lep ahm50 rev initialcrewserver1.piac.com.pk/documents/manual/atr42/42-500 ahm50 (issue 02).pdfldm...

ATR42-500

S.NO SHEET # DATE ISSUE #1 LEP 1 22/04/2010 012 A SHEET 1 22/04/2010 013 A SHEET 2 28/03/2007 INITIAL4 B SHEET 1 22/04/2010 015 B SHEET 2 28/03/2007 INITIAL6 B SHEET 3 28/03/2007 INITIAL7 C SHEET 1 28/03/2007 INITIAL8 C SHEET 2 22/04/2010 019 C SHEET 3 28/03/2007 INITIAL10 C SHEET 4 28/03/2007 INITIAL11 C SHEET 4A 28/03/2007 INITIAL12 C SHEET 4B 28/03/2007 INITIAL13 C SHEET 4C 28/03/2007 INITIAL14 C SHEET 4D 28/03/2007 INITIAL15 C SHEET 4E 28/03/2007 INITIAL16 C SHEET 5 28/03/2007 INITIAL17 C SHEET 6 22/04/2010 0118 C SHEET 7 28/03/2007 INITIAL19 C SHEET 8 28/03/2007 INITIAL20 C SHEET 9 28/03/2007 INITIAL21 C SHEET 10 28/03/2007 INITIAL

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ALL (FUEL DENSITY 0.78 Kg / litre)ALL (FUEL DENSITY 0.79 Kg / litre)

ALL (FUEL DENSITY 0.81 Kg / litre)ALL (FUEL DENSITY 0.82 Kg / litre)

ALL (FUEL DENSITY 0.80 Kg / litre)

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LIST OF EFFECTIVE PAGES ISSUE # 02

EFFECTIVITY

ALL (FUEL DENSITY 0.77 Kg / litre)

ALLALLALL

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EDP EXCHANGE FOR SEMI PERMANENT DATAFOR CHECK IN AND LOAD CONTROL

22 C SHEET 11 22/04/2010 0123 C SHEET 12 22/04/2010 0124 C SHEET 13 22/04/2010 0125 C SHEET 14 22/04/2010 0126 C SHEET 15 28/03/2007 INITIAL27 D SHEET 1 28/03/2007 INITIAL28 D SHEET 2 28/03/2007 INITIAL29 D SHEET 3 28/03/2007 INITIAL

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LEP 1 Date: 03/07/2018

EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL

Completed by Operations Engineer MUHAMMAD FARHAN KHAN Issue No: 01

Date: 22/04/2010

OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS

EDP-SYSTEM SEMI-PERMANENT DATA

COMMUNICATION ADDRESSES

A SHEET 1

CARRIER PK

1. HANDLING AGENT’S CONTACT ADDRESS Completed sheets and changes of basic data and procedure must be forwarded to:

MAILING ADDRESS:

TELETYPE ADDRESS:

EMAIL ADDRESS:

REMARKS: 2. CARRIER’S CONTACT ADDRESS

MAILING ADDRESS: OPERATIONS ENGINEERING TECHNICAL DIVISION FLIGHT OPERATIONS DEPARTMENT PIA HEAD OFFICE, JINNAH INTERNATIONAL AIRPORT KARACHI, 75200, PAKISTAN. TELETYPE ADDRESS: KHIOLPK KHIOXPK EMAIL ADDRESS: [email protected] REMARKS:


Completed by Operations Engineer AMIR MUKHTAR Issue No: INITIAL

Date: 28/03/2007



COMMUNICATION ADDRESSES

A SHEET 2

CARRIER PK

3. AUTOMATICALLY PRODUCED DOCUMENTS

(Tick as required) NOTAC SEATPLAN LOADPLAN PASSENGER INFO LIST LOAD SHEET LOADING INSTRUCTION/REPORT

4. MESSAGE REQUIREMENTS

(Tick as required)

LPM Load Planning Message AHM 580 LDM Load Message AHM 583 ALI Abbreviated Load Information Message AHM 584 CPM Container/Pallet Distribution Message AHM 587 UCM ULD Control Message AHM 388(Dispatch Only) MVT Movement Messages AHM 011 and 780 DIV Diversion Message AHM 781 SOM Seat Occupied Message RP 1712 PTM Passenger Transfer Message RP1718 PSM Passenger Service Message RP 1715 (Despatch Only) TPM Teletype Passenger Manifest RP 1717 (Despatch only) PFS Passenger Final Sales Message RP 1719 (Despatch) IDM Industry Discount Message RP 1714 RQL Request List Message RP 1709 (despatch) PNL/ADL Passenger Name List, and Additions and Deletions List (RP 1708) (acceptance Only) SAL Seats Available List RP 1713(Acceptance Only) SLS Statistical Load Summary AHM 588 RQM Request Information Message AHM 783 UWS ULD/Bulk Load Weight signal AHM 581 (Acceptance Only)

5. MESSAGE ADDRESSES

Attach a complete address list for all messages mentioned under paragraph 4 above


Completed by Operations Engineer MUHAMMAD FARHAN KHA

OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGH


GENERAL INFORMATION

B SHEET 1

CARRIER PK

1. PASSENGER AND BAGGAGE WEIGHTS 1.1 Passenger weights

Adult male 75 KG Adult female 75 KG Child 38 KG Infant 15 KG

Remarks: 1.2 Cabin Baggage Weight

YES NO Cabin weight is included in the above mentioned passenger weights. If NO; Actual cabin baggage weight must be used. Remarks:

1.3 Checked Baggage Weight

Weight per piece ACTUAL Weight per passenger ACTUAL

Enter “actual” if standard weight not permitted. Remarks:

b

N Issue No.: 01 Date: 22/04/2010

T OPERATIONS


Completed by Operations Engineer AMIR MUKHTAR

OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERAT


AIRCRAFT DATA B SHEET 2

CARRIER PK

ALL WEIGHTS IN KILOGRAMS (KG)

2. CREW AND CREW BAGGAGE WEIGHTS 2.1 Crew Weights

Cockpit crew 81 Cabin crew 75

YES NO Crew baggage is included in the above crew weights:

If NO: Crew baggage weight must be specified in 2.2 Remarks: 2.2 Crew Baggage Weights

For check purposes add list of valid weights and indices.

COCKPIT CABIN SHORTHAUL 30 20 LONGHAUL 30 20 OTHER’S *

* Specify conditions as appropriate Remarks: For International flights include crew baggage.

b

Issue No: INITIAL Date: 28/03/2007

IONS


Completed by Operations Engineer AMIR MUKHTAR Issue No: INITIAL Date: 28/03/2007 OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS


GENERAL INFORMATION

B SHEET 3

CARRIER PK

3. DRY OPERATING WEIGHT AND DRY OPERATING INDEX SPECIFICATIONS

(Tick as appropriate)

DOW DOI

Item Incl Excl Incl Excl Remarks

Basic Weight (EMPTY WEIGHT) b

b

Crew Weight b b

Crew Baggage b b

Pantry b b

Containers

Pallets

CONFIG Weight b b

FLIGHT PACK b b

REMARKS:-



Date: 28/03/2007



AIRCRAFT DATA C SHEET 1

A/C TYPE ATR42-500

CARRIER PK

1. BALANCE AND SPECIAL INFORMATION - OUTPUT ON LOADSHEET

1.1 Balance output

Please mark your requirements in respective box. Remarks Basic index BI

b

Dry operating index DOI b

Dead load index DLI Dead load MAC MACDLW Loaded Index at zero fuel weight LIZFW

b

Loaded index at take-off weight LITOW b

Loaded Index at landing weight LILAW MAC – at zero fuel weight MACZFW b MAC - at takeoff weight MACTOW

b

MAC at landing weight MACLAW Stabilizer trim setting at take-off STABTO *

* specify ANU or AND as appropriate. THE FOLLOWING EQUATION IS USED Y = -0.315789 X + 9.2368 Y = STAB TRIM X = C.G IN % MAC

1.2 Passenger trim output

Please mark your requirements in respective box. Remarks Class Trim Cabin Area Trim

b

Seat Row Trim



Date: 22/04/2010




A/C TYPE ATR42-500

CARRIER PK

ALL WEIGHTS IN KILOGRAMS (KG)

1.3 Seating Conditions

State below how the seating conditions are to be shown on the load sheet in the respective box (give example).

1.4 Special Information Specify the information to be entered in the lower parts of the EDP Load sheet.

1.4.1 Captain’s information/notes, Centre of Gravity limits, ramp weight, etc. (give examples). 1.4.2 Load message before LMC, if required, to be shown.

2. AIRCRAFT REGISTRATIONS, WEIGHT AND INDEX DETAILS

DRY OPERATING WEIGHT BASIC WEIGHT √ (tick as appropriate) For check purpose add list of valid weights and indices.

Standard Fleet Weight: 10824 Standard Fleet Index: 75.0

Registration

Weight Adjustment

Index Adjustment

Registration

Weight Adjustment

Index Adjustment

AP-BHH

00

00

AP-BHN

-34

+0.1

AP-BHI

-20

+1.1

AP-BHO

-22

+1.2

AP-BHJ

-61

+0.4

AP-BHP

-31

-0.1

AP-BHM

-26

-0.8

NOTE: Notification for data changes at short notice may also be made by means of data exchange message (AHM 052). PK does not take Fleet Average Basic Weight; Weight must be taken Tail Wise.


Completed by Operations Engineer ALI RAZA Issue No: 02

Date: 03/07/2018




A/C TYPE

ATR42-500 CARRIER

PK

3. BASIC INDEX AND MAC FORMULA 3.1 Examples and definitions

Index = W * (Sta - Ref. Sta) + K C

C*(I – K) + Ref.Sta - LEMAC W %MAC = MAC 100 W = Weight Actual Sta. = Station, horizontal distance in inches or metres from station zero to the location Ref. Sta. = Reference station/axis. Selected station around which all index values are calculated K = Constant used as a plus value to avoid negative index figures. C = Constant used as a denominator to convert moment values into index values. I = Index value corresponding to respective weight. MAC = Length of Mean Aerodynamic Chord in inches or meters. LEMAC = Horizontal distance in inches or meters from the station zero to location of the Leading Edge of MAC.

3.2 Index formula Ref. Sta at = 11.996 Meters from zero K (constant) = 50 C (constant) = 100

3.3 MAC Information

Length of MAC = 2.285 Meters LEMAC at = 11.425 Meters from zero

3.4 Stabilizer trim setting

MAC Range Min 15% Max 34% STAB Range Min + 4.5 Max - 1.5 Stabilizer change item per 1% MAC ------------------------------ Y = - 0.315789 X + 9.2368 (attach a table or diagram if item changing at different weights) Y = STAB TRIM , X = C. G in % MAC

EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTRO


Date: 28/03/2007




A/C TYPE ATR42-500

CARRIER PK

4. EFFECT OF FUEL/INJECTION WATER

Fuel loading Fuel Usage Standard Procedure Non-standard Procedure FUEL DENSITY: 0.77 kg/litre

Index value

Index value Fuel Weight

+/-

100

10

1

Fuel Weight

+/-

100

10

1

1 5 4 0 0 4 6 2 + 0 1 7 7 0 + 0 2

1 2 3 2 + 0 3 1 5 4 0 + 0 4 2 0 0 2 + 0 5 2 3 1 0 + 0 6

2 6 1 8 + 0 7 3 0 8 0 + 0 8 3 3 8 8 + 0 9 3 8 5 0 + 1 0

4 4 1 4 + 1 1

Note 1: Use additional sheets for other fuel densities or state correction factors. Note 2: Specify maximum capacities.



Date: 28/03/2007



AIRCRAFT DATA C SHEET 4A

A/C TYPE ATR42-500

CARRIER PK



Index value


+/-

100

10

1

Fuel Weight

+/-

100

10

1

1 5 6 0 0 4 6 8 + 0 1 7 8 0 + 0 2

1 2 4 8 + 0 3 1 5 6 0 + 0 4 1 8 7 2 + 0 5 2 3 4 0 + 0 6

2 6 5 2 + 0 7 3 1 2 0 + 0 8 3 4 3 2 + 0 9 3 9 0 0 + 1 0

4 4 7 1 + 1 1




Date: 28/03/2007



AIRCRAFT DATA C SHEET 4B

A/C TYPE ATR42-500

CARRIER PK



Index value


+/-

100

10

1

Fuel Weight

+/-

100

10

1

1 5 8 0 0 4 7 4 + 0 1 7 9 0 + 0 2

1 1 0 6 + 0 3 1 5 8 0 + 0 4 1 8 9 6 + 0 5 2 3 7 0 + 0 6

2 6 8 6 + 0 7 3 0 0 2 + 0 8 3 4 7 6 + 0 9 3 7 9 2 + 1 0

4 5 2 8 + 1 1




Date: 28/03/2007



AIRCRAFT DATA C SHEET 4C

A/C TYPE ATR42-500

CARRIER PK



Index value


+/-

100

10

1

Fuel Weight

+/-

100

10

1

1 6 0 0 0 4 8 0 + 0 1 8 0 0 + 0 2

1 1 2 0 + 0 3 1 6 0 0 + 0 4 1 9 2 0 + 0 5 2 2 4 0 + 0 6

2 7 2 0 + 0 7 3 0 4 0 + 0 8 3 3 6 0 + 0 9 3 8 4 0 + 1 0

4 4 8 0 + 1 1 4 5 8 6 + 1 2




Date: 28/03/2007



AIRCRAFT DATA C SHEET 4D

A/C TYPE ATR42-500

CARRIER PK



Index value


+/-

100

10

1

Fuel Weight

+/-

100

10

1

1 6 2 0 0 4 8 6 + 0 1 8 1 0 + 0 2

1 1 3 4 + 0 3 1 6 2 0 + 0 4 1 9 4 4 + 0 5 2 2 6 8 + 0 6

2 5 9 2 + 0 7 3 0 7 8 + 0 8 3 4 0 2 + 0 9 3 8 8 8 + 1 0

4 3 7 4 + 1 1 4 6 4 3 + 1 2




Date: 28/03/2007



AIRCRAFT DATA C SHEET 4E

A/C TYPE ATR42-500

CARRIER PK



Index value


+/-

100

10

1

Fuel Weight

+/-

100

10

1

1 6 4 0 0 3 2 8 + 0 1 8 2 0 + 0 2

1 1 4 8 + 0 3 1 6 4 0 + 0 4 1 9 6 8 + 0 5 2 2 9 6 + 0 6

2 6 2 4 + 0 7 2 9 5 2 + 0 8 3 4 4 4 + 0 9 3 7 7 2 + 1 0

4 4 2 8 + 1 1 4 7 0 0 + 1 2




28/03/2007


Date:



A/C TYPE ATR42-500

CARRIER PK

5. COCKPIT 5.1 Number of seats and average station

Length of arm from reference station Index influence Maximum number of

cockpit seats ± Inch / metre ± per 1 kg

CAPT

-

7.456 -

0 . 0 7 4 5 6

F/O

-

7.456 -

0 . 0 7 4 5 6

OBSERVER

-

6.496 - 0 . 0 6 4 9 6

Remarks:



Date: 22/04/2010




A/C TYPE ATR42-500

CARRIER PK

6. LIMITATIONS 6.1 Aircraft Weight Limitations Maximum weight for:

Aircraft Reg.

Or Subtype Nr. Ramp/Taxi Design take-off wet*

Design take-off dry Zero fuel Design landing

AP-BHH

AP-BHI

AP-BHJ

AP-BHM

AP-BHN

AP-BHO

AP-BHP

18770

18770

18770

18770

18770

18770

18770

N O T

A P P L I C A B L E

18600

18600

18600

18600

18600

18600

18600

16700

16700

16700

16700

16700

16700

16700

18300

18300

18300

18300

18300

18300

18300

*Valid for take-off with water- injection



Date: 03/07/2018




A/C TYPE

ATR42-500 CARRIER

PK

6.2. CG – Limits for Loadsheet

Purposes

Enter the forward and the aft balance limits in the boxes commencing at the lowest weight and terminating at the highest weight to be checked. IMPORTANT – If limits are affected and / or determined by passenger / fuel / version / or other conditions specify each set of limits on a separate sheet entering the special condition(s) in the box.

FORWARD AFT

Special condition if applicable

Special condition if applicable

Specify Applicability *

Weight

Index value Specify

Applicability * Weight

Index value

± 10

0

10

1 0.1

0.01

± 10

0

10

1 0.1

0.01

ZFW 1 1 0 0 0 + 2 9 8 7 ZFW 1 1 0 0 0 + 5 7 8 1 1 1 5 0 0 + 3 1 8 3 1 6 7 0 0 + 7 5 5 4 1 5 8 0 0 + 1 8 8 7 1 6 7 0 0 + 2 5 2 8

TOGW 1 1 0 0 0 + 2 9 8 7 TOGW 1 1 0 0 0 + 5 7 8 1 1 1 5 0 0 + 3 1 8 3 1 8 6 0 0 + 7 6 7 8 1 5 8 0 0 + 1 8 8 7

1 8 6 0 0 + 4 0 7 0

*Zero Fuel, Taxi, Take-off, In-flight, Landing NOTE: Attach a balance chart for check purposes. Remarks :


Com

OPE



Cabin-Configuration (s) 10YP/38Y

A/C TYPE ATR42-500 .

CARRIER PK

7. PASSENGER SEATS

Class codes :

(e.g. F, Y, C, M etc.) Class 1 YP Class 4

Class 2 Y Class 5

Class 3

NOTE: Fill in one table for each cabin configuration code. Number of seats Name of cabin

section Class 1

Class 2

Class 3

Class 4

Class 5

Total per cabin section

ZONE A 10 -

ZONE B - 24

ZONE C - 14

10 38

Sub total Total per Class

pleted by Operations Engineer AMIR MUKHTAR Issue No: INITIAL

Date: 28/03/2007

RATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS

Remarks



Date: 28/03/2007




Cabin-Configuration(s) 10YP/38Y

A/C TYPE ATR42-500

CARRIER PK

8. Average Station 8.1 Class / Cabin Sections

Length of arm from reference station Index influence Class / Cabin section

± Inch / metre ± per 1 kg ZONE A - 3.669 - . 0 3 6 6 9ZONE B + 0.051 + . 0 0 0 5 1ZONE C + 3.861 + . 0 3 8 6 1

8.2 Seating Layout

Show the passenger seating layout for the configurations given in the box at the top by inserting the seat row numbers and letters in the following table. For special seats use the facility codes listed below. B = Bassinet position P = Stretcher location C = Crew seat Q = Quiet zone E = Emergency exit S = Smoking G = Groups T = Near toilet H = Incapacitated passenger U = Unaccompanied minor I = Infant preference rows / seats V = Seat left vacant / offered last J = Rear facing seats W = No movie K = Near galley X = No facility seat, e.g. no distinction L = Leg space seat between smoking and non – smoking M = Wheel chair Y = Not fitted N = No smoking Z = Buffer zone O = Over wing seat A = Aisle Alpha / Characters --- D, F, R, Blank, not used.



Date: 28/03/2007




CABIN CONFIGURATION(S) 10YP/38Y

A/C TYPE ATR42-500

CARRIER PK

8.2.1 Seat plan Layout / Facilities and Row Index Influence.

ROW LETTER

SEC

TIO

N

RO

W N

O

A C J L

Index influence per seat row ± per 1 kg

1 X X - . 0 3 6 6 92 X X X X - . 0 3 6 6 93 X X X X - . 0 3 6 6 9

21 X X X X + . 0 0 0 5 122 X X X X + . 0 0 0 5 123 X X X X + . 0 0 0 5 124 X X X X + . 0 0 0 5 125 X X X X + . 0 0 0 5 126 X X X X + . 0 0 0 5 127 X X X X + . 0 3 8 6 128 X X X X + . 0 3 8 6 129 X X X X + . 0 3 8 6 130 X X + . 0 3 8 6 1

A A A B B B B B B C C C C


Completed by Operations Engineer MUHAMMAD FARHAN KHAN Issue No: 01 Date: 22/04/2010




Cabin-configuration(s) 10YP/38Y

A/C TYPE ATR42-500

CARRIER PK

8.3 Cabin Crew Seats

Crew seats location Max. No. of seats

Length of arm from reference station Index influence

± Inch / metre ± per 1 kg FWD 1 - 4.251 - . 0 4 2 5 1AFT 1 + 5.849 + . 0 5 8 4 9

Remarks: 8.4 Galley

Galley location Length of arm from

reference station

Index influence

± Inch / metre ± per 1 kg REAR CABIN RIGHT + 4.978 + . 0 4 9 7 8

Remarks:



Date: 22/04/2010





A/C TYPE ATR42-500

CARRIER PK

8.5 Pantry Weight / Pantry Code (normally used for above mentioned cabin configurations). NOTE: The columns “Pantry Weight” and “Location” must be filled in only if Basic Weight is specified under paragraph 2.

Pantry Code Pantry Weight Location *

International

Domestic

Test & Training

190 KG

160 KG

45 KG

* Use the locations as under paragraph 8.4. REMARKS:

8.6 Crew Distribution / Crew Code (normally used for above mentioned cabin configurations). NOTE: The column “Location” is to be filled in only if Basic Weight is specified under paragraph 2.

Crew Code Cockpit Crew Cabin Crew Location * Location of Crew

Baggage

REFER ENCLOSED PAGE FOR CREW

IN RH FWD HOLD

* Use the location as under paragraph 8.3.

Total



Date: 03/07/2018





A/C TYPE

ATR42-500 CARRIER

PK

9. DETAILS FOR COMPARTMENT TRIM

Compartment Number

Description

Maximum Capacity

Index value ± per 1 kg

Gross Weight (kg)

Volume * (m3)

RH FWD COMPT

BULK 288

1.8 - . 0 5 7 5 7

LH FWD COMPT

BULK 448

2.8 - . 0 5 2 9 9

FWD PART AFT COMPT

BULK 304

1.9 + . 0 6 7 5

4

AFT PART AFT COMPT

BULK 440 2.75 + . 0 7 8 1 8

* Volume information required for bulk compartments only.

Remarks: 9.1 Combined Load Limitations. Attach relevant company regulations.



Date: 03/07/2018


10. DETAILS FOR BAY / SECTION TRIM

* Volume information required for bulk compartments only. NOTE 1: Attach a plan for each compartment configuration. NOTE 2: Use additional sheets as required.

10.1 Unsymmetrical Load Limitations.

Attach relevant company regulations.




A/C TYPE

ATR42-500 CARRIER

PK

Bay / Section Description

Maximum Capacity

Index value ± per 1 kg

Gross Weight (kg)

Volume * (m3)

RH FWD COMPT

BULK 288

1.8 - . 0 5 7 5 7

LH FWD COMPT

BULK 448

2.8 - . 0 5 2 9 9

FWD PART AFT COMPT

BULK 304

1.9 + . 0 6 7 5

4

AFT PART AFT COMPT

BULK 440 2.75 + . 0 7 8 1 8



Date: 28/03/2007




A/C TYPE ATR42-500

CARRIER PK

11. BALLAST

FIXED PROVISIONS FOR CARRYING BALLAST.

Specify or attach a table.

Remarks:



Date: 28/03/2007



LOADPLANNING-DATA D SHEET 1

A/C TYPE ATR42-500

CARRIER PK



Date: 28/03/2007




A/C TYPE ATR42-500

CARRIER PK

2. UNIT LOAD DEVICES DETAILS

MAXIMUM CAPACITY TYPE CODE TARE WEIGHT GROSS WEIGHT VOLUME * REMARKS

------------- NOT -------------------- APPLICABLE --------------------

* Containers / lgloos only Note: For pallets, specify Lower Deck or Main Deck.



Date: 28/03/2007




A/C TYPE ATR42-500

CARRIER PK

3. SPECIAL LOAD

Attach relevant company regulations for special load (AVI, Dangerous Goods, etc.). PLEASE REFER TO PIA WEIGHT AND BALANCE MANUAL AND CARGO HANDLING MANUAL.

lep ahm50 rev initialcrewserver1.piac.com.pk/documents/manual/atr42/42-500 ahm50 (issue 02).pdfldm...

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