
Yes Icing Conditions..........EXIT/AVOID Altitude ........................MAX 25’000 FT,
MIN MEA At pilot’s discretion, on Reversionary Panel:
SG1............................PUSH IN MFD 1 control is possible through MFD 2 Bezel.
Brake effectiveness will be reduced. Monitor fuel quantity indication 1 through RMU 2.
CONTINUES ON NEXT PAGE
SMOKE DISSIPATES?
SMOKE DISSIPATES?
END
EMERGENCY/ABNORMAL PROCEDURES
Smoke
S-8 ORIGINAL
CONTINUED FROM PREVIOUS PAGE COM 2 on Digital
Audio Panel 1 .......PUSH IN Relevant Inoperative Items:
Autopilot Audio System 1 GPWS FMS 1 Transponder 1 RA 1 DME 1 Main Pitch Trim TCAS Pack 1 Speed Brake RMU 1 ADF/VHF/VOR/ILS/MB 1 Landing Gear Control (Down Override) W/S 1 Heating and Wiper
Do not set Thrust Lever 1 below idle in flight. Anticipate flap actuation. Do not actuate Thrust Reverser 1. Landing configuration:
Flaps........................22° VREF..........................VREF 45° + 10 KIAS
CAUTION: MULTIPLY BY 1.42 THE FLAPS 45° UNFACTORED LANDING DISTANCE.
SMOKE EVACUATION Procedure (S-11) .....AS REQUIRED
Generators 1 and 3 ...PUSH IN Battery 1.....................AUTO Fuel Pumps................1A OR 1C AND
2B Battery 2.....................OFF Generators 2 and 4 ...PUSH OUT
DC Bus 2 and Essential Bus 2 deenergized.
CONTINUES ON NEXT PAGE
END
EMERGENCY/ABNORMAL PROCEDURES
Smoke
ORIGINAL S-9
CONTINUED FROM PREVIOUS PAGE No
Yes Icing Conditions..........EXIT/AVOID Altitude ........................MAX 25’000 FT,
MIN MEA Airspeed ......................MAX 250 KIAS At pilot’s discretion, on Reversionary Panel:
SG 2 ..........................PUSH IN MFD 2 control is possible through MFD 1 Bezel.
Monitor fuel quantity indication 2 through RMU 1. COM 1 on Digital
Audio Panel 2...........PUSH IN Relevant Inoperative Items:
Transponder 2 Stick Pusher
Audio System 2 RMU 2
ISIS/Standby Altimeter FMS 2
Standby Attitude Indicator Pack 2
W/S 2 Heating and Wiper Steering
Landing Gear Control Landing lights
ADF 2/VOR 2/DME 2/VHF 2/ ILS 2/MB 2
Do not set Thrust Lever 2 below idle in flight. Do not actuate Thrust Reverser 2. Brake effectiveness will be reduced. When necessary to extend landing gear:
Gear Electrical Override.................DOORS
..............................WAIT 3 SECS CONTINUES ON NEXT PAGE
SMOKE DISSIPATES?
EMERGENCY/ABNORMAL PROCEDURES
Smoke
S-10 ORIGINAL
CONTINUED FROM PREVIOUS PAGE Gear Electrical
Override................ GEAR/DOORS
Anticipate flap actuation. Landing configuration:
Flaps......................... 22° VREF........................... VREF 45° + 10 KIAS
CAUTION: MULTIPLY BY 1.42 THE FLAPS 45° UNFACTORED LANDING DISTANCE.
SMOKE EVACUATION Procedure (S-11) ...... AS REQUIRED
Generators 2 and 4 .... PUSH IN Battery 2...................... AUTO APU Generator ........... PUSH IN Bus Ties ...................... AUTO Shed Buses ................ AUTO Backup Battery........... PUSH OUT
SMOKE EVACUATION Procedure (S-11)...... AS REQUIRED
END
END
EMERGENCY/ABNORMAL PROCEDURES
Smoke
ORIGINAL S-11
SMOKE EVACUATION
Condition: Smoke or odor inside the cabin and/or cockpit requiring removal.
Cockpit Door ...............CLOSE Recirculation Fan........PUSH OUT Gasper Fan ..................PUSH OUT Pressurization
Manual Controller ....1 O'CLOCK POSITION
................................WAIT 15 SECS Pressurization Mode
Selector ....................PUSH IN (MAN) Passenger Oxygen .....AS REQUIRED
Fast
Normal Pressurization Manual
Controller .................AS REQUIRED Turn the controller clockwise towards UP to adjust desired evacuation rate.
Pressurization Manual Controller .................UP
Packs 1 and 2 ..............PUSH OUT
CONTINUES ON NEXT PAGE
END
DESIRED EVACUATION RATE?
EMERGENCY/ABNORMAL PROCEDURES
Smoke
S-12 ORIGINAL
CONTINUED FROM PREVIOUS PAGE Bleeds (at least one) ....PUSH IN
Altitude..........................10’000 FT OR MEA, WHICHEVER IS HIGHER
Recover cabin pressure as soon as smoke has been cleared. EMERGENCY DESCENT
Procedure (NAP-6)....AS REQUIRED
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
REVISION 8 NAP-1 Q
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TABLE OF CONTENTS AIR CONDITIONING SMOKE ............................refer to S-4
AILERON RUNAWAY................................................NAP-3
AIRPLANE OVERSPEED..........................................NAP-4
APU OVERTEMPERATURE .....................................NAP-4
CABIN FIRE OR SMOKE ...................................refer to S-5
DITCHING .................................................................NAP-5
DUAL ENGINE FAILURE ...........................refer to EAP 6-3
ELECTRICAL SYSTEM FIRE OR SMOKE....................................................refer to S-6
EMERGENCY DESCENT..........................................NAP-6
EMERGENCY EVACUATION ...................................NAP-7
ENGINE FIRE, SEVERE DAMAGE OR SEPARATION ........................................refer to EAP 6-6
ENGINE OIL LOW PRESSURE .................refer to EAP 6-7
FORCED LANDING...................................................NAP-8
INADVERTENT SPOILER OPEN................refer to EAP 8-7
JAMMED AILERON...................................................NAP-10
JAMMED ELEVATOR ...............................................NAP-10
JAMMED RUDDER ...................................................NAP-11
PITCH TRIM INOPERATIVE .......................refer to EAP 8-3
PITCH TRIM RUNAWAY...........................................NAP-13
RAPID CABIN DEPRESSURIZATION ......................NAP-14
ROLL TRIM RUNAWAY ............................................NAP-3
SMOKE EVACUATION ......................................refer to S-11
ABNORMAL ENGINE START ...................................NAP-15
ABNORMAL LANDING GEAR EXTENSION.............NAP-16
AILERON ARTIFICIAL FEEL INOPERATIVE............NAP-17
ASYMMETRIC RUDDER OPERATION ....................NAP-17
CABIN DEPRESSURIZATION ...................refer to EAP 1-12
CAS MESSAGE MISCOMPARISON.........................NAP-17
CRACKED WINDSHIELD......................................... NAP-28
DISPLAY FAILURE .....................................refer to EAP 2-6
CDU DATA BUS FAIL FMS ANNUNCIATION...........NAP-18
EMERGENCY/PARKING BRAKE HANDLE DISAGREE ............................................NAP-18
ENGINE ABNORMAL VIBRATION............................NAP-18
ENGINE AIRSTART ..................................................NAP-19
ENGINE CONTROL FAILURE ....................refer to EAP 6-9
ENGINE FAILURE/SHUTDOWN...............................NAP-23
ENGINE OIL HIGH PRESSURE ...............................NAP-24
CONTINUES ON NEXT PAGE
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
NAP-2 REVISION 8
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CONTINUED FROM PREVIOUS PAGE
ENGINE OIL HIGH TEMPERATURE ...................... NAP-24
ENGINE OIL LOW LEVEL ....................................... NAP-24
ENGINE OIL LOW PRESSURE .............................. NAP-25
ENGINE OVERTEMPERATURE............................. NAP-25
ENGINE TAILPIPE FIRE ......................................... NAP-26
ERRONEOUS STALL PROTECTION ACTUATION.............................NAP-26A
GEAR LEVER CANNOT MOVE UP AFTER TAKEOFF ......................................... NAP-27
GUST LOCK FAILURE ............................................ NAP-27
IC BUS FAILURE....................................refer to EAP 2-8
IC FAILURE ............................................refer to EAP 2-8
IMPAIRED OR CRACKED WINDSHIELD ............... NAP-28
IRS/MSU FAILURE ANNUNCIATION ..................... NAP-29
LOSS OF ENGINE INDICATIONS .......................... NAP-30
LOSS OF PRESSURIZATION INDICATION ........... NAP-31
MAIN DOOR BLOCKED.......................................... NAP-33
NAV/FLIGHT INSTRUMENTS FAILURE................. NAP-33
ONE ENGINE INOPERATIVE APPROACH AND LANDING............................... NAP-35
OVERWEIGHT LANDING ....................................... NAP-36
OXYGEN LEAKAGE................................................ NAP-37
PARTIAL OR GEAR UP LANDING ......................... NAP-38
PRESSURIZATION AUTOMATIC SYSTEM FAILURE ............................refer to EAP 1-12
RADIO ALTIMETER FAIL.......................refer to EAP 2-14
RUDDER ARTIFICIAL FEEL INOPERATIVE .......... NAP-39
RUDDER RUNAWAY .............................................. NAP-40
SINGLE ENGINE BLEED OPERATION IN ICING CONDITIONS ...................................... NAP-41
STEERING SYSTEM INOPERATIVE.....refer to EAP 12-9
STIFFENED ELEVATOR......................................... NAP-41
STRUCTURAL DAMAGE ........................................ NAP-42
SUSPECTED FUEL LEAK....................................... NAP-42
UNCOMMANDED AILERON DISCONNECTION.... NAP-43
UNCOMMANDED ELEVATOR DISCONNECTION.......................... NAP-43
UNCOMMANDED SWERVING ON GROUND.....................................refer to EAP 12-9
UNRELIABLE AIRPEED.......................................... NAP-44
VOLCANIC ASH ...................................................... NAP-44
YAW TRIM RUNAWAY............................................ NAP-40
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
REVISION 10 NAP-3 Q
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RUNAWAY PERSISTS?
AILERON RUNAWAY/ ROLL TRIM RUNAWAY
Condition: Sudden roll.
Quick Disconnect Button.......................PRESS AND HOLD
Aileron Shutoff Sys 1 and 2...................PUSH OUT
Roll Trim CB (F22 or F23) ......................PULL Quick Disconnect Button.......................RELEASE Airspeed ..................................................MAX 250 KIAS Roll Trim Position...................................CHECK
No Yes
Roll Trim CB (F22) ..................................PUSH Prepare to overcome uncommanded roll. Aileron Shutoff Sys 1 .............................PUSH IN
No
Yes
Aileron Shutoff Sys 1 .............................PUSH OUT Prepare to overcome uncommanded roll. Aileron Shutoff Sys 2 .............................PUSH IN
No
Yes
Aileron Shutoff Sys 2 .............................PUSH OUT Expect greater aileron control force. If required both pilots should act together to control the airplane.
Avoid airports with anticipated turbulence or crosswind. Perform a long final approach. Landing configuration:
Landing Gear .....................................DOWN Flaps ...................................................22° VREF......................................................VREF45 + 10 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.45.
Aileron Shutoff Sys 1 and 2...................PUSH IN Roll trim is inoperative. Use aileron and rudder to control the airplane.
END
RUNAWAY STILL PERSISTS?
ROLL TRIM IN NEUTRAL POSITION?
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
NAP-4 ORIGINAL Q
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EGT REMAINS HIGH?
AIRPLANE OVERSPEED
Aural Warning: Voice Message HIGH SPEED.
INDICATION: Airspeed and Mach indications in red range.
Airspeed...................................................MAX VMO/MMO
APU OVERTEMPERATURE
EICAS Indication: EGT enter amber or red range. EICAS Caution: APU FAIL may be presented.
APU Bleed ...............................................PUSH OUT
.............................................................WAIT 10 SECONDS
No
Yes
APU Fuel Shutoff Valve ..........................PUSH IN
APU Master Knob....................................OFF
CAUTION: DO NOT ATTEMPT TO RESTART APU.
Consider the APU shutdown if it is not necessary.
END
END
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
REVISION 10 NAP-5 Q
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ICING CONDITIONS?
DITCHING
ATC ..........................................................NOTIFY
Transponder............................................7700 ELT ...........................................................ON Emerg Lts ................................................ON
FSTN Belts...............................................ON Cabin Crew (if applicable)......................NOTIFY Passengers (and Crew)..........................PREPARE FOR
DITCHING Below 10’000 ft:
Pressurization Dump Button............PUSH IN (ON)
EGPWS CB (D2 or J8) .......................PULL Aural Warn CB’s (B4 and E29
or B4 and E30) ..............................PULL At 1’000 ft:
Fuselage Tank Transfer Knob..........TURN OFF Packs 1 and 2.....................................PUSH OUT Engine Bleeds 1 and 2 ......................PUSH OUT
Plan ditching parallel to the line of the wave crests. On final, level the wings and avoid skidding. Touchdown with 4o nose up attitude, and rate of descent less than 180 ft/min. Use only overwing emergency exits for passenger evacuation. Do not open remaining doors.
Ditching configuration: No
Yes
Landing Gear...........................................UP Flaps ........................................................22° If it is not possible to achieve the selected flap position, maintain airspeed according to the following:
FLAPS POSITION MIN AIRSPEED
0 to 8° VREF45 + 30 KIAS
9° to 21° VREF45 + 10 KIAS
22° VREF45 + 5 KIAS
Upon water contact: Thrust Levers 1 and 2 ....................... IDLE Start/Stop Selectors 1 and 2.............STOP APU .....................................................SHUTDOWN Fire Extinguishing Handles ..............PULL APU Fuel Shutoff ...............................PUSH IN Engine and APU Fire Extinguishing
Bottles (if necessary) ...................DISCHARGE Fuel Pumps Pwr.................................OFF Hydraulic Elec Pumps.......................OFF Evacuation ......................................... INITIATE
CONTINUES ON NEXT PAGE END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
NAP-6 REVISION 8 Q
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CONTINUED FROM PREVIOUS PAGE
Landing Gear......................................UP
Flaps....................................................45° If it is not possible to achieve the selected flap position, maintain airspeed according to the following:
FLAPS POSITION MINIMUM AIRSPEED
0 to 8° VREF45 + 30 KIAS
9° to 21° VREF45 + 10 KIAS
22° to 44° VREF45 + 5 KIAS
45° VREF45
Upon water contact: Thrust Levers 1 and 2........................IDLE Start/Stop Selectors 1 and 2 .............STOP APU .....................................................SHUTDOWN Fire Extinguishing Handles ..............PULL APU Fuel Shutoff ...............................PUSH IN Engine and APU Fire Extinguishing
Bottles (if necessary) ...................DISCHARGE Fuel Pumps Pwr.................................OFF Hydraulic Elec Pumps .......................OFF Evacuation..........................................INITIATE
EMERGENCY DESCENT
Cabin Crew ...........................................NOTIFY
FSTN Belts............................................ON
Thrust Levers .......................................IDLE
Speed Brakes .......................................OPEN
Airspeed ...............................................MAX 250 KIAS
Landing Gear........................................DOWN
Speed Brakes .......................................CHECK OPEN
Landing Gear........................................CHECK DOWN
Descent.................................................INITIATE
Transponder.........................................7700
Altitude .................................................MEA OR 10’000 FT, WHICHEVER IS HIGHER
CAUTION: IF STRUCTURAL DAMAGE IS SUSPECTED, USE THE FLIGHT CONTROLS WITH CAUTION AVOIDING HIGH MANEUVERING LOADS AND REDUCING AIRSPEED AS APPROPRIATE.
END
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
REVISION 4 NAP-7 Q
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EMERGENCY EVACUATION
Parking Brake ......................................APPLY
Cabin.....................................................DEPRESSURIZE
Fire Extinguishing Handles................PULL
APU Fuel Shutoff Valve ......................PUSH IN
Fuel Pumps Pwr 1 and 2.....................OFF
Hydraulic Elec Pumps 1 and 2 ..........OFF
Engines and APU Fire Extinguishing Bottles (if necessary) ...................DISCHARGE
Cabin Crew...........................................NOTIFY
Emerg Lts.............................................ON
Evacuation ........................................... INITIATE
ATC........................................................NOTIFY Before leaving the airplane: Batteries 1 and 2 .............................OFF
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
NAP-8 REVISION 10 Q
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ICING CONDITIONS?
FORCED LANDING
ATC...........................................................NOTIFY Transponder ............................................7700
ELT ...........................................................ON Emerg Lts.................................................ON FSTN Belts...............................................ON
Cabin Crew (if applicable) ......................NOTIFY Passengers (and Crew) ..........................PREPARE FOR
FORCED LANDING Below 10’000 ft:
Pressurization Dump Button ............PUSH IN (ON) EGPWS CB (D2 or J8)........................PULL Aural Warn CB’s (B4 and E29
or B4 and E30)...............................PULL When committed to land:
No
Yes
Landing Gear...........................................AS REQUIRED The decision to land with all gear up or with any gear extended is left to pilots. The choice of configuration is based on the number of gear available, airplane load distribution, controllability and conditions of the landing field. Ground spoilers and thrust reversers will not operate if any main gear is up.
Flaps.........................................................22° If it is not possible to achieve the selected flap position, maintain airspeed according to the following:
FLAPS POSITION MIN AIRSPEED
0 to 8° VREF45 + 30 KIAS 9° to 21° VREF45 + 10 KIAS
22° VREF45 + 5 KIAS
Just before touchdown:
Fuselage Tank Transfer Knob ..........TURN OFF
Fire Extinguishing Handles ..............PULL
APU Fuel Shutoff Valve.....................PUSH IN When the airplane stops:
Engines and APU Fire Extinguishing Bottles (if necessary) ...................DISCHARGE
Fuel Pumps Pwr 1 and 2 ...................OFF
Hydraulic Elec Pumps 1 and 2 .........OFF
Evacuation..........................................INITIATE
CONTINUES ON NEXT PAGE
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
REVISION 7 NAP-9 Q
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CONTINUED FROM PREVIOUS PAGE
Landing Gear...........................................AS REQUIRED
The decision to land with all gear up or with any gear extended is left to pilots. The choice of configuration is based on the number of gear available, airplane load distribution, controllability and conditions of the landing field. Ground spoilers and thrust reversers will not operate if any main gear is up.
Flaps ........................................................45°
If it is not possible to achieve the selected flap position, maintain airspeed according to the following:
FLAPS POSITION MIN AIRSPEED
0 to 8° VREF45 + 30 KIAS 9° to 21° VREF45 + 10 KIAS 22° to 44° VREF45 + 5 KIAS
45° VREF45
Just before touchdown:
Fuselage Tank Transfer Knob..........TURN OFF
Fire Extinguishing Handles ..............PULL
APU Fuel Shutoff Valve ....................PUSH IN
When the airplane stops:
Engines and APU Fire Extinguishing Bottles (if necessary) ...................DISCHARGE
Fuel Pumps Pwr 1 and 2 ...................OFF
Hydraulic Elec Pumps 1 and 2 ........OFF
Evacuation ......................................... INITIATE
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
NAP-10 REVISION 3 Q
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ICING CONDITIONS?
JAMMED AILERON Condition: Both control wheels can not be moved to
either side.
Aileron Disconnection Handle .............PRESS AND PULL
Autopilot ..................................................DISENGAGE
Airspeed...................................................MAX 200 KIAS
If the right control wheel is jammed, roll trim and artificial feel are not available.
Maintain bank angle below 20°. If both ailerons are jammed, use rudder to control the airplane.
Avoid abrupt and large aileron inputs.
Avoid airports with anticipated turbulence or crosswind.
No
Yes
Landing configuration: Landing Gear......................................DOWN Flaps....................................................22° VREF ......................................................VREF45 + 15 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.55.
Landing configuration: Landing Gear......................................DOWN Flaps....................................................45° VREF ......................................................VREF45 + 5 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.13.
JAMMED ELEVATOR
Condition: Both control columns can not be moved either forward or backward.
EICAS Warning: SPS 1-2 INOP may be presented.
EICAS Caution: STICK PUSHER FAIL may be presented.
Elevator Disconnection Handle ...........PRESS AND PULL
Autopilot ..................................................DISENGAGE
Airspeed...................................................MAX 200 KIAS If left elevator is jammed, Stick Pusher will not be available. Avoid airports with anticipated turbulence or crosswind.
CONTINUES ON NEXT PAGE
END
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
REVISION 4 NAP-11 Q
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RUDDER FREE?
ICING CONDITIONS?
RUDDER FREE?
CONTINUED FROM PREVIOUS PAGE
Pitch Trim ................................................AS REQUIRED Elevator authority to flare during landing may be reduced. If both elevators are jammed, pitch trim may be used to land the airplane.
Landing configuration: Landing Gear .....................................DOWN Flaps ...................................................22° VREF......................................................VREF45 + 10 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.45.
JAMMED RUDDER
Condition: Pedals can not be moved.
Command rudder through yaw trim. If required, use asymmetric thrust to control the airplane. Rudder Shutoff Sys 2 .............................PUSH OUT
No
Yes
Rudder Shutoff Sys 2 .............................PUSH IN
Rudder Shutoff Sys 1 .............................PUSH OUT
No
Yes
Airspeed ..................................................MAX 200 KIAS Avoid airports with anticipated turbulence or crosswind. Do not reduce engine thrust during flare.
No
Yes
Landing configuration:
Landing Gear .....................................DOWN
Flaps ...................................................22°
VREF......................................................VREF45 + 15 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.85.
CONTINUES ON NEXT PAGE
END
END
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
NAP-12 REVISION 10 Q
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CONTINUED FROM PREVIOUS PAGE
During final approach and landing run:
Pilot not flying: Steering Disengage Button .........PRESS AND HOLD
Steering Handle.......................................AS REQUIRED Use Steering Handle still keeping the Steering Disengage Button pressed.
After the touchdown:
Thrust Levers .....................................IDLE If necessary, use differential braking to steer the airplane.
Landing configuration:
Landing Gear......................................DOWN
Flaps....................................................45°
VREF ......................................................VREF45 + 5 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.42.
During final approach and landing run:
Pilot not flying: Steering Disengage Button .........PRESS AND HOLD
Steering Handle.......................................AS REQUIRED Use Steering Handle still keeping the Steering Disengage Button pressed.
CAUTION: DO NOT RELEASE THE NOSEWHEEL STEERING HANDLE UNTIL THE AIRPLANE IS COMPLETELY STOPPED.
After the touchdown:
Thrust Levers .....................................IDLE If necessary, use differential braking to steer the airplane.
END
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
REVISION 9 NAP-13 Q
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RUNAWAY PERSISTS?
PITCH TRIM RUNAWAY
Condition: Uncommanded pitch and trim indication changes.
EICAS Warning: AUTOPILOT FAIL may be presented.
EICAS Caution: AUTO TRIM FAIL may be presented.
Quick Disconnect Button .....................PRESS AND HOLD
NOTE: Do not change flap setting.
At safe altitude:
Pitch Trim Main Sys Cutout..............PUSH OUT
Pitch Trim Backup Sys Cutout.........PUSH OUT
Quick Disconnect Button .................RELEASE
WARNING: DO NOT OPEN SPEED BRAKE.
Prepare to overcome unwanted pitch change.
Pitch Trim Backup Sys Cutout ..............PUSH IN
Pitch Trim ................................................ACTUATE No Yes
Pitch Trim Backup Sys Cutout ..............PUSH OUT
Prepare to overcome unwanted pitch change.
Pitch Trim Main Sys Cutout...................PUSH IN No Yes Pitch Trim Main Sys Cutout...................PUSH OUT
PITCH TRIM INOPERATIVE Procedure (EAP 8-3)..........................ACCOMPLISH
Autopilot can be used. Autopilot ..................................................DISENGAGE
END
END
END
RUNAWAY STILL PERSISTS?
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
NAP-14 ORIGINAL Q
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APU ABNORMAL INDICATION PRESENTS?
RAPID CABIN DEPRESSURIZATION
Aural Warning: Voice Message CABIN. EICAS Indication: CAB ALT Value in red.
Condition: Cabin altitude has exceeded 10’000 ft.
Crew Oxygen Masks ...............................DON
Crew Communication .............................ESTABLISH
EICAS Pressurization Indication ...........CHECK
Passenger Oxygen..................................AS REQUIRED
If Emergency Descent is necessary:
FSTN Belts..........................................ON
Cabin Crew .........................................NOTIFY
Thrust Levers .....................................IDLE
Speed Brakes .....................................OPEN
Airspeed..............................................MAX 250 KIAS
Landing Gear......................................DOWN
Descent ...............................................INITIATE
Altitude................................................MEA OR 10’000 FT, WHICHEVER IS HIGHER
CAUTION: IF STRUCTURAL DAMAGE IS SUSPECTED, USE THE FLIGHT CONTROLS WITH CAUTION AVOIDING HIGH MANEUVERING LOADS AND REDUCING AIRSPEED AS APPROPRIATE.
Altitude................................................MEA OR 10’000 FT, WHICHEVER IS HIGHER
APU Parameters.................................CHECK
No
Yes
APU .....................................................OFF
END
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
REVISION 10 NAP-15 Q
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ABNORMAL ENGINE START
Condition: Any abnormal engine indication during engine start.
To abort start:
Associated Thrust Lever .................. IDLE
Associated Start/Stop Selector........STOP
No
Yes
Fire Extinguishing Handle .....................PULL
ENGINE FIRE, SEVERE DAMAGE OR SEPARATION Procedure (EAP 6-6) or ENGINE FAILURE/SHUTDOWN Procedure (NAP-23)...........................ACCOMPLISH
No
Yes
FADEC in Command ..............................CHECK
FADEC Control Knob .............................ALTN No
Yes
Ignition.....................................................OFF Associated Start/Stop Selector.............START, THEN RUN
.............................................................WAIT 10 SECONDS N2 Indication ...........................................CHECK
No Yes
.............................................................WAIT 30 SECONDS Associated Start/Stop Selector.............STOP Ignition Selector .....................................AUTO Engine......................................................START
Do not attempt another start. ENGINE FAILURE/SHUTDOWN
Procedure (NAP-23)...........................ACCOMPLISH
END
FIRE OCCURS OR ENGINE STILL RUNNING?
END
ANOTHER START CONSIDERED?
FADEC ALTERNATES?
END
N2 INDICATES ROTATION?
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
NAP-16 ORIGINAL Q
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ABNORMAL LANDING GEAR EXTENSION
Condition: Landing gear has not extended by normal means.
Free Fall Electrical Override
NOTE: Hydraulic System 1 must be operative.
Airspeed...................................................MAX 250 KIAS
Landing Gear Lever ................................DOWN
Gear Electrical Override .........................DOORS
..............................................................WAIT 3 SECONDS
Gear Electrical Override .........................GEAR/DOORS
Landing Gear Indication.........................CHECK No Yes
Airspeed...................................................MAX 200 KIAS
Landing Gear Lever ................................UP
Gear Electrical Override .........................NORMAL
..............................................................WAIT 10 SECONDS
Free Fall Lever.........................................ACTUATE
Landing Gear Lever ................................DOWN
Landing Gear Indication.........................CHECK No Yes
Free Fall Lever.........................................CYCLE Cycle the free fall lever as necessary, limited to 10 times, leaving it at the latched position for 20 seconds between each cycle.
No
Yes
PARTIAL OR GEAR UP LANDING Procedure (NAP-38)...........................ACCOMPLISH
WHICH EXTENSION CONSIDERED?
THREE LEGS DOWN?
ANY LEG STILL UP?
END
END
ANY LEG STILL UP?
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
ORIGINAL NAP-17 Q
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AILERON ARTIFICIAL FEEL INOPERATIVE
Condition: Control Wheel excessively light and oversensitive.
Airspeed. .................................................MAX 200 KIAS Do not make abrupt and large aileron inputs.
ASYMMETRIC RUDDER OPERATION
Condition: Rudder pedals heavier to be moved to one side than the other.
Rudder Shutoff Sys 2 .............................PUSH OUT
No
Yes
Rudder Shutoff Sys 2 .............................PUSH IN
CAS MESSAGE MISCOMPARISON
PFD Indication: CAS MSG in amber.
Reversionary Panel:
MFD 1 Knob........................................EICAS
MFD 2 Knob........................................EICAS
Pilot’s/Copilot’s EICAS messages........COMPARE
Discrepant message...............................CHECK Analyze the situation to check whether the discrepant message is spurious or not, and take the appropriate corrective action.
END
END
END
FAILURE PERSISTS?
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
NAP-18 REVISION 4 Q
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CDU DATA BUS FAIL FMS ANNUNCIATION
Condition: Affected FMS is not updating CDU. CDU DATA BUS FAIL message presented on FMS.
Affected FMS .................................... OFF, then ON Power down the FMS using the ON-OFF DIM key. DO NOT use the circuit breaker to cycle power to the FMS.
No
Yes
Affected FMS .................................... OFF
EMERGENCY/PARKING BRAKE HANDLE DISAGREE
Light: BRAKE ON with Emergency/Parking Brake Handle not actuated for more than 10 seconds.
Do not takeoff.
ENGINE ABNORMAL VIBRATION
EICAS Indication: Engine vibration enters amber range.
Associated Thrust Lever ........................REDUCE TO KEEP VIBRATION WITHIN LIMITS
No Yes
Monitor engine vibration.
Affected ENGINE FAILURE/SHUTDOWN Procedure (NAP-23)...........................ACCOMPLISH
VIBRATION WHITIN GREEN LIMITS?
END
END
END
CDU DATA BUS FAIL MESSAGE PERSISTS?
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
ORIGINAL NAP-19
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ENGINE AIRSTART
Inoperative engine:
Fuel Pump Selector...........................A or B
Fuel Pump Pwr...................................ON
Ignition................................................AUTO
Start/Stop Selector ............................STOP
Engine Bleed......................................PUSH OUT
Thrust Lever....................................... IDLE
Engine Airstart Envelope.......................CHECK
ENGINE AIRSTART ENVELOPE
0
5000
10000
15000
20000
25000
30000
50 100 150 200 250 300 350
AL
TIT
UD
E -
ft
INDICATED AIRSPEED - KIAS
ASSISTED START
ASSISTED AND
WINDMILLING START
145J
AA
057A
- 1
6MA
Y20
06
AE 3007A ENGINES
NOTE: Shaded area may be below 1.23 VSR.
CONTINUES ON NEXT PAGE
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
NAP-20 REVISION 8 Q
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CONTINUED FROM PREVIOUS PAGE
Windmilling APU Assisted Crossbleed Assisted
CAUTION: ANTI-ICING SYSTEM WILL BE INOPERATIVE TEMPORARILY.
APU...........................................................START APU Bleed................................................PUSH IN XBleed......................................................AUTO OR OPEN Operative engine: Engine Bleed ......................................PUSH OUT Inoperative engine: Start/Stop Selector ............................START, THEN RUN Engine Indication ....................................MONITOR
No Yes
Engine Bleeds 1 and 2............................AS REQUIRED XBleed......................................................AUTO APU Bleed................................................AS REQUIRED
Consider another start procedure attempt.
Do not alternate FADEC.
NOTE: For AE3007A1E engines only, reset the FADEC of the inoperative engine if another airstart attempt is considered.
Operative Engine Bleed..........................AS REQUIRED Affected ENGINE FAILURE/SHUTDOWN
Procedure (NAP-23)...........................AS REQUIRED
Operative engine: N2 ........................................................MIN 80% XBleed.................................................AUTO OR OPEN
Engine Bleed ......................................PUSH IN Inoperative engine: Start/Stop Selector ............................START, THEN RUN Engine Indication ....................................MONITOR
CONTINUES ON NEXT PAGE
START PROCEDURE CONSIDERED?
END
NORMAL START?
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
REVISION 8 NAP-21
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CONTINUED FROM PREVIOUS PAGE
No
Yes
Engine Bleeds 1 and 2 ...........................AS REQUIRED XBleed......................................................AUTO APU Bleed ...............................................AS REQUIRED
Consider another start attempt.
NOTE: For AE3007A1E engines only, reset the FADEC of the inoperative engine if another airstart reattempt is considered.
Operative Engine Bleed .........................AS REQUIRED Affected ENGINE FAILURE/SHUTDOWN
Procedure (NAP-23)...........................AS REQUIRED
NOTE: - Due to the characteristics listed below, the windmilling start should be accomplished only if an assisted start is not an option.
- For AE3007A1E engines only, reset the FADEC of the inoperative engine if another airstart reattempt is considered.
- Initiate windmilling start with N2 as high as possible. Windmilling starts are not possible with N2 below 10%. Once N2 is below 10%, it may not be recovered.
- Windmilling start is slower than an assisted start. - During a Windmilling start, if N2 reaches 30% and
keeps increasing, the loss of altitude may be minimized by reducing airspeed.
- ITT peaks may occur during windmilling starts above 10000 ft with airspeed below 290 knots. In this case, the engine may operate above the ITT limit, up to 850°C, for a maximum 5 seconds. Abort the start if the engine remains operating above the ITT limit for more than 5 seconds.
Airspeed: Above 10000 ft ...................................MIN 250 KIAS Below 10000 ft....................................220 TO 250 KIAS
N2 .............................................................MIN 10% Inoperative engine: Start/Stop Selector ............................START, THEN RUN
ITT and N2 ...............................................MONITOR
CONTINUES ON NEXT PAGE
END
END
NORMAL START?
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
NAP-22 REVISION 8 Q
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CONTINUED FROM PREVIOUS PAGE
No Yes
Engine Bleeds 1 and 2............................AS REQUIRED XBleed......................................................AUTO APU Bleed................................................AS REQUIRED
Consider another start attempt.
NOTE: For AE3007A1E engines only, reset the FADEC of the inoperative engine if another airstart reattempt is considered.
Operative Engine Bleed..........................AS REQUIRED Affected ENGINE FAILURE/SHUTDOWN
Procedure (NAP-23)...........................AS REQUIRED
END
NORMAL START?
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
REVISION 4 NAP-23
QR
H-1
35
/15
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C
OD
E 0
1
ENGINE FAILURE/SHUTDOWN
Condition: Loss of thrust on an engine or abnormal engine indication or precautionary shutdown.
Associated Thrust Lever........................ IDLE
Associated Start/Stop Selector.............STOP
NOTE: If engine shutdown does not occur, pull the associated fire extinguishing handle.
Engine Thrust Rating .............................CON
APU (if available) ....................................START
APU Bleed ...............................................AS REQUIRED
XBleed......................................................AS REQUIRED
Fuel ..........................................................BALANCE
Altitude ....................................................MAX 25’000 FT, MIN MEA
No Yes
Affected ENGINE AIRSTART Procedure (NAP-19)...........................ACCOMPLISH
TCAS........................................................TA ONLY
LAND AT THE NEAREST SUITABLE AIRPORT.
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.44.
No Yes XBleed......................................................OPEN Altitude ....................................................MAX 15’000 FT,
MIN MEA If it is not possible to descend below 15’000 ft:
Icing Conditions ................................EXIT
ONE ENGINE INOPERATIVE
APPROACH AND LANDING Procedure (NAP-35)...........................AS REQUIRED
ENGINE RESTART CONSIDERED?
END
END
ICING CONDITIONS?
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
NAP-24 REVISION 4 Q
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5/1
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ENGINE OIL HIGH PRESSURE
EICAS Indication: Oil pressure pointer in amber range.
No
Yes
Associated Procedure............................ACCOMPLISH
ENGINE OIL HIGH TEMPERATURE
EICAS Indication: Oil temperature pointer and digits become red.
Associated Thrust Lever ........................REDUCE No Yes No Yes
Altitude.....................................................MAX 25’000 FT, MINIMUM MEA
No
Yes
Affected ENGINE FAILURE/SHUTDOWN Procedure (NAP-23)...........................ACCOMPLISH
ENGINE OIL LOW LEVEL
MFD Indication: Oil level digits become amber.
Oil Pressure, Oil Temperature ........ MONITOR
Affected ENGINE FAILURE/SHUTDOWN Procedure (NAP-23)..................... AS REQUIRED Consider shutting the engine down to preserve oil quantity, and if required restart it prior to landing.
END
FAILURE PERSISTS?
FAILURE PERSISTS?
ABOVE 25’000 FT?
END
OIL TEMPERATURE, OIL LEVEL OR ENGINE VIBRATION OUT OF LIMITS?
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
REVISION 4 NAP-25 Q
RH
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5/1
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ENGINE OIL LOW PRESSURE
EICAS Indication: Oil pressure in amber range.
Associated Thrust Lever........................REDUCE Reduce N2 below 88%.
ENGINE OVERTEMPERATURE
Condition: ITT pointer and digits flashing amber or red.
Associated Thrust Lever........................REDUCE No Yes
Operate at reduced thrust to keep ITT within limits.
Associated Bleed....................................PUSH OUT
Altitude ....................................................MAX 25’000 FT, MIN MEA
No Yes
Affected ENGINE FAILURE/SHUTDOWN Procedure (NAP-23)...........................ACCOMPLISH
Operate at reduced thrust to keep ITT within limits.
ITT INDICATION WITHIN LIMITS?
END
END
ITT INDICATION STILL OUT OF LIMITS?
END
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
NAP-26 REVISION 8 Q
RH
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5/1
56
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ENGINE TAILPIPE FIRE
Condition: Tailpipe fire was detected visually by crew or ground personnel. No EICAS message displayed.
Affected engine:
Thrust Lever .......................................IDLE Start/Stop Selector ............................STOP Ignition ................................................OFF Fuel Pump...........................................OFF XFEED Selector Knob .......................OFF Start/Stop Selector ............................START, THEN RUN
ITT.............................................................MONITOR ATC...........................................................NOTIFY
..............................................................WAIT 90 SECONDS Associated Start/Stop Selector .............STOP Associated Fire
Extinguishing Handle ........................PULL (DO NOT ROTATE)
If fire is not extinguished while the engine is motored, ground personnel support must be requested.
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
REVISION 5 NAP-26A Q
RH
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5/1
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ERRONEOUS STALL PROTECTION ACTUATION
Condition: Inadvertent shaker and/or pusher actuation.
Quick Disconnect Button.......................PRESS AND HOLD
Stall Protection Cutout 1 and 2 .............PUSH OUT
Quick Disconnect Button.......................RELEASE
Minimum Airspeed .................................FLAP MANEUVERING SPEED (PD-2)
Avoid skidding the airplane. No
Yes
Add 15 KIAS to go-around speed to prevent stall protection from being actuated. Landing configuration:
Landing Gear .....................................DOWN
Flaps ...................................................22°
VREF......................................................VREF45 + 15 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.55.
Add 5 KIAS to go-around speed to prevent stall protection from being actuated. Landing configuration:
Landing Gear .....................................DOWN
Flaps ...................................................45°
VREF......................................................VREF45 + 5 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.13.
ICING CONDITIONS?
END
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
NAP-26B REVISION 5 Q
RH
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5/1
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INTENTIONALLY BLANK
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
ORIGINAL NAP-27 Q
RH
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5/1
56
9
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GEAR LEVER CANNOT MOVE UP AFTER TAKEOFF
Condition: Landing gear cannot be moved to up position after takeoff in the normal manner.
.............................................................WAIT 10 SECONDS No Yes
Landing Gear Lever................................DO NOT MOVE LANDING GEAR AIR/GROUND SYSTEM
FAILURE Procedure (EAP 12-8) .......ACCOMPLISH
Downlock Release Button (DN LOCK REL).....................PRESS
Landing Gear Lever................................UP
GUST LOCK FAILURE
Light: GUST LOCK (amber).
On Ground In Flight
Consider diversion. Do not push control column full Nose Down. Avoid flying in turbulence conditions. Avoid airports with anticipated turbulence or crosswind.
Do not takeoff.
CONDITION?
END
END
LG AIR/GND FAIL MESSAGE DISPLAYED?
END
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
NAP-28 ORIGINAL Q
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FORWARD VISIBILITY GOOD IN ONE SIDE?
IMPAIRED OR CRACKED WINDSHIELD
Associated Ice Protection Windshield..........................................PUSH OUT
No Yes
Cockpit Door ...........................................CLOSE Oxygen Masks.........................................AS REQUIRED
Altitude.....................................................MEA OR 10’000 FT, WHICHEVER IS HIGHER
Pressurization Manual Controller .........1 O'CLOCK POSITION
.............................................................WAIT 15 SECONDS
Pressurization Mode Selector ...............PUSH IN (MAN)
Pressurization Manual Controller .........CAB MAX P = 1 PSI
Airspeed...................................................MAX 250 KIAS
Smoke Goggle.........................................DON
No
Yes
Pilot flying must be on non impaired side.
When reaching 10’000 ft:
Pressurization Mode Selector ..........PUSH OUT
Pressurization Dump Button ............PUSH IN
During approach and landing, when visibility is required:
Airspeed..............................................MAX 140 KIAS, MIN VREF45
Check no loose objects in the cockpit.
Direct Vision Window ........................REMOVE Landing must be made by looking through Direct Vision Window. Intercommunication will be impossible with window removed.
ONLY OUTER LAYER CRACKED?
END
END
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
ORIGINAL NAP-29 Q
RH
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5/1
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IRS/MSU FAILURE ANNUNCIATION
OPERATION PHASE LIGHT POWER ON ALIGNMENT IN FLIGHT
ALIGN
No light: Check IRS
CB’s. Set mode
select switch to ALIGN or NAV.
Press MSU Test switch. Annunciator bulb must be replaced if the other MSU annunciators do light.
Accomplish associated IRS ALIGNMENT FAULT Procedure (EAP 2-9).
Flashes: IRS data is not
normal. Accomplish
associated IRS OVERHEAT Procedure (EAP 2-11).
FAULT
Set mode select switch to OFF for at least 3 sec. Then set mode select switch back to ALIGN or NAV.
If the annunciator remains lighted, do not takeoff.
Associated with ALIGN annunciation: Check and
reenter latitude. Allow additional
time for alignment.
Try new alignment. Set mode select switch to OFF for at least 3 sec, then to ALIGN, and enter present position.
If on ground, do not takeoff.
Select the remaining IRU by pressing the IRS Button on the associated reversionary panel.
If necessary set mode select switch to ATT.
NO AIR
Do not takeoff.
*******
Operate IRU until flight completion.
If fault annunciator is ON or inertial data ceases to be transmitted by IRU, accomplish associated IRS OVERHEAT Procedure (EAP 2-11). IRS data is not normal.
BATT FAIL
Do not takeoff. ******* *******
ON BATT
Check IRS CB’s. If the annunciator
remains lighted, do not takeoff.
*******
The IRU operates on backup DC power and will operate for 30 minutes.
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
NAP-30 ORIGINAL Q
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LOSS OF ENGINE INDICATIONS
Condition: Loss of Thrust Mode, ITT, N1 and N2 indications.
No Yes
Associated FADEC .................................RESET No Yes
Associated FADEC .................................ALTN No
Yes
Associated ENGINE FAILURE/SHUTDOWN Procedure (NAP-23)...........................AS REQUIRED
Associated ENGINE FAILURE/SHUTDOWN
Procedure (NAP-23)...........................ACCOMPLISH
END
ASSOCIATED ENGINE OPERATING?
FAILURE PERSISTS?
FAILURE PERSISTS?
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
ORIGINAL NAP-31 Q
RH
-13
5/1
56
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LOSS OF PRESSURIZATION INDICATION
Condition: Cabin altitude or cabin P is not being presented or during use of the pressurization manual control.
Use the remaining indications to maintain cabin altitude below 10’000 ft, according to the table below: 41000 FT
39000 FT
AIRPLANE/CABIN ALTITUDE CONVERSION TABLE FOR AIRPLANES WITH MAXIMUM ALTITUDE CEILING OF 39000 FT
AIRPLANE ALTITUDE
(ft)
CABIN ALTITUDE
(ft)
DIFFERENTIAL PRESSURE
(psi) 10000 800 4.211000 1100 4.412000 1300 4.713000 1500 4.914000 1700 5.215000 2000 5.416000 2200 5.617000 2400 5.818000 2600 6.019000 2800 6.220000 3100 6.421000 3300 6.622000 3500 6.723000 3800 6.824000 4000 7.025000 4200 7.126000 4500 7.227000 4700 7.428000 4900 7.529000 5200 7.630000 5400 7.731000 5600 7.832000 5900 7.833000 6200 7.934000 6400 8.035000 6700 8.036000 7000 8.037000 7300 8.138000 7700 8.139000 8000 8.1
If pressurization can not be maintained, refer to PRESSURIZATION AUTOMATIC SYSTEM FAILURE/CABIN DEPRESSURIZATION Procedure (EAP 1-12).
CONTINUES ON THE NEXT PAGE
END
AIRPLANE MAXIMUM ALTITUDE CEILING?
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
NAP-32 ORIGINAL Q
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CONTINUED FROM PREVIOUS PAGE
AIRPLANE/CABIN ALTITUDE CONVERSION TABLE FOR AIRPLANES WITH MAXIMUM ALTITUDE CEILING OF 41000 FT
AIRPLANE ALTITUDE
(ft)
CABIN ALTITUDE
(ft)
DIFFERENTIAL PRESSURE
(psi) 10000 600 4.311000 900 4.512000 1100 4.813000 1300 5.014000 1500 5.315000 1700 5.516000 1900 5.717000 2100 6.018000 2300 6.219000 2500 6.420000 2700 6.621000 3000 6.722000 3200 6.923000 3400 7.024000 3600 7.225000 3800 7.326000 4000 7.527000 4200 7.628000 4500 7.729000 4700 7.830000 4900 7.931000 5100 8.032000 5400 8.133000 5600 8.134000 5800 8.235000 6100 8.236000 6400 8.337000 6700 8.338000 7100 8.339000 7400 8.340000 7700 8.341000 8000 8.4
If pressurization can not be maintained, refer to PRESSURIZATION AUTOMATIC SYSTEM FAILURE/CABIN DEPRESSURIZATION Procedure (EAP 1-12).
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
ORIGINAL NAP-33 Q
RH
-13
5/1
56
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MAIN DOOR BLOCKED
Light: DOOR BLOCKED (Attendant's Panel).
No
Yes
Hydraulic System 1 ................................OFF Main Door Alternative
Opening Valve....................................TURN CLOCKWISE AND HOLD
.............................................................WAIT 2 MINUTES
Outside Area ...........................................CHECK CLEAR
Door .........................................................OPEN
NAV/FLIGHT INSTRUMENTS FAILURE
LOCATION ANNUNCIATOR/FAILURE
ACTION
ATT: CAGE (amber)
Press the CAGE push button in order to recover attitude indication. Caging the ISIS in flight will result in loss of attitude indication for up to 10 seconds and the amber message ATT 10s will be presented during this time. Until attitude indication is available again use the primary indication source.
ISIS
ATT, ALT, SPD, M, HDG (red)
Use the primary indication source.
HDG FAIL (red)
Use cross-side heading by pressing the IRS button on associated reversionary panel or use RMU or standby attitude indicator. PFD and
MFD
HDG (amber)
Compare data with the Magnetic Compass. After identifying the failed side, use cross-side data by pressing the IRS button on associated reversionary panel.
MFD MENU INOP (amber) Crew awareness.
CONTINUES ON NEXT PAGE
END
ON GROUND?
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
NAP-34 ORIGINAL Q
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CONTINUED FROM PREVIOUS PAGE
LOCATION ANNUNCIATOR/FAILURE
ACTION
ATT FAIL (red) Use cross-side attitude by pressing the IRS Button on associated reversionary panel or use standby attitude indicator.
"X" (red) over IAS tape
Use cross-side airspeed by pressing the ADC button on associated reversionary panel or use standby airspeed indicator.
"X" (red) over altitude tape
Use cross-side altitude by pressing the ADC button on associated reversionary panel or use standby altimeter.
"X" (red) over course scale
Select another sensor.
VS (red) Use cross-side vertical speed by pressing the ADC button on associated reversionary panel.
ROL, PIT, ATT, IAS, or ALT
(amber)
Compare data with Standby Indicator. For altitude compare the PFD altimeters setting also. If required, use cross-side data by pressing the appropriate button on associated reversionary panel.
RA (amber) Compare both radio altimeter indications. If required, consider only the lower indication. Otherwise, disregard Radio Altitude.
RA1 (2) (amber) Radio altimeter automatic reversion has occurred. No action is required.
PFD
PFD or EICAS Blank or "X"
(red)
Use the MFD Knob to present the required information on MFD.
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
ORIGINAL NAP-35 Q
RH
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5/1
56
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01
ONE ENGINE INOPERATIVE APPROACH AND LANDING
Before Landing:
Inoperative Engine Thrust Lever.................................. IDLE
Landing Gear .....................................DOWN
Thrust Rating .....................................TAKEOFF MODE
Fuel XFeed .........................................OFF
Autopilot/Yaw Damper ......................DISENGAGE Landing configuration:
Flaps ...................................................22°
VREF......................................................VREF45 + 10 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.44.
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
NAP-36 REVISION 8 Q
RH
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5/1
56
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OVERWEIGHT LANDING
No
Yes
Landing configuration: Landing Gear......................................DOWN Flaps....................................................22° VREF ......................................................VREF45 + 10 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY AT LEAST 1.45.
Reduce the engine thrust only after the touchdown.
Before touchdown: Emerg Lts ...........................................AS REQUIRED APU Fuel Shutoff Valve.....................CLOSE Rate of Descent..................................MAX 300 FT/MIN
Touch smoothly the runway surface.
Landing configuration: Landing Gear......................................DOWN Flaps....................................................45° VREF ......................................................VREF45
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY AT LEAST 1.06.
Reduce the engine thrust only after the touchdown.
Before touchdown: Emerg Lts ...........................................AS REQUIRED APU Fuel Shutoff Valve.....................PUSH IN Rate of Descent..................................MAX 300 FT/MIN
Touch smoothly the runway surface.
END
ICING CONDITIONS?
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
ORIGINAL NAP-37 Q
RH
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5/1
56
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01
OXYGEN LEAKAGE
Condition: Evidence of oxygen leakage through the crew mask, mask hose, flow indicator (blinker), or oxygen line.
No Smoking ................................................. ON
No
Yes
Affected Mask .............................................. REMOVE FROM STOWAGE BOX
Stowage Box Doors..................................... CLOSE Shutoff Sliding Control ............................... ACTUATE Oxygen Pressure .........................................CHECK
No
Yes
Altitude .........................................................MEA OR 10’000 FT, WHICHEVER IS HIGHER
Keep one Portable Oxygen Cylinder available for the pilot of the affected side. The oxygen supply by the Portable Oxygen Cylinder will last at least 30 minutes. Oxygen Cylinder Shutoff Valve .................. OFF Altitude .........................................................MEA OR
10’000 FT, WHICHEVER IS HIGHER
END
END
IS THE LEAKAGE IN THE CREW MASK, MASK HOSE, OR FLOW INDICATOR?
OXYGEN PRESSURE BELOW MINIMUM REQUIRED FOR DISPATCH?
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
NAP-38 REVISION 10 Q
RH
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5/1
56
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PARTIAL OR GEAR UP LANDING
Condition: Airplane committed to land with gear up or in transit.
EICAS Indication: Abnormal landing gear position.
EICAS Warning: LG/LEVER DISAGREE may be presented.
ATC...........................................................NOTIFY Burn fuel to reduce touchdown speed. Transponder ............................................7700 FSTN Belts...............................................ON Cabin Crew ..............................................NOTIFY Passengers (and Crew) ..........................PREPARE FOR
EMERGENCY LANDING AND EVACUATION
Below 10’000 ft: GPWS CB (D2 or J8) ..........................PULL Aural Warn CB’s (B4 and E29
or B4 and E30)...............................PULL Emerg Lts ...........................................ON ELT ......................................................ON
Prior to approach: Hydraulic Elec Pumps 1 and 2 .........OFF Cabin ...................................................DEPRESSURIZE Engine Bleeds 1 and 2.......................PUSH OUT
When committed to land: FUS TK XFER .....................................OFF APU Master.........................................OFF APU Fuel Shutoff Valve.....................PUSH IN Landing Gear......................................AS REQUIRED
The decision to land with all gear up or with any gear extended is left to pilots. Ground spoilers, thrust reversers, steering and normal brakes may not operate if any main gear is up.
No Yes
Flaps.........................................................22° If it is not possible to achieve the selected flap position, maintain airspeed according to the following:
FLAPS POSITION MIN AIRSPEED0 to 8° VREF45 + 30 KIAS
9° to 21° VREF45 + 10 KIAS22° to 44° VREF45 + 5 KIAS
45° VREF45
Apply thrust reverser (if available) after touchdown. When the airplane stops:
Engines START/STOP Selectors......STOP Fire Extinguishing Handles ..............PULL AND ROTATE APU Fuel Shutoff Valve.....................CLOSE
ICING CONDITIONS?
CONTINUES ON NEXT PAGE
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
REVISION 7 NAP-39 Q
RH
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5/1
56
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CONTINUED FROM PREVIOUS PAGE Engines and APU Fire Extinguishing
Bottles (if necessary) ...................DISCHARGE Fuel Pumps Pwr 1 and 2 ...................OFF Evacuation ......................................... INITIATE
Before leaving the airplane: Batteries 1 and 2................................OFF
Flaps ........................................................45° If it is not possible to achieve the selected flap position, maintain airspeed according to the following:
FLAPS POSITION MIN AIRSPEED0 to 8° VREF45 + 30 KIAS
9° to 21° VREF45 + 10 KIAS22° to 44° VREF45 + 5 KIAS
45° VREF45
Apply thrust reverser (if available) after touchdown. When the airplane stops:
Engines START/STOP Selectors .....STOP Fire Extinguishing Handles ..............PULL AND ROTATE APU Fuel Shutoff Valve ....................CLOSE Engines and APU Fire Extinguishing
Bottles (if necessary) ...................DISCHARGE
Fuel Pumps Pwr 1 and 2 ...................OFF Evacuation ......................................... INITIATE
Before leaving the airplane: Batteries 1 and 2................................OFF
RUDDER ARTIFICIAL FEEL INOPERATIVE
Condition: Rudder pedals become light and do not center by themselves. Yaw trim does not operate properly.
Rudder Shutoff Sys 2 .............................PUSH OUT
No Yes
Rudder Shutoff Sys 1 .............................PUSH OUT
Expect greater rudder pedal force. If required, both pilots should act together to control the airplane.
Consider the use of aileron to help in yaw control, and asymmetric thrust to trim the airplane. Avoid airports with anticipated turbulence or crosswind.
END
FAILURE PERSISTS?
END
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
NAP-40 ORIGINAL Q
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5/1
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YAW TRIM DISPLACED FROM NEUTRAL?
RUDDER/YAW TRIM RUNAWAY
Condition: Sudden uncommanded yaw.
EICAS Indication: Associated yaw trim indication changes.
Quick Disconnect Button .....................PRESS AND HOLD
Rudder Shutoff Sys 1 and 2 .................PUSH OUT
Airspeed...................................................MAX 250 KIAS
Yaw Trim Position...................................CHECK
No
Yes
Yaw Trim CB (F12) ..................................PULL
Quick Disconnect Button.......................RELEASE Rudder Shutoff Sys 1 and 2...................PUSH IN
Quick Disconnect Button.......................RELEASE
Prepare to overcome uncommanded yaw. Rudder Shutoff Sys 1 .............................PUSH IN
No
Yes
Rudder Shutoff Sys 1 .............................PUSH OUT Prepare to overcome uncommanded yaw.
Rudder Shutoff Sys 2 .............................PUSH IN
No
Yes
Rudder Shutoff Sys 2 .............................PUSH OUT
LAND AT NEAREST SUITABLE AIRPORT. Avoid airports with anticipated turbulence or crosswind.
Expect greater rudder pedals force. If required, both pilots should act together to control airplane.
Consider the use of aileron to help in yaw control, and asymmetric thrust to trim the airplane.
END
RUNAWAY PERSISTS?
RUNAWAY STILL PERSISTS?
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
ORIGINAL NAP-41
QR
H-1
35
/15
69
C
OD
E 0
1
SINGLE ENGINE BLEED OPERATION IN ICING CONDITIONS
XBleed........................................................ OPEN
Altitude ...................................................... MAX 15’000 FT, MIN MEA
If it is not possible to descend below 15’000 ft:
Icing Conditions .................................. EXIT Refer to associated anti-icing failure procedure if any message is presented.
STIFFENED ELEVATOR
Condition: Elevator control columns movement is stiffened.
EICAS Warning: AUTOPILOT FAIL (may be presented), SPS 1-2 INOP (may be presented).
EICAS Caution: STICK PUSHER FAIL (may be presented).
Autopilot .................................................... DISENGAGE
Pitch Trim .................................................. AS REQUIRED
Avoid abrupt and large elevator inputs.
Consider descent to a warmer altitude. Freezing conditions may lead to de/anti-icing fluids residues to stiffen the elevator.
No
Yes
JAMMED ELEVATOR Procedure (NAP-10)............................. ACCOMPLISH
END
END
ELEVATOR CONTROL COLUMNS MOVEMENT RECOVERED?
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
NAP-42 REVISION 3 Q
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5/1
56
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STRUCTURAL DAMAGE
LAND AT THE NEAREST SUITABLE AIRPORT. At safe altitude, evaluate airplane aero dynamical behavior and take extra caution varying airspeed and attitude. Use the flight controls with caution avoiding high maneuvering loads.
Aileron and Rudder deflection ................ MAX 30%
Airspeed under turbulence ...................... MAX 200 KIAS
No
Yes
Oxygen Masks........................................... AS REQUIRED
Altitude....................................................... MEA OR 10’000 FT, WHICHEVER IS HIGHER
When reaching 10’000 ft:
Pressurization Dump Button............ PUSH IN
Rate of Descent......................................... MAX 300 FT/MIN Land as smooth as possible.
SUSPECTED FUEL LEAK
Condition: - FMS Fuel Remaining quantity is above the MFD or EICAS total fuel indication.
- Excessive Fuel flow from one of the engines.
- Fuel imbalance develops. - Fuel quantity of a tank decreases at an
abnormal rate.
No
Yes
LAND AT THE NEAREST SUITABLE AIRPORT. XFEED ...........................................................OFF Asymmetric Thrust ......................................AS REQUIRED
Use crossfeed operation in order to achieve fuel balance.
CONTINUES ON NEXT PAGE
END
FUSELAGE DAMAGED OR SUSPECTED DAMAGED?
FMS FUEL REMAINING QUANTITY IS MORE THAN 300 KG ABOVE MFD
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
REVISION 3 NAP-43 Q
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CONTINUED FROM PREVIOUS PAGE
Set engines at the same N1 and compare the Fuel Flow indications. No Yes
At pilot’s discretion.
LAND AT THE NEAREST SUITABLE AIRPORT.
When the desired balance is achieved:
XFEED........................................................... OFF
Monitor total fuel indication on MFD Fuel Page with FMS Fuel Remaining information.
UNCOMMANDED AILERON OR ELEVATOR DISCONNECTION
Light: Amber ELEV DISC or AIL DISC on Pedestal.
Condition: One control column or control wheel moves independently of the other.
Affected Surface Disconnection
Handle...................................................... PULL If aileron is affected, aileron artificial feel not available on left side.
Avoid airports with anticipated turbulence or crosswind.
FUEL FLOW INDICATION SUGGESTS FUEL LEAK?
END
END
END
EMERGENCY/ABNORMAL PROCEDURES Non Annunciated
NAP-44 REVISION 8 Q
RH
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5/1
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01
UNRELIABLE AIRSPEED
Autopilot/Yaw Damper..................... DISENGAGE
Flight Director 1 & 2 ......................... OFF
Rudder Shutoff Sys 1....................... PUSH OUT
CAUTION: AVOID USING THE SPEEDBRAKE.
Attitude/Thrust ................................. ADJUST Maintain airplane control. Refer to Unreliable Airspeed tables (PD-2A) in the Performance Data section. Altitude and/or Vertical Speed indications may also be unreliable.
Ground speed indication is available in the FMS for reference.
VOLCANIC ASH
LAND AT THE NEAREST SUITABLE AIRPORT. Volcanic Ash Area .................................... EXIT/AVOID
APU (if available)....................................... START
Thrust Levers (if altitude permits)........... IDLE
Anti-Icing Buttons (Engine, Wing and Stabilizer........................................ PRESSED
Ice Detection Override Knob.................... ALL
ITT............................................................... MONITOR No
Affected Engine......................................... SHUT DOWN After affected engine has cooled down:
Affected Engine ................................... RESTART If the affected engine fails to restart, repeated attempts should be made immediately.
Restore systems to normal operation.
ATC............................................................. NOTIFY
END
SPEED INDICATION ON BOTH PFD BELOW 135
Yes
No
END
ITT INCREASES?
Yes
EMERGENCY/ABNORMAL PROCEDURES Index
REVISION 9 EAP 0-1
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INDEX BY EICAS MESSAGE
TYPE MESSAGE PAGE OR
INSTRUCTION
AIRPLANE FUEL LOAD EAP 9-3 APU FIRE EAP 3-3 ATTCS FAIL EAP 6-3 AUTOPILOT FAIL EAP 2-3 BAGG SMOKE S-3 BATT 1 OVTEMP EAP 5-3 BATT 2 OVTEMP EAP 5-3 BLD 1 LEAK EAP 1-4 BLD 1 OVTEMP EAP 1-5 BLD 2 LEAK EAP 1-4 BLD 2 OVTEMP EAP 1-5 BLD APU LEAK EAP 1-3 E1 ATTCS NO MRGN EAP 6-5 E1 LOW N1 Crew Awareness
E1 OIL LOW PRESS EAP 6-7 E2 ATTCS NO MRGN EAP 6-5 E2 LOW N1 Crew Awareness
E2 OIL LOW PRESS EAP 6-7 ELEC ESS XFR FAIL EAP 5-3 ENG 1 FIRE EAP 6-6 ENG 2 FIRE EAP 6-6 ENG 1-2 OUT EAP 6-3 FUEL 1 LO LEVEL EAP 9-3 FUEL 2 LO LEVEL EAP 9-3 FUEL XFER CRITICAL EAP 9-4 ICE COND-A/I INOP EAP 11-3 LAV SMOKE S-3 LG/LEVER DISAGREE EAP 12-3 MAIN DOOR OPN EAP 4-3 NO TAKEOFF CONFIG EAP 14-4 PTRIM BACKUP INOP EAP 8-3 PTRIM MAIN INOP EAP 8-3 SPS 1 INOP EAP 14-3 SPS 1-2 INOP EAP 14-3
W A R N I N G
SPS 2 INOP EAP 14-3
EMERGENCY/ABNORMAL PROCEDURES Index
EAP 0-2 REVISION 9
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TYPE MESSAGE PAGE OR
INSTRUCTION
115 VAC BUS OFF EAP 5-4 A/ICE LOW CAPACIT EAP 11-4 A/ICE SWITCH OFF EAP 11-4 ACCESS DOORS OPN EAP 4-4 AIL SYS 1 INOP EAP 8-5 AIL SYS 1-2 INOP EAP 8-5 AIL SYS 2 INOP EAP 8-5 AOA 1 HEAT INOP EAP 11-4 AOA 2 HEAT INOP EAP 11-4 AP AIL MISTRIM EAP 2-3 AP ELEV MISTRIM EAP 2-3 APU BLD VLV FAIL EAP 1-5 APU CNTOR CLSD EAP 3-4 APU EXTBTL INOP EAP 7-3 APU FAIL EAP 3-4 APU FIREDET FAIL EAP 7-3 APU FUEL LO PRESS EAP 3-5 APU FUEL SOV INOP EAP 9-5 APU GEN OFF BUS EAP 5-12 APU GEN OVLD EAP 5-12 APU OIL HI TEMP EAP 3-6 APU OIL LO PRESS EAP 3-6 AURAL WARN FAIL EAP 14-6 AUTO TRIM FAIL EAP 2-3 BAGG ACCESS OPN EAP 4-5 BAGG EXTBTL INOP EAP 7-4 BAGGAGE DOOR OPN EAP 4-4 BATT1 OFF BUS EAP 5-4 BATT2 OFF BUS EAP 5-4 BKUP BATT OFF BUS EAP 5-4 BLD 1 LOW TEMP EAP 1-6 BLD 1 VLV FAIL EAP 1-7 BLD 2 LOW TEMP EAP 1-6 BLD 2 VLV FAIL EAP 1-7 BRAKE DEGRADED EAP 12-5 BRAKE OVERHEAT EAP 12-4 BRK INBD INOP EAP 12-6 BRK OUTBD INOP EAP 12-6 CHECK IC 1 SW Crew Awareness
CHECK IC 2 SW Crew Awareness
CHECK PFD 1 EAP 2-6
CHECK PFD 2 EAP 2-6
C A U T I O N
CHK IC CONFIG Crew Awareness
EMERGENCY/ABNORMAL PROCEDURES Index
REVISION 9 EAP 0-3
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TYPE MESSAGE PAGE OR
INSTRUCTION
CLR ICE 1 Crew Awareness
CLR ICE 2 Crew Awareness
CLR /I INOP 1 Crew Awareness
CLR /I INOP 2 Crew Awareness
CREW OXY LO PRESS EAP 13-3 CROSS BLD FAIL EAP 1-8 CROSS BLD SW OFF Crew Awareness
DAU AC ID MISCMP Crew Awareness
DAU1 A FAIL EAP 2-4 DAU1 ENG MISCOMP EAP 2-5 DAU1 SYS MISCOMP EAP 2-5 DAU1 WRN MISCOMP EAP 2-5 DAU2 A FAIL EAP 2-4 DAU2 ENG MISCOMP EAP 2-5 DAU2 SYS MISCOMP EAP 2-5 DAU2 WRN MISCOMP EAP 2-5 DC BUS 1 OFF EAP 5-5 DC BUS 2 OFF EAP 5-6 DFDR FAIL Crew Awareness
E1 A/ICE FAIL EAP 11-5 E1 ATS SOV OPN EAP 6-8 E1 CTL FAIL EAP 6-9 E1 EXCEEDANCE Crew Awareness
E1 EXTBTLA INOP EAP 7-5 E1 EXTBTLB INOP EAP 7-5 E1 FIREDET FAIL EAP 7-4 E1 FPMU NO DISP Crew Awareness
E1 FUEL LO PRESS EAP 9-6 E1 FUEL LO TEMP EAP 9-7 E1 FUEL SOV INOP EAP 9-7 E1 NO DISP Crew Awareness
E2 A/ICE FAIL EAP 11-5 E2 ATS SOV OPN EAP 6-8 E2 CTL FAIL EAP 6-9 E2 EXCEEDANCE Crew Awareness
E2 EXTBTLA INOP EAP 7-5 E2 EXTBTLB INOP EAP 7-5 E2 FIREDET FAIL EAP 7-4 E2 FPMU NO DISP Crew Awareness
E2 FUEL LO PRESS EAP 9-6 E2 FUEL LO TEMP EAP 9-7 E2 FUEL SOV INOP EAP 9-7 E2 NO DISP Crew Awareness
ELEC EMERG ABNORM EAP 5-7
C A U T I O N
ELEKBAY OVTEMP EAP 2-7
EMERGENCY/ABNORMAL PROCEDURES Index
EAP 0-4 REVISION 9
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TYPE MESSAGE PAGE OR
INSTRUCTION
EMERG EXIT OPN EAP 4-5 EMERG LT NOT ARMD EAP 5-7 EMRG BRK LO PRES EAP 12-7 ENG NO TO DATA Crew Awareness
ENG REF A/I DISAG Crew Awareness
ENG1 OUT EAP 6-10 ENG1 REV DISAGREE EAP 6-12 ENG1 REV FAIL EAP 6-12 ENG1 TLA FAIL EAP 6-11 ENG2 OUT EAP 6-10 ENG2 REV DISAGREE EAP 6-12 ENG2 REV FAIL EAP 6-12 ENG2 TLA FAIL EAP 6-11 ESS BUS 1 OFF EAP 5-8 ESS BUS 1-2 OFF EAP 5-10 ESS BUS 2 OFF EAP 5-9 FADEC ID NO DISP Crew Awareness
FLAP FAIL EAP 8-6 FUEL IMBALANCE EAP 9-13 FUEL TANK LO TEMP EAP 9-9 FUEL TK VENT OPEN EAP 9-10 FUEL XFEED FAIL EAP 9-8 FUEL XFEED MISCMD EAP 9-9 FUEL XFER 1 INOP EAP 9-11 FUEL XFER 2 INOP EAP 9-11 FUEL XFER CHECK EAP 9-10 FUEL XFER OVFLOW EAP 9-16 FUELING DOOR OPN Crew Awareness FUSELAGE FUEL IMB EAP 9-13 GEN 1-2-3-4 OFF BUS EAP 5-13 GEN 1 OFF BUS EAP 5-12 GEN 1 OVLD EAP 5-12 GEN 2 OFF BUS EAP 5-12 GEN 2 OVLD EAP 5-12 GEN 3 OFF BUS EAP 5-12 GEN 3 OVLD EAP 5-12 GEN 4 OFF BUS EAP 5-12 GEN 4 OVLD EAP 5-12 HGS FAIL Crew Awareness
HS VLV 1 FAIL EAP 1-8 HS VLV 2 FAIL EAP 1-8 HYD SYS 1 FAIL EAP 10-5 HYD SYS 1 OVHT EAP 10-8 HYD SYS 1-2 FAIL EAP 10-3 HYD SYS 2 FAIL EAP 10-6 HYD SYS 2 OVHT EAP 10-8 IC 1 OVERHEAT EAP 2-9
C A U T I O N
IC 1 WOW INOP Crew Awareness
EMERGENCY/ABNORMAL PROCEDURES Index
REVISION 9 EAP 0-5
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TYPE MESSAGE PAGE OR
INSTRUCTION
IC 2 OVERHEAT EAP 2-9 IC 2 WOW INOP Crew Awareness
IC BUS FAIL EAP 2-8 ICE DET1 FAIL EAP 11-5 ICE DET2 FAIL EAP 11-5 ICE DETECTORS FAIL EAP 11-5 IRS 1 ALN FAULT EAP 2-9 IRS 1 FAIL EAP 2-10 IRS 1 OVERHEAT EAP 2-11 IRS 2 ALN FAULT EAP 2-9 IRS 2 FAIL EAP 2-10 IRS 2 OVERHEAT EAP 2-11 LATERAL MODE OFF EAP 2-7 LG AIR/GND FAIL EAP 12-8 NLG UP/DOOR OPN EAP 12-9 NO ICE-A/ICE ON EAP 11-6 PACK 1 OVHT EAP 1-9 PACK 1 OVLD EAP 1-10 PACK 1 VLV FAIL EAP 1-11 PACK 2 OVHT EAP 1-9 PACK 2 OVLD EAP 1-10 PACK 2 VLV FAIL EAP 1-11 PAX OXY LO PRESS EAP 13-3 PITOT 1 INOP EAP 11-6 PITOT 2 INOP EAP 11-6 PITOT 3 INOP EAP 11-6 PRESN AUTO FAIL EAP 1-12 PTRIM BKP SW FAIL EAP 8-8 PTRIM CPT SW FAIL EAP 8-8 PTRIM F/O SW FAIL EAP 8-8 RAM AIR VLV FAIL EAP 1-13 RUD HDOV PROTFAIL EAP 8-8 RUDDER OVERBOOST EAP 8-9 RUDDER SYS 1 INOP EAP 8-10 RUDDER SYS 1-2 INOP EAP 8-10 RUDDER SYS 2 INOP EAP 8-10 RUD STOP DISAGREE EAP 8-8 SHED BUS 1 OFF Crew Awareness
SHED BUS 2 OFF Crew Awareness
SPBK LVR DISAGREE EAP 8-11 SPC FAIL Crew Awareness
SPOILER FAIL EAP 8-7 SPS ADVANCED EAP 14-5 STAB A/ICE FAIL EAP 11-8 STEER INOP EAP 12-9
C A U T I O N
STICK PUSHER FAIL EAP 14-7
EMERGENCY/ABNORMAL PROCEDURES Index
EAP 0-6 REVISION 9
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TYPE MESSAGE PAGE OR
INSTRUCTION
TAT 1 HEAT INOP EAP 11-7 TAT 2 HEAT INOP EAP 11-7 TERR INOP EAP 14-6 VERTICAL MODE OFF EAP 2-7 W/S 1 HEAT FAIL EAP 11-7 W/S 2 HEAT FAIL EAP 11-7 WG A/ICE FAIL EAP 11-8 WINDSHEAR INOP EAP 14-8 WING FUEL IMBALANCE EAP 9-15
C A U T I O N
YAW DAMPER FAIL EAP 2-12
EMERGENCY/ABNORMAL PROCEDURES Index
REVISION 10 EAP 0-7
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TYPE MESSAGE PAGE OR
INSTRUCTION
AIII NOT AVAIL Crew Awareness
APU FUEL SOV CLSD Crew Awareness
BLD 1 VLV CLSD EAP 1-14 BLD 2 VLV CLSD EAP 1-14 CHECK A1E PERF Crew Awareness
CHECK A1P PERF Crew Awareness
CMC FAIL Crew Awareness
CONFIG MISMATCH Crew Awareness
CROSS BLD OPEN Crew Awareness
DATALINK FAIL Crew Awareness
DAU1 B FAIL EAP 2-4 DAU 1 REVERSION Crew Awareness
DAU2 B FAIL EAP 2-4 DAU 2 REVERSION Crew Awareness
DU 1 FAN FAIL Crew Awareness
DU 1 OVHT Crew Awareness
DU 2 FAN FAIL Crew Awareness
DU 2 OVHT Crew Awareness
DU 3 FAN FAIL Crew Awareness
DU 3 OVHT Crew Awareness
DU 4 FAN FAIL Crew Awareness
DU 4 OVHT Crew Awareness
DU 5 FAN FAIL Crew Awareness
DU 5 OVHT Crew Awareness
E1 FUEL IMP BYP EAP 6-12 E1 FUELSOV CLSD Crew Awareness
E1 HYD PUMP FAIL EAP 10-8 E1 HYDSOV CLSD Crew Awareness
E1 IDL STP FAIL EAP 6-13 E1 OIL IMP BYP Crew Awareness
E1 SHORT DISP Crew Awareness
E1-2 HYD PUMP FAIL EAP 10-3 E2 FUEL IMP BYP EAP 6-12 E2 FUELSOV CLSD Crew Awareness
E2 HYD PUMP FAIL EAP 10-8 E2 HYDSOV CLSD Crew Awareness
E2 IDL STP FAIL EAP 6-13 E2 OIL IMP BYP Crew Awareness
E2 SHORT DISP Crew Awareness
ENG A/ICEOVERPRES Crew Awareness
A D V I S O R Y
FDAU FAIL Crew Awareness
EMERGENCY/ABNORMAL PROCEDURES Index
EAP 0-8 REVISION 10
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INSTRUCTION
FLAP LOW SPEED EAP 8-11 FUEL XFEED OPEN Crew Awareness
GEN1 BRG FAIL Crew Awareness
GEN2 BRG FAIL Crew Awareness
GEN3 BRG FAIL Crew Awareness
GEN4 BRG FAIL Crew Awareness
HI ALT LDG-T/O Crew Awareness
HYD PUMP SELEC OF Crew Awareness HYD1 LO QTY EAP 10-9 HYD2 LO QTY EAP 10-9 IC1 CONFIG FAIL Crew Awareness IC 1 FAN FAIL Crew Awareness IC2 CONFIG FAIL Crew Awareness IC 2 FAN FAIL Crew Awareness ICE CONDITION Crew Awareness SPS/ICE SPEEDS Crew Awareness IRS 1 ALN EAP 2-12 IRS 1 ATT MODE EAP 2-13 IRS 1 EXC MOTION Crew Awareness
IRS 1 NO MAG HDG Crew Awareness
IRS 1 NO PPOS Crew Awareness
IRS 1 ON BATT EAP 2-14 IRS 2 ALN EAP 2-12 IRS 2 ATT MODE EAP 2-13 IRS 2 EXC MOTION Crew Awareness
IRS 2 NO MAG HDG Crew Awareness
IRS 2 NO PPOS Crew Awareness
IRS 2 ON BATT EAP 2-14 PACK 1 VLV CLSD EAP 1-14 PACK 2 VLV CLSD EAP 1-14 RAAS INHIBITED Crew Awareness
RAAS NOT AVAIL Crew Awareness
RAD ALT 1 FAIL EAP 2-14 RAD ALT 2 FAIL EAP 2-14 RAD ALT FAIL EAP 2-14 SATCOM FAIL Crew Awareness
A D V I S O R Y
VHF 3 FAIL Crew Awareness
EMERGENCY/ABNORMAL PROCEDURES Air Conditioning, Pneumatics & Pressurization
ORIGINAL EAP 1-1
TABLE OF CONTENTS
ANNUNCIATED PROCEDURES
BLEED APU LEAK...............................................EAP 1-3
BLEED ENGINE LEAK.........................................EAP 1-4
BLEED OVERTEMPERATURE............................EAP 1-5
APU BLEED VALVE FAILURE............................EAP 1-5
BLEED LOW TEMPERATURE ............................EAP 1-6
BLEED VALVE FAILURE.....................................EAP 1-7
CABIN DEPRESSURIZATION .............................EAP 1-12
CROSSBLEED FAILURE.....................................EAP 1-8
HIGH STAGE VALVE FAILURE ..........................EAP 1-8
PACK OVERHEAT ...............................................EAP 1-9
PACK OVERLOAD...............................................EAP 1-10
PACK VALVE FAILURE.......................................EAP 1-11
PRESSURIZATION AUTOMATIC SYSTEM FAILURE / CABIN DEPRESSURIZATION......EAP 1-12
RAM AIR VALVE FAILURE .................................EAP 1-13
BLEED VALVE CLOSED .....................................EAP 1-14
PACK VALVE CLOSED .......................................EAP 1-14
NON ANNUNCIATED PROCEDURES
AIR CONDITIONING SMOKE. .................. refer to S-4
EMERGENCY DESCENT.......................... refer to NAP-6
RAPID CABIN DEPRESSURIZATION ...... refer to NAP-14
LOSS OF PRESSURIZATION INDICATION.......................................... refer to NAP-31
SINGLE ENGINE BLEED OPERATION IN ICING CONDITIONS .. refer to NAP-41
EMERGENCY/ABNORMAL PROCEDURES Air Conditioning, Pneumatics & Pressurization
EAP 1-2 ORIGINAL
LIST OF EICAS MESSAGES
BLD APU LEAK .................................................EAP 1-3
BLD 1 (2) LEAK .................................................EAP 1-4
BLD 1 (2) OVTEMP............................................EAP 1-5 APU BLD VLV FAIL ...........................................EAP 1-5
BLD 1 (2) LOW TEMP........................................EAP 1-6
BLD 1 (2) VLV FAIL ...........................................EAP 1-7
CROSS BLD FAIL..............................................EAP 1-8
HS VLV 1 (2) FAIL..............................................EAP 1-8
PACK 1 (2) OVHT ..............................................EAP 1-9
PACK 1 (2) OVLD ..............................................EAP 1-10
PACK 1 (2) VLV FAIL ........................................EAP 1-11
PRESN AUTO FAIL ...........................................EAP 1-12
RAM AIR VLV FAIL............................................EAP 1-13
BLD 1 (2) VLV CLSD .........................................EAP 1-14
PACK 1 (2) VLV CLSD.......................................EAP 1-14
EMERGENCY/ABNORMAL PROCEDURES Air Conditioning, Pneumatics & Pressurization
ORIGINAL EAP 1-3
BLEED APU LEAK
EICAS Warning: BLD APU LEAK
APU Bleed......................................... PUSH OUT Bleed 1 and 2 .................................... AS REQUIRED
...................................................... WAIT 3 MINUTES
No
Yes
APU.................................................... SHUTDOWN
No
Yes
BLEED ENGINE LEAK Procedure (EAP 1-4).................... ACCOMPLISH
Start the procedure considering BLD 1 LEAK.
MESSAGE PERSISTS?
END
END
MESSAGE STILL PERSISTS?
EMERGENCY/ABNORMAL PROCEDURES Air Conditioning, Pneumatics & Pressurization
EAP 1-4 ORIGINAL
BLEED ENGINE LEAK
EICAS Warning: BLD 1 (2) LEAK Light: Red LEAK inscription in affected push
button.
Consider diversion. XBleed ............................................... CLOSED Affected Bleed .................................. PUSH OUT APU Bleed......................................... PUSH OUT Altitude.............................................. MAX 25’000 FT,
MIN MEA Icing Conditions ............................... EXIT/AVOID
...................................................... WAIT 3 MINUTES No
Yes
BLD 1 (2) VLV FAIL
BLD 1 (2) VLV CLSD
Opposite Bleed................................. PUSH OUT Associated Bleed ............................. PUSH IN
...................................................... WAIT 3 MINUTES
No
Yes
Associated Bleed ............................. PUSH OUT Oxygen Masks .................................. AS REQUIRED Altitude.............................................. MEA OR
10’000 FT, WHICHEVER IS HIGHER
Associated Thrust Lever ................. IDLE
...................................................... WAIT 3 MINUTES
CONTINUES ON NEXT PAGE
BLD 1 (2 OR APU) LEAK MESSAGE EXTINGUISHES?
END
END
ASSOCIATED MESSAGE?
BLD 1 (2 OR APU) LEAK MESSAGE PERSISTS?
EMERGENCY/ABNORMAL PROCEDURES Air Conditioning, Pneumatics & Pressurization
ORIGINAL EAP 1-5
CONTINUED FROM PREVIOUS PAGE No Yes
Associated ENGINE FAILURE/SHUTDOWN Procedure (NAP-23)..................... ACCOMPLISH
BLEED OVERTEMPERATURE EICAS Warning: BLD 1 (2) OVTEMP MFD Indication: Bleed Temp pointer may be in red
range or out of view. XBleed ............................................... OPEN
Associated Bleed ............................. PUSH OUT Altitude.............................................. MAX 25’000 FT,
MIN MEA
...................................................... WAIT 3 MINUTES No
Associated Bleed ............................. PUSH IN Opposite Bleed................................. PUSH OUT
SINGLE ENGINE BLEED OPERATION IN ICING CONDITIONS Procedure (NAP-41)..................... AS REQUIRED
APU BLEED VALVE FAILURE EICAS Caution: APU BLD VLV FAIL
No
Yes
No
Yes
APU.................................................... SHUTDOWN
Bleeds 1 and 2 .................................. AS REQUIRED
FAILED IN THE OPEN POSITION?
ANY BLEED LEAK EXISTS?
END
END
BLD 1 (2 or APU) LEAK MESSAGE PERSISTS?
END
BLD 1 (2) OVTEMP MESSAGE PERSISTS?
Yes
EMERGENCY/ABNORMAL PROCEDURES Air Conditioning, Pneumatics & Pressurization
EAP 1-6 REVISION 9
BLEED LOW TEMPERATURE EICAS Caution: BLD 1 (2) LOW TEMP
MFD Indication: Bleed Temp pointer may be amber or may be out of view.
No
Yes
Message ............................................ DISREGARD
Ice Detection Override Knob........... ALL Associated Thrust Lever ................. ADVANCE
Adjust affected Thrust Lever until message disappears or pointer of the affected side reaches green range or opposite pointer.
...................................................... WAIT 1 MINUTE No
Yes
Affected Bleed .................................. PUSH OUT Altitude.............................................. MAX 25’000 FT,
MIN MEA
No
Yes
XBleed ............................................... OPEN Altitude.............................................. MAX 15’000 FT,
MIN MEA If it is not possible to descend below 15’000 ft:
Ice Conditions.............................. EXIT
...................................................... WAIT 2 MINUTES Ice Detection Override Knob........... AUTO
Ice Detection Override Knob........... AUTO
END
END
BLEED TEMP IN GREEN RANGE OR POINTER OUT OF VIEW?
MESSAGE PERSISTS?
END
ICING CONDITIONS?
EMERGENCY/ABNORMAL PROCEDURES Air Conditioning, Pneumatics & Pressurization
ORIGINAL EAP 1-7
BLEED VALVE FAILURE EICAS Caution: BLD 1 (2) VLV FAIL
No
Yes
Bleed 2
Bleed 1
No
Yes
XBleed ............................................... CLOSED APU.................................................... START Altitude.............................................. MAX 37’000 FT,
MIN MEA APU Bleed......................................... PUSH IN SINGLE ENGINE BLEED OPERATION
IN ICING CONDITIONS Procedure (NAP-41)..................... AS REQUIRED
XBleed ............................................... OPEN Altitude.............................................. MAX 25’000 FT,
MIN MEA SINGLE ENGINE BLEED OPERATION
IN ICING CONDITIONS Procedure (NAP-41)..................... AS REQUIRED
END
APU SERVICEABLE?
BLD 1 (2) VLV CLSD MESSAGE PRESENTED?
END
AFFECTED BLEED VALVE?
EMERGENCY/ABNORMAL PROCEDURES Air Conditioning, Pneumatics & Pressurization
EAP 1-8 ORIGINAL
CROSSBLEED FAILURE EICAS Caution: CROSS BLD FAIL
No
Yes
No
Yes
Consider diversion. Bleeds 1 and 2 .................................. PUSH OUT APU Bleed......................................... PUSH OUT Icing Conditions ............................... EXIT/AVOID Oxygen Masks .................................. AS REQUIRED Altitude.............................................. MEA OR 10’000 FT,
WHICHEVER IS HIGHER
HIGH STAGE VALVE FAILURE EICAS Caution: HS VLV 1 (2) FAIL
Yes
Associated BLEED OVERTEMPERATURE Procedure (EAP 1-5).................... ACCOMPLISH
Yes
Associated BLEED LOW TEMPERATURE Procedure (EAP 1-6).................... ACCOMPLISH
CROSS BLD OPEN MESSAGE PRESENTED?
END
ASSOCIATED MFD BLEED POINTER INDICATES RED RANGE?
END
ASSOCIATED TO BLEED LEAK OR ENGINE OVERTEMPERATURE?
END
ASSOCIATED MFD BLEED POINTER INDICATES WHITE RANGE?
END
No
No
EMERGENCY/ABNORMAL PROCEDURES Air Conditioning, Pneumatics & Pressurization
REVISION 10 EAP 1-9
PACK OVERHEAT EICAS Caution: PACK 1 (2) OVHT
Associated Temperature & Mode Selector .............................. AUTO/FULL COLD
Cabin Temperature .......................... MONITOR Affected Pack ................................... PUSH OUT
...................................................... WAIT 3 MINUTES Affected Pack ................................... PUSH IN
No
Yes
Associated Temperature & Mode Selector .............................. MANUAL/FULL
COLD Cabin Temperature .......................... MONITOR Affected Pack ................................... PUSH OUT
...................................................... WAIT 3 MINUTES Affected Pack ................................... PUSH IN
No
Yes
Affected Pack ..................................PUSH OUT No
Yes
Oxygen Masks .................................. AS REQUIRED Altitude.............................................. MEA OR 10’000 FT,
WHICHEVER IS HIGHER
At least one bleed source must be kept open. When reaching 10’000 ft:
Cabin............................................. DEPRESSURIZE
Altitude.............................................. MAX 25’000 FT, MIN MEA
MESSAGE PERSISTS?
MESSAGE PERSISTS?
END
END
END
BOTH PACKS AFFECTED?
EMERGENCY/ABNORMAL PROCEDURES Air Conditioning, Pneumatics & Pressurization
EAP 1-10 REVISION 10
PACK OVERLOAD EICAS Caution: PACK 1 (2) OVLD
Recirculation Fan .......................... PUSH IN Associated Temperature &
Mode Selector ........................... AUTO/ 12 O’CLOCK POSITION
Affected Pack ................................ PUSH OUT
................................................... WAIT 3 MINUTES Affected Pack ................................ PUSH IN
No
Yes
Associated Temperature & Mode Selector ........................... MANUAL/
12 O’CLOCK POSITION
Affected Pack ................................ PUSH OUT
................................................... WAIT 3 MINUTES Affected Pack ................................ PUSH IN No Yes
Affected Pack ................................ PUSH OUT Associated Engine Bleed ............. CHECK PUSHED IN
No
Yes
Oxygen Masks ............................... AS REQUIRED Altitude........................................... MEA OR 10’000 FT,
WHICHEVER IS HIGHER
At least one bleed source must be kept open. When reaching 10’000 ft:
Cabin.......................................... DEPRESSURIZE
Altitude........................................... MAX 25’000 FT,
MIN MEA
BOTH PACKS AFFECTED?
END
MESSAGE PERSISTS?
END
MESSAGE STILL PERSISTS?
EMERGENCY/ABNORMAL PROCEDURES Air Conditioning, Pneumatics & Pressurization
REVISION 5 EAP 1-11
PACK VALVE FAILURE EICAS Caution: PACK 1 (2) VLV FAIL
No
Yes
Altitude........................................... MAX 25’000 FT, MIN MEA
No
Yes
Oxygen Masks ............................... AS REQUIRED Altitude........................................... MEA OR 10’000 FT,
WHICHEVER IS HIGHER
When reaching 10’000 ft: Cabin.......................................... DEPRESSURIZE
Yes
Altitude........................................... MAX 25’000 FT, MIN MEA
Pack 2
Pack 1 or Both Packs
APU Bleed...................................... PUSH OUT
XBleed ............................................ CLOSED Associated Bleed(s)...................... PUSH OUT Icing Conditions ............................ EXIT/AVOID
No
Yes
Oxygen Masks ............................... AS REQUIRED Altitude........................................... MEA OR 10’000 FT,
WHICHEVER IS HIGHER
At least one bleed source must be kept open. When reaching 10’000 ft:
Cabin.......................................... DEPRESSURIZE
PACK 1 (2) VLV CLSD MESSAGE PRESENTED?
END
BOTH PACKS AFFECTED?
END
AFFECTED PACK(S)?
NEED TO CLOSE THE AFFECTED PACK?
BOTH PACKS AFFECTED?
No
EMERGENCY/ABNORMAL PROCEDURES Air Conditioning, Pneumatics & Pressurization
EAP 1-12 REVISION 5
PRESSURIZATION AUTOMATIC SYSTEM FAILURE/CABIN DEPRESSURIZATION
EICAS Caution: PRESN AUTO FAIL may be presented.
EICAS Indication: Abnormal cabin altitude (amber or red) may be presented.
Pressurization Manual Controller ........11 O'CLOCK
POSITION At least one bleed source must be kept open. Pressurization Mode Selector ..............PUSH IN (MAN) Pressurization Manual Controller ........AS REQUIRED
Wait for system response and stabilization.
No
Yes
Cabin Altitude........................................CONTROL Set and control cabin altitude according to the AIRPLANE/CABIN ALTITUDE conversion table on NAP-31.
No
Yes
RAPID CABIN DEPRESSURIZATION Procedure (NAP-14)..........................ACCOMPLISH
Oxygen Masks .......................................AS REQUIRED Altitude...................................................MEA OR
10’000 FT, WHICHEVER IS HIGHER
When reaching 10’000 ft: Pressurization Manual Controller ...FULL DOWN Pressurization Mode Selector .........PUSH OUT Pressurization Dump Button ...........PUSH IN (ON)
MANUAL CONTROL POSSIBLE?
END
CABIN AURAL WARNING VOICE MESSAGE SOUNDS?
END
END
EMERGENCY/ABNORMAL PROCEDURES Air Conditioning, Pneumatics & Pressurization
REVISION 5 EAP 1-13
RAM AIR VALVE FAILURE EICAS Caution: RAM AIR VLV FAIL
Air Conditioning System ................. MONITOR
No
Yes
Associated Pack............................... PUSH OUT Altitude.............................................. MAX 25’000 FT,
MIN MEA No
Yes
Oxygen Masks .................................. AS REQUIRED Altitude.............................................. MEA OR 10’000 FT,
WHICHEVER IS HIGHER
At least one bleed source must be kept open. When reaching 10’000 ft:
Cabin............................................. DEPRESSURIZE
ANY PACK 1 (2) OVLD OR PACK 1 (2) OVHTMESSAGE PRESENTED?
BOTH PACKS AFFECTED?
END
EMERGENCY/ABNORMAL PROCEDURES Air Conditioning, Pneumatics & Pressurization
EAP 1-14 REVISION 4
BLEED VALVE CLOSED EICAS Advisory: BLD 1 (2) VLV CLSD
Associated Pack............................... PUSH OUT, THEN PUSH IN
Associated Bleed ............................. PUSH IN
No
Yes
Affected BLEED VALVE FAILURE Procedure (EAP 1-7).................... ACCOMPLISH
PACK VALVE CLOSED EICAS Advisory: PACK 1 (2) VLV CLSD
Associated Pack............................... PUSH OUT, THEN PUSH IN
No
Yes
No
Yes
Oxygen Masks .................................. AS REQUIRED Altitude.............................................. MEA OR
10’000 FT, WHICHEVER IS HIGHER
When reaching 10’000 ft, if at least one bleed source is available:
Pressurization Mode Selector.................................... PUSH IN
Pressurization Manual Controller................................. AS REQUIRED
If required: Pressurization Manual
Controller ............................ FULL UP
Altitude...................................................MAX 25’000 FT,
MIN MEA
END
MESSAGE PERSISTS?
MESSAGE PERSISTS?
END
BOTH PACKS AFFECTED?
END
EMERGENCY/ABNORMAL PROCEDURES Autopilot, Flight Instruments & Navigation
ORIGINAL EAP 2-1
TABLE OF CONTENTS
ANNUNCIATED PROCEDURES
AUTOPILOT FAILURE........................................EAP 2-3
AUTOPILOT AILERON MISTRIM .......................EAP 2-3
AUTOPILOT ELEVATOR MISTRIM....................EAP 2-3
AUTOPILOT TRIM FAILED.................................EAP 2-3
DAU FAILURE.....................................................EAP 2-4
DAU MISCOMPARE............................................EAP 2-5
DISPLAY FAILURE .............................................EAP 2-6
ELECTRONIC BAY OVERTEMPERATURE.......EAP 2-7
FD LATERAL MODE OFF...................................EAP 2-7
FD VERTICAL MODE OFF..................................EAP 2-7
IC BUS FAILURE ................................................EAP 2-8
IC FAILURE .........................................................EAP 2-8
IC OVERHEAT.....................................................EAP 2-9
IRS ALIGNMENT FAULT ....................................EAP 2-9
IRS FAIL ..............................................................EAP 2-10
IRS OVERHEAT ..................................................EAP 2-11
YAW DAMPER FAILURE....................................EAP 2-12
IRS ALIGNMENT.................................................EAP 2-12
IRS ATTITUDE MODE.........................................EAP 2-13
IRS ON BATTERY...............................................EAP 2-14
RADIO ALTIMETER FAIL ...................................EAP 2-14
NON ANNUNCIATED PROCEDURES
CAS MESSAGE MISCOMPARISON......refer to NAP-17
IRS/MSU FAILURE ANNUNCIATION ....refer to NAP-29
NAV/FLIGHT INSTRUMENTS FAILURE ..............................................refer to NAP-33
EMERGENCY/ABNORMAL PROCEDURES Autopilot, Flight Instruments & Navigation
EAP 2-2 ORIGINAL
LIST OF EICAS MESSAGES
AUTOPILOT FAIL................................................EAP 2-3
AP AIL MISTRIM .................................................EAP 2-3
AP ELEV MISTRIM..............................................EAP 2-3
AUTO TRIM FAIL ................................................EAP 2-3
CHECK PFD 1 (2) ................................................EAP 2-6
DAU1 (2) A FAIL..................................................EAP 2-4
DAU1 (2) ENG MISCOMP ...................................EAP 2-5
DAU1 (2) SYS MISCOMP....................................EAP 2-5
DAU1 (2) WRN MISCOMP ..................................EAP 2-5
ELEKBAY OVTEMP............................................EAP 2-7
IC BUS FAIL ........................................................EAP 2-8
IC 1 (2) OVERHEAT ............................................EAP 2-9
IRS 1 (2) ALN FAULT..........................................EAP 2-9
IRS 1 (2) FAIL......................................................EAP 2-10
IRS 1 (2) OVERHEAT..........................................EAP 2-11
LATERAL MODE OFF.........................................EAP 2-7
VERTICAL MODE OFF .......................................EAP 2-7
YAW DAMPER FAIL ...........................................EAP 2-12
IRS 1 (2) ALN ......................................................EAP 2-12
IRS 1 (2) ATT MODE ...........................................EAP 2-13
IRS 1 (2) ON BATT..............................................EAP 2-14
RAD ALT 1 (2) FAIL ............................................EAP 2-14
RAD ALT FAIL.....................................................EAP 2-14
EMERGENCY/ABNORMAL PROCEDURES Autopilot, Flight Instruments & Navigation
REVISION 8 EAP 2-3
AUTOPILOT FAILURE
EICAS Warning: AUTOPILOT FAIL Aural Warning: AUTOPILOT Voice message (only
below 2500 ft Radio Altitude, when autopilot is disconnected).
No
Yes
Autopilot ................................................DISENGAGE Autopilot Disengagement.....................CHECK Trim ........................................................AS REQUIRED
AUTOPILOT AILERON MISTRIM
EICAS Caution: AP AIL MISTRIM for more than 10 s. Condition: Autopilot is engaged with aileron out
of trim.
Control Wheel........................................HOLD FIRMLY Quick Disconnect Button .....................PRESS Roll Trim.................................................AS REQUIRED Yaw Trim ................................................AS REQUIRED Autopilot ................................................AS REQUIRED
AUTOPILOT ELEVATOR MISTRIM
EICAS Caution: AP ELEV MISTRIM Condition: Autopilot is engaged with pitch out of
trim.
Control Column .....................................HOLD FIRMLY Quick Disconnect Button .....................PRESS Pitch Trim...............................................AS REQUIRED Autopilot ................................................AS REQUIRED
AUTOPILOT TRIM FAILED
EICAS Caution: AUTO TRIM FAIL
Control Column .....................................HOLD FIRMLY Quick Disconnect Button .....................PRESS Pitch Trim...............................................AS REQUIRED Autopilot ................................................AS REQUIRED
END
END
END
END
MESSAGE PRESENTED ON MFD?
EMERGENCY/ABNORMAL PROCEDURES Autopilot, Flight Instruments & Navigation
EAP 2-4 ORIGINAL
DAU FAILURE
EICAS Caution: DAU1 (2) A FAIL
The following message may be displayed: EICAS Advisory: DAU1 (2) B FAIL
No
Yes
No
Yes
Associated DAU on EICAS Rev (Pedestal Panel) ............PUSH IN
DAU 2
DAU 1
- Lost Indications: engine 1 oil (temperature, pressure and level), battery 1 and 2 temperature, fuel tank temperature, roll trim position, cockpit temperature, bleed 1 temperature and landing gear position (including RMU indication).
- Lost Messages: FUEL TANK LO TEMP, E1 FUEL LO TEMP, BLEED 1 OVTEMP.
- BLD 1 LOW TEMP message will appear.
- Lost Indications: engine 2 oil (temperature, pressure and level), engine 2 fuel temperature, hydraulic quantity 1 and 2, yaw trim position, cabin temperature, bleed 2 temperature and flaps indication (including RMU indication).
- Lost Messages: BLEED 2 OVTEMP, E2 FUEL LO TEMP, HYD 1 LO QTY, HYD 2 LO QTY.
- BLD 2 LOW TEMP and APU OIL HI TEMP messages will appear.
CONTINUES ON NEXT PAGE
END
ONLY CHANNEL B AFFECTED?
ONLY CHANNEL A AFFECTED?
END
WHICH DAU IS AFFECTED?
END
EMERGENCY/ABNORMAL PROCEDURES Autopilot, Flight Instruments & Navigation
ORIGINAL EAP 2-5
CONTINUED FROM PREVIOUS PAGE
LAND AT THE NEAREST SUITABLE AIRPORT. DAU 2
DAU 1
- All messages and indications of the following systems are lost: Oxygen, Steering, Landing Gear, Roll Trim, and the message EMERG LIGHT NOT ARMED.
- Some messages and indications of the following system are lost: Doors, Stall Protection, Electrical, Fire Protection, Fuel, APU, Power Plant, Thrust Reverser, Spoiler, Brakes, Air Conditioning, Ice and Rain Protection.
- All messages and indications of the following systems are lost: Smoke, Hydraulic, Rudder and Yaw Trim.
- Some messages and indications of the following systems are lost: Doors, Stall Protection, Electrical, Fire Protection, Fuel, APU, Power Plant, Thrust Reverser, Flap, Brakes, Air Conditioning, Ice and Rain Protection.
DAU MISCOMPARE
EICAS Caution: DAU1 (2) ENG MISCOMP or DAU1 (2) SYS MISCOMP or DAU1 (2) WRN MISCOMP
Associated DAU on EICAS Rev (Pedestal Panel) ............PUSH IN
NOTE: For each miscompare message and each side, check the following parameters before and after the reversion:
- Engine: N1, N2, ITT. - System: Battery voltage and temperature, Takeoff
temperature, Hydraulic pressure, Oxygen pressure. - Warning: all warning messages, if any.
END
END
WHICH DAU IS AFFECTED?
END
EMERGENCY/ABNORMAL PROCEDURES Autopilot, Flight Instruments & Navigation
EAP 2-6 ORIGINAL
DISPLAY FAILURE
EICAS Caution: CHECK PFD 1 (2) message is presented if PFD is the failed display.
No
Yes
IC FAILURE/IC BUS FAILURE Procedure (EAP 2-8).........................ACCOMPLISH
No
Yes
LAND AT THE NEAREST SUITABLE AIRPORT. Icing Conditions ....................................AVOID/EXIT RMU ........................................................AS REQUIRED
Use RMU to access Engine and Navigation back up pages.
Affected MFD Selector Knob................PFD
Any MFD Selector Knob .......................EICAS
FAILED DISPLAYS PRESENT A RED X?
END
ALL 5 DISPLAYS FAILED?
END
END
WHICH DISPLAY FAILED?
END
END
MFDPFD
EICAS
EMERGENCY/ABNORMAL PROCEDURES Autopilot, Flight Instruments & Navigation
REVISION 4 EAP 2-7
ELECTRONIC BAY OVERTEMPERATURE
EICAS Caution: ELEKBAY OVTEMP
Turn off non-essential equipment.
The following equipment is installed in the forward electronic compartment:
ADC;
Transponder Mode S;
Integrated Communication Unit;
Aural Warning Computer;
FMS;
IRS;
Passenger Address;
Integrated Navigation Unit;
Inverter;
Dimmers;
Backup Battery.
No
Yes
LAND AT THE NEAREST SUITABLE AIRPORT. Maintain a cross-check between main and standby instruments. In case of disagreement, follow the standby instruments indication.
FD LATERAL MODE OFF/ FD VERTICAL MODE OFF
EICAS Caution: LATERAL MODE OFF or VERTICAL MODE OFF
At crew discretion, re-select the affected Flight Director or select the other.
MESSAGE PERSISTS?
END
END
EMERGENCY/ABNORMAL PROCEDURES Autopilot, Flight Instruments & Navigation
EAP 2-8 REVISION 10
IC FAILURE/IC BUS FAILURE
EICAS Caution: IC BUS FAIL may be presented. Condition: Associated Display Units present a
red X.
The following features will be inoperative: - EICAS messages miscompare monitoring. - Takeoff speeds synchronization. - Check List Display synchronization. - Flight Director mode synchronization.
PFD 2 and MFD 2 (IC 2 Failed)
PFD 1, MFD 1 and EICAS (IC 1 Failed)
SG on Reversionary Panel 1 ................PUSH IN
NOTE: - The PIT TRIM 1 (2) INOP or PTRIM MAIN INOP and PTRIM BACKUP INOP messages may not be available.
- Do not press the SG button again within a 3-second interval. In some cases, this action may cause loss of PFD indication. The display indication can be recovered by reverting the MFD to PFD and returning to the normal configuration.
SG on Reversionary Panel 2 ................PUSH IN
NOTE: Do not press the SG button again within a 3-second interval. In some cases, this action may cause loss of PFD indication. The display indication can be recovered by reverting the MFD to PFD and returning to the normal configuration.
FAILED DISPLAYS?
END
END
EMERGENCY/ABNORMAL PROCEDURES Autopilot, Flight Instruments & Navigation
REVISION 10 EAP 2-9
IC OVERHEAT
EICAS Caution: IC 1 (2) OVERHEAT Associated CB (C3 or D32)...................PULL
No
Yes IC 2
IC 1
Backup Battery......................................PUSH OUT SG on Associated
Reversionary Panel ..........................PUSH IN
NOTE: Do not press the SG button again within a 3-second interval. In some cases, this action may cause loss of PFD indication. The display indication can be recovered by reverting the MFD to PFD and returning to the normal configuration.
No
Yes
ELECTRICAL SYSTEM FIRE OR SMOKE Procedure (S-6)...................ACCOMPLISH
IRS ALIGNMENT FAULT
EICAS Caution: IRS 1 (2) ALN FAULT
Check and reenter present position. If necessary, reenter present position once again.
END
WHICH IC IS AFFECTED?
SMOKE PERSISTS?
END
ASSOCIATED WITH SMOKE?
EMERGENCY/ABNORMAL PROCEDURES Autopilot, Flight Instruments & Navigation
EAP 2-10 ORIGINAL
IRS FAIL
EICAS Caution: IRS 1 (2) FAIL
In Flight
Power On or Alignment
Affected IRU...........................................OFF Wait MSU lights extinguish. Affected IRU...........................................NAV
IRS on Associated Reversionary Panel ..........................PUSH IN
No
Yes
Affected IRU...........................................ATT
Maintain wings level and constant airspeed for approximately 20 seconds until IRS 1 (2) ALN message is no longer displayed and attitude is recovered.
Magnetic Heading .................................ENTER
CAUTION: FOR IRS IN ATTITUDE MODE, NAVIGATION AND ATTITUDE OUTPUTS ARE NOT AS ACCURATE AS IN THE NAV MODE. MAGNETIC HEADING MUST BE ENTERED AND UPDATED PERIODICALLY FROM THE BEST AVAILABLE ALTERNATIVE SOURCE, THROUGH THE FMS CDU.
Relevant Inoperative Item: Autopilot
OPERATION PHASE?
END
REMAINING IRU DATA NORMAL?
END
END
EMERGENCY/ABNORMAL PROCEDURES Autopilot, Flight Instruments & Navigation
ORIGINAL EAP 2-11
IRS OVERHEAT
EICAS Caution: IRS 1 (2) OVERHEAT
No
Yes
Associated Circuit Breaker ..................PULL Backup Battery......................................PUSH OUT IRS FAIL Procedure (EAP 2-10)............ACCOMPLISH
Yes
Presented
Not presented
Not illuminated
IRS on Associated Reversionary Panel ..........................PUSH IN
Affected IRU...........................................OFF Autopilot ................................................DISENGAGE
During final approach, if additional attitude reference is necessary:
Affected IRU......................................ATT
CAUTION: FOR IRS IN ATT MODE, NAVIGATION AND ATTITUDE OUTPUTS ARE NOT AS ACCURATE AS IN THE NAV MODE. MAGNETIC HEADING MUST BE ENTERED AND UPDATED PERIODICALLY FROM THE BEST AVAILABLE ALTERNATIVE SOURCE, THROUGH THE FMS CDU.
Relevant Inoperative Item: Autopilot
END
IRS DATA NORMAL?
MSU FAULT LIGHT?
END
IRS 1 (2) FAIL MESSAGE?
ASSOCIATED TO SMOKE OR FIRE?
No
Illuminated
EMERGENCY/ABNORMAL PROCEDURES Autopilot, Flight Instruments & Navigation
EAP 2-12 ORIGINAL
YAW DAMPER FAILURE
EICAS Caution: YAW DAMPER FAIL
Yaw Damper...........................................DISENGAGE Autopilot ................................................AS REQUIRED
No
Yes
Autopilot ................................................DISENGAGE
Altitude...................................................MAX 35000 ft MINIMUM MEA
IRS ALIGNMENT
EICAS Advisory: IRS 1 (2) ALN
IRU mode select switch ........................CHECK NAV This message is only presented during alignment phase or
while the IRU mode select switch is set at ALIGN position.
FAILURE PERSISTS?
END
END
FLIGHT ABOVE MACH 0.7?No
Yes
EMERGENCY/ABNORMAL PROCEDURES Autopilot, Flight Instruments & Navigation
REVISION 2 EAP 2-13
IRS ATTITUDE MODE
EICAS Advisory: IRS 1 (2) ATT MODE
No
Yes
Affected IRU...........................................OFF
Wait MSU lights extinguish. Affected IRU...........................................NAV
END
ON GROUND?
END
EMERGENCY/ABNORMAL PROCEDURES Autopilot, Flight Instruments & Navigation
EAP 2-14 ORIGINAL
IRS ON BATTERY
EICAS Advisory: IRS 1 (2) ON BATT
Associated IRU will operate for 40 minutes.
RADIO ALTIMETER FAIL
EICAS Advisory: RAD ALT 1 (2) FAIL or RAD ALT FAIL may be presented.
No
Yes
Consider pulling respective radio altimeter circuit breaker (D14 or D21) to inhibit undesired nuisance warnings.
No
Yes
Do not perform CAT II or CAT III approaches.
No
Yes
Do not perform CAT II or CAT III approaches.
ASSOCIATED WITH ERRONEOUS EGPWS ACTIVATION?
END
ALL RADIO ALTIMETERS AFFECTED (RAD ALT FAIL MESSAGE PRESENTED)?
END
RA1 (2) AMBER ANNUNCIATOR PRESENTED IN BOTH PFDs?
END
END
EMERGENCY/ABNORMAL PROCEDURES Auxiliary Power Unit
ORIGINAL EAP 3-1
TABLE OF CONTENTS
ANNUNCIATED PROCEDURES
APU FIRE ............................................................EAP 3-3
BLEED APU LEAK................................ refer to EAP 1-3
APU BLEED VALVE FAILURE............. refer to EAP 1-5
APU CONTACTOR CLOSED..............................EAP 3-4
APU FAIL.............................................................EAP 3-4
APU FUEL LOW PRESSURE .............................EAP 3-5
APU FUEL SHUTOFF VALVE INOPERATIVE .................................. refer to EAP 9-5
APU OIL HIGH TEMPERATURE ........................EAP 3-6
APU OIL LOW PRESSURE.................................EAP 3-6
NON ANNUNCIATED PROCEDURES
APU OVERTEMPERATURE ..................refer to NAP-4
EMERGENCY/ABNORMAL PROCEDURES Auxiliary Power Unit
EAP 3-2 ORIGINAL
LIST OF EICAS MESSAGES
APU FIRE .............................................................EAP 3-3
BLD APU LEAK...................................... refer to EAP 1-3
APU BLD VLV FAIL ............................... refer to EAP 1-5
APU CNTOR CLSD ..............................................EAP 3-4
APU FAIL..............................................................EAP 3-4
APU FUEL LO PRESS .........................................EAP 3-5
APU FUEL SOV INOP............................ refer to EAP 9-5
APU OIL HI TEMP ................................................EAP 3-6
APU OIL LO PRESS.............................................EAP 3-6
EMERGENCY/ABNORMAL PROCEDURES Auxiliary Power Unit
ORIGINAL EAP 3-3
APU FIRE
EICAS Warning: APU FIRE Aural Warning: BELL
APU Fuel Shutoff Valve ................... PUSH IN
APU Master Knob............................. OFF
LAND AT THE NEAREST SUITABLE AIRPORT.
Fuel Pump Pwr 2 .............................. OFF XFeed ................................................ OFF Initiate the descent to MEA or 25’000 ft, whichever is higher.
...................................................... WAIT 30 SECONDS APU Fire Extinguishing Button................................................ PRESS
WARNING: DO NOT ATTEMPT TO RESTART APU.
END
APU FIRE MESSAGE PERSISTS?
APU FUEL SOV CLSD MESSAGE? Displayed
Not Displayed
No
Yes
EMERGENCY/ABNORMAL PROCEDURES Auxiliary Power Unit
EAP 3-4 ORIGINAL
APU CONTACTOR CLOSED
EICAS Caution: APU CNTOR CLSD Bus Ties ............................................ OFF Battery 2............................................ OFF
APU FAIL
EICAS Caution: APU FAIL Condition: APU automatically shuts down. Do not try to restart the APU. APU Start .......................................... AS REQUIRED
NOTE: - Up to three APU start attempts may be accomplished, including the first attempt in which the message was displayed.
- The APU Starter Cool-down Limit is 1 MINUTE OFF.
Do not try to restart the APU.
END
END
END
OBVIOUS SAFETY HAZARD?
END
No
No
SHUTDOWN DURING APU START CYCLE?
Yes
Yes
EMERGENCY/ABNORMAL PROCEDURES Auxiliary Power Unit
ORIGINAL EAP 3-5
QR
H-1
35
/15
69
END
No
Yes
No
Yes
MESSAGE REMAINS?
MFD UNAVAILABLE OR ALL PUMPS IN ONE TANK ARE INOPERATIVE?
END
APU FUEL LOW PRESSURE
EICAS Caution: APU FUEL LO PRESS Fuel Pump Sel 2 ............................... SELECT ANOTHER Repeat the procedure. Altitude.............................................. MAX 25’000 FT,
MIN MEA
NOTE: If required, Crossfeed may be open above 25’000 ft.
EMERGENCY/ABNORMAL PROCEDURES Auxiliary Power Unit
EAP 3-6 ORIGINAL
APU OIL HIGH TEMPERATURE/ APU OIL LOW PRESSURE
EICAS Caution: APU OIL HI TEMP and/or APU OIL LO PRESS
APU OVERTEMPERATURE
Procedure (NAP-4)....................... ACCOMPLISH
APU EGT and RPM........................... MONITOR
APU.................................................... SHUTDOWN
END
END
END
No
No APU RPM OUT OF THE RED RANGE?
APU EGT INTO AMBER OR RED RANGE?
IS APU ESSENTIAL FOR THE FLIGHT? No
Yes
Yes
Yes
EMERGENCY/ABNORMAL PROCEDURES Doors
ORIGINAL EAP 4-1
TABLE OF CONTENTS
ANNUNCIATED PROCEDURES
MAIN DOOR OPEN ..............................................EAP 4-3
ACCESS DOORS OPEN......................................EAP 4-4
BAGGAGE DOORS OPEN ..................................EAP 4-4
EMERGENCY EXIT OPEN...................................EAP 4-5
INTERNAL BAGGAGE ACCESS DOOR OPEN ...............................................................EAP 4-5
NON ANNUNCIATED PROCEDURES
MAIN DOOR BLOCKED........................... refer to NAP-33
EMERGENCY/ABNORMAL PROCEDURES Doors
EAP 4-2 ORIGINAL
LIST OF EICAS MESSAGES
MAIN DOOR OPN.................................................EAP 4-3
ACCESS DOORS OPN ........................................EAP 4-4
BAGG ACCESS OPN……………………………....EAP 4-5
BAGGAGE DOOR OPN .......................................EAP 4-4
EMERG EXIT OPN ...............................................EAP 4-5
EMERGENCY/ABNORMAL PROCEDURES Doors
REVISION 10 EAP 4-3
MAIN DOOR OPEN
EICAS Warning: MAIN DOOR OPN
MFD Indication: Red DOOR OPEN. FSTN Belts ........................................ ON Door Alignment Red Marks ............. CHECK
No
Yes
No
Yes
Cabin altitude ................................... MONITOR
LAND AT THE NEAREST SUITABLE AIRPORT. Oxygen Masks .................................. AS REQUIRED Altitude.............................................. MEA OR 10’000 FT,
WHICHEVER IS HIGHER
When reaching 10’000 ft: Cabin............................................. DEPRESSURIZE
END
END
DOOR CONFIRMED
CABIN PRESSURIZATION NORMAL?
EMERGENCY/ABNORMAL PROCEDURES Doors
EAP 4-4 ORIGINAL
ACCESS/BAGGAGE DOORS OPEN
EICAS Caution: ACCESS DOORS OPN or BAGGAGE DOOR OPN
MFD Indication: Red DOOR OPEN. Abrupt Maneuvers............................ AVOID
No
Yes
Message ............................................ DISREGARD
LAND AT THE NEAREST SUITABLE AIRPORT. Oxygen Masks .................................. AS REQUIRED Altitude.............................................. MEA OR 10’000 FT,
WHICHEVER IS HIGHER
When reaching 10’000 ft: Cabin............................................. DEPRESSURIZE
END
END
CABIN PRESSURIZATION NORMAL?
EMERGENCY/ABNORMAL PROCEDURES Doors
ORIGINAL EAP 4-5
EMERGENCY EXIT OPEN
EICAS Caution: EMERG EXIT OPN MFD Indication: Red DOOR OPEN.
FSTN Belts ........................................ ON Affected Exit ..................................... CHECK Remove passenger(s) from exit vicinity.
Emergency exit handle .................... CHECK PUSHED IN
No
Yes
No
Yes
Message ............................................ DISREGARD
LAND AT THE NEAREST SUITABLE AIRPORT. Oxygen Masks .................................. AS REQUIRED Altitude.............................................. MEA OR 10’000 FT,
WHICHEVER IS HIGHER
When reaching 10’000 ft: Cabin............................................. DEPRESSURIZE
INTERNAL BAGGAGE ACCESS DOOR OPEN
EICAS Caution: BAGG ACCESS OPN MFD Indication: Red DOOR OPEN.
Door Status on MFD......................... CHECK
If message is confirmed or MFD is not available:
Door................................................... CLOSE AND LOCK
END
EMERGENCY EXIT LOCKED?
CABIN PRESSURIZATION NORMAL?
END
END
EMERGENCY/ABNORMAL PROCEDURES Electrical & Lighting
ORIGINAL EAP 5-1
TABLE OF CONTENTS
ANNUNCIATED PROCEDURES
BATTERY OVERTEMPERATURE.................... EAP 5-3
ELECTRIC ESSENTIAL TRANSFER FAILURE ................................ EAP 5-3
115 V AC BUS OFF........................................... EAP 5-4
APU CONTACTOR CLOSED.............. refer to EAP 3-4
BACK-UP BATTERY OFF BUS........................ EAP 5-4
BATTERY OFF BUS.......................................... EAP 5-4
DC BUS 1 OFF .................................................. EAP 5-5
DC BUS 2 OFF .................................................. EAP 5-6
ELECTRICAL EMERGENCY ABNORMAL TRANSFER................................................. EAP 5-7
EMERGENCY LIGHTS NOT ARMED ............... EAP 5-7
ESSENTIAL BUS 1 OFF ................................... EAP 5-8
ESSENTIAL BUS 2 OFF ................................... EAP 5-9
ESSENTIAL BUS 1-2 OFF ................................ EAP 5-10
GENERATOR OFF BUS.................................... EAP 5-12
GENERATOR OVERLOAD............................... EAP 5-12
LOSS OF ALL GENERATORS ......................... EAP 5-13
NON ANNUNCIATED PROCEDURES
ELECTRICAL SYSTEM FIRE OR SMOKE....................................refer to S-6
ANNEX 01 - AFFECTED EQUIPMENT
DC BUS FAILURE ............................................. EAP 5-14 ESS BUS FAILURE ........................................... EAP 5-15
EMERGENCY/ABNORMAL PROCEDURES Electrical & Lighting
EAP 5-2 ORIGINAL
LIST OF EICAS MESSAGES
BATT 1 (2) OVTEMP ......................................... EAP 5-3
ELEC ESS XFR FAIL ........................................ EAP 5-3
115 VAC BUS OFF............................................ EAP 5-4
APU CNTOR CLSD ............................. refer to EAP 3-4
APU GEN OFF BUS .......................................... EAP 5-12
APU GEN OVLD................................................ EAP 5-12
BKUP BATT OFF BUS...................................... EAP 5-4
BATT1 (2) OFF BUS.......................................... EAP 5-4
DC BUS 1 OFF .................................................. EAP 5-5
DC BUS 2 OFF .................................................. EAP 5-6
ELEC EMERG ABNORM .................................. EAP 5-7
EMERG LT NOT ARMD .................................... EAP 5-7
ESS BUS 1 OFF ................................................ EAP 5-8
ESS BUS 2 OFF ................................................ EAP 5-9
ESS BUS 1-2 OFF ............................................. EAP 5-10
GEN 1-2-3-4 OFF BUS ...................................... EAP 5-13
GEN 1 (2, 3, 4) OFF BUS .................................. EAP 5-12
GEN 1 (2, 3, 4) OVLD ........................................ EAP 5-12
EMERGENCY/ABNORMAL PROCEDURES Electrical & Lighting
REVISION 9 EAP 5-3
BATTERY OVERTEMPERATURE
EICAS Warning: BATT 1 (2) OVTEMP
MFD Indication: Battery temperature in red.
Affected Battery ....................................OFF
No
Yes
LAND AT THE NEAREST SUITABLE AIRPORT.
ELECTRIC ESSENTIAL TRANSFER FAILURE
EICAS Warning: ELEC ESS XFR FAIL
Essential Power.....................................PUSH IN
No
Yes
Bus Ties .................................................OFF
No
Yes
LAND AT THE NEAREST SUITABLE AIRPORT.
Shed Buses............................................OFF
Turn off non essential equipment. Begin with DC Buses 1 and 2 (CB Panel rows D, E, F, G and H).
LOSS OF ALL GENERATORS Procedure (EAP 5-13).......................ACCOMPLISH
ASSOCIATED BATT 1 (2) OFF BUS MESSAGE DISPLAYED?
END
END
END
MESSAGE PERSISTS?
MESSAGE STILL PERSISTS?
EMERGENCY/ABNORMAL PROCEDURES Electrical & Lighting
EAP 5-4 ORIGINAL
115 V AC BUS OFF
EICAS Caution: 115 VAC BUS OFF
AC PWR..................................................PUSH OUT, THEN PUSH IN
No
Yes
AC PWR..................................................PUSH OUT Relevant Inoperative Items:
TCAS II Windshear Detection EGPWS
BACK-UP BATTERY OFF BUS
EICAS Caution: BKUP BATT OFF BUS
Backup Battery......................................CHECK PUSHED IN
BATTERY OFF BUS
EICAS Caution: BATT1 (2) OFF BUS MFD Indication: Battery may be amber.
Affected Battery.....................................AUTO
MESSAGE PERSISTS?
END
END
END
EMERGENCY/ABNORMAL PROCEDURES Electrical & Lighting
REVISION 8 EAP 5-5
DC BUS 1 OFF
EICAS Caution: DC BUS 1 OFF MFD Indication: DC BUS may be amber.
Bus Ties .................................................OVRD
No
Yes
Bus Ties .................................................AUTO Icing Conditions ....................................EXIT/AVOID Altitude...................................................25’000 FT OR
MEA, WHICHEVER IS HIGHER
At pilot’s discretion, on Reversionary Panel 1: MFD Knob..........................................PFD
Relevant Inoperative Items: Autopilot W/S 1 Heating and Wiper EGPWS
FMS 1 Transponder 1 RA 1
Speed Brake Main Pitch Trim TCAS 2000
Pack 1 Thrust Reverser 1 DME 1
Automatic Pressurization Control
Do not set Thrust Lever 1 below idle in flight. Anticipate flap actuation. Landing configuration:
Flaps .................................................... 22° VREF ...................................................... VREF 45° + 30 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.85.
Affected Equipment (EAP 5-14) ...........CHECK
MESSAGE PERSISTS?
END
EMERGENCY/ABNORMAL PROCEDURES Electrical & Lighting
EAP 5-6 ORIGINAL
DC BUS 2 OFF
EICAS Caution: DC BUS 2 OFF MFD Indication: DC BUS may be amber.
Condition: Noise increase due to nose landing gear doors open.
Bus Ties .................................................OVRD
No
Yes
Bus Ties .................................................AUTO Icing Conditions ....................................EXIT/AVOID Airspeed.................................................MAX 250 KIAS Altitude...................................................25’000 FT OR
MEA, WHICHEVER IS HIGHER
The overhead panel lighting is inoperative, therefore, all striped bars will not illuminate. SG ...........................................................PUSH IN At pilot’s discretion, on Reversionary Panel 2:
MFD Knob..........................................PFD MFD Control is possible through MFD 1 Bezel.
Relevant Inoperative Items: VHF2/ADF2/VOR2/ DME2/ILS2/MB2
W/S 2 Heating and Wiper Steering
Thrust Reverser 2 Transponder 2 Pack 2
Stick Pusher Landing lights FMS 2
Do not set Thrust Lever 2 below idle in flight. Anticipate flap actuation. Landing configuration:
Flaps.....................................................22° VREF.......................................................VREF 45° + 15 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.55.
Affected Equipment (EAP 5-14) ...........CHECK
MESSAGE PERSISTS?
END
EMERGENCY/ABNORMAL PROCEDURES Electrical & Lighting
REVISION 4 EAP 5-7
ELECTRICAL EMERGENCY ABNORMAL TRANSFER
EICAS Caution: ELEC EMERG ABNORM
Essential Power.....................................CHECK PUSHED OUT
No
Yes
LAND AT THE NEAREST SUITABLE AIRPORT. Emerg Lts...............................................OFF
If required, turn ON Emerg Lts just before landing.
Bus Ties .................................................OFF
Batteries 1 and 2 ...................................OFF
No
Yes
Bus Ties .................................................AUTO
Batteries 1 and 2 ...................................AUTO APU (if serviceable) ..............................START APU Generator ......................................CHECK
PUSHED IN
CAUTION: IF APU GENERATOR IS NOT AVAILABLE AND THE MESSAGE REMAINS, BATTERIES DURATION WILL BE 40 MINUTES.
EMERGENCY LIGHTS NOT ARMED
EICAS Caution: EMERG LT NOT ARMD EMERG LT Switch .................................ARM
No
Yes
EMERG LTS on Forward Attendant Control Panel ..................Check NORM
END
MESSAGE PERSISTS?
MESSAGE PERSISTS?
END
MESSAGE STILL PERSISTS?
EMERGENCY/ABNORMAL PROCEDURES Electrical & Lighting
EAP 5-8 REVISION 10
ESSENTIAL BUS 1 OFF
EICAS Caution: ESS BUS 1 OFF
On Reversionary panel 1: SG ................................................. PUSH IN
Fuel Pump 1...................................... 1B OR 1C NOTE: Start selecting the Fuel Pump 1B.
Fuel Pump 2...................................... 2A OR 2C Altitude.............................................. MAX 25’000 FT,
MIN MEA XFEED ............................................... OFF
NOTE: Use asymmetric thrust to improve or maintain wing fuel Balance.
No
Yes XBleed ............................................... OPEN Altitude.............................................. MEA OR
15’000 FT, WHICHEVER IS HIGHER
If it is not possible to descend below 15’000 ft: Icing Conditions .......................... EXIT
Monitor fuel quantity indication 1 through FMS. Fuselage Fuel Transfer System ...... CHECK
STATUS If fuel transfer is not observed consider a diversion.
Brake effectiveness will be reduced.
COM 2 on Digital Audio Panel 2...... PUSH IN
Relevant Inoperative Items: ENG 1 Fire Detection System CPAM RMU 1
ADF1/VHF1/VOR1/ILS1/MB1 Audio System 1
Landing Gear Control (Down Override)
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.49.
No
Yes
Affected Equipment (EAP 5-15 and EAP 5-16) .............................. CHECK
CONTINUES ON NEXT PAGE
ICING CONDITIONS?
END
EICAS ENERGIZED?
EMERGENCY/ABNORMAL PROCEDURES Electrical & Lighting
REVISION 10 EAP 5-9
CONTINUED FROM PREVIOUS PAGE
DAU 1 on EICAS Rev ....................... PUSH IN At pilots’s discretion, on Reversionary Panel 1:
MFD Knob..................................... EICAS
Affected Equipment (EAP 5-15 and EAP 5-16) .............................. CHECK
ESSENTIAL BUS 2 OFF
EICAS Caution: ESS BUS 2 OFF MFD Indication: ESS BUS may be amber.
Fuel Pump 1...................................... 1A OR 1C Fuel Pump 2...................................... 2B OR 2C
NOTE: Start selecting the Fuel Pump 2B.
Icing Conditions ............................... EXIT/AVOID Altitude.............................................. MAX 25’000 FT,
MIN MEA
Monitor fuel quantity indication 2 through FMS. Fuselage Fuel Transfer System ...... CHECK
STATUS If fuel transfer is not observed consider a diversion.
CAUTION: DO NOT USE CROSSFEED.
Brake effectiveness will be reduced. When necessary to extend landing gear:
Landing Gear ............................... DOWN Gear Electrical Override.............. DOORS
.................................................. WAIT 3 SECONDS Gear Electrical Override.............. GEAR/DOORS
Relevant Inoperative Items: ISIS/Standby altimeter (#) Audio System 2
APU Fire Detection System Pitot Heating 3
ENG 2 Fire Detection System Standby attitude indicator
APU Control RMU 2
Landing Gear Lever Control RH Wing A/Ice
(#) Inoperative ISIS - Applicable for airplanes S/N 484, 495, 528 and 555.
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.49.
Affected Equipment (EAP 5-15 and EAP 5-16) .............................. CHECK
END
END
EMERGENCY/ABNORMAL PROCEDURES Electrical & Lighting
EAP 5-10 REVISION 4
ESSENTIAL BUS 1-2 OFF
EICAS Caution: ESS BUS 1-2 OFF
Bus Ties .................................................OFF MFD Pictorial Electrical ........................CHECK
No
Yes
Battery 1 and 2.......................................OFF No
Yes
ESSENTIAL BUS 1 OFF Procedure (EAP 5-8).........................AS REQUIRED
No
Yes
ESSENTIAL BUS 2 OFF Procedure (EAP 5-9)..............................AS REQUIRED
No
Yes
Battery 1.................................................OFF ESSENTIAL BUS 1 (2) OFF Procedure
(EAP 5-8 or EAP 5-9) ........................AS REQUIRED No
Yes
Battery 2.................................................OFF ESSENTIAL BUS 1 (2) OFF Procedure
(EAP 5-8 or EAP 5-9) ........................AS REQUIRED
CONTINUES ON NEXT PAGE
BOTH DC BUSES ENERGIZED?
DC BUS 1 IS ENERGIZED?
DC BUS 2 IS ENERGIZED?
END
ESSENTIAL BUS 1 STILL OFF?
END
ESSENTIAL BUS 2 STILL OFF?
EMERGENCY/ABNORMAL PROCEDURES Electrical & Lighting
REVISION 4 EAP 5-11
CONTINUED FROM PREVIOUS PAGE
No
Yes
Landing configuration: Flaps ............................................. 22º VREF................................................ VREF45° + 10 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 2.18.
Affected Equipment (EAP 5-15) .... CHECK
Landing configuration:
Flaps ............................................. 22º VREF................................................ VREF45° + 30 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.85.
Affected Equipment (EAP 5-15) ...... CHECK
END
END
ICING CONDITIONS?
EMERGENCY/ABNORMAL PROCEDURES Electrical & Lighting
EAP 5-12 ORIGINAL
GENERATOR OFF BUS
EICAS Caution: GEN 1 (2, 3, 4) OFF BUS or APU GEN OFF BUS
MFD Indication: Generator voltage may be amber.
No
Yes
LOSS OF ALL GENERATORS Procedure (EAP 5-13).......................ACCOMPLISH
Affected Generator................................PUSH OUT, THEN PUSH IN
APU (if serviceable) ..............................AS REQUIRED
GENERATOR OVERLOAD
EICAS Caution: GEN 1 (2, 3, 4) OVLD or APU GEN OVLD
MFD Indication: Generator may be amber.
Shed Buses............................................OFF No
Yes
Electrical Load (affected generator).....REDUCE The equipments that require more electrical load and may be turned OFF, at pilot’s discretion, are: lights, hydraulic electric pump, ice protection and air conditioning related systems. Non-required equipment may also be turned OFF.
No
Yes
APU.........................................................STOP
APU.........................................................START APU GEN................................................CHECK
PUSHED IN
END
END
END
ALL GENERATORS OFF BUS?
MESSAGE PERSISTS?
APU GEN OVLD EICAS MESSAGE DISPLAYED?
END
EMERGENCY/ABNORMAL PROCEDURES Electrical & Lighting
REVISION 9 EAP 5-13
LOSS OF ALL GENERATORS
EICAS Caution: GEN 1-2-3-4 OFF BUS Condition: Noise increase due to nose landing
gear doors open. The following message may be displayed:
EICAS Caution: APU GEN OFF BUS
Generators .............................................PUSH OUT, THEN PUSH IN
APU Generator ......................................AS REQUIRED No
Yes
LAND AT THE NEAREST SUITABLE AIRPORT. CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED
LANDING DISTANCE BY 1.95. Essential Power.....................................PUSH IN Airspeed.................................................MAX 250 KIAS Altitude...................................................MEA OR
10’000 FT, WHICHEVER IS HIGHER
Crew Oxygen .........................................AS REQUIRED Passenger Oxygen................................AS REQUIRED Emerg Lts...............................................OFF
If required, turn on Emergency Lights before landing. Icing Conditions ....................................EXIT/AVOID Use standby instruments and RMU Navigation Backup Page.
CAUTION: BATTERY DURATION IS 40 MINUTES.
FUEL XFER CRITICAL or CHECK ACFT LOAD EICAS Message ................................MONITOR
Do not set Thrust Levers below idle in flight. Do not actuate Thrust Reversers. Landing configuration:
Landing Gear ...................................DOWN If necessary:
LG WARN Cutout.......................PRESS
FLAP POSITION MINIMUM AIRSPEED
0 to 8° VREF 45 + 30 KIAS
9 to 21° VREF 45 + 10 KIAS
22 to 44° VREF 45 + 5 KIAS
45° VREF 45
CONTINUES ON NEXT PAGE
ANY GENERATOR RECOVERED?
END
EMERGENCY/ABNORMAL PROCEDURES Electrical & Lighting
EAP 5-14 REVISION 9
CONTINUED FROM PREVIOUS PAGE
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.95.
Relevant Inoperative Items:
Autopilot W/S 1 and 2 Heating and Wiper EGPWS
FMS 1 and 2 Transponder 1 and 2 RA 1
Speed Brake Main Pitch Trim TCAS
Pack 1 and 2 Stick Pusher Steering
VHF2/ADF2/VOR2/DME2/ILS2/MB2 and DME1 Flaps
Afected Equipment
(EAP 5-15 and 5-16).........................CHECK END
EMERGENCY/ABNORMAL PROCEDURES Electrical & Lighting
REVISION 9 EAP 5-15
ANNEX 01
In case of electrical bus failure, refer to the following table to verify the affected equipment.
DC BUS 1 DC BUS 2
AILERON CONTROL SYSTEM 1 AIR/GND POSITION SYSTEM A AOA 1 SENSOR HEATING AUTOMATIC PRESSURIZATION CONTROL BRAKES TEMP INDICATION OUTBD CMC CREW PEDAL ADJUSTMENT CREW SEAT ADJUSTMENT 1 EICAS POWER (DAU 1B) ELECTRICAL FLIGHT IDLE STOP 1 ELECTRONIC BAY COOLING (EXHAUST
1 AND RECIRC 2) EMER/PARKING BRAKE ENG 1 FUEL PUMPS 1C ENG 1 THRUST REVERSER COMMAND ENGINE 1 LIP ANTI-ICE FLAP CHANNEL1 FUEL PRESSURE REFUELING FWD/AFT
A1 FUEL PRESSURE REFUELING FWD 1 FUEL TRANSFER 1 GROUND SPOILER OUTBD HYDRAULIC ELECTRIC PUMP 2 HYDR GEN SYS 2 INDICATION ICE DETECTOR 1 CLEAR ICE DET - CHANNEL 1 INVERTER LAVATORY FLUSH LAVATORY SMOKE DETECTOR LAVATORY WATER DRAIN HEATER LIGHTING CABIN 1 LIGHTING OVERHEAD PANEL LIGHT – COCKPIT READING LIGHTS – COURTESY/STAIR 2 LIGHTS – FLOOD/STORM LIGHTS – LANDING 1 LIGHTS – LAVATORY LIGHTS – LOGOTYPE LIGHTS – NAVIGATION LIGHTS – PASSENGER CABIN 1 MAIN DOOR CONTROL 1 PACK VALVE 1 PASSENGER SIGNS PITCH TRIM (MAIN) PITOT 1 HEATING PNEUMATIC HSV 1 SPEED BRAKE STABILIZER ANTI-ICE INDICATION STATIC PORT HEATING 1 STROBE LIGHTS TAT 1 SENSOR HEATING TCAS 2000 WINDSHIELD HEATING 1 WINDSHIELD WIPER 1 WING ANTI-ICE YAW TRIM
ADC 2 AHRS 2 AILERON CONTROL SYSTEM 2 AIR/GND POSITION SYSTEM C AOA 2 SENSOR HEATING AUDIO - OBSERVER (INTPH 3) AURAL WARNING SYSTEM 2 BAGGAGE SMOKE DETECTOR BRAKES TEMP INDICATION INBD CABIN RECIRCULATION CLEAR ICE DET - CHANNEL 2 CLOCK - COPILOT'S CREW SEAT ADJUSTMENT 2 DEFUELING DISPLAY PRCS/CTRL PWR 2 (IC2) EICAS POWER (DAU 2B) ELECTRICAL FLIGHT IDLE STOP 2 ELECTRONIC BAY COOLING (RECIRC 1
AND EXHAUST 2) ENG 2 FUEL PUMPS 2C ENG 2 THRUST REVERSER COMMAND ENGINE 2 LIP ANTI-ICE ENGINE VIBRATION SENSORS FLAP CHANNEL 2 FUEL FUS PUMPS AFT/FWD 2A FUEL FUS PUMPS FWD 2B FUEL TRANSFER 2 GASPER FAN GROUND SPOILER INBD GUST LOCK (ELECTROMECHANICAL) HYDR ELECTRIC PUMP 1 HYDR GEN SYS 1 INDICATION ICE DETECTOR 2 IRS 2 LANDING GEAR DOOR COMMAND LANDING GEAR LEVER SOLENOID LIGHTING OVERHEAD PANEL LIGHTS – COMPARTMENT LIGHTS – INSPECTION LIGHTS – LANDING LIGHTS – PASSENGER CABIN 2/3 LIGHTS – RED BEACON PACK VALVE 2 PITOT 2 HEATING PNEUMATIC HSV 2 ROLL TRIM SYSTEM SENSORS HEATING CONTROL SPOILER INDICATION SPS (SHAKER 2/CHANNEL 2) SPS PUSHER STABILIZER ANTI-ICE STATIC PORT HEATING 2 STEERING TAT 2 SENSOR HEATING WINDSHIELD WIPER 2 WING ANTI-ICE 1 INDICATION
EMERGENCY/ABNORMAL PROCEDURES Electrical & Lighting
EAP 5-16 REVISION 9
ANNEX 01
In case of electrical bus failure, refer to the following table to verify the affected equipment.
ESSENTIAL BUS 1 ESSENTIAL BUS 2
(#) Applicable for airplanes with AMPL 1 supplied by ESSENTIAL DC BUS 2.
(##) Applicable for airplanes S/N 484, 495, 528 and 555.
ADC 1 AHRS 1 AIR/GND POSITION SYSTEM B APU BLEED AUDIO PILOT/COPILOT (INTPH 1) AURAL WARNING SYSTEM 1 BRAKES OUTBOARD CABIN PRESSURE ACQUISITION MODULE (CPAM) CLOCK PILOT'S DISPLAY PRCS/CTRL PWR 1 (IC 1)EICAS DISPLAY EICAS (DAU 1A) ENG 1 FIRE DETECTION 1 ENG 1 FUEL PUMPS 1A ENG 2 FUEL PUMPS 2B ENGINES 1 AND 2 FADECS A ENGINE 1 STARTING ENGINES N2 SIGNALS 1A AND 2A FDR MANAGEMENT FUEL QUANTITY INDICATION 1 LDG CONTROL (DOWN OVRD) LANDING GEAR NOSE
INDICATION 1 LIGHTS COCKPIT DOME IRS 1 PANEL LIGHTING PILOT'S PASSENGER OXYGEN SYSTEM 1 PNEUMATIC 1 (EBV 1) RAM AIR DISTRIBUTION RMU 1 RUDDER CONTROL SYSTEM 2 SPS (SHAKER 1/CHANNEL 1) VHF 1
AIR/GND POSITION SYSTEM D APU CONTROL APU FIRE DETECTION APU FIRE EXTINGUISHING APU FUEL FEED AUDIO PILOT/COPILOT (INTPH 2) BRAKES INBOARD COCKPIT/ATTENDANT
INTERCOMM CROSSBLEED EICAS (DAU 2A) ENG 2 FIRE DETECTION 2 ENG 1 FUEL PUMPS 1B ENG 2 FUEL PUMPS 2A ENGINES 1 AND 2 FADEC B ENGINE 2 ANTI-ICE INDICATION ENGINE 2 STARTING ENGINES N2 SIGNALS 1B AND 2B FUEL CROSS FEED FUEL QUANTITY INDICATION 2 ISIS (##) LANDING GEAR CONTROL LDG NOSE INDICATION 2 LIGHTING EMERGENCY CTRL LIGHTING PANEL COPILOT'S AND
PEDESTAL PASSENGER OXYGEN SYSTEM 2 PITCH TRIM BACKUP PITOT HEATING 3 PNEUMATIC 2 (EBV 2) PUBLIC ADDRESS (#) RMU 2 RUDDER CONTROL SYSTEM 1 STANDBY ALTIMETER STANDBY ATTITUDE INDICATOR VOICE RECORDER WING ANTI-ICE INDICATION 2
EMERGENCY/ABNORMAL PROCEDURES Engine
REVISION 9 EAP 6-1 QR
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TABLE OF CONTENTS ANNUNCIATED PROCEDURES
ATTCS FAILURE.................................................EAP 6-3
BLEED ENGINE LEAK ......................... refer to EAP 1-4
DUAL ENGINE FAILURE....................................EAP 6-3
ENGINE ATTCS NO MARGIN.............................EAP 6-5
ENGINE FIRE, SEVERE DAMAGE OR SEPARATION .................................................EAP 6-6
ENGINE OIL LOW PRESSURE ..........................EAP 6-7
ENGINE ANTI-ICING FAILURE ............ refer to EAP 11-5
ENGINE ATS SHUTOFF VALVE OPEN .............EAP 6-8
ENGINE CONTROL FAILURE ............................EAP 6-9
ENGINE FUEL LOW PRESSURE......... refer to EAP 9-6
ENGINE FUEL LOW TEMPERATURE . refer to EAP 9-7
ENGINE FUEL SHUTOFF VALVE INOPERATIVE ...................................refer to EAP 9-7
ENGINE OUT.......................................................EAP 6-10
ENGINE THRUST LEVER FAILURE ..................EAP 6-11
ENGINE THRUST REVERSER FAILURE/DISAGREE .....................................EAP 6-12
ENGINE FUEL FILTER IMPENDING BYPASS ...................................EAP 6-12
ENGINE HYDRAULIC PUMP FAILURE...........................................refer to EAP 10-8
ENGINE IDLE STOP FAILURE..........................EAP 6-13
NON ANNUNCIATED PROCEDURES
ABNORMAL ENGINE START................refer to NAP-15
ENGINE ABNORMAL VIBRATION........refer to NAP-18
ENGINE AIRSTART ...............................refer to NAP-19
ENGINE FAILURE/SHUTDOWN............refer to NAP-23
ENGINE OIL HIGH PRESSURE.............refer to NAP-24
ENGINE OIL HIGH TEMPERATURE .....refer to NAP-24
ENGINE OIL LOW LEVEL......................refer to NAP-24
ENGINE OIL LOW PRESSURE .............refer to NAP-25
ENGINE OVERTEMPERATURE............refer to NAP-25
LOSS OF ENGINE INDICATIONS .........refer to NAP-30
ONE ENGINE INOPERATIVE APPROACH AND LANDING.............refer to NAP-35
SINGLE ENGINE BLEED OPERATION IN ICING CONDITIONS .....................refer to NAP-41
EMERGENCY/ABNORMAL PROCEDURES Engine
EAP 6-2 REVISION 9
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LIST OF EICAS MESSAGES
ATTCS FAIL ........................................................EAP 6-3
BLD 1 (2) LEAK..................................... refer to EAP 1-4
E1 (2) ATTCS NO MRGN ....................................EAP 6-5
E1 (2) OIL LOW PRESS......................................EAP 6-7
ENG 1 (2) FIRE....................................................EAP 6-6
ENG 1-2 OUT.......................................................EAP 6-3
E1 (2) A/ICE FAIL ................................. refer to EAP 11-5
E1 (2) ATS SOV OPN.........................................EAP 6-8
E1 (2) CTL FAIL ..................................................EAP 6-9
E1 (2) FUEL LO PRESS........................ refer to EAP 9-6
E1 (2) FUEL LO TEMP .......................... refer to EAP 9-7
E1 (2) FUEL SOV INOP......................... refer to EAP 9-7
ENG1 (2) OUT......................................................EAP 6-10
ENG1 (2) REV DISAGREE..................................EAP 6-12
ENG1 (2) REV FAIL.............................................EAP 6-12
ENG1 (2) TLA FAIL .............................................EAP 6-11
E1 (2) FUEL IMP BYP ........................................EAP 6-12
E1 (2) HYD PUMP FAIL........................ refer to EAP 10-8
E1 (2) IDL STP FAIL...........................................EAP 6-13
EMERGENCY/ABNORMAL PROCEDURES Engine
REVISION 9 EAP 6-3 QR
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ATTCS FAILURE
EICAS Warning: ATTCS FAIL
Thrust Levers ........................................MAX
Another takeoff is not permitted.
DUAL ENGINE FAILURE
EICAS Warning: ENG 1-2 OUT may be presented.
Oxygen Mask .........................................AS REQUIRED Fuel Pump Pwr Tank 1 and 2 ...............ON Fuel Pump Sel 1 and 2 ..........................A OR B APU.........................................................START Airspeed for engine windmilling start: Above 10’000 ft .................................MIN 250 KIAS Below 10’000 ft..................................220 TO 250 KIAS
Transponder ..........................................7700 TCAS ......................................................TA ONLY
No
Yes
Thrust Levers ........................................IDLE Engine 1 and 2 Start/Stop Selectors ...STOP APU Bleed..............................................PUSH IN Engine Bleeds 1 and 2 ..........................PUSH OUT Below 25’000 ft:
Engine 1 Start/Stop Selector ...........START, THEN RUN
No
Yes
ENGINE 2 AIRSTART Procedure (NAP-19)..........................ACCOMPLISH
Engine 1 Start/Stop Selector................STOP Engine 2 Start/Stop Selector................START, THEN
RUN
CONTINUES ON NEXT PAGE
END
END
ENGINE 1 STARTS?
APU SERVICEABLE?
EMERGENCY/ABNORMAL PROCEDURES Engine
EAP 6-4 REVISION 9 QR
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CONTINUED FROM PREVIOUS PAGE No
Yes ENGINE 1 AIRSTART
Procedure (NAP-19)..........................AS REQUIRED
NOTE: Windmilling starts can be attempted in both engines simultaneously.
N2............................................................MIN 10%
Initiate windmilling start with N2 as high as possible. Once N2 is below 10%, it may not be recovered.
Thrust Levers ........................................IDLE Engine 1 and 2 Start/Stop Selectors....STOP Engine 1 and 2 Start/Stop Selectors....START, THEN
RUN No
Yes No
Yes
ENGINE AIRSTART (inoperative engine) Procedure (NAP-19)..........................AS REQUIRED
ENGINE FAILURE/SHUTDOWN
(inoperative engine) Procedure (NAP-23)..........................AS REQUIRED
DITCHING (NAP-5) OR FORCED LANDING (NAP-8) Procedure ..........ACCOMPLISH
END
ENGINE 2 STARTS?
END
ANY ENGINE STARTS?
END
INOPERATIVE ENGINE START CONSIDERED?
END
EMERGENCY/ABNORMAL PROCEDURES Engine
REVISION 10 EAP 6-5 QR
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ENGINE ATTCS NO MARGIN
EICAS Warning: E1 (2) ATTCS NO MRGN
Do not takeoff. END
EMERGENCY/ABNORMAL PROCEDURES Engine
EAP 6-6 REVISION 9 QR
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ENGINE FIRE, SEVERE DAMAGE OR SEPARATION
EICAS Warning: ENG 1 (2) FIRE (in case of fire). Light: Engine Fire Handle Aural Warning: BELL (in case of fire).
Associated Thrust Lever ......................IDLE Associated Start/Stop Selector............STOP Associated Fire Extinguishing Handle................................................PULL (DO NOT
ROTATE) FUS TK XFER.........................................OFF
LAND AT THE NEAREST SUITABLE AIRPORT. TCAS ......................................................TA ONLY
Displayed
Not Displayed XFeed .....................................................OFF Associated Fuel Pump Power..............OFF
...........................................................WAIT 30 SECS No
Yes
Fire Extinguishing Handle (1st shot) ....ROTATE
...........................................................WAIT 30 SECS
No
Yes
Fire Extinguishing Handle (2nd shot). . ROTATE
No
Yes
Fire Extinguishing Handle (one shot, if available)......................ROTATE
No
Yes
Autopilot ................................................DISENGAGE Yaw Damper...........................................DISENGAGE Airspeed.................................................REDUCE
Chase the better airspeed to reduce the vibration. Airspeeds around 180 KIAS are recommended.
CONTINUES ON NEXT PAGE
ENG 1 (2) FIRE MESSAGE PERSISTS?
ENG 1 (2) FIRE MESSAGE PERSISTS?
E1 (2) FUELSOV CLSD MESSAGE?
ENGINE FAILURE ASSOCIATED TO HIGH VIBRATION?
E1 (2) FIREDET FAIL MESSAGE DISPLAYED?
EMERGENCY/ABNORMAL PROCEDURES Engine
REVISION 10 EAP 6-7 QR
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CONTINUED FROM PREVIOUS PAGE Associated Bleed ..................................PUSH OUT Remaining Engine Thrust Rating ........CON APU.........................................................START APU Bleed..............................................AS REQUIRED XBleed ....................................................AS REQUIRED
Altitude...................................................MAX 25’000 FT, MIN MEA
No
Yes
Altitude...................................................MAX 15’000 FT, MIN MEA
If it is not possible to descend below 15’000 ft: Icing Conditions ...............................EXIT
ONE ENGINE INOPERATIVE APPROACH AND LANDING Procedure (NAP-35) ........AS REQUIRED
ENGINE OIL LOW PRESSURE
EICAS Warning: E1 (2) OIL LOW PRESS may be presented.
EICAS Indication: Oil pressure may be red.
No
Yes
Associated Thrust Lever ......................IDLE
Reduce Thrust Lever to at least N2 below 88%, until pressure is within limits.
No
Yes
Associated ENGINE FAILURE/SHUTDOWN Procedure (NAP-23)..........................ACCOMPLISH
Message .................................................DISREGARD
END
ICING CONDITIONS?
END
OIL PRESSURE IN THE RED RANGE?
OIL PRESSURE STILL IN THE RED RANGE?
EMERGENCY/ABNORMAL PROCEDURES Engine
EAP 6-8 REVISION 10
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ENGINE ATS SHUTOFF VALVE OPEN
EICAS Caution: E1 (2) ATS SOV OPN
XBleed ....................................................CLOSE Associated Bleeds
(including APU bleed) ......................PUSH OUT No
Yes
Thrust Levers ........................................IDLE Associated Start/Stop Selector............STOP
NOTE: If engine shutdown does not occur, pull the fire extinguishing handle.
Icing Conditions ....................................EXIT/AVOID Altitude...................................................MAX 25’000 FT,
MIN MEA
END
END
ON GROUND?
EMERGENCY/ABNORMAL PROCEDURES Engine
REVISION 9 EAP 6-9
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1
ENGINE CONTROL FAILURE
EICAS Caution: E1 (2) CTL FAIL may be presented.
CAUTION: DO NOT MANUALLY ALTERNATE ASSOCIATED FADECS.
FADEC In Control ..................................CHECK Associated FADEC................................RESET
No
Yes
Avoid quick movements of the associated Thrust Lever.
NOTE: Thrust Lever movements may cause surge or an uncommanded engine shutdown.
Affected ENGINE FAILURE/SHUTDOWN Procedure (NAP-23)..........................AS REQUIRED
Engine control recovered.
FADEC IN CONTROL CHANGES?
END
END
EMERGENCY/ABNORMAL PROCEDURES Engine
EAP 6-10 REVISION 9
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ENGINE OUT
EICAS Caution: ENG1 (2) OUT
Associated Thrust Lever ......................IDLE Associated Start/Stop Selector............STOP
NOTE: If engine shutdown does not occur, pull the associated fire extinguishing handle.
Engine Thrust Rating............................CON APU (if available) ...................................START APU Bleed..............................................AS REQUIRED XBleed ....................................................AS REQUIRED Fuel.........................................................BALANCE
No
Yes
Affected ENGINE AIRSTART Procedure (NAP-19)..........................ACCOMPLISH
LAND AT THE NEAREST SUITABLE AIRPORT. TCAS ......................................................TA ONLY Altitude...................................................MAX 25’000 FT,
MIN MEA No
Yes
XBleed ....................................................OPEN Altitude...................................................MEA OR
15’000 FT, WHICHEVER IS HIGHER
If it is not possible to descend below 15’000 ft: Icing Conditions ...............................EXIT
ONE ENGINE INOPERATIVE
APPROACH AND LANDING Procedure (NAP-35)..........................AS REQUIRED
ENGINE RESTART CONSIDERED?
END
END
ICING CONDITIONS?
EMERGENCY/ABNORMAL PROCEDURES Engine
REVISION 9 EAP 6-11
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ENGINE THRUST LEVER FAILURE
EICAS Caution: ENG1 (2) TLA FAIL
Associated FADEC................................RESET No
Yes
Associated FADEC................................ALTN
No
Yes
Thrust can be partially controlled through the Thrust Rating Buttons.
Affected ENGINE FAILURE/SHUTDOWN Procedure (NAP-23)..........................AS REQUIRED
THRUST LEVER CONTROL RECOVERED?
END
THRUST LEVER CONTROL RECOVERED?
END
END
EMERGENCY/ABNORMAL PROCEDURES Engine
EAP 6-12 REVISION 9 QR
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ENGINE THRUST REVERSER FAILURE/DISAGREE
EICAS Caution: ENG1 (2) REV FAIL or ENG1 (2) REV DISAGREE
No
Yes
Do not takeoff.
No
Yes
LAND AT THE NEAREST SUITABLE AIRPORT. Associated Thrust Lever ......................IDLE
Airspeed.................................................MAX 200 KIAS
Associated ENGINE FAILURE/SHUTDOWN Procedure (NAP-23)..........................ACCOMPLISH
Message .................................................DISREGARD
ENGINE FUEL FILTER IMPENDING BYPASS
EICAS Advisory: E1 (2) FUEL IMP BYP No
Yes
LAND AT NEAREST SUITABLE AIRPORT.
END
ASSOCIATED N1 INDICATION BELOW THRUST LEVER SETTING?
ON GROUND?
END
END
BOTH FILTERS AFECTED?
END
EMERGENCY/ABNORMAL PROCEDURES Engine
REVISION 9 EAP 6-13
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ENGINE IDLE STOP FAILURE
EICAS Advisory: E1 (2) IDL STP FAIL
Protection against thrust lever movement below flight idle is not available.
Be careful when reducing engines near IDLE.
CAUTION: NEVER SET THRUST LEVER BELOW IDLE INFLIGHT.
END
EMERGENCY/ABNORMAL PROCEDURES Engine
EAP 6-14 REVISION 9 QR
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INTENTIONALLY BLANK
EMERGENCY/ABNORMAL PROCEDURES Fire Protection
ORIGINAL EAP 7-1
TABLE OF CONTENTS ANNUNCIATED PROCEDURES
BAGGAGE SMOKE................................refer to S-3
ENGINE FIRE, SEVERE DAMAGE OR SEPARATION ....................................refer to EAP 6-6
APU FIRE DETECTION FAILURE .......................EAP 7-3
APU FIRE EXTINGUISHING INOPERATIVE.......EAP 7-3
BAGGAGE COMPARTMENT FIRE EXTINGUISHING INOPERATIVE....................EAP 7-4
ENGINE FIRE DETECTION FAILURE.................EAP 7-4
ENGINE FIRE EXTINGUISHING INOPERATIVE .................................................EAP 7-5
NON ANNUNCIATED PROCEDURES
CABIN FIRE OR SMOKE .......................refer to S-5
ELECTRICAL SYSTEM FIRE OR SMOKE ............................................refer to S-6
EMERGENCY/ABNORMAL PROCEDURES Fire Protection
EAP 7-2 ORIGINAL
LIST OF EICAS MESSAGES
BAGG SMOKE .......................................refer to S-3
ENG 1 (2) FIRE.......................................refer to EAP 6-6
APU FIREDET FAIL .............................................EAP 7-3
APU EXTBTL INOP .............................................EAP 7-3
BAGG EXTBTL INOP...........................................EAP 7-4
E1 (2) FIREDET FAIL ..........................................EAP 7-4
E1 (2) EXTBTLA INOP ........................................EAP 7-5
E1 (2) EXTBTLB INOP ........................................EAP 7-5
EMERGENCY/ABNORMAL PROCEDURES Fire Protection
ORIGINAL EAP 7-3
APU FIRE DETECTION FAILURE
EICAS Caution: APU FIREDET FAIL
APU FIRE Procedure (EAP 3-3)............ACCOMPLISH
APU FIRE Procedure (EAP 3-3)............ACCOMPLISH
The APU fire detection system is inoperative.
APU FIRE EXTINGUISHING INOPERATIVE
EICAS Caution: APU EXTBTL INOP Condition: Affected bottle has not been
discharged intentionally.
APU fire protection is not available. Consider shutting the APU down. END
END
ASSOCIATED TO SUSPECTED APU FIRE OR OVERHEAT?
END
ASSOCIATED TO APU FAILURE?
END
No
Yes
No
Yes
EMERGENCY/ABNORMAL PROCEDURES Fire Protection
EAP 7-4 ORIGINAL
BAGGAGE COMPARTMENT FIRE EXTINGUISHING INOPERATIVE
EICAS Caution: BAGG EXTBTL INOP (if installed). Condition: Affected bottle has not been
discharged intentionally.
LAND AT THE NEAREST SUITABLE AIRPORT. BAGGAGE SMOKE Procedure (S-3)....AS REQUIRED
Baggage fire protection is not available.
ENGINE FIRE DETECTION FAILURE
EICAS Caution: E1 (2) FIREDET FAIL
Affected ENGINE FIRE, SEVERE DAMAGE OR SEPARATION Procedure (EAP 6-6).........................ACCOMPLISH
Affected ENGINE FIRE, SEVERE DAMAGE OR SEPARATION Procedure (EAP 6-6).........................ACCOMPLISH
The associated engine fire detection system is inoperative.
END
BAGG SMOKE MESSAGE DISPLAYED?
END
No
Yes
ASSOCIATED TO ENGINE FAILURE?
END
No
Yes
No
END
ASSOCIATED TO SUSPECTED ENGINE FIRE OR OVERHEAT?
END
Yes
EMERGENCY/ABNORMAL PROCEDURES Fire Protection
ORIGINAL EAP 7-5
ENGINE FIRE EXTINGUISHING INOPERATIVE
EICAS Caution: E1 (2) EXTBTLA INOP or E1 (2) EXTBTLB INOP
Condition: Affected bottle has not been discharged intentionally.
Only one bottle is available to protect both engines against fire.
END
EMERGENCY/ABNORMAL PROCEDURES Flight Controls
ORIGINAL EAP 8-1
TABLE OF CONTENTS
ANNUNCIATED PROCEDURES
PITCH TRIM INOPERATIVE ...............................EAP 8-3
AILERON SYSTEM INOPERATIVE ....................EAP 8-5
FLAP FAILURE ...................................................EAP 8-6
INADVERTENT SPOILER OPEN........................EAP 8-7
PITCH TRIM SWITCH INOPERATIVE ................EAP 8-8
RUDDER HARDOVER PROTECTION FAILURE.........................................................EAP 8-8
RUDDER MOVABLE STOPS DISAGREE ..........EAP 8-8
RUDDER OVERBOOST......................................EAP 8-9
RUDDER SYSTEM INOPERATIVE.....................EAP 8-10
SPEED BRAKE LEVER DISAGREE...................EAP 8-11
FLAP LOW ACTUATION SPEED .......................EAP 8-11
NON ANNUNCIATED PROCEDURES
AILERON RUNAWAY ........................... refer to NAP-3
JAMMED AILERON............................... refer to NAP-10
JAMMED ELEVATOR ........................... refer to NAP-10
JAMMED RUDDER ............................... refer to NAP-11
PITCH TRIM RUNAWAY....................... refer to NAP-13
ROLL TRIM RUNAWAY........................ refer to NAP-3
AILERON ARTIFICIAL FEEL INOPERATIVE .................................. refer to NAP-17
ASYMMETRIC RUDDER OPERATION ..................................... refer to NAP-17
GUST LOCK FAILURE.......................... refer to NAP-27
RUDDER ARTIFICIAL FEEL INOPERATIVE .................................. refer to NAP-39
RUDDER RUNAWAY ............................ refer to NAP-40
STIFFENED ELEVATOR....................... refer to NAP-41
UNCOMMANDED AILERON DISCONNECTION ............................ refer to NAP-43
UNCOMMANDED ELEVATOR DISCONNECTION ............................ refer to NAP-43
YAW TRIM RUNAWAY ......................... refer to NAP-40
EMERGENCY/ABNORMAL PROCEDURES Flight Controls
EAP 8-2 ORIGINAL
LIST OF EICAS MESSAGES
PTRIM BACKUP INOP........................................EAP 8-3
PTRIM MAIN INOP ..............................................EAP 8-3
AIL SYS 1 (2) INOP .............................................EAP 8-5
FLAP FAIL...........................................................EAP 8-6
PTRIM BKP SW FAIL..........................................EAP 8-8
PTRIM CPT SW FAIL ..........................................EAP 8-8
PTRIM F/O SW FAIL ...........................................EAP 8-8
RUD HDOV PROTFAIL .......................................EAP 8-8
RUD STOP DISAGREE.......................................EAP 8-8
RUDDER OVERBOOST......................................EAP 8-9
RUDDER SYS 1 (2) INOP....................................EAP 8-10
RUDDER SYS 1-2 INOP......................................EAP 8-10
SPBK LVR DISAGREE .......................................EAP 8-11
SPOILER FAIL.....................................................EAP 8-7
FLAP LOW SPEED .............................................EAP 8-11
EMERGENCY/ABNORMAL PROCEDURES Flight Controls
ORIGINAL EAP 8-3
PITCH TRIM INOPERATIVE
EICAS Warning: PTRIM MAIN INOP and/or PTRIM BACKUP INOP
The following message may be displayed: EICAS CAUTION: AUTO TRIM FAIL
Both
Main Backup
Pitch Trim Main Sys Cutout..................PUSH OUT Autopilot ................................................DISENGAGE
Back up system can be used to trim the airplane.
Pitch Trim Backup Sys Cutout.............PUSH OUT Main system can be used to trim the airplane. Autopilot is available.
Pitch Trim Main Sys Cutout..................PUSH OUT Pitch Trim Backup Sys Cutout.............PUSH OUT Consider LANDING AT THE NEAREST SUITABLE AIRPORT Autopilot ................................................DISENGAGE
Continue the flight using operative switch. If Main Pitch Trim System is inoperative, do not engage the Autopilot.
CONTINUES ON NEXT PAGE
END
END
INOPERATIVE SYSTEM(S)?
Yes
No MESSAGE DISPLAYED WITHOUT PRESSING ANY PITCH TRIM SWITCH?
AIRPLANE PITCH UP TENDENCY?
Yes
No
ANY PITCH TRIM SWITCH (PILOT, COPILOT OR BACKUP) WORKING?
END
Yes
No
EMERGENCY/ABNORMAL PROCEDURES Flight Controls
EAP 8-4 ORIGINAL
CONTINUED FROM PREVIOUS PAGE
WARNING: DO NOT OPEN SPEEDBRAKE.
Airspeed.................................................REDUCE If it is necessary to reduce airspeed below 180 KIAS (or 200 KIAS in icing conditions), extend flaps to 9° (at 20000 ft maximum). If it is necessary to reduce airspeed below 160 KIAS, extend flaps to 22°.
NOTE: Turning the airplane and extending the landing gear helps to maintain minimum airspeed with unwanted pitch up tendency.
Landing Configuration: Landing Gear ....................................DOWN Flaps ..................................................22° VREF.....................................................VREF45 + 10 KIAS CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED
LANDING DISTANCE BY 1.45.
WARNING: DO NOT OPEN SPEEDBRAKE.
Airspeed.................................................REDUCE Below 250 KIAS ................................FLAPS 9°
(MAX 20’000 FT) Below 180 KIAS ................................FLAPS 22°
Reducing speed and extending flaps helps to reduce control forces.
Landing Configuration:
Landing Gear ....................................DOWN Delay gear extension as long as possible. Flaps ..................................................22° VREF.....................................................VREF45 + 25 KIAS CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED
LANDING DISTANCE BY 1.75.
END
END
AIRPLANE PITCH DOWN TENDENCY?No
Yes
EMERGENCY/ABNORMAL PROCEDURES Flight Controls
ORIGINAL EAP 8-5
AILERON SYSTEM INOPERATIVE
EICAS Caution: AIL SYS 1 (2) INOP
Affected Aileron Shutoff .......................PUSH OUT Airspeed.................................................MAX 250 KIAS
Yes
Remaining Aileron Shutoff ...................PUSH OUT Autopilot ................................................DISENGAGE
Expect greater aileron control force. If required, both pilots should act together to control airplane.
Avoid landing at airports with anticipated turbulence, gusts or crosswind. Perform a long final approach. Landing Configuration:
Landing Gear ....................................DOWN Flaps ..................................................22° VREF.....................................................VREF45 + 10 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.45.
END
BOTH SYSTEMS FAILED? No
EMERGENCY/ABNORMAL PROCEDURES Flight Controls
EAP 8-6 REVISION 8
FLAP FAILURE
EICAS Caution: FLAP FAIL Condition: Flap operation is not possible. EICAS Indication: Flap position may become amber.
If flap indication on EICAS is not available, use the RMU Engine Backup Page 2 or flap position marks on the wing.
With flaps at intermediate positions, limit airspeed according to the following:
FLAPS POSITION MAX AIRSPEED
1° to 9° 250 KIAS
10° to 22° 180 KIAS
23° to 45° 145 KIAS
VREF:
FLAPS POSITION VREF
0 to 8° VREF45 + 30 KIAS
9° to 21° VREF45 + 10 KIAS
22° to 44° VREF45 + 5 KIAS
45° VREF45
At crew discretion: EGPWS CB’s (D2 or J8) ...................PULL
CAUTION: • IF FLAPS FAILED BETWEEN 22° AND 45° POSITIONS, EXIT OR AVOID ICING CONDITIONS.
MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY:
FLAPS POSITION FACTOR
0 to 8° 1.70
9° to 21° 1.40
22° to 44° 1.20
END
EMERGENCY/ABNORMAL PROCEDURES Flight Controls
REVISION 10 EAP 8-7
INADVERTENT SPOILER OPEN
EICAS Caution: SPOILER FAIL (may be presented). Condition: Sudden airspeed or altitude loss,
buffeting or roll tendency.
EICAS Indication: SPLRS OPN
Speed Brake ..........................................CLOSE
Spoilers CB’s F13, F14 and F20 or F21..........................................PULL
Do not reduce Thrust during flare.
Landing Configuration:
Flaps ..................................................22°
VREF45 ..................................................VREF45 + 10 KIAS
Jammed Open
Jammed Closed or Floating
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.50.
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.45.
END
PANEL FAILURE MODE?
END
EMERGENCY/ABNORMAL PROCEDURES Flight Controls
EAP 8-8 ORIGINAL
PITCH TRIM SWITCH INOPERATIVE
EICAS Caution: PTRIM CPT SW FAIL, PTRIM F/O SW FAIL or PTRIM BKP SW FAIL
No
Yes
Deenergize the airplane and energize it again.
Use another serviceable switch.
RUDDER HARDOVER PROTECTION FAILURE
EICAS Caution: RUD HDOV PROTFAIL
Rudder hardover protection is not available.
RUDDER MOVABLE STOPS DISAGREE
EICAS Caution: RUD STOP DISAGREE (some airplanes may have an indication light instead of EICAS message).
No
Yes
Confirm the stop position with maintenance personnel.
Beyond 10°
10°
Use takeoff performance charts.
Do not takeoff.
More rudder travel may be available. Use rudder with caution.
ON GROUND?
END
END
END
END
ON GROUND?
END
RUDDER STOP POSITION?
EMERGENCY/ABNORMAL PROCEDURES Flight Controls
ORIGINAL EAP 8-9
RUDDER OVERBOOST
EICAS Caution: RUDDER OVERBOOST
Rudder Shutoff 2 ...................................PUSH OUT
No
Yes
Rudder Shutoff 2 ...................................PUSH IN Rudder Shutoff 1 ...................................PUSH OUT Below 135 KIAS:
Rudder Shutoff 1 ..............................PUSH IN
Below 135 KIAS:
Rudder Shutoff 2 ..............................PUSH IN
END
RUDDER OVERBOOST MESSAGE PERSISTS?
END
EMERGENCY/ABNORMAL PROCEDURES Flight Controls
EAP 8-10 ORIGINAL
RUDDER SYSTEM INOPERATIVE
EICAS Caution: RUDDER SYS 1 (2) INOP or RUDDER SYS 1-2 INOP
No
Yes
RUDDER RUNAWAY Procedure (NAP-40)..........................ACCOMPLISH
Only one (1 or 2)
Affected Rudder Shutoff.......................PUSH OUT
Rudder Shutoff 2 ...................................PUSH OUT
Yes
Rudder Shutoff 1 ...................................PUSH OUT Rudder Shutoffs 1 and 2.......................PUSH IN
Yes
Expect heavier than normal rudder pedals. If required, combine effort of both pilots.
Consider use of aileron and asymmetric thrust to control the airplane.
Avoid airports with reported gusts, turbulence or crosswind.
CONTINUES ON NEXT PAGE
END
INOPERATIVE SYSTEM?
RUDDER 1-2 INOP MESSAGE PERSISTS?
RUDDER 1-2 INOP MESSAGE PERSISTS?
FOLLOWING A RUDDER RUNAWAY?
END
Both (1 and 2)
No
No
EMERGENCY/ABNORMAL PROCEDURES Flight Controls
ORIGINAL EAP 8-11
CONTINUED FROM PREVIOUS PAGE
No
Yes
Landing Configuration:
Flaps ..................................................22°
VREF45 ..................................................VREF45 + 10 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.45.
SPEED BRAKE LEVER DISAGREE
EICAS Caution: SPBK LVR DISAGREE
Speed Brake Lever................................CLOSE
FLAP LOW ACTUATION SPEED
EICAS Advisory: FLAP LOW SPEED
Anticipate flap actuation.
END
END
END
LANDING IN ICING CONDITIONS?
EMERGENCY/ABNORMAL PROCEDURES Fuel
REVISION 9 EAP 9-1
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TABLE OF CONTENTS
ANNUNCIATED PROCEDURES
CHECK AIRCRAFT LOAD................................ EAP 9-3
FUEL LOW LEVEL............................................ EAP 9-3
FUEL TRANSFER CRITICAL............................ EAP 9-4
APU FUEL LOW PRESSURE .............. refer to EAP 3-5
APU FUEL SHUTOFF VALVE INOPERATIVE ................................. EAP 9-5
ENGINE FUEL LOW PRESSURE..................... EAP 9-6
ENGINE FUEL LOW TEMPERATURE ............. EAP 9-7
ENGINE FUEL SHUTOFF VALVE INOPERATIVE .............................................. EAP 9-7
FUEL CROSSFEED FAILURE.......................... EAP 9-8
FUEL CROSSFEED MISCOMMAND ................ EAP 9-9
FUEL IMBALANCE ........................................... EAP 9-13
FUEL TANK LOW TEMPERATURE ................. EAP 9-9
FUEL TANK VENTILATION VALVE OPEN ............................................... EAP 9-10
FUEL TRANSFER CHECK................................ EAP 9-10
FUEL TRANSFER INOPERATIVE.................... EAP 9-11
FUSELAGE FUEL IMBALANCE....................... EAP 9-13
WING FUEL IMBALANCE................................. EAP 9-15
WING TANKS OVERFLOW .............................. EAP 9-16
ENGINE FUEL FILTER IMPENDING BYPASS ......................refer to EAP 6-12
EMERGENCY/ABNORMAL PROCEDURES Fuel
EAP 9-2 REVISION 9
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LIST OF EICAS MESSAGES
CHECK ACFT LOAD......................................... EAP 9-3
FUEL 1 (2) LO LEVEL....................................... EAP 9-3
FUEL XFER CRITICAL...................................... EAP 9-4 APU FUEL LO PRESS ......................... refer to EAP 3-5
APU FUEL SOV INOP....................................... EAP 9-5
E1 (2) FUEL LO PRESS.................................... EAP 9-6
E1 (2) FUEL LO TEMP ...................................... EAP 9-7
E1 (2) FUEL SOV INOP..................................... EAP 9-7
FUEL IMBALANCE ........................................... EAP 9-15
FUEL TANK LO TEMP...................................... EAP 9-9
FUEL TK VENT OPEN ...................................... EAP 9-10
FUEL XFEED FAIL............................................ EAP 9-8
FUEL XFEED MISCMD ..................................... EAP 9-9
FUEL XFER 1 (2) INOP ..................................... EAP 9-11
FUEL XFER CHECK.......................................... EAP 9-10
FUEL XFER OVFLOW....................................... EAP 9-16
FUSELAGE FUEL IMB...................................... EAP 9-13
E1 (2) FUEL IMP BYP .......................... refer to EAP 6-12
EMERGENCY/ABNORMAL PROCEDURES Fuel
REVISION 9 EAP 9-3
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CHECK AIRCRAFT LOAD
EICAS Warning: CHECK ACFT LOAD
Thrust Levers ................................... LONG RANGE SET
FUS TK XFER.................................... FUS 1 OR FUS 2 Fuel Transfer System....................... CHECK STATUS
Yes
Consider diversion. Remaining Fuel ................................ CHECK Avoid rapid maneuvers and flying in severe turbulence conditions.
Before touchdown: Rate of Descent ........................... MAX 450 FT/MIN
Touch smoothly the runway surface. Reduce engine thrust only after touchdown.
FUEL LOW LEVEL
EICAS Warning: FUEL 1 (2) LO LEVEL MFD Indication: Fuel quantity in red range.
Thrust Levers ..................................... LONG RANGE CRUISE
Level the airplane and check available fuel quantities. If necessary, use available auxiliary fuel tanks. No
Yes
LAND AT THE NEAREST SUITABLE AIRPORT. Avoid attitudes in excess of 10° nose down or 10° nose up attitude, uncoordinated maneuvers and negative g's.
XFeed Operation ................................ AS REQUIRED
FUEL TRANSFER OPERATIVE?
END
END
No
END
END
FUEL QUANTITY IS SUFFICIENT?
EMERGENCY/ABNORMAL PROCEDURES Fuel
EAP 9-4 REVISION 9
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FUEL TRANSFER CRITICAL
EICAS Warning: FUEL XFER CRITICAL
Thrust Levers ................................... LONG RANGE SET
FUS TK XFER.................................... FUS 1 OR FUS 2 Fuel Transfer System....................... CHECK STATUS
Yes
Consider diversion. Remaining Fuel ................................ CHECK Avoid rapid maneuvers and flying in severe turbulence conditions.
Before touchdown: Rate of Descent ........................... MAX 450 FT/MIN
Touch smoothly the runway surface. Reduce engine thrust only after touchdown.
FUEL TRANSFER OPERATIVE?
END
END
No
EMERGENCY/ABNORMAL PROCEDURES Fuel
REVISION 9 EAP 9-5
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APU FUEL SHUTOFF VALVE INOPERATIVE
EICAS Caution: APU FUEL SOV INOP
APU Fuel Shutoff Button ................. CHECK NOT PRESSED
No Yes
Disregard the message.
No Yes
APU Master Knob............................. OFF
APU RUNNING NORMALLY?
END
APU SHUTOFF VALVE REMAINS CLOSED?
END
EMERGENCY/ABNORMAL PROCEDURES Fuel
EAP 9-6 REVISION 10
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ENGINE FUEL LOW PRESSURE
EICAS Caution: E1 (2) FUEL LO PRESS Condition: One or more affected tank electric fuel
pump may be inoperative
Associated Fuel Pump Sel .............. SELECT ANOTHER
No
Yes
Altitude.............................................. MAX 25’000 FT, MIN MEA
Avoid rapid thrust lever movements and set minimum required thrust.
NOTE: If required, the flight may proceed above 25’000 ft using XFEED.
No
Yes
LAND AT THE NEAREST SUITABLE AIRPORT.
Avoid rapid thrust lever movements and set minimum required thrust.
NOTE: If required, the flight may proceed above 25’000 ft using XFEED.
OPERATING WITH TS-1 KEROSENE?
ALL PUMPS INOPERATIVE IN THE AFFECTED TANK?
END
EMERGENCY/ABNORMAL PROCEDURES Fuel
REVISION 9 EAP 9-7
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ENGINE FUEL LOW TEMPERATURE
EICAS Caution: E1 (2) FUEL LO TEMP
WARNING: ENGINE FLAMEOUT MAY OCCUR IF FUEL TANK LO TEMP MESSAGE IS PRESENTED, OR E1 (2) FUEL LO TEMP IS PRESENTED WITHOUT FUEL ICING INHIBITOR.
No Yes
Do not takeoff.
Descend to lower altitude and monitor engine indications as long as the message remains.
ENGINE FUEL SHUTOFF VALVE INOPERATIVE
EICAS Caution: E1 (2) FUEL SOV INOP Engine Fuel Indications..........................MONITOR
No Yes
XFEED ......................................................OFF Associated Fuel Pump Pwr ....................OFF
Fire Extinguishing Handle......................CHECK IN
No Yes
Message ...................................................DISREGARD
LAND AT THE NEAREST SUITABLE AIRPORT. Associated ENGINE FAILURE/SHUTDOWN
Procedure (NAP-23)............................ACCOMPLISH
END
AFTER PULLING FIRE HANDLE?
END
ENGINE OPERATION NORMAL?
END
END
ON GROUND?
END
EMERGENCY/ABNORMAL PROCEDURES Fuel
EAP 9-8 REVISION 9
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FUEL CROSSFEED FAILURE
EICAS Caution: FUEL XFEED FAIL
Crossfeed.......................................... OFF Fuel Imbalance ................................. MONITOR Asymmetric Thrust........................... AS REQUIRED No
Yes
Avoid uncoordinated maneuvers, flying in turbulence conditions and negative g's.
END
END
FUEL XFEED OPEN?
EMERGENCY/ABNORMAL PROCEDURES Fuel
REVISION 9 EAP 9-9
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FUEL CROSSFEED MISCOMMAND
EICAS Caution: FUEL XFEED MISCMD XFEED ............................................... OFF Fuel Imbalance ................................. CHECK XFEED ............................................... AS REQUIRED Check XFEED selector knob properly positioned to correct wing fuel imbalance.
FUEL TANK LOW TEMPERATURE
EICAS Caution: FUEL TANK LO TEMP MFD Indication: Fuel temperature in amber range.
WARNING: ENGINE FLAMEOUT MAY OCCUR.
No Yes
Do not takeoff.
Descend to lower altitude and monitor engine indications as long as the message remains.
END
END
END
ON GROUND?
EMERGENCY/ABNORMAL PROCEDURES Fuel
EAP 9-10 REVISION 9
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FUEL TANK VENTILATION VALVE OPEN
EICAS Caution: FUEL TK VENT OPEN
No
Yes
Do not takeoff.
While there is fuel in aft auxiliary fuel tanks: Altitude.............................................. MAX 25’000 FT,
MIN MEA Airspeed............................................ MAX 300 KIAS
Avoid pitch attitudes in excess of 5° nose up attitude, uncoordinated maneuvers and negative g's.
FUEL TRANSFER CHECK
EICAS Caution: FUEL XFER CHECK
FUS TK XFER.................................... FUS 1 OR FUS 2
ON GROUND?
END
END
END
EMERGENCY/ABNORMAL PROCEDURES Fuel
REVISION 9 EAP 9-11
QR
H-1
35
/15
69
C
OD
E 0
1
FUEL TRANSFER INOPERATIVE
EICAS Caution: FUEL XFER 1 (2) INOP
Yes
Do not takeoff.
Fuel Pump Sel ..............................SELECT ANOTHER
No
Yes
Altitude..........................................MIN 20’000 FT
No
Yes
FUS TK XFER Knob .....................CHECK POSITION
FUS TK XFER Knob .....................OFF
................................................. WAIT 10 SECS
FUS TK XFER Knob .................... RESELECT SAME CHECKED POSITION
Fuel Quantity ................................MONITOR
Check remaining fuel quantity available and consider diversion.
ON GROUND?
MESSAGE PERSISTS?
END
END
MESSAGE PERSISTS?
No
EMERGENCY/ABNORMAL PROCEDURES Fuel
EAP 9-12 REVISION 9
QR
H-1
35
/15
69
C
OD
E 0
1
INTENTIONALLY BLANK
EMERGENCY/ABNORMAL PROCEDURES Fuel
REVISION 9 EAP 9-13
QR
H-1
35
/15
69
C
OD
E 0
1
FUSELAGE FUEL IMBALANCE
EICAS Caution: FUSELAGE FUEL IMB If fuel imbalance is confirmed:
FUEL XFER MASTER Knob ...............OFF
Auxiliary Tanks Quantity on MFD .....CHECK
Yes
FUS TK XFER Knob ................................ FUS 1
Yes
FUS TK XFER Knob ................................ FUS 2
No
Yes
During approach:
Autopilot..............................................DISENGAGE
END
ANY LEFT SIDE AUXILIARY TANKS QUANTITY DECREASES?
ANY RIGHT SIDE AUXILIARY TANKS QUANTITY DECREASES?
END
No
No
END
MESSAGE PERSISTS?
EMERGENCY/ABNORMAL PROCEDURES Fuel
EAP 9-14 REVISION 9
QR
H-1
35
/15
69
C
OD
E 0
1
INTENTIONALLY BLANK
EMERGENCY/ABNORMAL PROCEDURES Fuel
REVISION 9 EAP 9-15
QR
H-1
35
/15
69
C
OD
E 0
1
WING FUEL IMBALANCE
EICAS Caution: WING FUEL IMBALANCE No Yes
FUEL LEAK Procedure (NAP-42) .............ACCOMPLISH
If wing fuel imbalance is confirmed:
XFEED Operation................................ACCOMPLISH
END
FUEL LEAK SUSPECTED?
END
EMERGENCY/ABNORMAL PROCEDURES Fuel
EAP 9-16 REVISION 9
QR
H-1
35
/15
69
C
OD
E 0
1
WING TANKS OVERFLOW
EICAS Caution: FUEL XFER OVFLOW
FUS TK XFER.........................................OFF When required: FUS TK XFER ....................................FUS 1 OR FUS 2
Wing Fuel Quantity...........................MONITOR Monitor wing fuel quantity and turn Fuselage Tank Transfer Knob OFF when wing fuel reaches 2400 kg.
END
EMERGENCY/ABNORMAL PROCEDURES Hydraulics
ORIGINAL EAP 10-1
TABLE OF CONTENTS
ANNUNCIATED PROCEDURES
BOTH HYDRAULIC SYSTEMS FAILURE ..........EAP 10-3
HYDRAULIC SYSTEM 1 FAILURE.....................EAP 10-5
HYDRAULIC SYSTEM 2 FAILURE.....................EAP 10-6
HYDRAULIC SYSTEM OVERHEAT ...................EAP 10-8
ENGINE HYDRAULIC PUMP FAILURE .............EAP 10-8
HYDRAULIC SYSTEM LOW QUANTITY............EAP 10-9
EMERGENCY/ABNORMAL PROCEDURES Hydraulics
EAP 10-2 ORIGINAL
LIST OF EICAS MESSAGES
HYD SYS 1-2 FAIL ..............................................EAP 10-3
HYD SYS 1 FAIL..................................................EAP 10-5
HYD SYS 2 FAIL..................................................EAP 10-6
HYD SYS 1 (2) OVHT ..........................................EAP 10-8
E1 (2) HYD PUMP FAIL.......................................EAP 10-8
HYD1 (2) LO QTY................................................EAP 10-9
EMERGENCY/ABNORMAL PROCEDURES Hydraulics
REVISION 10 EAP 10-3
BOTH HYDRAULIC SYSTEMS FAILURE
EICAS Caution: HYD SYS 1-2 FAIL MFD Indication: Hydraulic pressure may be amber. Condition: Noise increase due to nose landing
gear doors open.
The following messages will be displayed: EICAS Caution: AIL SYS 1-2 INOP,
RUDDER SYS 1-2 INOP
EICAS Advisory: E1-2 HYD PUMP FAIL
CAUTION: DO NOT OPEN THE SPEED BRAKES.
Airspeed............................................ MAX 250 KIAS
No
Yes
System(s) in green range: Hydraulic Elec Pump(s) .............. ON
No
Yes Hydraulic 2
Hydraulic 1
HYDRAULIC SYSTEM 2 FAILURE Procedure (EAP 10-6).................. AS REQUIRED
HYDRAULIC SYSTEM 1 FAILURE Procedure (EAP 10-5).................. AS REQUIRED
LAND AT THE NEAREST SUITABLE AIRPORT. CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED
LANDING DISTANCE BY 2.67.
Autopilot/Yaw Damper..................... DISENGAGE Both Hydraulic Elec Pumps ............ OFF
Expect greater aileron and rudder control force. If required, both pilots should act together to control airplane. Consider using aileron and asymmetric thrust to help yaw control.
NOTE: Pitch Trim and Roll Trim Systems are available.
ANY HYDRAULIC SYSTEM FLUID QUANTITY IN GREEN RANGE?
AT LEAST ONE SYSTEM RECOVERED?
END
WHICH SYSTEM RECOVERED?
END
CONTINUES ON NEXT PAGE
EMERGENCY/ABNORMAL PROCEDURES Hydraulics
EAP 10-4 REVISION 4
CONTINUED FROM PREVIOUS PAGE
Relevant Inoperative Items:
Normal gear extension Anti-skid Thrust reversers
Normal brakes Steering Spoilers
Main door retraction
Approach: APU ....................................................AS REQUIRED Altimeters ..........................................SET AND CROSS
CHECKED Approach Aids ..................................SET AND
CROSS CHECKED
Speed Bugs.......................................SET
Set speed bugs considering the new landing configuration presented below.
Pressurization...................................CHECK Go-Around Procedure...........................REVIEW
If necessary, accomplish a normal go-around procedure except that landing gear cannot be retracted.
Before Landing: Free Fall Lever ..................................ACTUATE Landing Gear Lever..........................DOWN
Perform a long final approach. Avoid landings at airports with anticipated crosswind or turbulence.
CAUTION: DO NOT FLARE.
Use rudder for directional control on ground. During landing run, pull Emergency Brake Handle carefully. Landing Configuration:
Landing Gear ....................................DOWN Flaps ..................................................22° VREF.....................................................VREF45 + 10 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 2.67.
END
EMERGENCY/ABNORMAL PROCEDURES Hydraulics
ORIGINAL EAP 10-5
HYDRAULIC SYSTEM 1 FAILURE
EICAS Caution: HYD SYS 1 FAIL MFD Indication: Hydraulic pressure may be amber. Condition: Noise increase due to nose landing
gear doors open.
The following messages will be displayed: EICAS Caution: AIL SYS 1 INOP,
RUDDER SYS 1 INOP
EICAS Advisory: E1 HYD PUMP FAIL
Yes
Hydraulic Elec Pump 1 .........................ON
No
Yes
Hydraulic Elec Pump 1 .........................OFF Airspeed.................................................MAX 250 KIAS Relevant Inoperative Items:
Inboard Spoiler Normal gear extension Thrust reverser 1
Steering Main door retraction Outboard brakes
Before Landing:
Free Fall Lever ..................................ACTUATE
Landing Gear Lever..........................DOWN
Brake effectiveness will be reduced.
Do not actuate engine 1 Thrust Reverser.
No
Yes
Landing Configuration:
Flaps ..................................................22° VREF.....................................................VREF45 + 10 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 2.38.
CONTINUES ON NEXT PAGE
HYDRAULIC SYSTEM 1 FLUID QUANTITY IN GREEN RANGE?
SYSTEM RECOVERED?
END
END
LANDING IN ICING CONDITIONS?
No
EMERGENCY/ABNORMAL PROCEDURES Hydraulics
EAP 10-6 ORIGINAL
CONTINUED FROM PREVIOUS PAGE
Landing Configuration:
Flaps ............................................. 45° VREF................................................ VREF45
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.64.
HYDRAULIC SYSTEM 2 FAILURE
EICAS Caution: HYD SYS 2 FAIL MFD Indication: Hydraulic pressure may be amber.
The following messages will be displayed: EICAS Caution: AIL SYS 2 INOP,
RUDDER SYS 2 INOP
EICAS Advisory: E2 HYD PUMP FAIL
CAUTION: DO NOT OPEN THE SPEED BRAKES.
Yes
Hydraulic Elec Pump 2..................... ON
No
Yes
Hydraulic Elec Pump 2..................... OFF Airspeed............................................ MAX 250 KIAS Relevant Inoperative Items:
Outboard Spoiler Thrust reverser 2 Inboard brakes
The Emergency/Parking Brake has accumulator pressure only.
Brake effectiveness will be reduced.
Do not actuate engine 2 Thrust Reverser.
CONTINUES ON NEXT PAGE
HYDRAULIC SYSTEM 2 FLUID QUANTITY IN GREEN RANGE?
SYSTEM RECOVERED?
END
END
No
EMERGENCY/ABNORMAL PROCEDURES Hydraulics
ORIGINAL EAP 10-7
CONTINUED FROM PREVIOUS PAGE
No
Yes
Landing Configuration: Landing Gear ............................... DOWN Flaps ............................................. 22° VREF................................................ VREF45 + 10 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 2.27.
Landing Configuration: Landing Gear ............................... DOWN Flaps ............................................. 45° VREF................................................ VREF45
CAUTION: MULTIPLY THE FLAPS 45 UNFACTORED LANDING DISTANCE BY 1.56.
END
END
LANDING IN ICING CONDITIONS?
EMERGENCY/ABNORMAL PROCEDURES Hydraulics
EAP 10-8 REVISION 9
HYDRAULIC SYSTEM OVERHEAT
EICAS Caution: HYD SYS 1 (2) OVHT
Turn the affected system OFF: Associated Hydraulic
Eng Pump Shutoff................... PUSH IN Associated Hydraulic
Elec Pump................................ OFF EICAS Messages related to associated hydraulic system will be displayed while system is set to OFF.
Airspeed............................................ MAX 250 KIAS For remainder of flight, even if the message is displayed:
Affected Hydraulic System ......... 15 MINUTES OFF, 1 MINUTE ON
NOTE: To turn the hydraulic system ON, first turn the Hydraulic Elec Pump to AUTO. As soon as the system pressure is recovered, push out the Hydraulic Eng Pump Shutoff button.
During Approach and Landing or when required: Affected Hydraulic System ......... ON
After reaching taxi speed or when the system is no longer required:
Affected Hydraulic System ......... OFF
ENGINE HYDRAULIC PUMP FAILURE
EICAS Advisory: E1 (2) HYD PUMP FAIL Altitude.............................................. MAX 37000 FT Associated Hydraulic Elec Pump ... CHECK ON
Hydraulic 2
Hydraulic 1
HYDRAULIC SYSTEM 1 FAILURE Procedure (EAP 10-5).................. AS REQUIRED
NOTE: Do not open the Speed Brakes.
HYDRAULIC SYSTEM 2 FAILURE Procedure (EAP 10-6).................. AS REQUIRED
END
END
AFFECTED SYSTEM?
END
EMERGENCY/ABNORMAL PROCEDURES Hydraulics
ORIGINAL EAP 10-9
HYDRAULIC SYSTEM LOW QUANTITY
EICAS Advisory: HYD1 (2) LO QTY MFD Indication: Hydraulic fluid quantity may be amber.
Affected Hydraulic System.............. MONITOR
Hydraulic 2
Hydraulic 1
HYDRAULIC SYSTEM 1 FAILURE Procedure (EAP 10-5).................. AS REQUIRED
NOTE: Do not open the Speed Brakes.
HYDRAULIC SYSTEM 2 FAILURE Procedure (EAP 10-6).................. AS REQUIRED
END
END
AFFECTED SYSTEM?
EMERGENCY/ABNORMAL PROCEDURES Ice & Rain Protection
ORIGINAL EAP 11-1
TABLE OF CONTENTS
ANNUNCIATED PROCEDURES
ICING CONDITIONS WITH ANTI-ICING INOPERATIVE...............................................EAP 11-3
ANTI-ICING LOW CAPACITY.........................EAP 11-4
ANTI-ICING SWITCH OFF ..............................EAP 11-4
AOA HEATING INOPERATIVE.......................EAP 11-4
ENGINE ANTI-ICING FAILURE ......................EAP 11-5
ICE DETECTOR FAIL .....................................EAP 11-5
NO ICE - ANTI-ICE ON....................................EAP 11-6
PITOT HEATING INOPERATIVE ....................EAP 11-6
STABILIZER ANTI-ICING FAILURE...............EAP 11-8
TAT HEATING INOPERATIVE........................EAP 11-7
WINDSHIELD HEATING FAILURE.................EAP 11-7
WING ANTI-ICING FAILURE ..........................EAP 11-8
NON ANNUNCIATED PROCEDURES
SINGLE ENGINE BLEED OPERATION IN ICING CONDITIONS..................... refer to NAP-41
EMERGENCY/ABNORMAL PROCEDURES Ice & Rain Protection
EAP 11-2 ORIGINAL
LIST OF EICAS MESSAGES
ICE COND-A/I INOP ........................................EAP 11-3
A/ICE LOW CAPACIT .....................................EAP 11-4
A/ICE SWITCH OFF ........................................EAP 11-4
AOA 1 (2) HEAT INOP ....................................EAP 11-4
E1 (2) A/ICE FAIL............................................EAP 11-5
ICE DET1 (2) FAIL...........................................EAP 11-5
ICE DETECTORS FAIL ...................................EAP 11-5
NO ICE-A/ICE ON............................................EAP 11-6
PITOT 1 (2, 3) INOP ........................................EAP 11-6
STAB A/ICE FAIL............................................EAP 11-8
TAT 1 (2) HEAT INOP .....................................EAP 11-7
W/S 1 (2) HEAT FAIL ......................................EAP 11-7
WG A/ICE FAIL ...............................................EAP 11-8
EMERGENCY/ABNORMAL PROCEDURES Ice & Rain Protection
ORIGINAL EAP 11-3
ICING CONDITIONS WITH ANTI-ICING INOPERATIVE
EICAS Warning: ICE COND-A/I INOP
No
Yes
Thrust Levers .................................IDLE Ice Detection Override Knob.........AUTO Ice Detection Test Knob ................1, FOR 5 SECONDS,
THEN 2, FOR 5 SECONDS
No
Yes
No
Yes
TAKEOFF Procedure .....................ACCOMPLISH
Do not takeoff. Ice Detection Override Knob.........ALL Associated Failure Procedure ......ACCOMPLISH Icing Conditions .............................EXIT
END
END
END
ON GROUND?
ALL OPEN INSCRIPTIONS FLASH AT LEAST ONCE AND ICE DET 1 (OR 2) FAIL AND ICE CONDITION DISPLAYED?
ANTI-ICING SYSTEM EICAS MESSAGES DISAPPEAR WITHIN 60 SECONDS?
EMERGENCY/ABNORMAL PROCEDURES Ice & Rain Protection
EAP 11-4 REVISION 4
ANTI-ICING LOW CAPACITY
EICAS Caution: A/ICE LOW CAPACIT
The following message will be displayed: EICAS Warning: ICE COND-A/INOP
The following messages may be displayed: EICAS Caution: WG A/ICE FAIL,
STAB A/ICE FAIL
Thrust Levers ................................... ADVANCE Advance Thrust Levers to at least 55% N1.
...................................................... WAIT 5 SECONDS No
Yes WING ANTI-ICING FAILURE OR
STABILIZER ANTI-ICING FAILURE Procedure (EAP 11-8).................. AS REQUIRED
ANTI-ICING SWITCH OFF
EICAS Caution: A/ICE SWITCH OFF
All Ice Protection Buttons ............... PUSH IN
AOA HEATING INOPERATIVE
EICAS Caution: AOA 1 (2) HEAT INOP
Minimum Airspeed ........................... FLAP MANEUVERING SPEED (PD-2)
END
END
MESSAGE PERSISTS?
END
EMERGENCY/ABNORMAL PROCEDURES Ice & Rain Protection
ORIGINAL EAP 11-5
ENGINE ANTI-ICING FAILURE
EICAS Caution: E1 (2) A/ICE FAIL
Thrust Levers ........................................ADVANCE No
Yes
Ice Detection Override Knob................ALL
No
Yes
Ice Protection Engine Air Inlet .............PUSH OUT, THEN PUSH IN
No
Yes
Icing Conditions ....................................AVOID/EXIT Two minutes after exiting icing conditions:
Ice Detection Override Knob ...........AUTO
Engine Vibration....................................MONITOR If vibration increases, advance thrust levers one at a time, to 60% N1 minimum for 5 seconds. If vibration increases to unacceptable values or engine parameters indicate abnormal values, exit icing conditions.
ICE DETECTOR FAIL
EICAS Caution: ICE DET1 (2) FAIL or ICE DETECTORS FAIL
When flying in icing conditions: Ice Detection Override Knob ...........ALL
Two minutes after exiting icing conditions: Ice Detection Override Knob ...........AUTO
END
MESSAGE PERSISTS?
MESSAGE STILL PERSISTS?
MESSAGE STILL PERSISTS?
END
EMERGENCY/ABNORMAL PROCEDURES Ice & Rain Protection
EAP 11-6 ORIGINAL
NO ICE - ANTI-ICE ON
EICAS Caution: NO ICE-A/ICE ON
Ice Detection Override Knob........... AUTO No
Yes
No
Yes
Altitude.............................................. MAX 25’000 FT, MIN MEA
APU.................................................... START APU Bleed......................................... PUSH IN XBleed ............................................... OPEN Engine Bleeds .................................. PUSH OUT
Ice Protection Buttons..................... PUSH OUT
Operate the Anti-Icing Systems through the buttons, pushing them in again whenever icing conditions are encountered.
PITOT HEATING INOPERATIVE
EICAS Caution: PITOT 1 (2, 3) INOP
Instruments information supplied by the affected system may be unreliable. Cross-check and do not use the affected system if a disagreement is found. If the Pitot 3 heating is inoperative, standby instruments and pressurization system may be affected. If necessary:
ADC on Associated Reversionary Panel................. PUSH IN
END
MESSAGE PERSISTS?
ASSOCIATED TO EITHER WG A/ICE FAIL OR STAB A/ICE FAIL MESSAGE?
END
END
EMERGENCY/ABNORMAL PROCEDURES Ice & Rain Protection
REVISION 10 EAP 11-7
TAT HEATING INOPERATIVE
EICAS Caution: TAT 1 (2) HEAT INOP
Associated TAT, TAS and SAT indication may be unreliable.
WINDSHIELD HEATING FAILURE
EICAS Caution: W/S 1 (2) HEAT FAIL
Associated Ice Protection Windshield ................................... PUSH OUT
END
END
EMERGENCY/ABNORMAL PROCEDURES Ice & Rain Protection
EAP 11-8 REVISION 4
WING ANTI-ICING FAILURE OR STABILIZER ANTI-ICING FAILURE
EICAS Caution: WG A/ICE FAIL or STAB A/ICE FAIL
Ice Detector Override Knob..................ALL Thrust Levers ........................................ADVANCE
No
Yes
Affected Ice Protection Button.............PUSH OUT, THEN PUSH IN
No
Yes
Associated Ice Protection Button........PUSH OUT Icing Conditions ....................................AVOID/EXIT Two minutes after exiting icing conditions: Ice Detector Override Knob .............AUTO Bank Angle ............................................MAX 30° Airspeed (Flaps 0° or 9°).......................MIN 190 KIAS
No
Yes
Stab
Wing or Wing+Stab
Landing configuration: Landing Gear ....................................DOWN Flaps ..................................................22° VREF.....................................................VREF45 + 30 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.85.
Landing configuration: Landing Gear ....................................DOWN Flaps ..................................................22° VREF.....................................................VREF45 + 15 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.55.
END
MESSAGE PERSISTS?
MESSAGE STILL PERSISTS?
AFFECTED SYSTEM(S)?
LANDING IN ICING CONDITIONS OR WITH ICE ACCRETION?
END
EMERGENCY/ABNORMAL PROCEDURES Landing Gear & Brakes
ORIGINAL EAP 12-1
TABLE OF CONTENTS
ANNUNCIATED PROCEDURES
LANDING GEAR/LEVER DISAGREE............... EAP 12-3
BRAKE OVERHEAT.......................................... EAP 12-4
BRAKES DEGRADED....................................... EAP 12-5
BRAKES INOPERATIVE................................... EAP 12-6
EMERGENCY/PARKING BRAKE LOW PRESSURE ......................................... EAP 12-7
LANDING GEAR AIR/GROUND SYSTEM FAILURE ....................................... EAP 12-8
NOSE LANDING GEAR UP DOOR OPEN ....... EAP 12-9
STEERING SYSTEM INOPERATIVE................ EAP 12-9
UNCOMMANDED SWERVING ON GROUND............................ EAP 12-9
NON ANNUNCIATED PROCEDURES
ABNORMAL LANDING GEAR EXTENSION ..........................................refer to NAP-16
EMERGENCY/PARKING BRAKE HANDLE DISAGREE..............................refer to NAP-18
GEAR LEVER CANNOT MOVE UP AFTER TAKEOFF ..................................refer to NAP-27
PARTIAL OR GEAR UP LANDING........refer to NAP-38
EMERGENCY/ABNORMAL PROCEDURES Landing Gear & Brakes
EAP 12-2 ORIGINAL
LIST OF EICAS MESSAGES
LG/LEVER DISAGREE...................................... EAP 12-3
BRAKE DEGRADED......................................... EAP 12-5
BRAKE OVERHEAT.......................................... EAP 12-4
BRK INBD INOP................................................ EAP 12-6
BRK OUTBD INOP............................................ EAP 12-6
EMRG BRK LO PRES....................................... EAP 12-7
LG AIR/GND FAIL ............................................. EAP 12-8
NLG UP/DOOR OPN ......................................... EAP 12-9
STEER INOP ..................................................... EAP 12-9
EMERGENCY/ABNORMAL PROCEDURES Landing Gear & Brakes
REVISION 4 EAP 12-3
LANDING GEAR/LEVER DISAGREE
EICAS Warning: LG/LEVER DISAGREE EICAS Indication: Landing gear abnormal indication. Condition: Landing gear cannot move to desired
position.
The following message may be displayed:
EICAS Caution: NLG UP/DOOR OPN No
Yes
Consider to stop the airplane. Takeoff is not permitted.
Confirm the message on EICAS, check landing gear indication and, even if Landing Gear Indication shows three green lights:
Airspeed.................................................MAX 200 KIAS Landing Gear .........................................CYCLE
No
Yes Extended
Retracted
LAND AT THE NEAREST SUITABLE AIRPORT. Landing Gear Lever ..............................DOWN Airspeed.................................................MAX 250 KIAS Icing Conditions ....................................AVOID/EXIT Fuel Consumption.................................MONITOR
ABNORMAL LANDING GEAR EXTENSION Procedure (NAP-16)..........................ACCOMPLISH
END
END
LG/LEVER DISAGREE MESSAGE PERSISTS?
DESIRED LANDING GEAR POSITION?
END
ON GROUND?
EMERGENCY/ABNORMAL PROCEDURES Landing Gear & Brakes
EAP 12-4 ORIGINAL
BRAKE OVERHEAT EICAS Caution: BRAKE OVERHEAT
No
Yes
If necessary, reduce brake pressure. Use of full reverse thrust is recommended. Airplane..................................................STOP Chocks ...................................................ON Parking Brake ........................................RELEASE Airspeed.................................................MAX 250 KIAS Landing Gear Lever ..............................DOWN Brakes Temperature .............................CHECK IN THE
GREEN RANGE Airspeed.................................................MAX 200 KIAS Landing Gear Lever ..............................UP
END
END
ON GROUND?
EMERGENCY/ABNORMAL PROCEDURES Landing Gear & Brakes
ORIGINAL EAP 12-5
ICING CONDITIONS?
BRAKES DEGRADED EICAS Caution: BRAKE DEGRADED
During landing run: Brakes........................................... APPLY NORMALLY Use thrust reverser if available.
Brake effectiveness and symmetry may be affected.
Approach Configuration:
Yes
Landing configuration: Landing Gear ............................... DOWN Flaps ............................................. 22° VREF................................................ VREF45 + 10 KIAS
MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.71.
Landing configuration:
Landing Gear ............................... DOWN Flaps ............................................. 45° VREF................................................ VREF45
MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.20.
END
END
No
EMERGENCY/ABNORMAL PROCEDURES Landing Gear & Brakes
EAP 12-6 ORIGINAL
ICING CONDITIONS?
BRAKES INOPERATIVE EICAS Caution: BRK OUTBD (INBD) INOP
During landing run:
If available, use thrust reverser.
Both (OUTBD and INBD)
Only one (OUTBD or INBD)
Brakes ............................................... APPLY NORMALLY
No
Yes
Landing configuration: Landing Gear ....................................DOWN Flaps ..................................................22° VREF.....................................................VREF45 + 10 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 2.18.
Landing configuration: Landing Gear ....................................DOWN Flaps ..................................................45° VREF.....................................................VREF45
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.49.
Emergency Brake Handle ................ PULL CAREFULLY
Relevant Inoperative Item: Anti-skid
Landing configuration: Landing Gear ....................................DOWN Flaps ..................................................22° VREF.....................................................VREF45 + 10 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 2.18.
CONTINUES ON NEXT PAGE
END
BRAKES INOPERATIVE?
END
END
ICING CONDITIONS?
Yes
No
EMERGENCY/ABNORMAL PROCEDURES Landing Gear & Brakes
ORIGINAL EAP 12-7
CONTINUED FROM PREVIOUS PAGE
Landing configuration: Landing Gear ....................................DOWN Flaps ..................................................45° VREF.....................................................VREF45
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.49.
EMERGENCY/PARKING BRAKE LOW PRESSURE
EICAS Caution: EMRG BRK LO PRES
Emergency/Parking Brake performance may be degraded. When parking the airplane, use wheel chocks.
END
END
EMERGENCY/ABNORMAL PROCEDURES Landing Gear & Brakes
EAP 12-8 REVISION 4
ICING CONDITIONS?
LANDING GEAR AIR/GROUND SYSTEM FAILURE
EICAS Caution: LG AIR/GND FAIL
Thrust Reversers and Ground Spoilers may not be available.
Depending on the failed condition, Ground Idle may not be selectable.
If the message is presented on ground, a loss of the main brake capacity may occur (below 10 kt ground speed) and steering may not be available.
Refer to the associated procedure for each case.
No
Yes
Anti-Icing System..................................MONITOR If any anti-ice valve does not open or anti-ice failure messages appear, leave and avoid icing conditions.
After exiting icing conditions, proceed as follows: Bank Angle........................................MAX 30° Airspeed for Flaps up or 9°..............MIN 190 KIAS
Landing configuration: Landing Gear ....................................DOWN Flaps ..................................................22° VREF.....................................................VREF45 + 10 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 2.00.
Icing Conditions ....................................AVOID
Landing configuration: Landing Gear ....................................DOWN Flaps ..................................................45° VREF.....................................................VREF45
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.70.
END
END
EMERGENCY/ABNORMAL PROCEDURES Landing Gear & Brakes
REVISION 10 EAP 12-9
NOSE LANDING GEAR UP DOOR OPEN EICAS Caution: NLG UP/DOOR OPN EICAS Indication: Landing gear abnormal indication. Condition: Landing gear cannot move to desired
position.
The following message may be displayed: EICAS Warning: LG/LEVER DISAGREE
Confirm the message on EICAS, check landing gear indication and, even if Landing Gear Indication shows three green lights:
Airspeed.................................................MAX 200 KIAS Landing Gear .........................................CYCLE
No
Yes Extended
Retracted
LAND AT THE NEAREST SUITABLE AIRPORT. Landing Gear Lever ..............................DOWN Airspeed.................................................MAX 250 KIAS Icing Conditions ....................................AVOID/EXIT Fuel Consumption.................................MONITOR
ABNORMAL LANDING GEAR EXTENSION
Procedure (NAP-16)..........................ACCOMPLISH
STEERING SYSTEM INOPERATIVE OR UNCOMMANDED SWERVING ON GROUND EICAS Caution: STEER INOP may be displayed.
Steering Handwheel..............................DO NOT USE Steering Disengagement Button .........PRESS
Control the airplane using differential brakes and rudder. If serviceable, consider the use of differential thrust reverser.
END
END
LG/LEVER DISAGREE MESSAGE PERSISTS?
DESIRED LANDING GEAR POSITION?
END
EMERGENCY/ABNORMAL PROCEDURES Oxygen
ORIGINAL EAP 13-1
TABLE OF CONTENTS
ANNUNCIATED PROCEDURES
CREW OXYGEN LOW PRESSURE...................EAP 13-3
PASSENGER OXYGEN LOW PRESSURE .......EAP 13-3
NON ANNUNCIATED PROCEDURES
OXYGEN LEAKAGE ................................ refer to NAP-37
EMERGENCY/ABNORMAL PROCEDURES Oxygen
EAP 13-2 ORIGINAL
LIST OF EICAS MESSAGES
CREW OXY LO PRESS......................................EAP 13-3
PAX OXY LO PRESS .........................................EAP 13-3
EMERGENCY/ABNORMAL PROCEDURES Oxygen
ORIGINAL EAP 13-3
CREW OXYGEN LOW PRESSURE
EICAS Caution: CREW OXY LO PRESS
MFD Indication: Oxygen pressure red or amber.
Altitude.............................................. MEA OR 10’000 FT,
WHICHEVER IS HIGHER
PASSENGER OXYGEN LOW PRESSURE
EICAS Caution: PAX OXY LO PRESS
MFD Indication: Oxygen pressure red or amber.
Altitude.............................................. MEA OR 10’000 FT,
WHICHEVER IS HIGHER
END
END
EMERGENCY/ABNORMAL PROCEDURES Warning System
REVISION 9 EAP 14-1
TABLE OF CONTENTS
ANNUNCIATED PROCEDURES
STALL PROTECTION INOPERATIVE.............. EAP 14-3
TAKEOFF CONFIGURATION WARNING ........ EAP 14-4
ADVANCED STALL PROTECTION.................. EAP 14-5
AURAL WARNING FAIL ................................... EAP 14-6
EGPWS INOPERATIVE..................................... EAP 14-6
STICK PUSHER FAILURE................................ EAP 14-7
WINDSHEAR DETECTION INOPERATIVE ...... EAP 14-8
NON ANNUNCIATED PROCEDURES
AIRPLANE OVERSPEED.......................refer to NAP-4
ERRONEOUS STALL PROTECTION ACTUATION ......................................refer to NAP-26A
EMERGENCY/ABNORMAL PROCEDURES Warning System
EAP 14-2 REVISION 4
LIST OF EICAS MESSAGES
SPS 1 (2) INOP.................................................. EAP 14-3
SPS 1-2 INOP .................................................... EAP 14-3
NO TAKEOFF CONFIG..................................... EAP 14-4
AURAL WARN FAIL.......................................... EAP 14-6
SPS ADVANCED............................................... EAP 14-5
STICK PUSHER FAIL........................................ EAP 14-7
TERR INOP........................................................ EAP 14-6
WINDSHEAR INOP ........................................... EAP 14-8
EMERGENCY/ABNORMAL PROCEDURES Warning System
REVISION 4 EAP 14-3
STALL PROTECTION INOPERATIVE
EICAS Warning: SPS 1 (2) INOP or SPS 1-2 INOP
The following messages will be displayed: EICAS CAUTION: SPS ADVANCED STICK PUSHER FAIL
Affected Stall Protection Cutout Button ...................................PUSH OUT
Avoid skidding the airplane.
NOTE: - The remaining stick shaker is available. - Stick pusher is not available.
Yes
Add 15 KIAS to go-around speed. Landing configuration:
Landing Gear ....................................DOWN Flaps ..................................................22° VREF.....................................................VREF45 + 15 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.55.
Add 5 KIAS to go-around speed. Landing configuration:
Landing Gear ....................................DOWN Flaps ..................................................45° VREF.....................................................VREF45 + 5 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.13.
END
END
ICING CONDITIONS? No
EMERGENCY/ABNORMAL PROCEDURES Warning System
EAP 14-4 REVISION 10
TAKEOFF CONFIGURATION WARNING
EICAS Warning: NO TAKEOFF CONFIG Aural Warning: Voice Messages TAKEOFF-BRAKES,
TAKEOFF-FLAPS, TAKEOFF-TRIM, TAKEOFF-SPOILERS, TAKEOFF-FUEL
EICAS Indication: Spoiler and pitch trim may be red.
Do not takeoff.
Airplane Configuration .........................CORRECT
TO Config Button ..................................PRESS
END
EMERGENCY/ABNORMAL PROCEDURES Warning System
REVISION 4 EAP 14-5
ADVANCED STALL PROTECTION
EICAS Caution: SPS ADVANCED
Above 25’000 ft: Minimum Airspeed ...........................150 KIAS
Below 25’000 ft: Minimum Airspeed ...........................FLAP
MANEUVERING SPEED (PD-2)
No
Yes Add 15 KIAS to go-around speed. Landing configuration:
Landing Gear ....................................DOWN Flaps ..................................................22° VREF.....................................................VREF45 + 15 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.55.
Add 5 KIAS to go-around speed. Landing configuration:
Landing Gear ....................................DOWN Flaps ..................................................45° VREF.....................................................VREF45 + 5 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.13.
END
ICING CONDITIONS?
END
EMERGENCY/ABNORMAL PROCEDURES Warning System
EAP 14-6 REVISION 10
AURAL WARNING FAIL
EICAS Caution: AURAL WARN FAIL
Visually monitor every EICAS, MFD and PFD indication specially related to TCAS, Windshear Detection, GPWS, IC-600, Fire Detection, Stall Protection, Trims, Flaps, Brakes, Spoilers, Radio Altimeter, Autopilot, Landing gear, ADC, Pressurization, SELCAL. No aural warning will be available. Do not perform CAT II or CAT III approaches.
EGPWS INOPERATIVE
EICAS Caution: TERR INOP, GPWS INOP, WINDSHEAR INOP
Monitor visually any trend toward terrain contact, excessive sink rate, marginal flight path and airplane configuration. No aural warning related to the system will be available.
END
END
EMERGENCY/ABNORMAL PROCEDURES Warning System
REVISION 4 EAP 14-7
STICK PUSHER FAILURE
EICAS Caution: STICK PUSHER FAIL The following message will be displayed:
EICAS Warning: SPS 1-2 INOP
Control Column .....................................TOWARD NEUTRAL
Airspeed.................................................MIN FLAP MANEUVERING SPEED (PD-2)
No
Yes
JAMMED ELEVATOR Procedure (NAP-10)..........................ACCOMPLISH
Both stick shaker 1 and 2 are still available. No
Yes
Add 15 KIAS to go-around speed.
Landing configuration:
Landing gear .....................................DOWN
Flaps ..................................................22°
Airspeed ............................................VREF 45 + 15 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.55.
Add 5 KIAS to go-around speed.
Landing configuration:
Landing gear .....................................DOWN
Flaps ..................................................45°
Airspeed ............................................VREF 45 + 5 KIAS
CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.13.
STICK PUSHER JAMMED?
END
ICING CONDITIONS?
END
END
EMERGENCY/ABNORMAL PROCEDURES Warning System
EAP 14-8 REVISION 4
WINDSHEAR DETECTION INOPERATIVE
EICAS Caution: WINDSHEAR INOP
Windshear detection is not available.
END
PERFORMANCE DATA ALL ENGINES
REVISION 5 PD-1
5 10 15 20 25 30 35 40 45 50
80 100
5 10 15 20 25 30 34 39 44 49
70 110
5 9 14 19 23 28 33 38 42 47
60 120
4 9 13 17 22 26 30 35 39 43
50 130
4 8 11 15 19 23 27 31 34 38
40 140
3 6 10 13 16 19 22 26 29 32
30 150
3 5 8 10 13 15 18 20 23 25
20 160
2 3 5 7 9 10 12 14 15 17
10 170
1 2 3 3 4 5 6 7 8 9
-5 -10
-15
-20
-25
-30
-34
-39
-44
-49
-5 -9 -14
-19
-23
-28
-33
-38
-42
-47
-4 -9 -13
-17
-22
-26
-30
-35
-39
-43
-4 -8 -11
-15
-19
-23
-27
-31
-34
-38
-3 -6 -10
-13
-16
-19
-22
-26
-29
-32
-3 -5 -8 -10
-13
-15
-18
-20
-23
-25
-2 -3 -5 -7 -9 -10
-12
-14
-15
-17
-1 -2 -3 -3 -4 -5 -6 -7 -8 -9
1 2 3 3 4 5 6 7 8 9
2 3 5 7 9 10 12 14 15 17
3 5 8 10 13 15 18 20 23 25
3 6 10 13 16 19 22 26 29 32
4 8 11 15 19 23 27 31 34 38
4 9 13 17 22 26 30 35 39 43
5 9 14 19 23 28 33 38 42 47
5 10 15 20 25 30 34 39 44 49
5 10 15 20 25 30 35 40 45 50
Exa
mpl
e: G
iven
Win
d S
peed
=20
kt
and
Ang
le (
betw
een
win
d an
d no
se)=
30°
, th
e H
eadw
ind
Com
pone
nt is
17
kt a
nd t
he C
ross
win
d co
mpo
nent
is 1
0 kt
.
WIN
D C
OM
PO
NE
NT
TA
BL
E
AN
GL
E B
ET
WE
EN
WIN
D D
IRE
CT
ION
AN
D H
EA
DIN
G (
LE
FT
OR
RIG
HT
)
170
HE
AD
WIN
D C
OM
PO
NE
NT
(kt
)C
RO
SS
WIN
D C
OM
PO
NE
NT
(kt
)
130
140
1020
3040
TA
ILW
IND
CO
MP
ON
EN
T (
kt)
5060
7015
016
080
100
110
120
MAXIMUM RECOMMENDED CROSSWIND
SURFACE CONDITION MAXIMUM
CROSSWIND
Dry 30 kt
Wet 25 kt
Contaminated by Compacted Snow 20 kt
Contaminated by Standing Water, Slush or Loose Snow
15 kt
Contaminated by Ice (no melting) 10 kt
PERFORMANCE DATA ALL ENGINES
PD-2 REVISION 7
PITCH TRIM UNITS
CG POSITION
(%)
LESS THAN OR
EQUAL TO 26.0
26.1 UP TO
28.5
28.6 UP TO
30.5
30.6 UP TO
33.5
ABOVE OR EQUAL TO
33.6
PITCH TRIM UNITS
8 7 6 5 4
FLAP RETRACTION SCHEDULE
For a flaps 9° takeoff: Flaps 9° to UP
V2 + 15 KIAS
FLAP MANEUVERING SPEED
GEAR/FLAP No Icing Conditions Icing Conditions
UP/0° 180 KIAS 200 KIAS
UP/9° 160 KIAS 160 KIAS
(DN/22°/45°) 140 KIAS 140 KIAS
PERFORMANCE DATA AE3007A1P ENGINES
REVISION 5 PD-2A
UNRELIABLE AIRSPEED (Climb)
Airplane: EMB-145 – Engine: AE3007A1P & A1E – Anti-Ice: OFF
WEIGHT (kg) PRESSURE ALTITUDE (ft)
14000 16000 18000 20000 22000 240000 Pitch (deg) 13 12 11 10 10 9
(240 KIAS) V/S (ft/min) 5018 4248 3656 3192 2818 2504 10000 Pitch (deg) 10 9 8 8 8 8
(240 KIAS) V/S (ft/min) 3582 3011 2573 2221 1939 1709 20000 Pitch (deg) 6 6 5 5 5 5
(270 KIAS) V/S (ft/min) 2562 2110 1764 1486 1257 1070 30000 Pitch (deg) 5 5 5 5 5 5
(0.65 M) V/S (ft/min) 1681 1358 1095 889 721 575 40000 Pitch (deg) 5 5 5 5 5 -
(0.65 M) V/S (ft/min) 785 583 402 201 38 -
UNRELIABLE AIRSPEED (Cruise)
Airplane: EMB-145 – Engine: AE3007A1P & A1E – Anti-Ice: OFF
WEIGHT (kg) PRESSURE ALTITUDE (ft)
14000 16000 18000 20000 22000 2400015000 Pitch (deg) 1 2 2 2 3 3
(250 KIAS) N1 (%) 68.0 68.9 69.7 70.6 71.4 72.2 20000 Pitch (deg) 1 2 2 2 3 3
(250 KIAS) N1 (%) 70.6 71.6 72.7 73.8 74.9 75.8 25000 Pitch (deg) 1 2 2 2 3 3
(250 KIAS) N1 (%) 73.9 75.2 76.5 77.8 79.0 80.0 30000 Pitch (deg) 2 2 2 3 3 4
(0.63 M) N1 (%) 76.2 77.7 79.1 80.2 81.3 82.5 35000 Pitch (deg) 2 3 3 4 4 5
(0.63 M) N1 (%) 77.2 78.5 80.0 81.4 83.4 85.7 40000 Pitch (deg) 3 4 5 5 6 6
(0.63 M) N1 (%) 79.5 81.3 83.9 87.6 90.9 92.3 45000 Pitch (deg) 5 5 6 6 7 7
(0.63 M) N1 (%) 83.6 88.2 92.2 92.2 92.2 92.2
UNRELIABLE AIRSPEED (Descent)
Airplane: EMB-145 – Engine: AE3007A1P & A1E – Anti-Ice: OFF
WEIGHT (kg) PRESSURE ALTITUDE (ft)
14000 16000 18000 20000 22000 240000 Pitch (deg) -3 -2 -1 -1 0 0
(240 KIAS) V/S (ft/min) -1756 -1649 -1572 -1504 -1445 -139810000 Pitch (deg) -3 -2 -1 -1 0 0
(240 KIAS) V/S (ft/min) -1828 -1709 -1619 -1547 -1483 -143220000 Pitch (deg) -6 -5 -5 -4 -4 -3
(310 KIAS) V/S (ft/min) -3806 -3384 -3057 -2842 -2693 -256630000 Pitch (deg) -6 -5 -4 -4 -3 -3
(310 KIAS) V/S (ft/min) -3317 -2952 -2731 -2604 -2494 -240440000 Pitch (deg) -2 -2 -2 -1 -1 -1
(0.78 M) V/S (ft/min) -1668 -1606 -1652 -1693 -1781 -1949
PERFORMANCE DATA AE3007A1P ENGINES
PD-2B REVISION 5
UNRELIABLE AIRSPEED (Holding)
Airplane: EMB-145 – Engine: AE3007A1P & A1E – Anti-Ice: OFF
WEIGHT (kg) PRESSURE ALTITUDE (ft)
14000 16000 18000 20000 22000 240005000 Pitch (deg) 3 3 4 5 5 6
(200 KIAS) N1 (%) 54.0 55.3 56.5 58.3 59.8 61.4 10000 Pitch (deg) 3 3 4 5 5 6
(200 KIAS) N1 (%) 57.6 58.9 60.2 62.0 63.6 65.2
UNRELIABLE AIRSPEED (Terminal Area)
Terminal Area (5000 ft) - %N1 for Level Flight
Airplane: EMB-145 – Engine: AE3007A1P & A1E – Anti-Ice: OFF
WEIGHT (kg) FLAP POSITION (VREF + INCREMENT)
14000 16000 18000 20000 22000 240000 Pitch (deg) 7 7 7 7 8 8
(VREF45 + 30) N1 (%) 47.2 50.2 53.1 55.8 58.3 60.6 9 Pitch (deg) 7 8 8 8 8 10
(VREF45 + 15) N1 (%) 50.7 54.2 57.3 60.2 63.1 71.5
UNRELIABLE AIRSPEED (Final Approach)
Final Approach (1500 ft) - %N1 for 3° Glideslope
Airplane: EMB-145 – Engine: AE3007A1P & A1E – Anti-Ice: OFF
WEIGHT (kg) FLAP POSITION (VREF + INCREMENT)
14000 16000 18000 20000 22000 2400022 Pitch (deg) 3 3 3 4 4 4
(VREF22 + 10) N1 (%) 45.8 48.7 51.5 54.1 56.4 58.7 45 Pitch (deg) 0 0 0 0 1 0
(VREF45 + 10) N1 (%) 59.0 62.2 65.3 68.2 70.6 72.9
PERFORMANCE DATA AE3007A1P ENGINES
ORIGINAL PD-3
TAKEOFF SPEEDS (Balanced Field Length)
V1/VR/V2 SPEEDS ALT T/O-1 MODE - FLAPS 9°
PRESSURE ALTITUDE
(ft)
STATIC AIR TEMPERATURE (C)
SL -40 to 47 48 to 50 1000 -40 to 45 46 to 48 2000 -40 to 41 42 to 46 3000 -40 to 38 39 to 44 4000 -40 to 33 34 to 41 42 to 42 5000 -40 to 29 30 to 37 38 to 40 6000 -40 to 18 19 to 30 31 to 38 7000 -40 to 23 24 to 36 8000 -40 to 9 10 to 29 30 to 348500 -40 to 25 26 to 32
WEIGHT (kg) V1 VR V2 V1 VR V2 V1 VR V2 V1 VR V2
12000 101 120 128 98 115 123 95 110 117 91 105 11212500 100 119 127 98 114 122 95 109 116 93 105 11213000 100 118 126 98 114 121 95 108 115 95 106 11213500 100 118 125 98 113 119 96 109 116 96 107 11314000 101 117 123 98 112 118 98 109 116 98 108 11414500 101 115 122 99 112 118 99 110 116 100 110 11515000 101 114 121 101 112 119 101 111 117 103 111 11715500 102 114 121 102 113 119 103 113 119 105 113 11816000 103 114 121 103 114 120 105 115 120 107 115 12016500 105 116 122 106 116 122 108 117 122 110 117 12217000 107 117 124 108 118 124 110 119 124 112 119 12417500 109 119 125 110 120 125 112 120 125 114 121 12518000 112 121 127 113 122 127 115 122 127 117 123 12718500 114 123 129 115 124 129 117 124 129 117 124 12819000 116 125 130 117 125 130 119 126 130 118 125 12819500 118 127 132 119 127 132 121 128 132 118 125 12820000 120 129 133 121 129 133 123 130 133 118 125 12820500 122 130 135 123 131 135 124 131 134 118 125 12821000 124 132 136 125 132 136 125 132 135 118 125 12821500 126 134 138 127 134 138 125 132 135 118 125 12822000 128 135 139 129 136 139 125 132 135 118 125 12822500 130 137 141 129 136 140 125 132 135 118 125 12823000 131 138 142 130 137 140 125 132 135 118 125 128
PERFORMANCE DATA AE3007A1P ENGINES
PD-4 ORIGINAL
TAKEOFF SPEEDS (Balanced Field Length)
V1/VR/V2 SPEEDS T/O MODE - FLAPS 9°
PRESSURE ALTITUDE
(ft)
STATIC AIR TEMPERATURE (C)
SL -40 to 39 40 to 46 47 to 50 1000 -40 to 37 38 to 43 44 to 48 2000 -40 to 33 34 to 40 41 to 46 3000 -40 to 35 36 to 44 4000 -40 to 31 32 to 40 41 to 42 5000 -40 to 27 28 to 35 36 to 40 6000 -40 to 28 29 to 38 7000 -40 to 21 22 to 36 8000 -40 to 11 12 to 32 33 to 348500 -40 to 2 3 to 28 29 to 32
WEIGHT (kg) V1 VR V2 V1 VR V2 V1 VR V2 V1 VR V2 V1 VR V2
12000 105 127 137 101 121 130 98 115 124 94 110 118 91 104 11212500 105 126 135 101 120 129 98 114 123 94 109 117 93 105 11213000 104 125 134 101 119 128 97 113 121 94 108 115 95 106 11313500 104 124 133 101 118 127 97 113 120 96 109 116 97 107 11414000 104 123 132 101 117 126 98 112 120 98 110 117 98 108 11514500 104 122 131 101 117 124 99 113 120 99 111 118 101 110 11615000 104 122 129 101 116 123 100 114 120 101 112 118 103 112 11715500 104 120 128 102 116 123 102 114 121 103 113 119 105 114 11816000 104 119 126 103 116 123 103 115 121 105 115 120 108 116 12016500 104 119 126 104 117 123 105 116 122 107 117 122 110 118 12217000 104 118 125 105 117 124 107 118 124 109 119 124 112 120 12417500 107 119 126 108 119 125 110 120 125 112 121 125 115 121 12518000 109 120 127 110 121 127 112 122 127 114 122 127 117 123 12718500 111 122 129 113 123 129 114 124 129 116 124 129 119 125 12819000 113 124 130 115 125 130 117 125 130 119 126 130 120 126 13019500 115 126 132 117 126 132 119 127 132 121 128 132 120 126 13020000 118 128 133 119 128 133 121 129 133 123 130 133 120 126 13020500 120 129 135 121 130 135 123 131 135 125 131 135 120 126 13021000 122 131 136 123 132 136 125 132 136 126 133 136 120 126 13021500 124 133 138 125 133 138 126 134 138 126 133 136 120 126 13022000 126 134 139 127 135 139 128 136 139 126 133 136 120 126 13022500 127 136 141 129 137 141 130 137 140 126 133 136 120 126 13023000 129 138 142 131 138 142 131 138 142 126 133 136 120 126 130
PERFORMANCE DATA AE3007A1P ENGINES
ORIGINAL PD-5
APPROACH CLIMB SPEED (VAPPCLB) &
REFERENCE SPEED (VREF) and FINAL SEGMENT SPEED (VFS)
Approach Flaps 9° Landing Flaps 22°
Approach Flaps 9° Landing Flaps 45°
Weight (kg)
VAPPCLB & VREF (KIAS)
VAPPCLB & VREF (KIAS)
VFS
(KIAS)
No ice encounter
After ice encounter
No ice encounter
After ice encounter
13000 116 116 118 118 135
13500 116 118 118 118 137
14000 116 120 118 118 140
14500 116 122 118 119 142
15000 116 124 118 120 144
15500 118 126 118 121 147
16000 120 128 119 123 149
16500 121 129 120 125 151
17000 123 131 121 127 153
17500 125 133 123 129 155
18000 126 134 124 131 157
18500 128 136 126 132 159
19000 130 138 128 134 161
19500 131 139 129 136 162
20000 133 141 131 138 164
20500 134 142 133 139 166
21000 136 144 134 141 168
21500 137 145 136 143 169
22000 139 147 137 144 171
22500 140 148 139 146 173
23000 142 150 141 148 174
APPROACH SPEED (VAPP)
VAPP = VREF + ½ steady headwind component + gust increment above steady wind.
PERFORMANCE DATA AE3007A1P ENGINES
PD-6 ORIGINAL
HOLDING - (All Engines)
CRUISE CONFIGURATION BLEED OPEN ANTI-ICE: OFF MINIMUM FUEL CONSUMPTION SPEED STANDARD ATMOSPHERE
0 5000 10000 15000 20000 25000 30000 35000 39000
IAS KT 180 182 182 183 185 185 188 189 -N1 % 56.5 60.3 64.2 68.0 71.7 76.0 80.5 84.8 -FF kg/H/ENG 489 469 452 441 436 435 442 455 -
IAS KT 175 178 179 179 181 181 183 185 187N1 % 55.3 59.2 63.1 67.0 70.6 74.8 79.4 83.6 90.4FF kg/H/ENG 471 451 434 422 416 414 420 431 454
IAS KT 171 173 175 174 176 177 179 180 182N1 % 54.2 58.0 61.9 65.8 69.5 73.6 78.2 82.4 89.0FF kg/H/ENG 454 433 417 404 397 394 398 408 428
IAS KT 167 168 171 170 171 173 174 176 177N1 % 53.1 56.7 60.7 64.6 68.4 72.3 76.8 81.2 87.4FF kg/H/ENG 438 416 400 386 378 375 376 385 403
IAS KT 163 163 166 166 167 169 169 171 172N1 % 51.9 55.4 59.4 63.3 67.1 71.0 75.5 80.0 85.8FF kg/H/ENG 421 399 382 368 359 355 356 363 378
IAS KT 158 159 161 162 162 164 164 167 167N1 % 50.6 54.1 58.0 62.1 65.9 69.7 74.1 78.7 84.2FF kg/H/ENG 404 382 365 351 341 336 335 341 354
IAS KT 154 154 156 158 157 159 160 161 162N1 % 49.2 52.8 56.6 60.6 64.6 68.3 72.5 77.3 82.8FF kg/H/ENG 388 365 347 334 323 317 315 319 330
IAS KT 150 149 150 153 152 153 155 156 157N1 % 47.9 51.4 55.0 59.1 63.1 66.9 71.0 75.7 81.4FF kg/H/ENG 371 349 330 316 305 298 296 297 308
IAS KT 146 145 145 147 148 148 150 150 152N1 % 46.5 49.9 53.5 57.4 61.5 65.4 69.4 73.9 79.7FF kg/H/ENG 355 332 313 299 288 280 277 277 285
IAS KT 141 140 140 141 143 143 144 145 146N1 % 45.0 48.3 51.9 55.8 59.9 63.9 67.7 72.2 78.0FF kg/H/ENG 339 316 297 282 270 262 257 257 263
17000
16000
15000
14000
21000
20000
19000
18000
ALTITUDE (FT)WEIGHT(kg)
23000
22000
PERFORMANCE DATA AE3007A1P ENGINES
ORIGINAL PD-7
HOLDING - (All Engines)
CRUISE CONFIGURATION, BLEED OPEN, AIRSPEED: 1.3 VS OR 200 KIAS WHICHEVER IS HIGHER ANTI-ICE: ON (NO ICE ACCRETION) STANDARD ATMOSPHERE
0 5000 10000 15000 20000 25000 30000 35000 39000
IAS KT 200 200 200 200 200 200 200 200 -N1 % 57.5 61.2 65.0 68.7 72.2 76.5 80.8 85.0 -FF kg/H/ENG 506 484 467 455 449 448 453 465 -
IAS KT 200 200 200 200 200 200 200 200 -N1 % 56.7 60.4 64.2 67.9 71.4 75.6 80.0 83.9 -FF kg/H/ENG 494 472 454 442 434 432 436 447 -
IAS KT 200 200 200 200 200 200 200 200 -N1 % 56.0 59.5 63.4 67.2 70.6 74.6 79.1 83.0 -FF kg/H/ENG 482 460 442 429 421 418 420 429 -
IAS KT 200 200 200 200 200 200 200 200 -N1 % 55.3 58.7 62.6 66.5 69.9 73.7 78.2 82.1 -FF kg/H/ENG 471 449 430 417 408 404 405 413 -
IAS KT 200 200 200 200 200 200 200 200 -N1 % 54.5 57.9 61.9 65.8 69.2 72.8 77.3 81.3 -FF kg/H/ENG 461 438 419 405 396 391 391 397 -
IAS KT 200 200 200 200 200 200 200 200 200N1 % 53.8 57.2 61.1 65.0 68.5 72.0 76.3 80.5 85.7FF kg/H/ENG 451 428 409 394 384 378 378 383 397
IAS KT 200 200 200 200 200 200 200 200 200N1 % 53.1 56.5 60.3 64.2 67.8 71.3 75.4 79.7 84.7FF kg/H/ENG 442 418 399 384 373 367 365 369 382
IAS KT 200 200 200 200 200 200 200 200 200N1 % 52.4 55.8 59.5 63.5 67.1 70.5 74.6 78.9 83.9FF kg/H/ENG 433 409 390 374 363 356 354 356 368
IAS KT 200 200 200 200 200 200 200 200 200N1 % 51.7 55.2 58.8 62.8 66.5 69.9 73.7 78.2 83.2FF kg/H/ENG 425 401 381 365 354 346 343 344 355
IAS KT 200 200 200 200 200 200 200 200 200N1 % 51.2 54.5 58.1 62.2 65.9 69.2 72.9 77.5 82.4FF kg/H/ENG 417 393 373 357 345 337 333 333 343
17000
16000
15000
14000
21000
20000
19000
18000
WEIGHT(kg)
ALTITUDE (FT)
23000
22000
PERFORMANCE DATA AE3007A1P ENGINES
PD-8 ORIGINAL
DRIFTDOWN TABLE
ANTI-ICE OFF
WEIGHT INITIAL GROSS LEVEL OFF ALTITUDE - FT
(KG) DRIFTDOWN (NET LEVEL OFF ALTITUDE - FT)
START LEVEL SPEED
DRIFTDOWN OFF (KIAS) ISA ISA + 10 ISA + 20
21825 21683 21093 22000 21020 171
(16578) (16379) (16026)
23477 23319 22558 21000 20099 168
(18627) (18368) 17978
24877 24777 23867 20000 19160 164
(20375) (20224) (19722)
26285 26174 25092 19000 18262 161
(21809) (21670) (21086)
27952 27861 26530 18000 17320 157
(23442) (23327) (22581)
29872 29701 28015 17000 16348 153
(25146) (25038) (24086)
31969 31629 29461 16000 15401 149
(26870) (26777) (25588)
33540 33280 30994 15000 14461 144
(28782) (28646) (27181)
PERFORMANCE DATA AE3007A1P ENGINES
ORIGINAL PD-9
UNFACTORED LANDING DISTANCE
UNFACTORED LANDING DISTANCE (METERS) EMB-135BJ - FLAPS 45o
NO ICE ENCOUNTER ISA CONDITIONS - SLOPE 0%
ALTITUDE WEIGHT 0 ft 1000 ft
(kg) WIND WIND -10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
13000 861 732 692 653 878 748 707 667 14000 857 729 689 650 874 745 704 665 15000 855 727 687 648 872 742 702 662 16000 869 740 700 660 887 756 715 675 17000 905 773 731 691 924 790 748 707 18000 942 806 764 722 962 824 781 739 19000 979 840 796 754 1000 859 815 772 20000 1019 876 831 788 1041 896 851 806
ALTITUDE
WEIGHT 2000 ft 3000 ft
(kg) WIND WIND -10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
13000 895 764 722 682 914 780 739 698 14000 892 761 720 680 910 777 736 695 15000 889 758 717 677 907 775 733 693 16000 905 772 731 690 923 789 747 706 17000 943 807 764 723 963 825 782 740 18000 982 843 799 757 1004 862 818 775 19000 1022 879 834 790 1045 899 854 810 20000 1064 917 871 826 1088 939 892 847
ALTITUDE
WEIGHT 4000 ft 5000 ft
(kg) WIND WIND -10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
13000 933 798 755 714 953 816 773 732 14000 929 795 752 711 949 813 770 729 15000 926 792 750 709 946 810 768 726 16000 943 807 764 723 963 826 782 740 17000 984 844 800 758 1006 864 820 777 18000 1026 883 838 794 1049 904 858 814 19000 1068 921 875 830 1093 944 897 851 20000 1113 962 914 868 1140 986 937 891
PERFORMANCE DATA AE3007A1P ENGINES
PD-10 ORIGINAL
UNFACTORED LANDING DISTANCE
UNFACTORED LANDING DISTANCE (METERS) EMB-135BJ - FLAPS 45o
NO ICE ENCOUNTER ISA CONDITIONS - SLOPE 0%
ALTITUDE WEIGHT 6000 ft 7000 ft
(kg) WIND WIND -10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt
13000 974 835 792 749 996 855 811 768 14000 970 832 788 746 992 852 807 765 15000 967 829 786 744 989 849 805 762 16000 985 845 801 759 1007 865 821 778 17000 1028 885 840 796 1052 906 860 816 18000 1074 926 879 834 1099 949 902 856 19000 1119 967 919 873 1146 991 943 896 20000 1167 1011 961 914 1195 1036 987 938
ALTITUDE
WEIGHT 8000 ft
(kg) WIND -10 kt 0 kt 10 kt 20 kt
13000 1018 875 831 787 14000 1014 872 827 784 15000 1011 869 825 781 16000 1030 886 841 797 17000 1077 929 882 837 18000 1125 973 925 878 19000 1174 1017 968 920 20000 1225 1063 1013 963
PERFORMANCE DATA AE3007A1P ENGINES
REVISION 7 PD-11
EMB-135BJ UNFACTORED LANDING DISTANCES -
CONTAMINATED RUNWAYS (m)
ALL ENGINES TYPES – EASA CERTIFICATION
STANDING WATER 4 mm/SLUSH 4 mm
WET SNOW 8 mm/DRY SNOW 32 mm
WEIGHT (kg) FLAP 22° FLAP 45°
13000 1857 1606 13500 1920 1623 14000 1982 1640 14500 2044 1657 15000 2106 1674 15500 2169 1723 16000 2232 1772 16500 2296 1821 17000 2359 1870 17500 2427 1923 18000 2493 1975 18500 2560 2028 19000 2626 2081 19500 2696 2138 20000 2766 2194 20500 2836 2251 21000 2906 2308 21500 2975 2364 22000 3043 2420 22500 3112 2475
CORRECTIONS
ALTITUDE LANDING DISTANCE + 4% per 1000 ft above sea level (Altitude correction limited up to 10000 ft above sea level).
WIND LANDING DISTANCE + 9% per 5 kt tailwind.
OVERSPEED LANDING DISTANCE + 9% per 5 kt above VREF.
TEMPERATURE LANDING DISTANCE + 2% per 5ºC above ISA.
SLOPE LANDING DISTANCE + 8% per 1% slope downhill.
PERFORMANCE DATA AE3007A1P ENGINES
PD-12 REVISION 7
EMB-135BJ UNFACTORED LANDING DISTANCES -
CONTAMINATED RUNWAYS (m)
ALL ENGINES TYPES – EASA CERTIFICATION
STANDING WATER 8 mm/SLUSH 9 mm
WET SNOW 16 mm/DRY SNOW 64 mm
WEIGHT (kg) FLAP 22° FLAP 45°
13000 1650 1466 13500 1703 1481 14000 1755 1496 14500 1808 1510 15000 1860 1525 15500 1914 1568 16000 1968 1612 16500 2021 1655 17000 2075 1698 17500 2132 1744 18000 2189 1791 18500 2247 1838 19000 2304 1885 19500 2364 1936 20000 2424 1986 20500 2484 2037 21000 2544 2087 21500 2604 2138 22000 2664 2188 22500 2724 2238
CORRECTIONS
ALTITUDE LANDING DISTANCE + 4% per 1000 ft above sea level (Altitude correction limited up to 10000 ft above sea level).
WIND LANDING DISTANCE + 9% per 5 kt tailwind.
OVERSPEED LANDING DISTANCE + 8% per 5 kt above VREF.
TEMPERATURE LANDING DISTANCE + 2% per 5ºC above ISA.
SLOPE LANDING DISTANCE + 8% per 1% slope downhill.
PERFORMANCE DATA AE3007A1P ENGINES
REVISION 7 PD-13
EMB-135BJ UNFACTORED LANDING DISTANCES -
CONTAMINATED RUNWAYS (m)
ALL ENGINES TYPES – EASA CERTIFICATION
STANDING WATER 12 mm/SLUSH 14 mm
WET SNOW 24 mm/DRY SNOW 96 mm
WEIGHT (kg) FLAP 22° FLAP 45°
13000 1529 1379 13500 1576 1393 14000 1623 1407 14500 1670 1420 15000 1718 1434 15500 1766 1474 16000 1814 1513 16500 1862 1553 17000 1911 1592 17500 1963 1635 18000 2014 1678 18500 2065 1721 19000 2117 1764 19500 2171 1810 20000 2225 1857 20500 2279 1903 21000 2334 1950 21500 2388 1996 22000 2441 2042 22500 2495 2089
CORRECTIONS
ALTITUDE LANDING DISTANCE + 4% per 1000 ft above sea level (Altitude correction limited up to 10000 ft above sea level).
WIND LANDING DISTANCE + 9% per 5 kt tailwind.
OVERSPEED LANDING DISTANCE + 8% per 5 kt above VREF.
TEMPERATURE LANDING DISTANCE + 3% per 5ºC above ISA.
SLOPE LANDING DISTANCE + 8% per 1% slope downhill.
PERFORMANCE DATA AE3007A1P ENGINES
PD-14 REVISION 7
EMB-135BJ UNFACTORED LANDING DISTANCES -
CONTAMINATED RUNWAYS (m)
ALL ENGINES TYPES – EASA CERTIFICATION
COMPACTED SNOW
WEIGHT (kg) FLAP 22° FLAP 45°
13000 1270 1263 13500 1302 1270 14000 1335 1277 14500 1367 1284 15000 1400 1290 15500 1429 1321 16000 1459 1351 16500 1489 1381 17000 1518 1411 17500 1548 1441 18000 1578 1472 18500 1608 1503 19000 1637 1533 19500 1666 1563 20000 1694 1593 20500 1723 1622 21000 1751 1652 21500 1780 1682 22000 1808 1712 22500 1837 1742
CORRECTIONS
ALTITUDE LANDING DISTANCE + 3% per 1000 ft above sea level (Altitude correction limited up to 10000 ft above sea level).
WIND LANDING DISTANCE + 9% per 5 kt tailwind.
OVERSPEED LANDING DISTANCE + 7% per 5 kt above VREF.
TEMPERATURE LANDING DISTANCE + 2% per 5ºC above ISA.
SLOPE LANDING DISTANCE + 4% per 1% slope downhill.
PERFORMANCE DATA AE3007A1P ENGINES
REVISION 7 PD-15
EMB-135BJ UNFACTORED LANDING DISTANCES -
CONTAMINATED RUNWAYS (m)
ALL ENGINES TYPES – EASA CERTIFICATION
ICE
WEIGHT (kg) FLAP 22° FLAP 45°
13000 3119 3061 13500 3119 3055 14000 3118 3050 14500 3118 3044 15000 3118 3039 15500 3136 3069 16000 3155 3100 16500 3174 3130 17000 3192 3161 17500 3235 3204 18000 3277 3248 18500 3320 3291 19000 3362 3334 19500 3405 3380 20000 3447 3426 20500 3490 3472 21000 3533 3519 21500 3575 3565 22000 3618 3611 22500 3660 3657
CORRECTIONS
ALTITUDE LANDING DISTANCE + 3% per 1000 ft above sea level (Altitude correction limited up to 10000 ft above sea level).
WIND LANDING DISTANCE + 6% per 5 kt tailwind.
OVERSPEED LANDING DISTANCE + 7% per 5 kt above VREF.
TEMPERATURE LANDING DISTANCE + 2% per 5ºC above ISA.
SLOPE LANDING DISTANCE + 69% per 1% slope downhill.
EMERGENCY/ABNORMAL PROCEDURES Appendix
APP-2 REVISION 4
QR
H-1
35
/15
69
EMERGENCY EVACUATION
Parking Brake ................................ APPLY
Cabin .............................................. DEPRESSURIZE
Fire Extinguishing Handles .......... PULL
APU Fuel Shutoff Valve ................ PUSH IN
Fuel Pumps Pwr 1 and 2 ............... OFF
Hydraulic Elec Pumps 1 and 2 .... OFF
Engines and APU Fire Extinguishing Bottles (if necessary).............. DISCHARGE
Cabin Crew..................................... NOTIFY
Emerg Lts....................................... ON
Evacuation ..................................... INITIATE
ATC.................................................. NOTIFY Before leaving the airplane: Batteries 1 and 2........................ OFF
END