msn 7707 reports - 11-25-09

Status Date: 8-Apr-23

A/C REG N486CA

MODEL CL600-2B19

S/N 7707

T.A.T 15,685.59

T.A.C. 12,231

ENGINES - CF34-3B1

POSITION SERIAL NO. TSN CSN

#1 873331 17,373.41 14,795

#2 873333 17,373.41 14,795

APU SERIAL NO. TSN CSN

3800488-3 P-1150 13839.27 1845

LANDING GEARS P/N S/N TSN CSN

NOSE LANDING GEAR 16040-117 DCL750/02 15,685.59 12,231

LH MAIN LANDING GEAR 17002-113 DCL738/02 15,685.59 12,231

RH MAIN LANDING GEAR 17002-114 DCL730/02 15,685.59 12,231

Times and Cycles StatusTimes and Cycles Status

of 158

MSN: 7707 A/C TSN: 15685.59MFG Date: 20-Nov-02 A/C CSN: 12231


Description PROG Task Card TASK MRM DATE C/W HR C/W CY CW INTERVAL DATE DUE HR DUE CY DUE NOTE REM HRS

1 Service Check MRB 000-05-900-991 See MRB 3 DAYS 2-Jan-00

2 Routine Check MRB 000-05-900-992 See MRB 100HR 100.00 -15,585.6

3 500 FH Check MRB See MRB See MRB 15-Jun-09 15679 500HR 16179.0 493.4

4 1,000 FH Check MRB See MRB See MRB 15-Jun-09 15679 1000HR 16679.0 993.4

5 1500 FH Check MRB See MRB See MRB 15-Jun-09 15679 1500HR 17179.0 1,493.4



8 4000 FH Check MRB See MRB See MRB 12-Nov-08 14578 4000HR 18578.0 2,892.4



11 10,000 FH Check MRB See MRB See MRB 16-Dec-06 10,698 10000HR 20698.0 5,012.4

12 15,000 FH Check MRB See MRB See MRB 16-Dec-06 10698 15000HR 25698.0 10,012.4

13 20,000 FH Check MRB See MRB See MRB 20000HR 20000.0 4,314.4




16 12 MONTH INSPECTION MRB See MRB See MRB 3-Jun-09 15,679 12MO 3-Jun-10

17 24 MONTH INSPECTION MRB See MRB See MRB 12-Nov-08 14,578 24MO 12-Nov-10

18 36 MONTH INSPECTION MRB See MRB See MRB 36MO 30-Dec-02

19 60 MONTH INSPECTION MRB See MRB See MRB 60MO 29-Dec-04

20 24/24 MONTH MRB See MRB See MRB 12-Nov-08 14,578 24MO 12-Nov-10

21 48/24 MONTH MRB See MRB See MRB 24MO 30-Dec-01

22 48/48 MONTH MRB See MRB See MRB 18-Dec-06 48MO 17-Dec-10



25 96/48 MONTH MRB See MRB See MRB 96MO/48MO 29-Dec-07

26 96/72 MONTH MRB See MRB See MRB 96MO/72MO 29-Dec-07

27 SUP 000-79-310-702 R72-21-802-01 30FH/3Days 30.0 Pre−GE SB 72−0109

28 SYS 000-21-310-705 21-51-13-01 400 FH 400.0 NOTE 14 -15,285.6

29 SYS 000-21-310-004 21-51-16-03 600 FH -15,085.6

30 SUP 000-52-830-701 R52-11-878-01 600 FH 600.0 -15,085.6

31 Discard of the Air−Cycle−Machine Oil SYS 000-21-310-706 21-51-13-05 1200 FH 1200.0 NOTE 14 -14,485.6

32 Detailed Inspection of the APU Exhaust SYS 000-49-310-711 49-81-00-01 3000 FH 3000.0 -12,685.6

33 SYS 000-27-220-705 27-40-01-19 5500 FH -10,185.6

34 SYS 000-27-220-706 27-40-01-19 5500 FH -10,185.6

35 SYS 000-12-320-701 27-40-01-14 5500 FH 5500.0 -10,185.6

Visual Check of the Engine Master Chip Detector Indicator

Detailed Inspection of the Air Cycle Machine (ACM) Oil Level

Operational Check of the Water Separtor Overboard- Drain- Line

Detailed Inspection of the Phase IV Passenger−Door Upper Latch−Fitting Sleeve Bushings

Post−Modsum TC601R13193 Pre−Modsum TC601R15596 or Post−Modsum TC601R13193 Pre−SB 601R−52−110

Discard of the Left Horizontal-Stabilizer Pitch-Trim Disconnect Switch

Discard of the RightHorizontal-Stabilizer Pitch-Trim Disconnect Switch

Lubrication of the Horizontal Stabilizer Trim Actuator Screw Jack

Maintenance StatusMaintenance Status

of 158





36 SUP 000-12-160-700 R27-11-A082-02 5500 FH 5500.0 -10,185.6

37 SUP 000-12-590-702 R27-11-A082-01 5500 FH 5500.0 -10,185.6

38 SUP 000-12-690-702 R27-11-A082-01 5500 FH 5500.0 -10,185.6

39 SYS 000-21-170-702 21-51-21-11 6000 FH

40 SYS 000-21-170-703 21-51-21-11 6000 FH

41 SYS 000-30-900-701 30-12-00-03 6000 FH

42 Lubrication of the Aileron Servo Clutch SUP 000-12-160-701 6500 FH 6500.0 -9,185.6

43 Lubrication of the Elevator Servo Clutch SYS 000-12-320-700 22-11-00-09 6500 FH 6500.0 -9,185.6

44 Discard of the Left−Wing Outboard Aileron Pulleys SUP 000-27-590-722 R27-00-A053-01 10500 FH 10500.0 -5,185.6

45 Discard of the Right−Wing Outboard Aileron Pulleys SUP 000-27-690-722 R27-00-A053-01 10500 FH 10500.0 -5,185.6

46 Zone 000-53-210-330 53-200-02 12000 FH 12000.0 -3,685.6

47 Zone 000-53-210-331 53-200-03 12000 FH 12000.0 -3,685.6

48 Restoration of the Precoolers by Cleaning SYS 000-21-310-704 21-51-04-01 16000 FH 16000.0 314.4

49 SYS 000-26-900-703 26-22-00-01 16000 FH 16000.0 314.4

50 SYS 000-26-900-704 26-14-01-01 16000 FH 16000.0 314.4

51 General Visual Inspection of the External Tail Cone Zone 000-53-360-340 53-300-05 16000 FH 16000.0 314.4

52 Zone 000-57-540-340 57-500-12 16000 FH 16000.0 314.4

53 Zone 000-57-640-340 57-600-12 16000 FH 16000.0 314.4

54 Zone 000-57-900-340 16000 FH 16000.0 314.4

55 Zone 000-57-900-342 16000 FH 16000.0 314.4

56 Detailed Inspection of the Cargo Door−Stop Fittings STR 000-53-280-500 53-61-21-01 18 MONTHS 23-Jun-01

57 SYS 000-24-900-750 24-23-11-05

58 Inspection of the APU Fuel and Oil System SYS 000-49-310-701 300 APU HR 300.0 -15,385.6

59 Discard of the APU Fuel−Filter Element SYS 000-49-310-703 49-31-05-03 750 APU HR 750.0 -14,935.6

60 Discard of the APU Oil−Filter Element SYS 000-49-310-704 49-91-10-03 750 APU HR 750.0 -14,935.6

Lubrication of the Aileron Rear Quadrant and Trim Lever Bearings

Lubrication of the Left−Wing Aileron Control Cables at the Wing Pulley Interfaces

Lubrication of the Right−Wing Aileron Control Cables at the Wing Pulley Interfaces

Detailed Inspection of the Pressure Bulkhead Check Valve (Flight Compartment Distribution System)

Detailed Inspection of the Pressure Bulkhead Check Valve (Passenger Compartment Distribution System)

Functional Check of the Outboard Sufficient Heat Switches

22-11-00-09R22-11-A083-01

General Visual Inspection of the Internal Left Forward Equipment Compartment

General Visual Inspection of the Internal Right Forward Equipment Compartment

Functional Test of the APU Fire−Extinguishing System

Functional Test of the Main Landing Gear (MLG) Wheel−Well Detector−Loops

General Visual Inspection of the Internal Left Wing Rear Spar to Auxiliary Spar

General Visual Inspection of the Internal Right Wing Rear Spar to Auxiliary Spar

General Visual Inspection of the Internal Left Wing Leading Edge

57-500-0457-500-06

General Visual Inspection of the Internal Right Wing Leading Edge

57-600-0457-600-06

Discard of the Air Driven Genator (ADG) Uplock- Mechanism Cartridge

60 MONTHS/42 MONTHS

49-24-00-0349-24-00-0549-31-00-0149-31-05-0149-91-10-01

of 158





61 SYS 000-49-310-702 49-42-10-01 1200 APU HR 1200.0 -14,485.6

62 Detailed Inspection of the APU Gearbox Vent Line SYS 000-49-310-731 49-24-00-11 1500 APU HR 1500.0 -14,185.6

63 SYS 000-28-160-700 28-24-00-05 1800 APU HR 1800.0

64 Detailed Inspection of the APU Starter brush SYS 000-49-310-709 49-44-00-01 3000 APU HR 3000.0 -12,685.6

65 SYS 000-49-310-707 49-60-00-01 3500 APU HR 3500.0 -12,185.6

66 Restoration of the APU Oil Cooler SYS 000-49-310-710 49-91-07-01 3500 APU HR 3500.0 -12,185.6

67 SYS 000-72-430-700 72-52-00-01 3000 EH -12,685.6

68 SYS 000-72-430-708 3000 EH -12,685.6

69 SYS 000-72-440-700 72-52-00-01 3000 EH -12,685.6

70 SYS 000-72-440-708 3000 EH -12,685.6

71 SUP 000-32-220-701 R32-31-828-02 300 FC 300

72 SUP 000-32-220-700 R32-31-828-01 1000 FC 1000

73 SUP 000-32-220-702 R32-31-828-03 4000 FC 4000

74 SYS 000-33-900-722 33-50-00-05

Yellow lines are N/A to this aircraft

Detailed Inspection of the APU Igniter Plugs and Leads

Pre−Honeywell SB GTCP36−49−7749

Restoration of the Auxiliary Power Unit (APU) Fuel Pump Brushes

Task not required if brushless pump Installed

General Visual Inspection of the APU Wiring Harness and Connectors

Borescope Inspection of the Left Engine HPT Stages 1 and 2 Rotor Blades

Borescope Inspection of the Left Engine Combustion Liner, Stage 1 Turbine Nozzle and Fuel Injectors

72-42-00-0172-42-00-0373-11-11-01

Borescope Inspection of the Right Engine HPT Stages 1 and 2 Rotor Blades

Borescope Inspection of the Right Engine Combustion Liner, Stage 1 Turbine Nozzle and Fuel Injectors

72-42-00-0172-42-00-0373-11-11-01

Restoration of the Landing Gear Control−Handle Assembly

Detailed Inspection of the Landing Gear Control−Handle Slider

Restoration of the Landing Gear Control−Handle Assembly

General Visual Inspection of the Emergency Floor Path Lighting Assemblies

Task interval based on

manufacturer’s recommendation

of 158

REM CYC

MSN: 7707

MFG Date: 20-Nov-02


MSN 7707 FAA/TCCA Airframe Airworthiness Directive Listing

US FAA Canadian AD

74-08-09R2 N/A

93-21-04 CF-93-26R3

93-21-04 CF-93-26R3

93-22-04 CF-93-23

94-01-09 CF-93-32R1

CF-93-29

CF-93-27R1

94-24-02 N/A

94-01-14

94-22-06

Airframe AD StatusAirframe AD Status

95-04-05 CF-93-02R1

95-10-06 CF-94-14

CF-94-23

95-26-07 N/A

CF-95-10

97-14-11 CF-97-11R2

CF-96-18

CF-95-14R1

98-04-45

98-04-45 CF-94-21R1

N/A

CF-96-12R1

95-18-07

96-19-15

97-18-10

97-19-11

CF-94-21R1

98-13-24

98-16-25

98-20-01 CF-98-14R4

CF-98-35

99-09-52 CF-99-09R1

CF-99-01

CF-98-40

2000-01-12 CF-97-11R2

2000-02-34 N/A

2000-14-17 CF-96-16R1

CF-2000-28

2001-03-04 CF-2000-15R1

98-26-14

99-19-39

99-21-11

2000-20-03 R1

2001-03-08 CF-2000-10

2001-06-07 CF-2001-02

2001-12-24 CF-2000-15R1

2001-22-09 CF-99-32R3

2001-26-51 CF-2001-47

2002-03-14 CF-2001-15R1

2002-09-05 CF-2000-31

2002-16-02 CF-2002-20

2002-16-14 CF-2001-27

2002-19-07 CF-2002-35R2

2003-01-02 CF-2001-21

2003-04-21 R1 CF-2002-12

2003-09-04 R1 CF-2002-39

2003-11-11 CF-99-32 R2

2003-11-20 CF-93-26R3

2003-11-20 CF-93-26R3

2003-14-02 CF-2001-35R1

2003-14-17 CF-2000-35R1

2003-16-13 CF-2001-31

2003-19-04 CF-2000-17R1

2003-20-03 CF-2003-08

2004-01-01 CF-2001-45

2004-02-07 CF-2003-26

2004-05-12 CF-2004-01R1

2004-07-18 CF-2003-03

2004-10-03 CF-2001-26R1

2004-10-03 CF-2001-26R1

2004-14-16 CF-2003-09R1

2004-20-09 CF-2004-18R1

2004-22-08 CF-2003-05R1

2004-22-08 CF-2003-05R1

2004-22-23 CF-2002-41

2005-03-13 CF-2004-13

2005-04-07 CF-2005-01

2005-04-07 CF-2005-01

2005-06-04 CF-2004-01R1

2005-06-04 CF-2004-01R1

2005-07-15 CF-2002-21

2005-10-10 CF-2005-04

2005-17-03 CF-2004-20

2005-17-12 CF-2005-26R1

2005-18-04 CF-2003-14R1

2005-18-06 CF-2002-35R2

2005-18-06 CF-2002-35R2

2005-18-06 CF-2002-35R2

2005-18-06 CF-2002-35R2

2005-23-01 CF-2005-13R1

2005-23-01 CF-2005-13R1

2006-02-05 CF-2004-23R1

2006-02-05 CF-2004-23R1

2006-02-10 CF-2005-18

2006-05-11 R1 CF-2005-41

2006-09-08 CF-2006-07

2006-10-01 CF-2000-35R1

2006-10-06 CF-2005-35

2006-11-09

2006-12-21 CF-98-14R4

2006-12-21 CF-98-14R4

2006-17-14 CF-2006-17R1

2006-22-06 CF-2006-20R1

CF-2005-05

2007-01-07 CF-2004-18R1

2007-03-11 CF-2006-11

2007-03-19 CF-2003-09R1

2007-04-24 CF-2006-19

2007-05-11 CF-2006-20R1

2007-15-02 CF-2006-04

2007-15-02 CF-2006-04

2007-15-02 CF-2006-04

2007-17-07 CF-2007-10

2008-01-04 CF-2007-10R1

2008-02-07 CF-2007-18

2008-02-07 CF-2007-18

2008-03-19 CF-2007-17

2008-03-19 CF-2007-17

2008-04-08 CF-2007-23

2008-04-08 CF-2007-23

2008-05-13 CF-2006-17R1

2008-06-02 CF-2007-29

2008-06-10 CF-2003-12

2008-08-06 CF-2008-15

2008-08-09 CF-2005-41

2008-09-12 CF-2007-35

2008-12-10 CF-2007-36

2008-12-10 CF-2007-36

2008-21-09 CF-2008-15R1

2008-22-01 N/A

2008-22-03 CF-2007-29

2008-22-03 CF-2007-29

2008-22-03 CF-2007-29

2008-22-03 CF-2007-29

2008-22-03 CF-2007-29

2008-22-03 CF-2007-29

2008-22-03 CF-2007-29

2008-23-11 CF-99-32R3

2008-23-16 CF-2008-30

2008-23-16 CF-2008-30

2008-24-14 CF-2008-21

2008-26-09 CF-2008-20

2008-26-09 CF-2008-20

2009-04-11 CF-2008-35

2009-04-11 CF-2008-35

2009-04-11 CF-2008-35

2009-04-11 CF-2008-35

2009-06-04 CF-2007-34

2009-06-04 CF-2007-34

2009-06-12 CF-2007-10R1

2009-06-12 CF-2007-10R1

2009-06-12 CF-2007-10R1

2009-06-12 CF-2007-10R1

2009-06-12 CF-2007-10R1

2009-06-12 CF-2007-10R1

2009-06-12 CF-2007-10R1

2009-06-12 CF-2007-10R1

2009-06-17 CF-2008-09

2009-06-17 CF-2008-09

2009-10-05 CF-2009-13

N/A CF-95-08R2

N/A CF-97-05

N/A CF-2003-26

N/A CF-2008-33R1

N/A CF-2009-02

NameTitleDateSignature

A/C TSN:

A/C CSN:


FAA Requirements

< Lavatory Trash Receptacles Inspection > Every 1000 FH, inspect all lavatory paper and linen waste receptacle enclosure access doors and disposal doors for proper operation, fit, sealing, and latching for the containment of possible trash fires

< Brake Control Valve > Lubrication of Brake Control Valve to Prevent Freezing of Input Plunger of the Dual Brake Control Valve

<Rudder Control Quadrant> - To Prevent Failure of a Rudder Control Quadrant (Part Number 600-92614-1) due to Stress Corrosion. Superseded by AD 95-18-07.

< Elevator Flutter Damper Fittings and Shear Pins > To Reduce Undampened Vibration of Elevators in the Event of Hydraulic System Failure (Superseded by AD 94-24-02)

< Integrated Drive Generator (IDG) > To Prevent Integrated Drive Generator (IDG) Failure.

< Stall Protection System (SPS) > Interim Corrective Action to Disconnect the Right Channel AHRS / Restore System to Type Approval Configuration

< Elevator Flutter Damper Fittings and Shear Pins > To Reduce Undampened Vibration of Elevators in the Event of Hydraulic System Failure (Superseded by CF-94-21R1 and FAA AD 94-24-02)

Airframe AD StatusAirframe AD Status

< Passenger Door Freezing > - Lubrication To Prevent Freezing of Passenger Door Mechanism.g(1) - SB A601R-52-009 Rev. Bg(2) - SB A601R-52-021 Rev. A

< ADG Uplock Assembly (Sundstrand) > - To Detect and Correct Problems with the Manual Deployment System (Uplock Assembly, Part Number 721863B)

< Rudder Control Quadrant (Part Number 600-92614-1 > Replacement of the Quadrant to Prevent Possibility of Stress Corrosion of the Quadrant Spigot.

<Aileron hinge fittings> Aileron travel range check and shear pin inspections

< NLG Spring Bungee > Reduced Stroke Due To Possible Incorrect Assembly During Manufacture that Could Result in Improper NLG Door Operation Which Could Prevent Extension Of The NLG.

< Inspection of Underfloor Pressure Bulkhead at Fuselage Frame FS409+128 > Perform a detailed inspection of the bulkhead web P/N 601R32208-123 at FS 409+128.

< DC Power Distribution System > Repair of Loose Fuse Holders. Perform one-time inspection / repair of the DC power distribution system IAW ASB A601R-24-056 Rev A.

< Aileron Flutter Dampers > Installation of Newly Designed Aileron Flutter Dampers And Improved Shear Pins

< Elevator Flutter Dampers > Restore Elevator System to Its' Type Approval Configuration

< Mach Trim System > HSTCU Circuits Deactivation to Prevent Unsafe Nose-Up Trim Runaway

< Main Landing Gear Shock Strut Upper and Lower Attachment Pins > To Prevent Main Landing Gear Failure. Within 6 months of Sep 11, 1998, install new MLG shock strut upper and lower attach pins IAW SB 601R-32-065

< Flap System > Install Flap Skew Detection Modification to Prevent Flap System Failure. Embodiment of SB 601R 27-116 & 601R 27-115 Due 31-Dec-2006.

< Centre Fuel Tank > To Reduce The Potential For a Centre Fuel Tank Fire or Explosion Inspect the Electrical Conduits in the Centre Fuel Tank inspect electrical conduits in the centre fuel tank IAW ASB A601R-28-036 Rev A, Section 2, Part A.

< Chaffing Between IDG Cables and Fuel Lines at 10th Stage Bleed Check Valve > Inspect / repair / replace IDG cables IAW ASB A601R-24-095 Rev A. 2) For S/N's 7003 thru 7067 and 7069 thru 7303, inspect / correct clearance between 10th stage bleed air valve and fuel manifold pigtails IAW ASB A601R-73-008 Rev A

< Emergency Overwing Exits > Removal of Insulation Blankets surrounding the overwing emergency exit hatches IAW ASB A601R-25-152.

< Main and APU Battery Connectors Short Circuit Protection > Conduct a one-time inspection / repair of the main and APU battery charger input connector and wire harness IAW ASB A601R-24-085 Rev C


< Wing Ice Detection > Revise the FAA- Approved AFM

< Air Data Systems > To Prevent Uncommanded Changes To The Pilot's And Copilot's Air Data Systems. Within 18 months of Aug. 28, 1998, modify aircraft IAW SB 601R-34-094.

< Aileron - To Prevent Ice / Slush / Water Accumulation on Aileron Quadrant Cable Pulleys >. Install splash guards in the wheel wells PN 601R310401-5/SB and -6/SB.(a) Comply with SB 601R27-104 Rev. Orig. within 45 days of effective date. Effective Date 2-Oct-2000.

< Flight Spoilers > To Detect / Prevent Fracture of the Spoiler Actuator Lug

< Elevator Flutter Damper Shear Pins - Replacement of Flutter Damper Shear Pins > Install pin PN 601R24063-31/S per SB 601R-27-100 Rev. A. Discard stock of all pins PN 601R24063-31 and/or 601R24063-953.

< Integrated Drive Generator Cables > To Detect / Prevent Chaffing of the IDG Cables on the Engine Cowl Door.(a) Inspect within 50 hrs from effective date and repair if required. (b) Install conduit within 550 hrs from par. (a) per part B of SB A601R-24-103 Rev. B. Effective date: 9-Apr-01.

< Flight Spoilers > Applicable to MSN 7003-7340. To Detect / Prevent Fracture of the Spoiler Actuator Lug.(c) Installation of redesigned flight spoliers per SB 601R-57-029 Rev. Orig. constitutes terminating action.

< Main Landing Gear >-To Prevent Failure of the Main Landing Gear Fittings. Part I (ECI 500FC) Part II (DVI 100 FC) Part III (Serv 500 FC) Part IV (Strut Insp 500 FC) Part VI (R&R Fittings)

<Center Tank Fuel Transfer Shutoff Valve - Inspect to Eliminate Potential Fire Hazard > Replace any PN 601R62256-5 with PN 601R62256-3.

< Left and Right Lower Wing Planks - Inspect for Cracks > Visually inspect for cracking and repair any cracks prior to further flight IAW A601R-57-031 Rev. A. Repeat every 5000 cycles.

< Fuel Level Sensor Wiring > Inspect for Chafing of the Fuel-Level Sensing Wiring

<HSTA - Life Limit Introduction at 19,200 FH> Within 14 days revise the approved maint schedule per TR 2B-816 dated 28-Nov-01 to establish Life limit at 19,200 FH.

<Power Transfer Relays (Leach "H" series) - Replace Suspect Contactors > From the effective date of this AD, no PN: H-A4A-039 contactors having a mfr date code of 0011 through 0050 shall be installed in any aircraft. Replace the suspect K1XC contactors within 500 FH. Replace the suspect K2XD and K3XD contactors within 1000FH per SB 601R-24-105 Rev. A.

<Flight Controls - To Prevent Aileron Stiffness> Amend the AFM adding TR RJ/109-2 and the maintenance program by adding tasks R22-11-A083-01, R27-00-A053-01, R27-11-A082-01 and R27-11-A082-02.

< Cargo Compartment Smoke Detectors - Replace P/N 473052 with P/N 473597-19 > Within 18 months from 18-Feb-03, replace the existing cargo compartment smoke detectors (PN 473052) with new smoke detectors PN 473597-19 IAW 601R-26-016 Rev. B or C.

<Overwing Exit Placards - Install Placards Showing Person Standing While Throwing> Within 12 months of 4 Apr. 03 replace placards with ones showing pictorial of person sitting for both door opening and throwing out procedure per SB 601R-11-077 Rev. A.

< Pressure Floor Skin - Perform Detailed Inspection to Detect Cracks>. Within 14 days change the operator approved maintenance schedule. Perform the AWL 53-41-149 IAW the AD schedule (by 10000 FC for aircraft with less than 8000 FC). Repeat inspection every 10,000 FC for aircraft inspected with no cracks found.

< Main Landing Gear >-To Prevent Failure of the Main Landing Gear Fittings. Part I (ECI 500FC) Part II (DVI 100 FC) Part III (Serv 500 FC) Part IV (Strut Insp 500 FC)

< Brake Control Valve > (b) Modify brake control valve per SB 601R-32-017 Rev. Orig. (c) Lubrication of Brake Control Valve every 1500 hours to Prevent Freezing of Input Plunger of the Dual Brake Control Valve per SB 601R-32-017 Rev. Orig.

<Left and Right Main Windshields > Check windshields for a placard with PN CSB-NP-139321-002-1 located on aft edge of the main windshields. For placards with a different P/N modify before further flight. Inspect and modify per SB 601R-56-004 Rev. Orig.

< APU Overheat Control Unit - Inspection and Installation of Tape on Fire Protection Control Unit >Install Tape within 250 Hrs. or 30 days after the eff date of this AD

<Fuel Tubing - Modify Fuel Vent Tubing to Prevent Fire Hazard> Install new vent tubing iaw the SB 601R-28-024 (Applies to serial numbers 7003 through 7067 and 7069 through 7109)

IDG Cables - To Detect / Prevent Chaffing on the Firewall Separators > Damaged cables with temp. repairs must be replaced within 4000 hours.

<Pressure Bulkheads - Incorporate AWL 53-41-116 > Initial Compliance Due at 14,906 CSN for Aircraft with Less 10,906 FC.

<Flight Data Recorder (FDR) and Cockpit Voice Recorder (CVR) - Chemical Resistant Dust Covers for Flight Data Recorder (FDR) and Cockpit Voice Recorder (CVR)> Within 18 months, FDR and CVR must comply with chemical resistant coatings (marked "CLR CTD" on cover). Inspect and modify per SB 601R-31-026 Rev. Orig and 601R-23-056 Rev. Orig.

<Revise AWL - PFS Input Lever> Accomplish function check of PFS input lever IAW Task R27-31-A024-01 (SB A601R-27-144)

< Engine Throttle Control Gearboxes - Inspect for Wear of the L/H & R/H Engine Throttle Control Gearboxes> Inspect gearboxes every 1,000 HRS and replace or reinspect IAW SB 601R-76-019.

< Landing Gear Control Handle - Replace P/N 7-45502-1 (601R50967-7) or P/N 7-45502-3 (601R50967-9) with PN 601R50967-11. Installation of the new handle IAW SB 601R-32-084 Rev. Orig. Terminates this AD.

<Engine Support Beam - To Detect and Repair Cracks on the Upper and Lower Web on the Engine Support Beam at FS 640> Inspect IAW SB A601R-53-059 Rev. D at Intervals of 1,100 FC.

<Main Landing Gear Fittings - To Prevent / Detect Cracking of the Main Landing Gear Fittings> Visual inspection (100 CYC). Eddy Current (500 CYC). Strut Service (500 CYC). Applicable to Aircraft with main Fitting P/N 17064-5 & 17064-6 )

R/H and L/H Main Landing Gear - Replace Main Fittings By 30 June 2007> Both RH and LH MLG main fittings must be replaced with the new main fittings, P/N 17064-107 and 17064-108) in accordance with Bombardier SB 601R-32-093.

<Air Supply Ducts & Bulkhead Check Valves - To Prevent Disconnection of an Air Supply Ducts and Loss of Pressurization> (b)(1)- Within 500 FH inspect per SB 601R-21-054 Rev. Orig. Repeat at 4000 FH. For 7003-7477: (b)(2) Inspect air supply ducts every 500FH. (c) Within 5000 FH from effective date replace/rework (REO 601R-21-51-009 Rev C) affected ducts per ASB 601R-21-053 Rev. A. Installation of NEW ducts terminates repeat inspection of paragraph (b)(2).

< Main Landing Gear - To Prevent Factures of MLG Side-Brace Fitting Shafts> Inspect Side-Brace Fitting Shafts for Corrosion / Replace IAW SB 601R-57-036 Rev. C.

<Aileron power control unit (PCU) - Prevent Failure of Both Links of the Aileron Power Control Unit (PCU)> Inspection per Part A of SB A601R-27-130 Rev B every 1000 flt hrs. to detect fractures / cracks and replace any fractured / cracked link.

<Amend AFM - Prevent possible loss of control on take-off> Amend AFM by Inserting Temporary Revision RJ/149-1 dated 1-Feb-05

< Engine Throttle Control Gearboxes - Inspect for Wear of the L/H & R/H Engine Throttle Control Gearboxes> Inspect gearboxes every 1,000 HRS and replace or reinspect IAW SB 601R-76-019 Rev. Orig. or Rev. A.

< APU Cooling Air Exhaust - To Prevent Incomplete Drainage of the Auxiliary Power Unit Enclosure > Terminate by accomplishing SB 601R-49-015 Rev. Orig.

<Amend Maintenance Program - Incorporation of New Task No. C27-42-103-01 "Detailed Inspection of the HSTA Secondary Load Path Indicator"> Revise the AWL incorporating new Task No. C27-42-103-01 as introduced by Temporary Revision (TR) 2A-8 the MRM

<Hydraulic Line Shields - Install Additional Hydraulic Line Shields IAW SB 601R-57-021> (Applies to serial numbers 7003 - 7067, 7069 - 7165, 7167 - 7169 and 7171 - 7188)

<Failed Wing Anti-Ice Ducts (Piccolo Tubes) In The Leading Edge Of The Wing> Installation of a complete set of new inboard, centre and outboard piccolo tubes, constitutes terminating action.

< Chafing of the electrical cables of the spoiler and brake pressure sensor unit (BPSU) on both sides of the wing root> (a) Visual inspection of the electrical harnesses of the spoiler / BPSU at L/H & R/H wing root IAW Part A of SB A601R-27-133 Rev. A. (d) Modify Wiring (Terminating Action) IAW A601R-27-133 Part E or F.

<Flight Controls - To Prevent Aileron Stiffness> Amend the AFM adding TR RJ/109-2 dated 19 Aug 2002, insert a copy of the AD in the AFM, advise all flight crews of the AFM change. An aileron control check procedure (flight crew) is required at TSN 5000 FH or more. Note: Task Requirements as indicated a) R22-11-A083-01 - Lube (6,500 FH) b) R27-00-A053-01 - R&R Pulley (10,500 FH) c) R27-11-A082-01 - Lube (5,500 FH) d) R27-11-A082-02 - Lube (5,500 FH).

<Aft Pressure Bulkhead - To Detect And Correct Cracking of the Aft Pressure Bulkhead> Revise the Approved Maintenance Schedule by incorporating the revised inspection requirements of Airworthiness Limitations (AWL) Number 53-61-153, as introduced by Temporary Revision (TR) 2B-2109 of the MRM

<Camlock Fasteners on Center Pedistal - Replace Camlocks with Nut Plates> Replace camlocks with nut plates. Within 5500 flight hours of the effective date of this directive, 24-Feb-06, IAW SB 601R-31-030 Rev. F.

<Missing Restrictor on Refuel / Defuel Valves - Replace Part Number 202297 “Gask-o-Seals”> Replace part number 202297 “Gask-o-Seals” with part number 601R62085-1 IAW SB A601R-28-064 Rev. A.


<Short Circuit Failures Of Certain Alternating Current (AC) Contactors> (f) Modify the wiring on the AC Service Bus Contactor K4XA IAW A601R-24-121 Rev. Orig. (g) Aircraft that have been modified IAW In-Service Modification Package IS601R2450-0025 meet the requirements of paragraph 1.

< APU Overheat Control Unit - Inspection and Installation of Tape on Fire Protection Control Unit > IAW SB 601R-26-017 Rev. D: (a) Install Tape within 250 Hrs. (d) Inspect within 5,000 Hrs. (d)(1) Reinspect within 5,000 Hrs or 24 months (WCL). IAW SB 601R-26-018 Rev. B: (e) Replace Control within 20,000 Hrs or 89 months from effective date (12-Jun-2006). That constitutes terminating action.

<Junction Boxes - Leach TDH-Series Relay Malfunctions> Within 5500 hours or 36 months (WCF) from effective date (16-Jun-06): Visually inspect the identified Leach TDH-Series relays - K4WQ and K5WQ, K3QA and K4QA, K4WG, K1CN and K2CN IAW SB 601R-24-118 Rev. A for the manufactures date codes listed. (b) If the date code on relay is included replace the relay with a serviceable relay prior to further flight.

<To Detect And Correct Cracking In The Lower Forward Corner Of The Cargo Door Skin Cut-Out, Which Could Result In Reduced Structural Integrity Of The Airplane> Revise the Approved Maintenance schedule by incorporating the revised threshold and repeat inspection interval for Airworthiness Limitations (AWL) Number 53-61-141 (TR 2B-2109 of the MRM)

< Flap System > Install Flap Skew Detection Modification to Prevent Flap System Failure. Effective Date 21-Jul-06.(f)(g) AFM revision;(h) Within 12 months of effective date install new #3 and #4 flap actuators per SB 601R-27-114 Rev. C;(i) Within 30 months of effective date install SDS per SB 601R-27-115 Rev. E, SB 601R-27-116 Rev. C, SB 601R-34-128 Rev. C, SB 601R-11-080 Rev. A and SB 601R-27-111.

<To Prevent Short Circuit Failures Of Certain AC Contactors Which Could Result In Arcing And Consequent Smoke Or Fire> IAW SB 601R-24-122 (1a Visually inspect AC bus contactors 1K4XD and 2K4XD, part number (P/N D-7GRZ) to determine if contactors have an Ultem 2200 terminal base plate 1b) Apply RTV sealant to base plate of the 1K4XD, 2K4XD and K4XA AC contactors that have an Ultem 2200 base plate.

<Uncommanded Horizontal Stabilizer Trim Motion> (g), (j) and (m) insert TR into AFM. (o) Within 9 months of effective date, install HSTCU P/N 7060-10 or higher per SB 601R-27-147 Rev. Orig. (o)(1) Reverse paragraphs (g) and (j). Effective Date 20-Mar-2007.

R/H and L/H Main Landing Gear - Replace Main Fittings by 16-May-2008 Both RH and LH MLG main fittings must be replaced with the new main fittings, P/N 17064-107 and 17064-108 in accordance with Bombardier SB 601R-32-093 Rev. B. Applicable to aircraft equipped with main fittings P/N 17064-101, -102, -103 and -104.

< Inspection of Chemical Oxygen Generator for incorrect installation of release pin on Safety Pin Hole > (Applicable to aircraft MSNs listed in Bombardier Service Bulletin A601R-35-014 Rev. Orig and 601R-35-016 rev. orig).

R/H and L/H Main Landing Gear - Replace Main Fittings By 14 June 2010> Both RH and LH MLG main fittings must be replaced with the new main fittings, P/N 17064-107 and 17064-108 in accordance with Bombardier SB 601R-32-093. Applicable to aircraft equipped with main fittings P/N 17064-105 and -106.

<Engine Exhaust Nozzle - Loss In-Flight> (f) DVI of the hardware attaching the engine exhaust nozzle to the aft flange IAW Part A of SB 601R-78-021 Rev. Orig. If no bolt is missing or fractured, no further action is required until the next inspection. Repeat inspection every 1500 flight hours(g) if a bolt is missing or fractured on the engine exhaust nozzle, before next flight, replace the existing engine exhaust nozzle attachment hardware with new hardware in accordance with paragraph (h) of this directive.(h) Replace hardware within 4000 flight hours of 3-Apr-2007 IAW Part B of SB 601R-78-021 Rev. Orig.

<Uncommanded Horizontal Stabilizer Trim Motion> (g), (j) and (m) insert TR into AFM. (o) Within 9 months of effective date, install HSTCU P/N 7060-10 or higher per SB 601R-27-147 Rev. Orig. (o)(1) Reverse paragraphs (g) and (j). Effective Date 20-Mar-2007.

<Amend the Certification Maintenance Manual - Aileron PCU Leak and Backlash Checks> Revise the approved maintenance schedule by (1). Amending the CMR Manual ( 2), Airworthiness Requirements IAW TR 2A-20 (a) Added Task C27-10-105-06 (aileron PCU internal leakage at 5,000 FH) & Task C27-10-105-05 (Backlash check and functional test of the Aileron control sys.at 5,000 FH)

< To Prevent Flap Failure > Part I AFM Change. Part II Operational Procedures Part lll Training Procedures Part IV Maintenance Actions IAW SB 601R 27-150.

< To Prevent Flap Failure > Part I AFM Change. Part II Operational Procedures Part lll Training Procedures Part IV Maintenance Actions IAW SB 601R 27-150.

<Fuel System Safety - Insufficient Electrical Bonding Between Fuel Boost Pump Canister and the Pressure Pick-Up Line> Within 5,000 FH after the effective date this AD (26-Feb-2008) carry out a detailed visual inspection for the presence of an anodized fuel boost pump reducer coupling according to SB 601R-28-057 Rev. Orig.

<Fuel System Safety - Lack of Sealant on Collector Fuel Tank Bolts and Transfer Ejector Pumps> Within 5000 FH from 17-Mar-08: (f)(1) Apply sealant to bolts on the collector fuel tanks IAW Rev A of SB 601R-28-051. (f)(2) GVI of the left and right transfer ejector pumps IAW SB 601R-28-060 rev A. (f)(3) If sealant is missing from the edge of the transfer ejector pump or from any of the bolts, prior to further flight, apply sealant to the affected areas according to SB 601R-28-060 rev A.

<Fuel System Safety - Replace Fuel Tube Couplings> Within 5000 hrs after the effective date of this AD (28-Mar-2008) replace fuel tube couplings inside the wing and center fuel tanks IAW SB 601R-28-054 Rev. A

<To Prevent Short Circuit Failures Of Certain AC Contactors Which Could Result In Arcing And Consequent Smoke Or Fire> (f) IAW SB 601R-24-122 Rev. A, 800 hours after 7-Sep-06 or 4 months (WCF): Visually inspect AC bus contactors 1K4XD, 2K4XD and K4XA to determine if contactors have an Ultem 2200 terminal base plate and Apply RTV sealant to base plate. (h) Accomplish SB 601R-24-123 Rev. B within 12 months from effective to terminate AD. Effective date: 8-Apr-08.

<Fuel System safety - MRM Task additions> Within 60 days after the effective date of this AD (16 Apr. 2008) revise revise the Airworthiness Limitations Section (ALS) of the Instructions for Continued Airworthiness to incorporate the inspection and maintenance requirements, as applicable, in Appendix D, ''Fuel System Limitations,'' of Part 2, ''Airworthiness Requirements,'' of Bombardier CL-600-2B19 Maintenance Requirements Manual CSP A-053, Revision 7, dated May 10, 2007 (''the MRM''), task numbers 28-11-00-601, 28-11-00-602, 28-11-00-603, 28-11-00-604, 29-33-01-601, and 29-33-01-602. See the AD for the the initial compliance time

<Engine Support Beam - To Detect and Repair Cracks on the Upper and Lower Web on the Engine Support Beam at FS 640> (f) Perform DVI of the LH & RH frame & angles at FS 640 between Str 9 & Str 12 IAW SB 601R-53-061 Rev. E. (g) Repeat inspection every 1100 FC. (h) Repair cracks per SB 601R-53-061 Rev. E. Effective date: 16-Apr-08.

<Amend AFM - Prevent possible loss of control on take-off> Amend AFM by Inserting Temporary Revisions RJ/149-1 dated 1-Feb-05 (AD 2005-04-05) and RJ/155-3 dated 25-Mar-2008

<Revise AWL - PFS Input Lever> (f) Add Task R27-31-A024-01 to the MRM. (g) Repetitive inspections per SB A601R-27-144 rev B. Paragraph (g) terminates par. (f).

<Revise AWL - Fuel system Safety> Within 60 days after the effective date of this AD, or before December 16, 2008, whichever occurs first, revise the ALS of the Instructions for Continued Airworthiness to include the CDCCLs specified in Canadair Temporary Revision (TR) 2D-2, dated March 31,2006, to Appendix D, ''Fuel System Limitations,'' of Part 2, ''Airworthiness Requirements,'' of the Bombardier CL-600-2B19 Maintenance Requirements Manual CSP A-053. Effective date: 6-Jun-08.

<Fuel Quantity Gauging System> Within 10,000 flight hours after the effective date of this AD (16-Jul-08), unless already done, (1) Modify the FQGS harness routing according to the Accomplishment Instructions of SB 601R-28-059, Revision E.

<Cold weather operation limitations> Amend AFM by Inserting Temporary Revision RJ/155-3 dated 25-Mar-2008 and RJ/155-5 dated 07-Aug-2008

<Auxiliary fuel tanks> This AD applies to airplanes, certificated in any category and equipped with auxiliary fuel tanks installed.

<Fuel System safety - MRM Task additions> Within 60 days after the effective date of this AD (16-Apr-2008) revise revise the Airworthiness Limitations Section (ALS) of the Instructions for Continued Airworthiness to incorporate the inspection and maintenance requirements, as applicable, in Appendix D, ''Fuel System Limitations,'' of Part 2, ''Airworthiness Requirements,'' of Bombardier CL-600-2B19 Maintenance Requirements Manual CSP A-053, Revision 7, dated May 10, 2007 (''the MRM''), task numbers 28-11-00-601, 28-11-00-602, 28-11-00-603, 28-11-00-604, 29-33-01-601, and 29-33-01-602. See the AD for the the initial compliance time

Task 28-11-00-601 - Post SB 601R-28-055 (AD CF-2007-34)Task 28-11-00-602 - Post SB 601R-28-055 (AD CF-2007-34) Task 28-11-00-604 - Post SB 601R-28-059 (AD CF-2007-36)

< Main Landing Gear >-This AD applies to Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes, certificated in any category; having serial numbers (S/Ns) 7003 and subsequent, equipped with main landing gear (MLG) main fittings having part numbers (P/Ns) 601R85001-3 and -4 (Messier-Dowty P/Ns 17064-101, -102, -103, and - 104).

< Wing anti-ice ducts (piccolo tubes)> For airplanes having S/Ns 7014, 7017, 7037, 7046, 7059, 7076, 7105, 7127, 7151, 7157, 7163, 7179, 7203, 7228, 7271, 7347, 7359, 7362, 7378, 7381, 7417 through 7990 inclusive, and 8000 through 8055 inclusive, on which Bombardier Service Bulletin 601R-30-029 has been accomplished: Within 30 days after the effective date of this AD (1-Dec-08):(f) Inspect for affected piccolo tubes before 21-Sep-07;(g) thru (m) - Corrective actions;For all aircraft:(n) Insert TR RJ/155-6 into the AFMFor airplanes having SN 7003 through 7013, 7015, 7016, 7018 through 7036, 7038 through 7045, 7047 through 7058, 7060 through 7067, 7069 through 7075, 7077 through 7104, 7106 through 7126, 7128 through 7150, 7152 through 7156, 7158 through 7162, 7164 through 7178, 7180 through 7202, 7204 through 7227, 7229 through 7270, 7272 through 7346, 7348 through 7358, 7360, 7361, 7363 through 7377, 7379, 7380, 7382 through 7416, 8056 through 8076, 8082, 8086, 8090 though 8092, 8096 and 8097:(p)(q) Records check before 31-Dec-08;(w) Replace affected piccolo ducts per SB 601R-30-032 Rev. Orig.

< Landing gear trunnion> Cracks on the main landing gear trunnion fitting web have been discovered during fatigue testing. Failure of the main landing gear trunnion fitting web could compromise the structural integrity of the trunnion fitting and result in a main landing gear collapse. Incorporate the (AWL) No. 57-21-161, as identified in Bombardier Temporary Revision 2B-2136.

<Fuel System Safety - Insufficient Electrical Bonding at the Refuel/Defuel Shutoff Valves> Within 5000 hours air time after 28-Jan-2009, unless already accomplished. C/W Bombardier Service Bulletin (SB) 601R-28-053 rev D.

< Angle of Attack Transducer – Heating Element Degradation and Inaccurate Calibration >For airplanes equipped with a transducer having accumulated more than 7,500 total flight hours as of the effective date of this AD: Within 250 flight hours after the effective date of this AD, measure the inrush current of both AOA transducers in accordance with Part A of the Accomplishment Instructions of Bombardier Service Bulletin 601R-27-153, Revision A, dated December 16, 2008.

(i) If both AOA transducers are found to have an inrush current of 1.60 amps or more, repeat the measurement thereafter at intervals not to exceed the applicable interval specified in Table 1 of this AD. Do the measurement in accordance with Part A of the Accomplishment Instructions of Bombardier Service Bulletin 601R-27- 153, Revision A, dated December 16, 2008.

<Insufficient Electrical Bonding for Lightning Protection Inside Fuel Tanks> Within 5000 hours air time after the effective date of this directive (30-Apr-09), modify bonding jumpers inside the wing and centre fuel tanks, according to the Accomplishment Instructions of Bombardier Service Bulletin (SB) 601R-28-055, Revision F.

< To Prevent Flap Failure > (h)(1) New AFM change within 30 days after 15-Apr-09 (h)(2) New operational procedures (h)(3) New training(f)(4) Within 120 days after 5-Sep-2007 peform Part A of SB 601R-27-150 Rev. Orig.

(g)(2) Within 24 months or 4000 FH of 15-Feb-08 perform Part B of SB 601R-27-150 Rev. Orig.

(g)(3) Within 24 months after 15-Feb-08 perform Part C of SB 601R-27-150 Rev. Orig. (h)(8) Repeat inspections after 12 months

(h)(8) - Within 120 days of 15-Apr-09 perform SB 601R-11-090 Rev. Orig. or later

<Air-Driven Generator - Internal Wiring> Within 12 months after 30-Apr-09, check and, if required, modify the ADG IAW SB 601R-24-113 Rev A or later.

<Flap Actuator Pinion Gear Non Conformance >(f)(1) - Within 100 flight cycles from the effective date of this directive, inspect the serial number of each of the Flap Actuators P/N 601R93101-21 and P/N 601R93101-25 installed on the aircraft. (f)(2) - Within 500 flight cycles from the effective date of this directive, inspect the serial number of each of the P/N 601R93101-25 installed on the aircraft. Replace affected S/N's before further flight. Effective date: 28-May-09

15,685.9

13,231


TCCA Requirements

< Brake Control Valve > Lubrication of Brake Control Valve to Prevent Freezing of Input Plunger of the Dual Brake Control Valve

<Rudder Control Quadrant> - To Prevent Failure of a Rudder Control Quadrant (Part Number 600-92614-1) due to Stress Corrosion. Superseded by CF-94-23.

< Elevator Flutter Damper Fittings and Shear Pins > To Reduce Undampened Vibration of Elevators in the Event of Hydraulic System Failure (Superseded by CF-94-21R1)

< Integrated Drive Generator (IDG) > To Prevent Integrated Drive Generator (IDG) Failure.

< Stall Protection System (SPS) > Interim Corrective Action to Disconnect the Right Channel AHRS / Restore System to Type Approval Configuration

< Passenger Door Freezing > - Lubrication To Prevent Freezing of Passenger Door Mechanism.Part 6(a) - SB A601R-52-009 Rev. B or later;Part 6(b) - SB A601R-52-021 Rev. A or later.

< ADG Uplock Assembly (Sundstrand) > - To Detect and Correct Problems with the Manual Deployment System (Uplock Assembly, Part Number 721863B)

< Rudder Control Quadrant (Part Number 600-92614-1 > Replacement of the Quadrant to Prevent Possibility of Stress Corrosion of the Quadrant Spigot.

< NLG Spring Bungee > Reduced Stroke Due To Possible Incorrect Assembly During Manufacture that Could Result in Improper NLG Door Operation Which Could Prevent Extension Of The NLG.

< DC Power Distribution System > Repair of Loose Fuse Holders. Perform one-time inspection / repair of the DC power distribution system IAW ASB A601R-24-056 Rev A.

< Aileron Flutter Dampers > Installation of Newly Designed Aileron Flutter Dampers And Improved Shear Pins

< ELEVATOR DAMPER SHEAR PINS> The shear pins and lugs of the elevator flutter damper fittings have been found sheared-off on two aircraft that had improved shear pins installed per Airworthiness Directive (AD) CF-93-32R1

< Main Landing Gear Shock Strut Upper and Lower Attachment Pins > To Prevent Main Landing Gear Failure. Within 6 months of 14-Mar-97, install new MLG shock strut upper and lower attach pins IAW SB 601R-32-065 or later.

< Centre Fuel Tank > To Reduce The Potential For a Centre Fuel Tank Fire or Explosion Inspect the Electrical Conduits in the Centre Fuel Tank inspect electrical conduits in the centre fuel tank IAW ASB A601R-28-036 Rev A, Section 2, Part A.

< Chaffing Between IDG Cables and Fuel Lines at 10th Stage Bleed Check Valve > Inspect / repair / replace IDG cables IAW ASB A601R-24-095 Rev A. 2) For S/N's 7003 thru 7067 and 7069 thru 7303, inspect / correct clearance between 10th stage bleed air valve and fuel manifold pigtails IAW ASB A601R-73-008 Rev A

< Emergency Overwing Exits > Removal of Insulation Blankets surrounding the overwing emergency exit hatches IAW ASB A601R-25-152.

< Main and APU Battery Connectors Short Circuit Protection > Conduct a one-time inspection / repair of the main and APU battery charger input connector and wire harness IAW ASB A601R-24-085 Rev C


< Air Data Systems > To Prevent Uncommanded Changes To The Pilot's And Copilot's Air Data Systems. Within 18 months of Aug. 28, 1998, modify aircraft IAW SB 601R-34-094.

< Aileron - To Prevent Ice / Slush / Water Accumulation on Aileron Quadrant Cable Pulleys >. Install splash guards in the wheel wells PN 601R310401-5/SB and -6/SB.Comply with SB 601R27-104 Rev. Orig. or later within 90 days of effective date. Effective Date 29-Sep-2000.

< Elevator Flutter Damper Shear Pins - Replacement of Flutter Damper Shear Pins > Install pin PN 601R24063-31/S per SB 601R-27-100 Rev. Orig or later. Discard stock of all pins PN 601R24063-31 and/or 601R24063-953.

< Integrated Drive Generator Cables > To Detect / Prevent Chaffing of the IDG Cables on the Engine Cowl Door. Part A inspect within 50 hrs from effective date and repair if required. Part B Install conduit within 550 hrs from effective date per part B of SB A601R-24-103 Rev. Orig. or later. Effective date: 22-Jan-01.

< Flight Spoilers > Applicable to MSN 7003-7340. To Detect / Prevent Fracture of the Spoiler Actuator Lug.Part C - Installation of redesigned flight spoliers per SB 601R-57-029 Rev. Orig. or later constitutes terminating action.

<Center Tank Fuel Transfer Shutoff Valve - Inspect to Eliminate Potential Fire Hazard > Replace any PN 601R62256-5 with PN 601R62256-3.

< Left and Right Lower Wing Planks - Inspect for Cracks > Visually inspect for cracking and repair any cracks prior to further flight IAW A601R-57-031 Rev. Orig. or later. Repeat every 5000 cycles.

< Fuel Level Sensor Wiring > Inspect for Chafing of the Fuel-Level Sensing Wiring

<HSTA - Life Limit Introduction at 19,200 FH> Within 14 days revise the approved maint schedule per TR 2B-816 dated 28-Nov-01 to establish Life limit at 19,200 FH.

Superseded by AD CF-2009-02

<Power Transfer Relays (Leach "H" series) - Replace Suspect Contactors > From the effective date of this AD, no PN: H-A4A-039 contactors having a mfr date code of 0011 through 0050 shall be installed in any aircraft. Replace the suspect K1XC contactors within 500 FH. Replace the suspect K2XD and K3XD contactors within 1000FH per SB 601R-24-105 Rev. Orig. or later.

< Cargo Compartment Smoke Detectors - Replace P/N 473052 with P/N 473597-19 > Within 18 months from 29-Jun-01, replace the existing cargo compartment smoke detectors (PN 473052) with new smoke detectors PN 473597-19 IAW 601R-26-016 Rev. Orig. or later.

< Pressure Floor Skin - Perform Detailed Inspection to Detect Cracks>. Within 14 days change the operator approved maintenance schedule. Perform the AWL 53-41-149 IAW the AD schedule (by 10000 FC for aircraft with less than 8000 FC). Repeat inspection every 10,000 FC for aircraft inspected with no cracks found.

< Brake Control Valve > Bombardier confirmed that all affected aircraft have been modified. Incorporation of task 32-43-06-05 into maintenance program constitutes terminating action to AD requirements.

<Left and Right Main Windshields > Check windshields for a placard with PN CSB-NP-139321-002-1 located on aft edge of the main windshields. For placards with a different P/N modify before further flight. Inspect and modify per SB 601R-56-004 Rev. Orig or later.

<Fuel Tubing - Modify Fuel Vent Tubing to Prevent Fire Hazard> Install new vent tubing iaw the SB 601R-28-024 (Applies to serial numbers 7003 through 7067 and 7069 through 7109)

IDG Cables - To Detect / Prevent Chaffing on the Firewall Separators > Damaged cables with temp. repairs must be replaced within 4000 hours.

<Pressure Bulkheads - Incorporate AWL 53-41-116 > Initial Compliance Due at 14,906 CSN for Aircraft with Less 10,906 FC.

<Flight Data Recorder (FDR) and Cockpit Voice Recorder (CVR) - Chemical Resistant Dust Covers for Flight Data Recorder (FDR) and Cockpit Voice Recorder (CVR)> Within 18 months, FDR and CVR must comply with chemical resistant coatings (marked "CLR CTD" on cover). Inspect and modify per SB 601R-31-026 Rev. Orig or later and 601R-23-056 Rev. Orig. or later.


< Landing Gear Control Handle - Replace P/N 7-45502-1 (601R50967-7) or P/N 7-45502-3 (601R50967-9) with PN 601R50967-11. Installation of the new handle IAW SB 601R-32-084 Rev. Orig. or later terminates this AD.

<Engine Support Beam - To Detect and Repair Cracks on the Upper and Lower Web on the Engine Support Beam at FS 640> Inspect IAW SB A601R-53-059 Rev. Orig. or later at Intervals of 740 FC. Modification per Part B of the SB constitutes terminating action.

<Air Supply Ducts & Bulkhead Check Valves - To Prevent Disconnection of an Air Supply Ducts and Loss of Pressurization> Part A- Within 500 FH inspect per SB 601R-21-054 Rev. Orig. or later. Repeat per Task 21-51-21-07. Part B (7003-7477 only) - Within 5000 FH from 18-Mar-03 replace/rework (REO 601R-21-51-009 Rev C) affected ducts per ASB 601R-21-053 Rev.Orig. or later. Installation of NEW ducts terminates repeat inspection of paragraph part B.5.

< Main Landing Gear - To Prevent Factures of MLG Side-Brace Fitting Shafts> Inspect Side-Brace Fitting Shafts for Corrosion / Replace IAW SB 601R-57-036 Rev. B or later.

<Aileron power control unit (PCU) - Prevent Failure of Both Links of the Aileron Power Control Unit (PCU)> Inspection per Part A of SB A601R-27-130 Rev A or later every 1000 flt hrs. to detect fractures / cracks and replace any fractured / cracked link.

<Amend AFM - Prevent possible loss of control on take-off> Amend AFM by Inserting Temporary Revision RJ/149-1 dated 1-Feb-05

< Engine Throttle Control Gearboxes - Inspect for Wear of the L/H & R/H Engine Throttle Control Gearboxes> Inspect gearboxes every 1,000 HRS and replace or reinspect IAW SB 601R-76-019 Rev. B or later.

< APU Cooling Air Exhaust - To Prevent Incomplete Drainage of the Auxiliary Power Unit Enclosure > Terminate by accomplishing SB 601R-49-015 Rev. Orig or later.

<Amend Maintenance Program - Incorporation of New Task No. C27-42-103-01 "Detailed Inspection of the HSTA Secondary Load Path Indicator"> Revise the AWL incorporating new Task No. C27-42-103-01 as introduced by Temporary Revision (TR) 2A-8 the MRM

Superseded byCF- 2008-30

<Hydraulic Line Shields - Install Additional Hydraulic Line Shields IAW SB 601R-57-021> (Applies to serial numbers 7003 - 7067, 7069 - 7165, 7167 - 7169 and 7171 - 7188)

< Chafing of the electrical cables of the spoiler and brake pressure sensor unit (BPSU) on both sides of the wing root> Part A1 Visual inspection of the electrical harnesses of the spoiler / BPSU at L/H & R/H wing root IAW Part A of SB A601R-27-133 Rev. A or later . Part B Modify Wiring (Terminating Action) IAW A601R-27-133 Part E or F.

<Flight Controls - To Prevent Aileron Stiffness> Amend the AFM adding TR RJ/109-2 dated 19 Aug 2002, insert a copy of the AD in the AFM, advise all flight crews of the AFM change. An aileron control check procedure (flight crew) is required at TSN 5000 FH or more. Note: Task Requirements as indicated a) R22-11-A083-01 - Lube (6,500 FH) b) R27-00-A053-01 - R&R Pulley (10,500 FH) c) R27-11-A082-01 - Lube (5,500 FH) d) R27-11-A082-02 - Lube (5,500 FH).

<Aft Pressure Bulkhead - To Detect And Correct Cracking of the Aft Pressure Bulkhead> Revise the Approved Maintenance Schedule by incorporating the revised inspection requirements of Airworthiness Limitations (AWL) Number 53-61-153, as introduced by Temporary Revision (TR) 2B-2109 of the MRM

<Camlock Fasteners on Center Pedistal - Replace Camlocks with Nut Plates> Replace camlocks with nut plates. Within 5500 flight hours of the effective date of this directive, 18-Aug-05, IAW SB 601R-31-030 Rev. D or later.

<Missing Restrictor on Refuel / Defuel Valves - Replace Part Number 202297 “Gask-o-Seals”> Replace part number 202297 “Gask-o-Seals” with part number 601R62085-1 IAW SB A601R-28-064 Rev. Orig. or later.

<Short Circuit Failures Of Certain Alternating Current (AC) Contactors> 1) Modify the wiring on the AC Service Bus Contactor K4XA IAW A601R-24-121 Rev. Orig or later. 2) Aircraft that have been modified IAW In-Service Modification Package IS601R2450-0025 meet the requirements of paragraph 1.

< APU Overheat Control Unit - Inspection and Installation of Tape on Fire Protection Control Unit > IAW SB 601R-26-017 Rev. A or later: Part 1 (Install Tape) within 250 Hrs. Part 2 (Inspect) within 5,000 Hrs. Part 3 (Reinspect) within 5,000 Hrs. IAW SB 601R-26-018 Rev. Orig. or later: Part 4 (Replace Control) within 20,000 Hrs from effective date or by 31-Dec-2010 WCF. That constitutes terminating action. Effective 15-Aug-2003

<Junction Boxes - Leach TDH-Series Relay Malfunctions> Within 5500 hours or 36 months (WCF) from effective date (3-Oct-05): Visually inspect the identified Leach TDH-Series relays - K4WQ and K5WQ, K3QA and K4QA, K4WG, K1CN and K2CN IAW SB 601R-24-118 Rev. A or later for the manufactures date codes listed. (b) If the date code on relay is included replace the relay with a serviceable relay prior to further flight.

<To Detect And Correct Cracking In The Lower Forward Corner Of The Cargo Door Skin Cut-Out, Which Could Result In Reduced Structural Integrity Of The Airplane> Revise the Approved Maintenance schedule by incorporating the revised threshold and repeat inspection interval for Airworthiness Limitations (AWL) Number 53-61-141 (TR 2B-2109 of the MRM)

< Flap System > Install Flap Skew Detection Modification to Prevent Flap System Failure. Effective Date 25-Jun-04.Part I - AFM revision;Part V - Within 12 months of effective date install new #3 and #4 flap actuators per SB 601R-27-114 Rev. Orig. or later;Part VI - By 31-Dec-06 comply with Part VI and install SDS per SB 601R-27-115 Rev. D or later, SB 601R-27-116 Rev. Orig. or later, SB 601R-34-128 Rev. B or later and SB 601R-11-080 Rev. Orig. or later. Part VI constitutes terminating action.

R/H and L/H Main Landing Gear - Replace Main Fittings by 30-Jun-2007 Both RH and LH MLG main fittings must be replaced with the new main fittings, P/N 17064-107 and 17064-108 in accordance with Bombardier SB 601R-32-093 Rev. A or later. Applicable to aircraft equipped with main fittings P/N 17064-101, -102, -103 and -104.

< Inspection of Chemical Oxygen Generator for incorrect installation of release pin on Safety Pin Hole > (Applicable to aircraft MSNs listed in Bombardier Service Bulletin A601R-35-014 Rev. Orig and 601R-35-016 rev. orig).

R/H and L/H Main Landing Gear - Replace Main Fittings By 31 Dec 2008> Both RH and LH MLG main fittings must be replaced with the new main fittings, P/N 17064-107 and 17064-108 in accordance with Bombardier SB 601R-32-093 Rev. Orig. or later. Applicable to aircraft equipped with main fittings P/N 17064-105 and -106.

<Engine Exhaust Nozzle - Loss In-Flight> Part 1 DVI of the hardware attaching the engine exhaust nozzle to the aft flange IAW Part A of SB 601R-78-021 Rev. Orig. or later. 1a) if a bolt is missing or fractured on the engine exhaust nozzle, before next flight, replace the existing engine exhaust nozzle attachment hardware with new hardware in accordance with paragraph 3 of this directive. 1b) If no bolt is missing or fractured, no further action is required until the next inspection. 2). Repeat inspection every 1500 flight hours 3) Replacement of hardware Replace hardware within 4000 flight hours of 25-Aug-06 IAW Part B of SB 601R-78-021 Rev. Orig. or later.

<Uncommanded Horizontal Stabilizer Trim Motion> Part 1 insert TR into AFM. Part 2 Within 12 months of effective date, install HSTCU P/N 7060-10 or higher per SB 601R-27-147 Rev. Orig. or later. Part 3 Reverse paragraphs (g) and (j). Effective Date 16-Oct-2006.

<Amend the Certification Maintenance Manual - Aileron PCU Leak and Backlash Checks> Revise the approved maintenance schedule by (1). Amending the CMR Manual ( 2), Airworthiness Requirements IAW TR 2A-20 (a) Added Task C27-10-105-06 (aileron PCU internal leakage at 5,000 FH) & Task C27-10-105-05 (Backlash check and functional test of the Aileron control sys.at 5,000 FH)

<Fuel System Safety - Insufficient Electrical Bonding Between Fuel Boost Pump Canister and the Pressure Pick-Up Line> Within 5,000 FH after the effective date this AD (24-Sep-2007) carry out a detailed visual inspection for the presence of an anodized fuel boost pump reducer coupling according to SB 601R-28-057 Rev. Orig or later.

<Fuel System Safety - Lack of Sealant on Collector Fuel Tank Bolts and Transfer Ejector Pumps> Within 5000 FH from 24-Sep-07: 1.) Apply sealant to bolts on the collector fuel tanks IAW Rev A of SB 601R-28-051 Rev. Orig or later. 2.) GVI of the left and right transfer ejector pumps IAW SB 601R-28-060 Rev Orig. or later. 3.) If sealant is missing from the edge of the transfer ejector pump or from any of the bolts, prior to further flight, apply sealant to the affected areas according to BBD SB 601R-28-060 Rev Orig. or later.

<Fuel System Safety - Replace Fuel Tube Couplings> Within 5000 hrs after the effective date of this AD (1-Nov-2007) replace fuel tube couplings inside the wing and center fuel tanks IAW SB 601R-28-054 Rev. A or later.

<To Prevent Short Circuit Failures Of Certain AC Contactors Which Could Result In Arcing And Consequent Smoke Or Fire> IAW SB 601R-24-123 rev. B or later, 12 months 20-Jun-07: Visually inspect AC bus contactors 1K4XD, 2K4XD and K4XA to determine if contactors have an Ultem 2200 terminal base plate and apply corrections as required. Effective date: 20-Jun-07.

<Engine Support Beam - To Detect and Repair Cracks on the Upper and Lower Web on the Engine Support Beam at FS 640> 1) Perform DVI of the LH & RH frame & angles at FS 640 between Str 9 & Str 12 IAW SB 601R-53-061 Rev. B or later. 2) Repeat inspection every 1100 FC. 3) For repair of any cracks contact Bombardier for instructions. Effective date: 20-Jun-03.

<Revise AWL - PFS Input Lever> Part 1 - Repetitive inspections per SB A601R-27-144 Rev Orig. or later. Part 3 - Inspections per SB replace requirements of TR 2B-1784 (Task R27-31-A024-01)

<Revise AWL - Fuel system Safety> Within 60 days after the effective date of this AD, revise the ALS of the Instructions for Continued Airworthiness to include the CDCCLs specified in Canadair Temporary Revision (TR) 2D-2, dated March 31,2006, to Appendix D, ''Fuel System Limitations,'' of Part 2, ''Airworthiness Requirements,'' of the Bombardier CL-600-2B19 Maintenance Requirements Manual CSP A-053. Effective date: 10-Jan-08.

<Fuel Quantity Gauging System> Within 10,000 flight hours after the effective date of this AD (11-Jan-08), unless already done, (1) Modify the FQGS harness routing according to the Accomplishment Instructions of SB 601R-28-059, Revision E or later.

<Cold weather operation limitations> Amend AFM by Inserting Temporary Revision RJ/155-5 dated 07-Aug-2008

<Fuel System safety - MRM Task additions> Within 60 days after the effective date of this AD (10-Dec-07) revise revise the Airworthiness Limitations Section (ALS) of the Instructions for Continued Airworthiness to incorporate the inspection and maintenance requirements, as applicable, in Appendix D, ''Fuel System Limitations,'' of Part 2, ''Airworthiness Requirements,'' of Bombardier CL-600-2B19 Maintenance Requirements Manual CSP A-053, Revision 7, dated May 10, 2007 (''the MRM''), task numbers 28-11-00-601, 28-11-00-602, 28-11-00-603, 28-11-00-604, 29-33-01-601, and 29-33-01-602. See the AD for the the initial compliance time.

Task 28-11-00-601 - Post SB 601R-28-055 (AD CF-2007-34)Task 28-11-00-602 - Post SB 601R-28-055 (AD CF-2007-34) Task 28-11-00-604 - Post SB 601R-28-059 (AD CF-2007-36)

< Main Landing Gear >-This AD applies to Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes, certificated in any category; having serial numbers (S/Ns) 7003 and subsequent, equipped with main landing gear (MLG) main fittings having part numbers (P/Ns) 601R85001-3 and -4 (Messier-Dowty P/Ns 17064-101, -102, -103, and - 104).

< Wing anti-ice ducts (piccolo tubes)> Part I - Ammend AFM with TR RJ/155-6.For airplanes having SN 7003 through 7013, 7015, 7016, 7018 through 7036, 7038 through 7045, 7047 through 7058, 7060 through 7067, 7069 through 7075, 7077 through 7104, 7106 through 7126, 7128 through 7150, 7152 through 7156, 7158 through 7162, 7164 through 7178, 7180 through 7202, 7204 through 7227, 7229 through 7270, 7272 through 7346, 7348 through 7358, 7360, 7361, 7363 through 7377, 7379, 7380, 7382 through 7416, 8056 through 8076, 8082, 8086, 8090 though 8092, 8096 and 8097:Part II.A - Records check for replacement of piccolo ducts before 1-Dec-08;For airplanes having S/Ns 7014, 7017, 7037, 7046, 7059, 7076, 7105, 7127, 7151, 7157, 7163, 7179, 7203, 7228, 7271, 7347, 7359, 7362, 7378, 7381, 7417 through 7990 inclusive, and 8000 through 8055 inclusive:Part II.B - Check accomplishment of SB 601R-30-029 and records check before 1-Dec-08;Part III - Check P/N and S/N of piccolo ducts;Part IV - Repetitive inspections;Part VI - Replace affected piccolo ducts per SB 601R-30-032 Rev. Orig. or later within 24 months of effective date.Effective date: 3-Nov-08

< Landing gear trunnion> Cracks on the main landing gear trunnion fitting web have been discovered during fatigue testing. Failure of the main landing gear trunnion fitting web could compromise the structural integrity of the trunnion fitting and result in a main landing gear collapse. Incorporate the (AWL) No. 57-21-161, as identified in Bombardier Temporary Revision 2B-2136.

<Fuel System Safety - Insufficient Electrical Bonding at the Refuel/Defuel Shutoff Valves> Within 5000 hours air time after 30-June-2008, unless already accomplished. C/W Bombardier Service Bulletin (SB) 601R-28-053 rev C or later.

< Angle of Attack Transducer – Heating Element Degradation and Inaccurate Calibration > All Bombardier Inc. Model CL-600-2B19, serial number 7003 and subsequent equipped with Thales AOA transducers.

Part 1 - Within 900 FH after effective date (5-Jan-09) inspect AOA transducers for P/N and S/N per SB 601R-27-154 Rev. Orig. or later. Part 2 - Measure the inrush current and repeat measurement in accordance with Part A of SB 601R-27-153 Rev. Orig. or later.

<Insufficient Electrical Bonding for Lightning Protection Inside Fuel Tanks> Within 5000 hours air time after the effective date of this directive (10-Jan-08), modify bonding jumpers inside the wing and centre fuel tanks, according to the Accomplishment Instructions of Bombardier Service Bulletin (SB) 601R-28-055, Revision D or later.

< Flap System > CANADAIR - CL600 2B19(RJ)

< To Prevent Flap Failure > Part I AFM Change. Part II Operational Procedures Part lll Training Procedures Part IV Maintenance Actions IAW SB 601R 27-150 Rev. Orig or later. Effective 25-Aug-08.

Within 24 months or 4000 FH from 31-Jul-07 (WCF) perform Part B of SB 601R-27-150 Rev. Orig. or later.Within 24 months after 31-Jul-07 perform Part C of SB 601R-27-150 Rev. Orig. or later.Part VI - Before 1-Dec-08 perform SB 601R-11-090 Rev. Orig. or later

<Air-Driven Generator - Internal Wiring> Within 12 months after 18-Feb-2008, check and, if required, modify the ADG IAW SB 601R-24-113 Rev A or later.

<Flap Actuator Pinion Gear Non Conformance > Part A - Within 100 flight cycles from the effective date of this directive, inspect the serial number of each of the Flap Actuators P/N 601R93101-21 and P/N 601R93101-25 installed on the aircraft. Part B - Within 500 flight cycles from the effective date of this directive, inspect the serial number of each of the P/N 601R93101-25 installed on the aircraft. Replace affected S/N's before further flight. Effective date: 26-Apr-09

< Mach Trim System > HSTCU Circuits Deactivation to Prevent Unsafe Nose-Up Trim Runaway

<PFS Input Lever> Bombardier Inc. Model CL-600-2B19 “Regional Jet” serial numbers 7003 through 7999.

<Inboard Flap Actuator> Within 30 days after the effective date of this directive, amend the Transport Canada approved maintenance schedule by incorporating the new inspection requirements of CMR Number C27-50-300-01, as introduced by TR 2A-41 of Canadair Regional Jet MRM, Appendix A, CMR. Initial compliance with the new CMR task is 500 FH from effective date of this AD (9-Feb-2009). Applies only to inboard flap actuators P/N 852D100-19.

<Overwing Emergency Exit Placards - Supersedes and cancels Airworthiness Directive (AD) CF-2002-12> Within 24 months from effective date replace placards per SB 601-11-088 Rev. Orig. or later. Effective date: 19-Feb-09


Accomplished by Date Time Cycles Interval

ExelTech Aerospace 28-May-09 15676.6 13226 1000

N/A - Superseded by 2003-11-20


Mods Accomplished at Manufacture. Lubrication. Task # 32-43-06-05

incorporated into maintenance program.

N/A - Superseded by 95-18-07N/A - Superseded by CF-94-23

N/A - Superseded by 94-24-02N/A - Superseded by CF-94-21R1

N/A to MSN 7707. Applies to serial numbers 7003 to 7028.

N/A to MSN 7707. Applies to Serial Numbers 7003 through 7026.

ExelTech Aerospace 28-May-09 15676.6 13226 300





N/A to MSN 7707. Applies to serial numbers 7003 through 7040

N/A to MSN 7707. Applies to Serial Numbers 7003 Through 7038

N/A to MSN 7707. Applies to Serial Numbers 7003 Through 7048



N/A to MSN 7707. Applies to Serial Numbers 7003 through 7054





N/A to MSN 7707. Applies to Serial Numbers 7003 through 7067 and 7069

through 7303




Incorporated into the AFM Rev 58 Dated 28 Apr. 2008




Chautauqua Airlines 6-Jan-09 14907 12606 5000

Installed at Time of Manuacture. 25-Nov-02 0 0 19200

N/A to MSN 7653 Applies to Serial Numbers 7003 through 7357



Fuel Transfer SOV valve PN 601R62256-5 has been replaced by 601R62256-3 at

time of manufacture.



Comair Airlines 4-Dec-06 10698 9422 10000


27-May-09 15676.6 13226 1500



N/A to MSN 7707. Applies to Serial Numbers following table:

7003 through 7434 inclusive.7436 through 7442 inclusive.7444 through 7452 inclusive.7454 through 7458 inclusive.7460 through 7497 inclusive.7499 through 7504 inclusive.

Brake control valve modified at manufacture. Lubrication: ExelTech


Comair Airlines 30-Nov-06 10698 9422 12823



Task 32-43-06-05 incorporated into current MRM revision

N/A due to Part number not installed on aircraft. PN:601R33033-21, & -14 are installed and not covered by the AD


through 7109



ExelTech Aerospace 25-May-09 15676 13226 1100




Chautauqua Airlines 23-Nov-08 14645 12417 4000


Chautauqua Airlines 23-Nov-08 14645 12417 4000



TR incorporated into AFM Rev. 58F


ExelTech Aerospace 26-Jun-09 15676 13226 1000

Chautauqua Airlines 18-Jun-09 15679 13228 5000



through 7254.

11-Dec-06 10698 9422

29-May-09 15676 13226 6500

23-Apr-07 10707 9425 10500

29-May-09 15676 13226 5500

29-May-09 15676 13226 5500

28-Aug-08 14097 11993 4360

N/A to MSN 7707 Applies to Serial Numbers 7003 - 7067, 7069 - 7165, 7167

- 7169 and 7171 - 7188.

N/A - Superseded by 2008-23-16N/A - Superseded by CF-2008-30

Comair Airlines Accomplished SB A601R-27-133 Part E

R22-11-A083-01 (TC 000-12-160-701) ExeTech

R27-00-A053-01 (TC 000-27-590-722)(TC 000-27-690-722)

ExelTech

R27-11-A082-01 (TC 000-12-590-702)(TC 000-12-690-702)

ExelTech

R27-11-A082-02 (TC 000-12-160-700)Alma

Chautauqua AirlinesAWL 53-61-153 (TC 000-53-280-607)

AWL 53-61-153 (TC 000-53-280-608)N/A - SDI was chosen

2-Dec-05 8841 7636

2-Dec-05 8841 7636


6-Apr-06 9517 8264

4-Mar-09 15273 12896

Comair AirlinesSB A601R-31-030 rev F

Comair AirlinesSB A601R-31-030 rev F

None - N/A to MSN 7707 SB 601R-28-053 never Embodied / Effected Seals not

Installed.

Comair Airlines MOD-2-24M0003SB 601R-24-121 Rev. Orig.

N/A to MSN 7707 Applies to Serial Numbers 7003 through 7067, 7069 thru

7545.

Chautauqua Airlines EO AD061006SB 601R-24-118 Rev. A Part ASB 601R-24-118 Rev. A Part BSB 601R-24-118 Rev. A Part CSB 601R-24-118 Rev. A Part DSB 601R-24-118 Rev. A Part E

28-May-09 15676 13226 5291

27-Apr-07 10698 9422

27-Apr-07 10698 9422



ExelTechTC 000-53-280-602

ExelTechSB 601R-27-116 Rev. CSB 601R-11-080 Rev. A

ExelTechSB 601R-27-116 Rev. CSB 601R-11-080 Rev. A

ExelTech 24-Apr-07 10706 9424

26-May-09 15273 12896

22-Aug-07 11255 9838

N/A To MSN 7707. This aircraft is fitted with -105 & -106 MLG Fittings

ExelTechSB 601R-32-093 Rev. B

Chautauqua EO AD070424BSB 601R-78-021

16-Dec-0726-Jun-08

1212213582

1050811625

Chautauqua Airlines EO AD2007-05-11SB 601R-27-147 Rev. Orig.

27-Jan-09 15047 12714 5000

3-Jun-09 15676 13226 5000

25-May-09 15676 13226 2000



29-May-09 15676 13226

29-May-09 15676 13226

Chautauqua AirlinesC27-10-105-06 (TC 000-27-900-150)

ExelTech AerospaceC27-10-105-05

(TC 000-27-900-712)(TC 000-27-900-714)

ExelTech Aerospace27-11-00-09 (TC 000-27-900-015)

ExelTech AerospaceCHQ EO AD080207SB A601R-28-057

ExelTech AerospaceCHQ EO AD080207SB A601R-28-057

2-Jun-09 15676 13226

2-Jun-09 15,676.00 13226

29-May-09 15676 13226

29-May-09 15676 13226

ExelTech AerospaceSB 601R-28-051

ExelTech AerospaceSB 601R-28-060 Rev. A

ExelTech AerospaceSB 601R-28-051

ExelTech AerospaceSB 601R-28-060 Rev. A

ExelTech Aerospace IAW CHQ EO AD080408

SB A601R-28-054 Rev A

ExelTech Aerospace IAW CHQ EO AD080408

SB A601R-28-054 Rev A

Comair Card AD-2-24M0001 IAWSB 601R-24-122 Rev. A

Chautauqua Airlines EO024024 IAWSB 601R-24-123 Rev B

22-Aug-06

21-Jun-09

10239

15679

8980

13228


29-May-09 15676 13226 1100


8-Jun-09 15,676.00 13226 100

ExelTech Aerospace CHQ EO080610 IAW

SB 601R-53-061 Rev. E

ExelTech Aerospace CHQ EO2008-08-09

SB 601R-27-144

TR-2D-2 has been Incorporated in Rev 7 of the MRM

SB A601R-28-059 not complied yet.


TR incorporated into AFM Rev. 58F

23-May-09 15676 13226 5000

NA - The aircraft has not installed auxiliary Fuel tanks.

28-11-00-601 (TC 000-28-900-140)28-11-00-602 (TC 000-28-900-141)28-11-00-603 (TC 000-28-900-142) 28-11-00-604 (TC 000-24-900-140)

(TC 000-24-900-141) (TC 000-24-900-142)

ExelTech Aerospace29-33-01-601 (TAC 000-29-220-100)

29-33-01-602 (TC 000-29-900-160)Not complied yet

23-May-09 15676 13226 5000

28-11-00-601 (TC 000-28-900-140)28-11-00-602 (TC 000-28-900-141)28-11-00-603 (TC 000-28-900-142) 28-11-00-604 (TC 000-24-900-140)

(TC 000-24-900-141) (TC 000-24-900-142)

ExelTech Aerospace29-33-01-601 (TAC 000-29-220-100)

29-33-01-602 (TC 000-29-900-160)Not complied yet

This aircraft is fitted with -105 & -106 MLG Fittings

Par. (l) Comair Airlines Replaced 6 Piccolo Tubes

SB 601R-30-029 Rev. A

TR RJ/155-6 is included on revision 58F of the AFM

Par. (x)Comair Terminated IAW SB 601R-30-029

SB 601R-30-032 Rev. Orig.

6/5/2006 9834 8569

AWL 57-21-161 not complied yet



Par. (l) Comair Airlines Replaced 6 Piccolo Tubes

SB 601R-30-029 Rev. A

TR RJ/155-6 is included on revision 58F of the AFM

Par. (x)Comair Terminated IAW SB 601R-30-029

SB 601R-30-032 Rev. Orig.

6/5/2006 9834 8569

3-Jun-09 15676 13226 2000

3-Jun-09 15676 13226 2000

3-Jun-09 15676 13226 2000

3-Jun-09 15676 13226 2000

LH - ExelTech AerospaceSB 601R-27-153 Rev. A

RH - ExelTech AerospaceSB 601R-27-153 Rev. A

LH - ExelTech AerospaceSB 601R-27-153 Rev. A

RH - ExelTech AerospaceSB 601R-27-153 Rev. A

SB A601R-28-055

SB A601R-28-055

4-Oct-07 11569 10085

SB 601R-27-150 Part C 365

SB 601R-11-090 not complied yet

4-Oct-07 11569 10085

SB 601R-27-150 Part C 365


5-Aug-05 7493 6855

5-Aug-05 7493 6855

Chautauqua Airlines EO27077-1/ EO 27077-2 SB 601R-27-150 Rev. Orig. Part

A

SB 601R-27-150 Rev. Orig. Part B

Chautauqua Airlines EO27077-1/ EO 27077-2 SB 601R-27-150 Rev. Orig. Part

A

SB 601R-27-150 Rev. Orig. Part B

Comair EO 24-60SB 601R-24-113 Rev.

Comair EO 24-60SB 601R-24-113 Rev.


CANCELLATION NOTICE - AD SUPERSEDED BY CF-98-14


CANCELLATION NOTICE - AD SUPERSEDED BY CF-2005-41

Incorporated into the Maintenance Program


Next Due Status

16676.6

CLOSED

CLOSED

CLOSED

CLOSED

CLOSED

OPEN/ REPETITIVE

NOT APPLICABLE

NOT APPLICABLE

15976.6

CLOSED

CLOSED

CLOSED

CLOSED

OPEN/ REPETITIVE

NOT APPLICABLE

NOT APPLICABLE

NOT APPLICABLE

NOT APPLICABLE

NOT APPLICABLE

NOT APPLICABLE

NOT APPLICABLE

CLOSED

CLOSED

CLOSED

NOT APPLICABLE

NOT APPLICABLE

NOT APPLICABLE

NOT APPLICABLE

NOT APPLICABLE

NOT APPLICABLE

NOT APPLICABLE

CLOSED

CLOSED

17606

19200

NOT APPLICABLE

NOT APPLICABLE

NOT APPLICABLE

OPENREPETITIVE

NOT APPLICABLE

OPENREPETITIVE

CLOSED

19422

CLOSED

17176.6

NOT APPLICABLE

NOT APPLICABLE

NOT APPLICABLE

OPEN/ REPETITIVE

OPEN/ REPETITIVE

CLOSED

CLOSED

23521 OPEN

CLOSED

CLOSED

CLOSED

NOT APPLICABLE

NOT APPLICABLE

NOT APPLICABLE

14326

13966

CLOSED

CLOSED

18645

NOT APPLICABLE

OPEN/ REPETITIVE

OPEN/ REPETITIVE

OPEN/ REPETITIVE

18645

CLOSED

16676

CLOSED

CLOSED

16676 OK

16676 OK

20679

OPEN/ REPETITIVE

OPEN/ REPETITIVE

OPEN/ REPETITIVE

OPEN/ REPETITIVE

NOT APPLICABLE

OPEN/ REPETITIVE

CLOSED

CLOSED

22176

21207

21176

21176

16353 OK

NOT APPLICABLE

OPENREPETITIVE

OPENREPETITIVE

OPENREPETITIVE

OPENREPETITIVE

OPENREPETITIVE

NOT APPLICABLE

CLOSED

CLOSED

CLOSED

CLOSED

CLOSED

NOT APPLICABLE

NOT APPLICABLE

18517

CLOSED

CLOSED

CLOSED

CLOSED

OPENREPETITIVE

CLOSED

Open

CLOSED

CLOSED

NOT APPLICABLE

20047

20676

17676

CLOSED

CLOSED

CLOSED

CLOSED

OPEN/ REPETITIVE

OPEN/ REPETITIVE

OPEN/ REPETITIVE

CLOSED

CLOSED

CLOSED

CLOSED

CLOSED

CLOSED

14326

CLOSED

15776

CLOSED

OPEN/ REPETITIVE

OPEN/ REPETITIVE

23749.4 OPEN

23749.4 OPEN

CLOSED

20000 OPEN

20676

30000 OPEN

NOT APPLICABLE

OPEN/ REPETITIVE

20000 OPEN

20000 OPEN

20676

30000 OPEN

OPEN/ REPETITIVE

NOT APPLICABLE

CLOSED

CLOSED

25000 OPEN OK

20685.9 OPEN OK

18616.47 OPEN

17676 CLOSED

17676 CLOSED

17676

17676

20638.31 OPEN

17308.44 OPEN

OPEN/ REPETITIVE

OPEN/ REPETITIVE

CLOSED

OPEN

30-Dec-00 OPEN

OPEN

CLOSED

OPEN

30-Dec-00 OPEN

OPEN

CLOSED

CLOSED

OPEN

CLOSED

NOT APPLICABLE

CLOSED

0

19-Feb-11 OPEN

EACH OPERATOR

MUST COMPLY

of 158

MSN: 7707 A/C TSN: 15,685.90MFG Date: 20-Nov-02 A/C CSN: 13,231


MSN 7707 Appliance Airworthiness Directives Listing

US FAA AD Canadian AD Description

72-19-04 1996-21

79-18-05 N/A

81-04-06 N/A

93-04-02 N/A

93-14-12 N/A

93-23-01 N/A

93-24-16 N/A

94-01-06 N/A Incorporated in production Incorporated in production

94-06-04 N/A

94-14-03 N/A

94-19-06 N/A

95-22-01 N/A

97-11-10 N/A

97-18-03 N/A

98-24-27 N/A

Last Accomplishment Date(TSN / CSN)

Next Due Date(TSN / CSN)

<Nicad Battery Maintenance> FAA jurisdiction- N/A if aircraft has charging, monitoring and shutdown systems

N/A if Aircraft has Charging, Monitoring and Shutdown Systems

Closed - N/A if Aircraft has Charging, Monitoring and Shutdown Systems / Affected Parts not Fitted

< (LiSO2) batteries - ELT emergency equipment > TSO-C97 N/A - Affected Equipment Not Fitted to MSN 7707

Closed - Affected Equipment Not Fitted to MSN 7707

< (Fairchild)Cockpit Voice Recorder model A100 > Serial Number 4733 thru 5260

N/A - Affected Equipment Not Fitted to MSN 7707


< (TDR-94D)Mode S Trasponder > PN: 622-9210-002 N/A - Affected Equipment Not Fitted to MSN 7707


< To prevent leakage from PBE neck seal > Essex SB 001 R1 dated 10-03-91 - Applies to ESSEX PBE's manufactured between Mar89 and May 89. PBE's



< To prevent explosions of galley water heaters and coffee makers > Nordskog SB 93-34 - Applicable to Nordskog P/N SS-2C4-65 PER Nordscog SB 93-34(PN: SS-2C4-65)



< To prevent failure of the PBE due to deteriorated neck seal > Applicable to Puritan Bennett PN 119003 and 11903-01 IAW SB 119003-35-1 dated 02-15-93 - SB 119003-35-1



< To prevent collisions or near misses due to incompatibility TCAS II processors and ATC > Modify TCAS II processor IAW SB Collins SB 'C',7,10 &16.

< To prevent the failure of the pin securing the mask shell to the face piece > Replace the face piece and mask shell securing screw IAW EROS MF 10-35-44 and -46Rev 1



< To prevent explosions of galley water heaters and coffee makers > Inspect for galley heaters for affected PN per Nordskog SB 93-35 (P/N SS-2C4-65)



< Crew Oxygen Masks > Inspect IAW Puritan Bennet SB 174250-35-1 N/A - Affected Equipment Not Fitted to MSN 7707


< To prevent smoke, fire and possible electrical shock or electromagnetic interference > Inspect cabin fluorescent lighting system IAW Aerospace Lighting IB 90-001



< To prevent restricted O2 flow to passengers > Applicable to Nellcor P/N 174290-35-1



< To prevent Failure of the ultrasonic weld on the cone & seal assembly > Applicable to P/N 210543 & 210543-01 Manufactured or repaired from Aug 1996 thru July 1997



< To prevent fire extinguisher failure due to leakage > Inspect First Technology Fire & Safety IAW SB 26-110 R1



Appliance AD StatusAppliance AD Status

of 158




US FAA AD Canadian AD Description Last Accomplishment Date(TSN / CSN)



99-08-21 N/A

99-23-22R2 N/A N/A - AD Rescinded Closed - AD Rescinded

2000-07-27 N/A

2001-15-17 N/A

2001-22-14 N/A

2002-06-05 N/A

2002-06-06 N/A

2002-13-07 N/A

2002-14-19 N/A

2002-20-09 N/A

2002-21-01 N/A < OHG water boilers, coffee and beverage makers >

2002-22-12 N/A

2002-22-13 N/A

2003-26-14 N/A

< To prevent reduced O2 consumption due to defective O2 masks > Inspect the passenger and portable O2 masks for any tears IAW Puritan Bennet SB C351-2000-35



< Prevent false TCAS advisories > Perform the test procedures specified in paragraphs (a)( 1) through (a) (9) of this AD.

Air data inertial reference unit (ADIRU) > Applicable IAW Honeywell ASB: HG2050AC-34-A0008, HG2030AD-34-A0009



< Collins CTL-92 Transponder control panel > Inspect IAW Rockwell Collins Service Bulletin 33



< Extinguishing system bottles cartridges > Inspect / Repair OAS Service Bulletin 22-09-97



< Aircraft with Rockwell Collins Mode "C" 621A-3 ATC Transponders > Perform pulse width test to detect malfunctions of any Mode "C" 621A-3 transponders P/N 522-2703-XXX IAW Rockwell Collins O/H Manual TR 34-44-00-38.



< Aircraft with Rockwell Collins TDR-94 and TDR-94D Mode S Transponders > Modify TDR-94 transponders from P/N 622-9352-004 to P/N 622-9352-005 or -006 and modify TDR94D transponders from P/N 622-9210-004 to P/N 622-9210-005 or -006 IAW Rockwell Collins SB 17 or SB 20



< Aircraft with Honeywell P/N HG1075AB05 & HG1075GB05 Inertial Reference Units > Do not install IRU's unless modified by Honeywell Inc. to Mod 6 or Mod 7. For P/N HG1075GB05 - S/N's ending in 0652 or 0659 with Mod 2 (N/A if Mod 6 incorporated).



< Aircraft with Rockwell Collins ADC-85, ADC-85A, ADC-850D & ADC-850F ADC's > Replace or modify affected ADC IAW Rockwell Collins SB 62.



< Aircraft with Rockwell Collins AFD-3010 Adaptive Flight Display Units > inspect and/or modify affected AFD-3010 units IAW Rockwell Collins SB 12.





< Titeflex Corporation hose fire sleeve > Inspect and/or replace affected hoses IAW SB 73-2. on Bombardier CL-600-1A11 A/C



< Aircraft with Rockwell Collins FMC-4200, FMC-5000 and FMC-6000 Flight Management Computers > Remove affected FMC units and install a modified or new FMC unit as specified in paragraph (e) of the AD



< Kidde Portable Fire Extinguishers > Inspect IAW Kidde Aerospace Service Bulletin 898052-26-449 (P/N 898052)



of 158




US FAA AD Canadian AD Description Last Accomplishment Date(TSN / CSN)



2005-23-11 N/A

2007-07-12 N/A

< Remove compressor impeller assemblies from service > Applicable to Honeywell / Sundstrand



< Navigation Systems > In-flight unannunciated shifts of computed position in airplanes with the subject flight management system (FMS) computers identified in HONEYWELL NEWSLETTER A23-6111-008



of 158



SB No. AD SB Title Effectivity Issue Date Last Done by Date TSN CSN Interval Next Due Status

601R-11-071A 7003-7067,7069-7319 3-May-99 NA by Aircraft serial Number NA NA NA NA NA

601R-11-077B 14-Jun-04 NA by Aircraft serial Number NA NA NA NA NA

601R-21-015D 7003-7051,7069 10-Sep-96 NA by Aircraft serial Number NA NA NA NA NA

601R-21-017A 27-Jun-95 NA by Aircraft serial Number NA NA NA NA NA

601R-21-053A 7003-7067,7069-7477 28-Jan-03 NA by Aircraft serial Number NA NA NA NA NA

601R-21-054C 7003-7067,7069-7491 7-Jul-05 Chautauqua Airlines 11/23/2008 14645 12417 4000 FH 18645

601R-22-006A 7003-7032 26-Jul-94 NA by Aircraft serial Number NA NA NA NA NA

601R-24-015A 7003-7028 1-Dec-93 NA by Aircraft serial Number NA NA NA NA NA


601R-24-019A 7003-7040 9-Aug-94 NA by Aircraft serial Number NA NA NA NA NA

601R-24-040 7003-7060 10-Mar-95 NA by Aircraft serial Number NA NA NA NA NA

601R-24-048A 21-Mar-97 NA by Aircraft serial Number NA NA NA NA NA


601R-24-079 7042 20-Mar-97 NA by Aircraft serial Number NA NA NA NA NA

601R-24-081B 7281-7284 19-Dec-07 NA by Aircraft serial Number NA NA NA NA NA

601R-24-085E 7003-7250,7274-7325 3-Mar-99 NA by Aircraft serial Number NA NA NA NA NA

601R-24-090A 7003-7067,7069-7294 23-Aug-99 NA by Aircraft serial Number NA NA NA NA NA

601R-24-091D 7003-7067,7069-7269 1-Feb-05 NA by Aircraft serial Number NA NA NA NA NA

601R-24-092 7003-7067,7069-7304 25-Nov-99 NA by Aircraft serial Number NA NA NA NA NA

Placards and Markings - Flight Compartment - Airspeed Limitation Placard (Reduced Maximum Flap Extended Speed VFE ) Installatio

NOT APPLICABLE

2003-04-21CF-2002-12

Placards And Markings - Passenger Compartment - Installation Of New Overwing Emergency Exit Placards

7003-7074,7076-7098,7100-7135,7137-7139,7141-7151,7153-7175,7177-7350,7352-7434,7436-7442,7444-7452,7454-

7458,7460-7497,7499-7504

NOT APPLICABLE

Air Conditioning - Distribution - Replacement of Environmental Control System (ECS) Supply Duct Assembly

NOT APPLICABLE

Air Conditioning - Flight Compartment Distribution - Air Conditioning Check Valve Inspection

7032-7033,7036,7052,7059-7060

NOT APPLICABLE

2004-22-08CF-2003-05R1

Air Conditioning - Air Distribution - Rework Or Installation Of New Air Supply Ducts

NOT APPLICABLE

2004-22-08CF-2003-05R1

Air Conditioning - Bulkhead Check Valve -Visual Inspection of Bulkhead Check Valves

OPENREPETITIVE

Auto Flight - Autopilot Servo Clutch - Torque Settings Revision

NOT APPLICABLE

Electrical Power - Integrated Drive Generator (IDG) - Oil Level Check and Modification

NOT APPLICABLE

Electrical Power - Integrated Drive Generator (IDG) - Installation of a New Bearing Retainer and New Input Shaft Bearings in Co

NOT APPLICABLE

Electrical Power - Air Driven Generator - Special Inspection/Rectification of Uplock Assembly Pin

NOT APPLICABLE

Electrical Power - Ac Electrical Load Distribution System Harness Installation - Chafing Damage

NOT APPLICABLE

Electrical Power - Wiring Harnesses - Inspection and Rectification of Electrical Harnesses for P16 and P17

7004-7010,7015-7016,7019,7021,7023,7025,

7032-7033,7036,7039

NOT APPLICABLE

Electrical Power - General - Replacement of the P181 Connector and Backshell in the MLG Wheel Well

NOT APPLICABLE

Electrical Power - Alternator - General Drive - Special Inspection Of The Air Driven Generator (ADG)

NOT APPLICABLE

Electrical Power - DC Generation - Transformer Rectifier Unit (TRU) Fan Inspection

NOT APPLICABLE

99-21-11CF-98-40

Electrical Power - Battery System - Inspection of the Main and APU Battery Charger Input Connectors Wires

NOT APPLICABLE

Electrical Power - General - Addition of 50 Amp Circuit Breaker to Protect the Main and APU Battery Charger Output Feed Wire

NOT APPLICABLE

Electrical Power - IDG Cables And Fire Wall Separator - Installation Of Teflon Tubing And Teflon Strips

NOT APPLICABLE

Electrical Power -Emergency AC Generation System - Inspection And Lubrication Of The Air Driven Generator ADG Pivot Joint

NOT APPLICABLE

Alert Service Bulletin StatusAlert Service Bulletin Status

of 158


601R-24-095A 7003-7067,7069-7301 25-Mar-99 NA by Aircraft serial Number NA NA NA NA NA

601R-24-098A 7035-7438 9-May-01 NA by Aircraft serial Number NA NA NA NA NA

601R-24-103B 7003-7067,7069-7462 13-Jun-08 NA by Aircraft serial Number NA NA NA NA NA

601R-24-105A 20-Jul-01 NA by Aircraft serial Number NA NA NA NA NA

601R-24-112 7848,7851,7853-7856 24-Dec-03 N/A by Aircraft Serial number NA NA NA NA NA

601R-24-120B 7305-7990, 8000-8051 7-Dec-06 Comair 4-Mar-06 9342.18 8113 NA NA CLOSED

601R-24-121 4-Apr-07 Comair 6-Apr-06 9517 8264 NA NA CLOSED

601R-25-152A 7003-7067,7069-7292 25-Feb-99 NA by Aircraft serial Number NA NA NA NA NA

601R-25-177 7-Jul-03 N/A by Aircraft Serial number NA NA NA NA NA

601R-25-193 See SB for P/N's affected 26-May-05 NA NA NA NA NA

601R-26-003C 7004-7024 14-Dec-94 NA by Aircraft serial Number NA NA NA NA NA

601R-26-008 7004-7029 18-Dec-95 NA by Aircraft serial Number NA NA NA NA NA

Electrical Power -Electrical Harnesses - IDG Inspection For Clearance And Chafing (Right Hand Side Engine Only)

NOT APPLICABLE

Electrical Power - Dry Air Driven Generator - Inspection Of The Turbine Lock Pin And Of The Downlock Pin Assembly And Replaceme

NOT APPLICABLE

2001-06-07CF-2001-02

Electrical Power - IDG - Inspect The IDG Cable Harness Assembly From The IDG To The Service Pylon For Damage/Chafing

NOT APPLICABLE

2002-16-14CF-2001-27

Electrical Power - AC Electrical Load Distribution - Replacement Of Leach 'H' Series Relays H-A4A-039

7003-7067,7069-7495,7497-7502,7505-7507

NOT APPLICABLE

Electrical Power - Integrated Drive Generator (IDG) - Inspection Of The Integrated Drive Generators (IDG)

NOT APPLICABLE

Electrical Power System - Emergency AC Power Generation System - Special Detailed Inspection of the Air Driven Generator (ADG)

2006-09-08CF-2006-07

Electrical Power - Electrical Power System - Wire Location Change on the AC Service Bus Contactor K4XA

7003-7067,7069-7990,8000-8066

Equipment/Furnishings - Passenger Compartment Equipment - Removal Of the Fiberglass/Foam Insulation Surrounding the Overwing Em

NOT APPLICABLE

Equipment/Furnishings - Cargo Compartment - Installation Of Grommets (P/N B303502-1) On The Cargo Post Caps

7003 thru 7010, 7015, 7016, 7019 thru 7021, 7023

thru 7025, 7032, 7033, 7036, 7039, 7041, 7045, 7047,

7049, 7051 thru 7054, 7057 thru 7061, 7063 thru 7065, 7071, 7073, 7074, 7078,

7081 thru 7084, 7086, 7087, 7089, 7090, 7093, 7095 thru 7098, 7104, 7107, 7112 thru

7115, 7118 thru 7122,7124 thru 7126, 7128, 7130, 7135, 7144, 7153 thru 7155,

7160, 7161, 7164, 7165, 7177, 7182 thru 7184, 7197,

7198, 7200, 7201,7206, 7209, 7220, 7223, 7224, 7227, 7249, 7252, 7266, 7282, 7298, 7309, 7316, 7323, 7332, 7378, 7391, 7394, 7403, 7407, 7413, 7419, 7431, 7439, 7449,7464, 7478, 7486, 7494, 7499, 7567, 7570, 7573, 7583, 7607, 7619, 7625,

7629, 7630, 7738 and subsequent which have the

option CR25-01

NOT APPLICABLE

Equipment and Furnishings - Passenger Seats - Replacement of the Lock Quadrants P/N 122488-01 and P/N 122488-02

N/A by S/N not installed - Replaced by Weber Seats

NOT APPLICABLE

Fire Protection - Detection - Installation of New Brackets and Clamps for the Zone A Fire Detector Harness and Shortening of th

NOT APPLICABLE

Fire Protection - Fire Extinguishing System - Inspection Tube Assembly Replacement

NOT APPLICABLE

of 158


601R-26-017D 7003-7067,7069-7545 6-Nov-03 NA by Aircraft serial Number NA NA NA NA NA

601R-26-019B 7003-7067,7069-7438 20-Jan-05 NA by Aircraft serial Number NA NA NA NA NA

601R-27-004A 7003-7076 28-Mar-97 NA by Aircraft serial Number NA NA NA NA NA

601R-27-011A 7004-7019,7021-7023 21-Sep-93 NA by Aircraft serial Number NA NA NA NA NA

601R-27-039B 7003-7042 1-Dec-94 NA by Aircraft serial Number NA NA NA NA NA

601R-27-041 Flight Controls - Elevator - Flutter Damper Removal 7003-7049 28-Oct-94 NA by Aircraft serial Number NA NA NA NA NA

601R-27-054 7003-7070,7075 12-Jun-95 NA by Aircraft serial Number NA NA NA NA NA

601R-27-058A 7003-7079 8-Sep-95 NA by Aircraft serial Number NA NA NA NA NA

601R-27-062 7013 6-Sep-96 NA by Aircraft serial Number NA NA NA NA NA

601R-27-067E 7003-7134 23-Aug-96 NA by Aircraft serial Number NA NA NA NA NA

601R-27-074 7003-7140 10-Oct-01 NA by Aircraft serial Number NA NA NA NA NA


601R-27-092D 28-Jul-05 NA NA NA NA NA CLOSED


601R-27-101B 7003-7067,7069-7351 2-Feb-05 NA by Aircraft serial Number NA NA NA NA NA

601R-27-124 17-Jul-02 NA by Aircraft serial Number NA NA NA NA NA

601R-27-128B 7003-8999 Chautauqua Airlines 18-Jun-09 15679 13228 5000 20679

601R-27-129A 7003-7067,7069-7999 9-Sep-03 NA NA OPEN

601R-27-130C 7003-7067,7069-8999 ExelTech Aerospace 26-May-09 15676 13226 1000 FH 16676

601R-27-133A 7003-7067,7069-7947 Comair 11-Dec-06 10698 9422 NA NA CLOSED

601R-27-144C 8-Jun-09 15676 13226 100 FH 15776

601R-27-152 12-May-08 NA NA OPEN

601R-28-036A 7003-7067,7069-7246 4-Sep-98 NA by Aircraft serial Number NA NA NA NA NA

601R-28-042B 7003-7067,7069-7295 18-Nov-04 NA by Aircraft serial Number NA NA NA NA NA

601R-28-045B 21-Dec-01 NA by Aircraft serial Number NA NA NA NA NA

2006-10-01CF-2000-35R1

Fire Protection - Control Unit System - Installation Of Protective Tape To Prevent Fluid Ingress

NOT APPLICABLE

Fire Protection - Overheat Detection System - Inspection Of The Fire Loop Detection And The Electrical Wires In The Pylon Area

NOT APPLICABLE

Flight Controls - Flaps - Special Inspection Of Flap Actuator And Rectification

NOT APPLICABLE

Flight Controls - Rudder Control Quadrant - Special Inspection

NOT APPLICABLE

Flight Controls - Stall Protection System Special Inspection and Rectification Stick Pusher Quadrant Rivets

NOT APPLICABLE

NOT APPLICABLE

Flight Controls - De-Activation Of The MACH TRIM ENGAGE/DISENGAGE Switch/Light

NOT APPLICABLE

Flight Controls - Ailerons - Special Inspection and Flutter Damper AssemblyRemoval

NOT APPLICABLE

Flight Controls - Aileron Power - Control System - Inspection Of the PCU Link Hardware Replacement Of the Aileron Bushings

NOT APPLICABLE

Flight Controls - Flaps - Inboard and Outboard Flap Actuators - Change of Lubricant Mix Ratio

NOT APPLICABLE

Flight Controls - Elevator- Inspection Of The Control Column Bearings

NOT APPLICABLE

Flight Controls - Stall Protection System - Special Inspection and Rectification of the Stick Shaker Connector P5CG and P6CG

NOT APPLICABLE

Flight Controls - Spoilers - Inspection and Test of the Flight Spoiler and Spoileron Power Control Units (PCUs) Autostow Circui

7003-7067,7069-7990,8000-8999

TC 000-27-900-149 (5000FH) covers requirements of this SB

Flight Controls - Flap Control Surface System - Inspection and Rework of the Outboard Flaps Alignment Fitting Assembly and Adja

NOT APPLICABLE

Flight Controls - Spoiler System - Addition Of Standoffs And Harness Clamps on Both Sides Of The Wing Root To Support Harnesses

NOT APPLICABLE

Flight Controls - Flap Control System - Inspection And Replacement Of The Ballnut Trunnion Bolts Of The Inboard Actuators 601r9

7590, 7592, 7597, and 7616.

NOT APPLICABLE

2005-10-10CF-2005-04

Flight Controls - Horizontal Stabilizer Trim-Actuating System - Inspection Of The Secondary Load Path Indicator

OPENREPETITIVE

Flight Controls - Aileron Control System - Inspection of the Aileron Wing Pulleys

2005-03-13CF-2004-13

Flight Controls - Inspection of the Aileron Power Control Unit (PCU) Links

OPENREPETITIVE

2005-18-04CF-2003-14R1

Flight Controls - Spoiler System - Installation of a Feedthru Angle and a Feedthru Plate on the Two Sides of the Wing Root

2008-08-09CF-2005-41

Flight Controls - Pitch Feel Simulator - Functional Test of the Pilot Input Lever of the Pitch-Feel Simulator (PFS) P/N 601R923

7003-7067,7069-7990,8000-8999

ExelTech Aerospace OPENREPETITIVE

Flight Controls - Pitch Trim Switch - Lubrication of Pitch Trim Switch P/N 309-4334

7003-7067,7069-7990,8001-8999

Fuel System - Fuel Tanks System - Examination of the Electrical Conduits in the Center Wing Tank

NOT APPLICABLE

Fuel System - Fuel Tank System - Inspection Of Fuel-Level Sensor Wires In The Center Fuel Tank

NOT APPLICABLE

2001-26-51CF-2001-47

Fuel - Fuel Transfer Shutoff Valve - Isolate The Circuit Breaker Of The Fuel Transfer Shutoff Valve (P/N 601R62256-5) To Remov

7003-7574,7577-7578,7580-7587,7589,7591

NOT APPLICABLE

of 158


601R-28-064C 7003-7067,7069-7988 19-Apr-06 N/A by P/N installed NA NA NA NA NA


601R-29-017B 7003-7112 1-Aug-97 NA by Aircraft serial Number NA NA NA NA NA

18-Oct-07 NA NA OPEN

18-Oct-07 1500 FC 1500

23-Dec-08 NA NA OPEN

23-Dec-08 NA NA OPEN

601R-29-031 23-Dec-08 OPEN

601R-30-005A 7004-7006,7008-7010 31-Mar-93 NA by Aircraft serial Number NA NA NA NA NA


601R-30-026A 7003-7067,7069-7323 3-May-01 NA by Aircraft serial Number NA NA NA NA NA

601R-30-032 18-Sep-08 Comair CLOSED

601R-31-006 7003-7031,7033-7035 19-Mar-94 NA by Aircraft serial Number NA NA NA NA NA

601R-32-010 7004-7006,7008-7010 13-Mar-93 NA by Aircraft serial Number NA NA NA NA NA

601R-32-022B 7003-7042 18-May-94 NA by Aircraft serial Number NA NA NA NA NA


601R-32-038 7003-7050 18-Nov-94 NA by Aircraft serial Number NA NA NA NA NA




601R-32-053B 7003-7109 21-Apr-97 NA by Aircraft serial Number NA NA NA NA NA

601R-32-057 7003-7107 9-Oct-96 NA by Aircraft serial Number NA NA NA NA NA

601R-32-060 7003-7110 9-May-96 NA by Aircraft serial Number NA NA NA NA NA

601R-32-062C 7003-7990 18-Sep-96 Superseded by A601R-32-065 NA NA NA NA NA

2006-02-10CF-2005-18

Fuel System - Refuel/Defuel Shut Off Valve (SOV) - Installation of a New Gask-O-Seal in the Coupling of the Refuel/Defuel SOVs

NOT APPLICABLE

Hydraulic Power - Special Inspection and Rectification of the Engine Driven Hydraulic Pump Hose, Engine Fuel Feed and Flow Tube

NOT APPLICABLE

Hydraulic Power - Hydraulic System No.1 - Hydraulic Tube Assemblies Replacement and Bracket Re-Work

NOT APPLICABLE

601R-29-029 Part A

Hydraulic Power - Hydraulic System No.1 and No.2 - Inspection of the Accumulator Screw-Caps

7003-7067,7069-7990,8000-8999

601R-29-029 Part B

Hydraulic Power - Hydraulic System No.1 and No.2 - Inspection of the Accumulator Screw-Caps

7003-7067,7069-7990,8000-8999

OPENREPETITIVE

601R-29-030B Part A

Hydraulic Power - Hydraulic System No.3 - Inspection of the System Accumulator Screw-Caps

7003-7067,7069-7990,8000-8999

601R-29-030B Part B

Hydraulic Power - Hydraulic System No.3 - Inspection of the System Accumulator Screw-Caps

7003-7067,7069-7990,8000-8999

Hydraulic Power - Hydraulic System No. 3- Deactivation and Removal of the Accumulator Assembly

7003-7067,7069-7990,8000-8999

Ice and Rain Protection - Air Intake - Special Inspection/Replacement of the Cowl Anti-Ice Valve

NOT APPLICABLE

Ice and Rain Protection - Wing anti-Ice Duct System - Wing Anti-Ice Boot Cover Inspection

NOT APPLICABLE

Ice and Rain Protection - Bleed Air Leak Detection System - Inspection Of The Bleed Leak Detector/Boot Coupling Orientation

NOT APPLICABLE

2008-23-16CF-2008-30

Ice and Rain Protection - Wing Anti-Ice System - Inspection of the Wing Anti-Ice Wing Ducts (Piccolo Tubes)

7003-7067,7069-7990,8000-8076,8082,8086,8090-

8092,8096-8097 6/5/2006 9834 8569

Indicating/Recording Systems - Electronic Flight Display (EFD) System - Terminal Block Contact Inspection

NOT APPLICABLE

Landing Gear - Wheels and Brakes - Temporary Deactivation of Hydraulic Antispin System

NOT APPLICABLE

Landing Gear - Main Gear Doors - Special Inspection and Replacement of the Stay Pin and Bellcrank

NOT APPLICABLE

Landing Gear - Nose Landing Gear and Door - Nose Landing Gear Spring Bungee Replacement

NOT APPLICABLE

Landing Gear - Wheels and Brakes - Brake Inspection And Replacement

NOT APPLICABLE

Landing Gear - Nose Landing Gear - Nose Landing Gear Uplock Pin Replacement

NOT APPLICABLE

Landing Gear - Nose Landing Gear - Position and Warning - Microswitch Adjustment

NOT APPLICABLE

Landing Gear - Nose Landing Gear - Extension and Retraction - Uplock Pin Inspection

NOT APPLICABLE

Landing Gear - Extension and Retraction - Inspection And Repair Of The MLG Extension/Retraction Side Stay Actuator

NOT APPLICABLE

Landing Gear - Main Landing Gear - Inspection of the MLG Upper Brake Swivel and Integral Hydraulic Line for Damage

NOT APPLICABLE

Landing Gear - Main Landing Gear - Brake and Wheel Inspection

NOT APPLICABLE

98-16-25CF-96-12R1

Landing Gear - Main Landing Gear System - MLG Shock Strut Ends - Attachment Fitting - Inspection and Replacement

NOT APPLICABLE

of 158


601R-32-065 7003-7157 11-Nov-96 NA by Aircraft serial Number NA NA NA NA NA

601R-32-067C 7003-7067,7069-7337 23-Feb-01 NA by Aircraft serial Number NA NA NA NA NA


601R-32-073 11-Nov-98 NA by Aircraft serial Number NA NA NA NA NA

601R-32-074A 7003-7067,7069-7999 4-Feb-00 NA NA NA NA NA

601R-32-075B 7003-7067,7069-7230 4-Feb-00 NA by Aircraft serial Number NA NA NA NA NA

601R-32-079F 20-Jun-05 N/A by P/N installed NA NA NA NA NA

601R-32-083 7375-7438,7440-7451 26-Dec-00 NA by Aircraft serial Number NA NA NA NA NA

601R-32-085 7529,7533,7537,7540 20-Nov-01 NA by Aircraft serial Number NA NA NA NA NA

601R-32-086C 7003-7067,7069-7999 16-Jun-04 NA by Main Fitting P/N NA NA NA NA NA

601R-32-088A 18-Dec-06 Main fittings Need Changed NA NA NA NA NA OPEN

601R-32-091 7003-7067,7069-7850 28-Jul-03 N/A by P/N installed NA NA NA NA NA

601R-32-099B 16-Jun-05 N/A by P/N installed NA NA NA NA NA

18-Oct-07 N/A NA OPEN

18-Oct-07 1500 FC 1500

601R-33-020A 10-Jun-96 NA by Aircraft serial Number NA NA NA NA NA

601R-34-028B 7003-7026 16-Mar-94 NA by Aircraft serial Number NA NA NA NA NA

601R-34-050A 7032,7052,7059 10-Mar-95 NA by Aircraft serial Number NA NA NA NA NA

601R-34-121 8-Jun-00 NA by Aircraft serial Number NA NA NA NA NA

601R-34-130 7003-7516,7518-7519 30-Aug-01 N/A by Aircraft Serial number NA NA NA NA NA

Landing Gear - Main Landing Gear (MLG) System - MLG Shock Strut Ends - Attachment Fitting - Incorporation of a New Type Pin

NOT APPLICABLE

Landing Gear - Main Landing Gear (MLG) - Inspection/Replacement Of The Hinge Pin Cross-Bolt On The Trailing Arm

NOT APPLICABLE

Landing Gear - Main Landing Gear (MLG) System - MLG Shock Strut Joint Inspection and RH Shock Strut Replacement

NOT APPLICABLE

Main Landing Gear (MLG) System - MLG Trunnion Cross Pin Replacement

7075,7086,7154,7161-7171,7173-7174,7176-

7236,7238

NOT APPLICABLE

Landing Gear - Main Landing Gear- Visual Inspection Of The Main Landing Gear (MLG) Fitting

Alert SB. This service bulletin is superceded

by Alert Service Bulletin A601R-32-079 and

is no longer required.

NOT APPLICABLE

Landing Gear - Main Landing Gear (MLG) - Eddy Current Inspection Of The MLG Fitting

NOT APPLICABLE

2008-23-11CF-99-32R3

Landing Gear - Main Landing Gear (MLG) - Visual And Eddy Current Inspection Of The Mlg Main Fitting P/N 601r85001-3/-4 (Mdi P/N

7003-7067,7069-7857,7859,7861-7866

NOT APPLICABLE

Landing Gear - Landing Gear Control Panel - Replacement of the Landing Gear Control Handle Assembly

NOT APPLICABLE

Landing Gear - Nose Landing Gear - Replacement Of The Nose Landing Gear (NLG) Piston/Axle Assembly

NOT APPLICABLE

Landing Gear - Main Landing Gear (MLG) - Inspections Of The Main Fitting Assembly Of The MLGs

NOT APPLICABLE

2004-14-16CF-2003-09R1

Landing Gear - Main Landing Gear (MLG) - Visual, Eddy Current and Fluorescent Penetrant Inspections of the MLG Main Fitting P/N

7003-7067,7069-7857,7859,7861-7866

Landing Gear - Wheels And Brakes - Goodyear Tire Inspection (P/N 299k63-1)

NOT APPLICABLE

2007-01-07CF-2004-18R1

Landing Gear - Main Landing Gear (MLG) - Inspection of the Main Fitting Assembly of the MLG

7003-7067,7069-7857,7859,7861-7866

NOT APPLICABLE

601R-32-103B Part A

Inspection of the Accumulator Screw-Caps (P/N 08-60163-001, 08-60163-002)

7003-7067,7069-7990,8000-8999

601R-32-103B Part B

Inspection of the Accumulator Screw-Caps (P/N 08-60163-001, 08-60163-002)

7003-7067,7069-7990,8000-8999

OPENREPETITIVE

Lights - Passenger Compartment - Inspection and Replacement of The Fluorescent Lighting-Tube Holders (Sidewall And Galley Ceil

7003-7007,7009-7074,7076-7089,7091-7092

NOT APPLICABLE

Navigation - Attitude and Heading Reference System - Wiring Changes (AHRS)

NOT APPLICABLE

Navigation - Heads Up Guidance System (HUGS) Wiring Changes At Electrical Connector P129

NOT APPLICABLE

Navigation - Attitude and Heading - Installation of Caution Plates 601R720803-2005 and 601R720803-2007 Below the AHC Mounting T

CL-600-2B19 Canadair Regional Jet (CRJ) Aircraft

SerialNumbers 7003 thru 7067,

7069 thru 7268 which have the

AHRS system installed (Option TS34-002 or TS34-

320).

NOT APPLICABLE

Navigation - Electronic Flight Display (EFD) - Inspection/Replacement of the EFD-4076 (622-9810-016/202)

NOT APPLICABLE

of 158



601R-35-014 25-Sep-03 NA by Aircraft serial Number NA NA NA NA NA

601R-36-014A 7003-7067,7069-7999 25-Aug-00 This service bulletin is no longer required

601R-38-013C 7003-7063 12-Apr-95 NA by Aircraft serial Number NA NA NA NA NA


601R-38-038C 7003-7127 25-Nov-96 NA by Aircraft serial Number NA NA NA NA NA

601R-49-020 7754-7823 26-Aug-03 NA by Aircraft serial Number NA NA NA NA NA

601R-52-002C 7004-7990 1-Dec-93 ExelTech Aerospace 28-May-09 15676.6 13226

601R-52-008B 7004-7006,7008-7010 1-Dec-93 NA by Aircraft serial Number NA NA NA NA NA

601R-52-021B 7003-7990 9-Aug-94 ExelTech Aerospace 28-May-09 15676.6 13226

601R-52-065A 7003-7083 28-Mar-97 NA by Aircraft serial Number NA NA NA NA NA

601R-52-071A 7003-7184 23-Sep-96 NA by Aircraft serial Number NA NA NA NA NA

601R-52-073 7003-7169 27-Jun-96 NA by Aircraft serial Number NA NA NA NA NA

601R-52-096 9-Dec-97 NA by Aircraft serial Number NA NA NA NA NA

601R-52-097 7003-7015 21-Apr-98 NA by Aircraft serial Number NA NA NA NA NA

601R-52-105C 6-Jan-05 NA by Aircraft serial Number NA NA NA NA NA

601R-52-108A 3-Mar-05 NA by Aircraft serial Number NA NA NA NA NA


601R-53-017B 7003-7107 28-Feb-96 NA by Aircraft serial Number NA NA NA NA NA

601R-53-027C 7003-7005,7008-7025 20-Oct-00 NA by Aircraft serial Number NA NA NA NA NA

601R-53-033B 7030-7075 4-Nov-97 NA by Aircraft serial Number NA NA NA NA NA

601R-53-045D 7003-7185 22-Dec-97 NA by Aircraft serial Number NA NA NA NA NA

601R-53-059F 7003-7067,7069-7909 21-Apr-06 ExelTech Aerospace 25-May-09 15676 13226 1100 FC 16776

601R-54-002 7003-7048 10-Feb-95 NA by Aircraft serial Number NA NA NA NA NA

601R-57-002B 7003-7044 10-Jan-97 NA by Aircraft serial Number NA NA NA NA NA

Oxygen - General - Replacement Of The Chemical Oxygen Generator

7782,7786,7790-7792,7794-7795

NOT APPLICABLE

Oxygen - Passenger Oxygen System - Inspection Of The Release Pin Of The Oxygen Generators

7673-7683,7685-7689,7691-7696,7698-7703,7705-7784

NOT APPLICABLE

Pneumatic - Bleed Air Leak Detection System - Inspection Of The Engine Pylon 14th Stage Sensing Element

NOT APPLICABLE

Water/Waste - Potable Water Service - Installation of a New Dust Cap, Placards and the Application of Sealant

NOT APPLICABLE

Water/Waste - Potable Water - Correction of Galley Control Cable Fouling

7004-7019,7021-7035,7037-7052,7054-7056,7058-7069,7071-7074,7077-

7080,7082-7083,7087,7089-7098,7100-7127

NOT APPLICABLE

Water/Waste - Galley and Lavatory Water System - De-Activation of the Potable Water System Composite Tank Heaters

NOT APPLICABLE

Airborne Auxiliary Power - Auxiliary Power Unit - Engine Fuel And Control - Inspection Of The Fuel Solenoid Shut Off Valve

NOT APPLICABLE

95-04-05CF-93-02R1

Doors - Passenger/Service/Overwing Emergency Exits - Application of Anti-Icing Compound, Dry Lubrication to Seals and Lubricati

OPENREPETITIVE

Doors - Passenger/Crew - Isolation of the Passenger Door Pull-Out Handle

NOT APPLICABLE

95-04-05CF-93-02R1

Doors - Passenger Door - Outer Handle Freezing Protection

OPENREPETITIVE

Doors - Passenger Door - Inspection of the Passenger Door Seal Installation of Vent Holes as Required

NOT APPLICABLE

Doors - Passenger Door - Inspection of the Handrail Hinge Shield Rework/Replacement of the Handrail Hinge Shield

NOT APPLICABLE

Doors - Passenger Door - Rework of the Inner-Handle Roller-Spring Mechanism

NOT APPLICABLE

Doors - Service Door Inspection and Repair of Service-Door Lifting-Device Housing

7003-7074,7076-7098,7100-7125,7127

NOT APPLICABLE

Doors - Exit, Overwing Emergency - Inspection/Replacement of the Stop Fittings

NOT APPLICABLE

Doors - Passenger Door - Latch Box Inspection And / Or Repair

7390,7396,7409,7412,7416,7423,7432,7444,7452,7455,

7457-7528

NOT APPLICABLE

Doors - Passenger Door - Outer Handle Detent Spring Replacement

7469-7480,7482-7555,7557-7558,7561,7571

NOT APPLICABLE

Fuselage - Forward Fuselage - Special Inspection and Repair of Nose Landing Gear Wheel Well

NOT APPLICABLE

Fuselage - Main Landing Gear Wheel Bin - Special Inspection, Repair of Main Landing Gear Wheel Bin Flange

NOT APPLICABLE

Fuselage - Fuselage Main Structure - Inspection and Repair of the NLG Aft Door Surround Structure

NOT APPLICABLE

Fuselage - General - Inspection of the Channels Under the Vertical Stabilizer Cruciform-Fitting

NOT APPLICABLE

Fuselage - General - Repair of the Underfloor Pressure Bulkhead at FS409+128

NOT APPLICABLE

2004-10-03CF-2001-26R1

Fuselage - Fuselage General - Visual Inspection And Modification Of The Engine Support Beam

OPENREPETITIVE

Nacelle / Pylons - Pylon Main Structure - Inspection of Loose Fasteners

NOT APPLICABLE

Wings - Spoileron Shroud - Special Inspection of Structure for Cracking

NOT APPLICABLE

of 158


601R-57-027C 7003-7067,7069-7340 30-May-00 NA by Aircraft serial Number NA NA NA NA NA

601R-57-028C 2-May-07 NA by Aircraft serial Number NA NA NA NA NA

601R-57-031C 7003-7067,7069-7869 22-Jul-03 Chautauqua Airlines 6-Jan-09 14907 12606 5000 FC 17606

601R-57-035A 30-Apr-02 NA NA NA NA NA

601R-57-039B 7012,7014,7139,7680 12-May-03 NA by Aircraft serial Number NA NA NA NA NA

601R-71-002C 7004-7042 29-Jun-94 NA by Aircraft serial Number NA NA NA NA NA

601R-71-010C 7003-7122 21-Nov-96 NA by Aircraft serial Number NA NA NA NA NA

601R-71-015 7003-7018,7021,7023-7024 31-Jan-96 NA by Aircraft serial Number NA NA NA NA NA

601R-73-008A 7003-7067,7069-7303 10-Apr-99 NA by Aircraft serial Number NA NA NA NA NA

601R-76-012B 20-Feb-98 NA by Aircraft serial Number NA NA NA NA NA

601R-76-013C 7003-7067,7069-7999 15-Oct-01 NA NA NA NA NA

601R-76-017A 7003-7100 15-Feb-01 NA by Aircraft serial Number NA NA NA NA NA

601R-78-001 7004 19-Nov-92 NA by Aircraft serial Number NA NA NA NA NA

601R-78-012 7080-7104 1-Feb-96 NA by Aircraft serial Number NA NA NA NA NA


601R-78-020A 22-Dec-05 NA by Aircraft serial Number NA NA NA NA NA

Wings - Spoilers - Inspection of the LH and RH Flight Spoilers Actuator Lugs of the Center Hinge Fittings at Spoiler Station 19

NOT APPLICABLE

Wings - Structure - Attachment Fittings - Visual Inspection And Replacement Of The Bushings In The Wing-To-Fuselage Attachment

7003-7011,7013,7015-7016,7018-7025,7027-7056,7058-7067,7069-7073,7075-7108,7110-7116,7118-7128,7130-7138,7140-7158,7160-

7167,7169-7679, 7681-7701

NOT APPLICABLE

2002-03-14CF-2001-15R1

Wings - Lower Wing Plank - Inspection Of The Left And Right Wing In The Area Of The Rear Spar And WS 148.019

OPENREPETITIVE

Wings - Auxiliary - Removal and Installation of the Shaft for the Main Landing Gear (MLG) Side Brace Fitting (601R10237-1)

7285-7289,7291,7296-7298,7302,7339,7396

This Service Bulletin has been superseded by Service Bulletin

601R-57-036 and this is not Alert SB.

NOT APPLICABLE

Wings - Structure - Attachment Fittings - Replacement Of The Forward Wing To Fuselage Attachment Fitting

NOT APPLICABLE

Power Plant - Cowling - Inspection and Repair of Core-Cowl Latches

NOT APPLICABLE

Power Plant - Mounts - Inspection and Replacement of Forward Engine Mounts Bolts and Nuts

NOT APPLICABLE

Cowling - Core Cowl Doors - Inspection of the Formers for Holes Drilled in Error - Replacement of Damaged Core Cowl Doors

NOT APPLICABLE

Engine Fuel and Control - Fuel Manifold - Inspection for Clearance and Chafing (Both Engines)

NOT APPLICABLE

Engine Controls - Power Controls - Modification of the Engine Throttle Quadrant

7003,7007,7011-7031,7033,7035,7038,7040,

7078,7081-7126

NOT APPLICABLE

Engine Controls - Power Controls - Engine Throttle Cable Moisture Ingress Rectification

This Alert Service Bulletin has been superceded by Service

Bulletin 601R-76-018 and this is not Alert SB.

NOT APPLICABLE

Engine - Throttles - Backlash Inspection and Replacement of the Throttle Control Gearbox P/N 2100140-003

NOT APPLICABLE

Exhaust - Thrust Reverser - Stow Switch Replacement

NOT APPLICABLE

Exhaust - Thrust Reverser - Thrust Reverser Pylon Tracks Inspection

NOT APPLICABLE

Exhaust - Thrust Reverser - Cycling to Ensure Satisfactory Performance

NOT APPLICABLE

Engine Exhaust - Pneumatic Drive Unit (PDU) - Replacement of the Pneumatic Drive Unit

7958,8005,8007-8008,8010,8014,8016,8028

NOT APPLICABLE

of 158



S/B Number Part FAA AD TCCA AD DESCRIPTION Accomplished by DFP Hours Cycles

117003-35-4 B/E Aerospace - Release Pin Inspection

35A573-SB-46-03 1-Feb-04 Comair Airlines EO 27-087 3536.00 3098

601R-11-080 2006-12-21 CF-98-14R4 27-Apr-07 ExelTech Aerospace SB 10698 9422

601R-11-090 2009-06-12 CF-2007-10R1

601R-24-041 26-Nov-02 Comair Airlines EO 24-044 10.00 21

601R-24-113 CHANGE WIRING OF ADG CONNECTOR 5-Aug-05 Comair Airlines EO 24-060 7938.00 6850

601R-24-118B 2006-10-06 CF-2005-35 4-Mar-09 ExelTech Aerospace EO AD061006 15273.00 12896

601R-24-122A 2008-05-13 CF-2006-17R1 22-Aug-06 Comair Airlines AD-2-24M0001 10239.00 8980

601R-24-123B 2008-05-13 CF-2006-17R1 21-Jun-09 Chautauqua Airlines EO024024 15679.00 13228

601R-25-164

601R-27-098 11/26/02 Comair Airlines EO 27-048 10 21

601R-27-116 2006-12-21 CF-98-14R4 27-Apr-07 ExelTech Aerospace SB 10698.00 9422

601R-27-147 2007-05-11 CF-2006-20R1 22-Aug-07 Chautauqua Airlines EO AD2007-05-11 11255.00 9838

601R-27-150 PART A 2009-06-12 CF-2007-10R1 4-Oct-07 Chautauqua Airlines 11569.00 10085

601R-27-150 PART B 2009-06-12 CF-2007-10R1

601R-27-150 PART C 2009-06-12 CF-2007-10R1

601R-27-153 2009-04-11 CF-2008-35 3-Jun-09 ExelTech Aerospace SB 15676 13226

601R-28-051 2008-03-19 CF-2007-17 2-Jun-09 ExelTech Aerospace SB 15676 13226

601R-29-025

601R-30-029 2008-23-16 CF-2008-30 5-Jun-06 Comair Airlines 9834.00 8569

601R-31-030F 2006-02-05 CF-2004-23R1 2-Dec-05 Comair Airlines SB-2-31M0001 8841.00 7636

601R-32-090 15-Nov-03 Comair Airlines EO 32-080 2893.00 2537

AccomplishmentDate

CRJ STALL SYSTEM: STICK SHAKER GROUND WIRE REMOVAL

Placards And Markings - Flight Compartment, Placards And Markings - Installation Of The New Airspeed Limitation Placard And Rem

Placards and Marking - Flight Compartment Placard - Installation of the Maximum Flap Operating Speed Placard

Electrical Power - Circuit Breaker Panels - Relocation Of The Spare Fuse Holder

Electrical Power - Junction Boxes - Inspection of the Date Code on the Leach TDH-Series Relays in the Junction Boxes JB-2, JB-3

Electrical power - Electrical Power System - Application of RTV Sealant on theTerminal Base Plate of Contactors 1K4XD, 2K4XD,

Electrical Power - Electrical Power System - Replacement of the Terminal Base Plate on Contactors 1K4XD, 2K4XD, and K4XA

Equipment and Furnishings - Emergency Locator Transmitter (ELT) - Change the Two Frequency Artex ELT to the Three Frequency Artex ELT

Flight Controls--- General --- Application of Witness Marks on the Outboard Flap for 8 and/or 20 Degree Position

Flight Controls - Flap Control System - Installation And Activation Of The Flaps Skew Detection System

Flight Controls - Horizontal Stabilizer Control System - Change the Horizontal Stabilizer Trim Control Unit (HSTCU)

Flight Controls - Flap Power Drive System - Inspection of the Flexible Drive-Shafts and Flap Actuators for Contamination

EO27077-1 EO 27077-2



Flight Controls --- Stall Protection System --- Inrush Current Test and Replacement of the Angle---of---Attack (AOA) Transducers P/N C16258AA and P/N 45150340

Fuel System - Collector Tank - Application Of Sealant On The Bolts Of The Collector Tanks

Hydraulic Power - Hydraulic System No. 1 - Inspection Of The Pressure And Suction Lines P/N 601R75286-61 And 601R75286-37.

Ice and Rain Protection - Wing Anti-Ice System - Detailed Inspection of the Wing Anti-Ice Wing Ducts (Piccolo Tubes)

R&R-2-30J0003R&R-2-30J0004R&R-2-30J0005R&R-2-30J0006R&R-2-30J0007R&R-2-30J0008

Indicating/Recording Systems - Panels, Instrument And Control - Installation of a Plate Assembly to Replace the Camlocs Install

Landing Gear -Extension And Retraction - Inspection Of The End Caps Installed On The Selector Valves Of The Nose-Landing-Gear A

Service Bulletin StatusService Bulletin Status

of 158



S/B Number Part FAA AD TCCA AD DESCRIPTION Accomplished by DFP Hours CyclesAccomplishmentDate

Service Bulletin StatusService Bulletin Status

601R-32-093B

601R-34-080Z 17-Mar-06 Comair Airlines EC-01520 9421.00 8175

601R-34-107D PART B 3/28/04 Comair Airlines EO 34-107 4010 3494

601R-49-023A 21-May-08 Chautauqua Airlines EO 49025 13294.00 11409

601R-52-009 95-04-05 CF-93-02R1 5/28/2009 ExelTech Aerospace SB 15676.00 13226

601R-52-110C 9-Jan-06 Comair MOD-2-52M0002 9096.01 7,887

601R-53-061 2008-06-10 CF-2003-12 29-May-09 ExelTech Aerospace CHQ EO080610 15676.00 13226

601R-76-019A 2005-06-04 CF-2004-01R1

601R-78-021 PART B 2007-04-24 CF-2006-19 Chautauqua Airlines EO AD070424B

2004-20-092007-01-072007-03-19

CF-2004-18R1CF-2003-09R1

Landing Gear - Main Landing Gear System -Landing Gear - Main Landing Gear System - Replacement Of The Main Fitting Of The Main

Navigation - Flight Environment - Reduced Vertical Separation Minimum (RVSM) to 1000 Ft. Aircraft Qualification Requirements

Navigation -Air Data System - Installation Of New Air Data Computer Calibrated For Reduced Vertical Separation Minimum (RVSM)

Airborne Auxiliary Power - APU Inlet Door - Modification of APU Inlet Door Potentiometer Installation

Doors - Passenger/Crew - Addition of Latch Pin Grease Fittings and Grease Retainers and the Application of Anti-Icing Compound

REPLACEMENT OF THE BUSHINGS IN THE UPPER LATCH FITTINGS

Fuselage - General - Visual Inspection of Fuselage Station (FS)640.00 at Buttock Line (BL)45 between Stringer (STR)9 and Stringer (STR)12

Engine - Throttles - Inspection Of The Throttle Control Gearbox (P/N 2100140-005 And P/N 2100140-007)

5/26/20096/21/09

ExelTech AerospaceChautauqua Airlines

Components changed

1567615679

1322613228

Engine Exhaust-Engine Nozzle-Inspection and Replacement of Exhaust Nozzle Fairing Attachment Hardware

12/16/076/26/08

1212213582

1050811625

of 158



Part Number Description S/N POSITION TASK_REF FREQ HRS REM HRS

601R10179-1 AILERON FLUTTER DAMPER SHEAR PIN N/A 1 27-11-01 5,400 27-May-09 15676 13226 0 18,626 6,395

601R10179-1 AILERON FLUTTER DAMPER SHEAR PIN N/A 2 27-11-01 5,400 27-May-09 15676 13226 0 18,626 6,395

F33337000001 AILERON INPUT / OUTPUT UNIT (CFMS) FR030 RH 27-11-05 12,000 2-Nov-02 0 0 12,000 -231

F33337000001 AILERON INPUT / OUTPUT UNIT (CFMS) FR036 LH 27-11-06 12,000 2-Nov-02 0 0 12,000 -231

FE337000001 RUDDER FORCE TRANSDUCER (CFMS) FR0132 F/O LH 27-21-06 26,667 2-Nov-02 0 0 26,667 14,436

FE337000001 RUDDER FORCE TRANSDUCER (CFMS) FR0134 F/O RH 27-21-06 26,667 2-Nov-02 0 0 26,667 14,436

FE337000001 RUDDER FORCE TRANSDUCER (CFMS) FR0130 CAPT / LH 27-21-06 26,667 2-Nov-02 0 0 26,667 14,436

FE337000001 RUDDER FORCE TRANSDUCER (CFMS) FR0136 CAPT / RH 27-21-06 26,667 2-Nov-02 0 0 26,667 14,436

FE336000001 ELEVATOR FORCE TRANSDUCER (CFMS) FR092 LH 27-31-02 26,667 2-Nov-02 0 0 26,667 14,436

FE336000001 ELEVATOR FORCE TRANSDUCER (CFMS) FR102 RH 27-31-02 26,667 2-Nov-02 0 0 26,667 14,436

601R24063-31 ELEVATOR FLUTTER DAMPER SHEAR PIN N/A 1 27-31-01 20,000 25-Nov-02 0 0 20,000 7,769




8396-3 ACTUATOR HORZ STAB TRIM (AD 2002-16-02) 970 ONLY 27-42-01 19,200 25-Nov-02 0.00 0 0.00 19,200.00 3,514.41

855D100-11 FLAP BRAKE AND POSITION SENSOR (BPSU) 1955 LH 27-51-10 50,000 25-Nov-02 0.00 0 0.00 0 50,000 37,769

855D100-11 FLAP BRAKE AND POSITION SENSOR (BPSU) 4494 RH 27-51-10 50,000 25-Nov-02 0.00 0 0.00 0 50,000 37,769

852D100-21 ACTUATOR, INBD FLAP 6022 LH OUTBD 27-53-01 30,000 COMPONENT N/A - PN 852D100-25 Installed

852D100-19 ACTUATOR, INBD FLAP 3900 LH INBD 27-53-01 30,000 COMPONENT N/A - PN 852D100-25 Installed

852D100-21 ACTUATOR, INBD FLAP 7207 RH OUTBD 27-53-01 30,000 COMPONENT N/A - PN 852D100-25 Installed

852D100-21 ACTUATOR, INBD FLAP 7205 RH INBD 27-53-01 30,000 COMPONENT N/A - PN 852D100-25 Installed

853D100-19 ACTUATOR, OUTB FLAP 2205 LH INBD 27-53-05 33,333 COMPONENT N/A - PN 853D100-23 Installed

854D100-19 ACTUATOR, OUTB FLAP 3649 LH OUTBD 27-53-05 33,333 COMPONENT N/A - PN 854D100-23 Installed

853D100-20 ACTUATOR, OUTB FLAP 1966 RH INBD 27-53-05 33,333 COMPONENT N/A - PN 853D100-24 Installed

854D100-20 ACTUATOR, OUTB FLAP 2815 RH OUTBD 27-53-05 33,333 COMPONENT N/A - PN 854D100-24 Installed

857SD100-1 FLEXIBLE DRIVE SHAFT N/A N/A 27-53-10 18,000 COMPONENT N/A TO MSN 7707

601R14002-1 INBOARD FLAP ASSY SB/RJ/745 LH 25-Nov-02 0.00 0 0.00 0

601R14202-5 ACTUATOR, INBD FLAP VANE UNKNOWN LH OUTBD 27-54-15 40,000 25-Nov-02 0.00 0 0.00 0 40,000 27,769

.601R14202-5 ACTUATOR, INBD FLAP VANE UNKNOWN LH CTR 27-54-15 40,000 25-Nov-02 0.00 0 0.00 0 40,000 27,769

.601R14202-5 ACTUATOR, INBD FLAP VANE UNKNOWN LH INBD 27-54-15 40,000 25-Nov-02 0.00 0 0.00 0 40,000 27,769

601R14002-2 INBOARD FLAP ASSY SB/RJ/729 RH 25-Nov-02 0.00 0 0.00 0

.601R14202-5 ACTUATOR, INBD FLAP VANE UNKNOWN RH OUTBD 27-54-15 40,000 25-Nov-02 0.00 0 0.00 0 40,000 27,769

FREQ CYC

MFG/INST Date

ACFT HRS at Install

ACFT CYC at Install

Component HRS at Install

Component CYC at Install

ACFT HRS Due

ACFT CYC Due

REM CYC

Airframe LLP StatusAirframe LLP Status

of 158



Part Number Description S/N POSITION TASK_REF FREQ HRS REM HRSFREQ CYC

MFG/INST Date

ACFT HRS at Install

ACFT CYC at Install

Component HRS at Install

Component CYC at Install

ACFT HRS Due

ACFT CYC Due

REM CYC

Airframe LLP StatusAirframe LLP Status

.601R14202-5 ACTUATOR, INBD FLAP VANE UNKNOWN RH CTR 27-54-15 40,000 25-Nov-02 0.00 0 0.00 0 40,000 27,769

.601R14202-5 ACTUATOR, INBD FLAP VANE UNKNOWN RH INBD 27-54-15 40,000 25-Nov-02 0.00 0 0.00 0 40,000 27,769

228077-2 APU FUEL PUMP CARTRIDGE N/A APU 28-24-01 18,000 COMPONENT N/A TO MSN 7707

848431 AC MOTOR DRIVEN PUMP N/A ALL 29-11-03 12,000 COMPONENT N/A TO MSN 7707

601R10241-5 SHAFT - MLG SIDE STAY FITTING 0699 LH 32-11-104 COMPONENT NA TO MSN 7707

601R10241-6 SHAFT - MLG SIDE STAY FITTING 0671 RH 32-11-104 COMPONENT NA TO MSN 7707

0856KV9 PITOT STATIC TUBE 229654 LH 34-11-01 9,600 6-Apr-06 9,517 0.00 19,117.00 3,431.41

0856KV10 PITOT STATIC TUBE 232936 RH 34-11-01 9,600 6-Apr-06 9,517 0.00 19,117.00 3,431.41

601R318911-1 PAX DOOR LOCK MECHANISM TORSION SPRING N/A ONLY 52-11-02 2,300 COMPONENT N/A TO MSN 7707

LC085H8 PAX DOOR OUTER HANDLE SPRING N/A ONLY 52-11-03 1,000 COMPONENT N/A TO MSN 7707

NAS537B16P034W PAX DOOR UPPER LATCH FITTING BUSHING N/A ONLY 52-11-04 4,500 N/A BUSHING REPLACED BY COMAIR 09-JAN-06

2R5206B MOTOR ASSY A1132 ONLY 52-11-08 50,000 17-Jun-08 11,571 1,558 60,013 47,782

of 158

MSN: 7707 A/C TSN: 15,685.59

MFG Date: A/C CSN: 12,231


Part Number Part Description S/N Pos. ATA Task No. Task Card No. Task Description Date C/W Hour C/W Interval Date Due REM HRS REM CYC

753355-4 HEAT EXCHANGER 940617 LH 21-51 MRB 21-51-13-09 000-21-310-707 RESTORE THE HEAT EXCHANGER (CORE) 24-Apr-07 10,698 8000H 0.00 3,012.41

753355-9 HEAT EXCHANGER 200205147 RH 21-51 MRB 21-51-13-09 000-21-310-707 RESTORE THE HEAT EXCHANGER (CORE) 16-Apr-09 15,679 8000H 0.00 7,993.41

2100-1020-00 COCKPIT VOICE RECORDER 000189017 CVR 23-71 MRB 23-71-01-01 000-23-900-730 FUNCTIONAL CHECK OF CVR 17-Dec-08 36 MONTHS 17-Dec-11

2100-1020-00 CVR ULB 000189017 CVR 23-71 MRB 23-71-03-01 000-23-360-720 FUNCTIONAL CHECK OF CVR ULB 17-Dec-08 24 MONTHS 17-Dec-10

DK120 BATTERY BEACON SC13371 CVR 23-71 MRB 23-71-03-03 000-23-360-760 RESTORE THE CVR ULB 25-May-09 72 MONTHS 1-Feb-13

756652 CARTRIDGE - ADG UPLOCK N/A 24-23 MRB 24-23-11-05 000-24-900-750 DISCARD THE ADG UPLOCK MECH. CARTRIGES COMPONENT N/A TO MSN 7707 60 MONTHS

024453-000 APU BATTERY 105087 APU 24-32 MRB 24-32-03-03 000-24-310-701 RESTORE APU BATTERY 17-Jun-09 12 MONTHS 17-Jun-10

024453-000 APU BATTERY 105087 APU 24-32 MRB 24-32-03-01 000-24-310-002 FUNCTIONAL CHECK OF APU BATTERY 17-Jun-09 15,679 500H 493.41

024637-000 MAIN BATTERY 0905200075B8B MAIN 24-32 MRB 24-32-01-01 000-24-310-001 FUNCTIONAL CHECK OF MAIN BATTERY 17-Jun-09 15,679 1500H 1,493.41

024637-000 MAIN BATTERY 0905200075B8B MAIN 24-32 MRB 24-32-01-03 000-24-310-700 RESTORE AIRCRAFT MAIN BATTERY 17-Jun-09 12 MONTHS 17-Jun-10

452-0133 BATTERY, ELT Unkown ONLY 25-60 MRB 000-25-360-720 DISCARD THE ELT BATTERY 16-Jun-09 24 MONTHS 16-Jun-11

453-0150 EMERGENCY LOCATOR XMTR 70441 ONLY 25-60 MRB 000-25-220-700 OPERATIONAL CHECK OF THE ELT 16-Jun-09 12 MONTHS 16-Jun-10

3505-101CW LIFE VEST P0904508 CAPT 25-60 MRB 25-61-01-01 000-25-900-720 REMOVE AND REPLACE LIFE VEST 9-Jun-09 60 MONTHS 8-Jun-14

P0723E105PWC LIFE VEST MISSING F/O 25-60 MRB 25-61-01-01 000-25-900-720 REMOVE AND REPLACE LIFE VEST 60 MONTHS 29-Dec-04

3505-101W LIFE VEST LW0203452 OBS 25-60 MRB 25-61-01-01 000-25-900-720 REMOVE AND REPLACE LIFE VEST 25-Feb-09 60 MONTHS 24-Feb-14

3505-101W LIFE VEST LW0203400 FA 25-60 MRB 25-61-01-01 000-25-900-720 REMOVE AND REPLACE LIFE VEST 24-Feb-09 60 MONTHS 23-Feb-14

473597-19 CARGO COMPT SMOKE DETECTOR 1778 FWD 26-15 MRB 26-15-00-01 000-26-900-001 RESTORE (CLEAN) THE SMOKE DETECTOR 2-Jun-09 15,679 2500H 2,493.41

473597-19 CARGO COMPT SMOKE DETECTOR 1050 AFT 26-15 MRB 26-15-00-01 000-26-900-001 RESTORE (CLEAN) THE SMOKE DETECTOR 2-Jun-09 15,679 2500H 2,493.41

899074-1 ENGINE FIRE BOTTLE 64713EL ENGINE RH 26-20 MRB 26-21-07-06 000-26-310-750 HYDROSTATIC TEST OF ENGINE FIREX BOTTLE 17-Nov-06 60 MONTHS 16-Nov-11

899074-1 ENGINE FIRE BOTTLE 64750EL ENGINE LH 26-20 MRB 26-21-07-06 000-26-310-750 HYDROSTATIC TEST OF ENGINE FIREX BOTTLE 6-Nov-06 60 MONTHS 5-Nov-11

897776-01 ENGINE SQUIB-CARTRIDGE 2324 LH1 26-21 MRB 26-21-10-01 000-26-310-760 DISCARD THE ENGINE FIREX BOTTLE CARTRIDGE 30-Apr-02 120 MONTHS 27-Apr-12

897776-01 ENGINE SQUIB-CARTRIDGE 2307 LH2 26-21 MRB 26-21-10-01 000-26-310-760 DISCARD THE ENGINE FIREX BOTTLE CARTRIDGE 30-Apr-02 120 MONTHS 27-Apr-12

897776-01 ENGINE SQUIB-CARTRIDGE 2210 RH1 26-21 MRB 26-21-10-01 000-26-310-760 DISCARD THE ENGINE FIREX BOTTLE CARTRIDGE 30-Apr-02 120 MONTHS 27-Apr-12

897776-01 ENGINE SQUIB-CARTRIDGE 2204 RH2 26-21 MRB 26-21-10-01 000-26-310-760 DISCARD THE ENGINE FIREX BOTTLE CARTRIDGE 30-Apr-02 120 MONTHS 27-Apr-12

897889-1 APU FIRE BOTTLE 8690EL APU 26-20 MRB 26-22-07-06 000-26-310-751 HYDROSTATIC TEST OF APU FIREX BOTTLE 3-Jun-05 60 MONTHS 2-Jun-10

897776-01 APU SQUIB-CARTRIDGE 03562 APU 26-22 MRB 26-22-10-01 000-26-310-761 DISCARD THE APU FIREX BOTTLE CARTRIDGE 31-Jul-06 120 MONTHS 28-Jul-16

C352 PORTABLE FIREX - HALON W745761 COCKPIT 26-20 MRB 26-23-00-05 00-26-900-750 HYDRO TEST OF THE PORTABLE FIREX BOTTLES 1-Sep-06 72 MONTHS 30-Aug-12

C352TS PORTABLE FIREX - HALON X-329600 GALLEY 26-20 MRB 26-23-00-05 000-26-900-750 HYDRO TEST OF THE PORTABLE FIREX BOTTLES 1-Sep-06 72 MONTHS 30-Aug-12

C352TS PORTABLE FIREX - HALON X-329896 AFT 26-20 MRB 26-23-00-05 000-26-900-750 HYDRO TEST OF THE PORTABLE FIREX BOTTLES 1-Sep-06 72 MONTHS 30-Aug-12

C352 PORTABLE FIREX - HALON W745761 COCKPIT 26-20 MRB 26-23-01-03 000-26-900-700 WEIGHT CHECK OF PORTABLE FIREX BOTTLES 23-Jun-09 12 MONTHS 23-Jun-10

C352TS PORTABLE FIREX - HALON X-329600 GALLEY 26-20 MRB 26-23-01-03 000-26-900-700 WEIGHT CHECK OF PORTABLE FIREX BOTTLES 23-Jun-09 12 MONTHS 23-Jun-10

C352TS PORTABLE FIREX - HALON X-329761 AFT 26-20 MRB 26-23-01-03 000-26-900-700 WEIGHT CHECK OF PORTABLE FIREX BOTTLES 23-Jun-09 12 MONTHS 23-Jun-10

C352TS PORTABLE FIREX - HALON X-329896 AFT 26-20 MRB 26-23-01-03 000-26-900-700 WEIGHT CHECK OF PORTABLE FIREX BOTTLES 23-Jun-09 12 MONTHS 23-Jun-10

BA23217-1 LAVATORY FIRE BOTTLE 22508 LAV 26-20 MRB 26-23-01-07 000-26-270-750 WEIGHT CHECK OF THE LAVATORY FIREX BOTTLE 17-Jun-09 60 MONTHS 16-Jun-14

36500018-3 CARGO FIRE BOTTLE 24214D1 CARGO LH 26-20 MRB 26-25-01-01 000-26-310-752 HYDRO TEST OF CARGO COMPARTMENT FIREX BOTTLE 8-Apr-09 60 MONTHS 7-Apr-14

34600037-1 CARGO FIRE BOTTLE 22623F1 CARGO RH 26-20 MRB 26-25-01-01 000-26-310-753 HYDRO TEST OF CARGO COMPARTMENT FIREX BOTTLE 27-Jan-09 60 MONTHS 26-Jan-14

30903870 CARGO SQUIB-CARTRIDGE 02777 LH1 26-25 MRB 26-25-01-07 000-26-310-762 DISCARD THE CARGO COMP. FIREX BOTTLE SQUIBS 1-Apr-04 120 MONTHS 30-Mar-14

30903870 CARGO SQUIB-CARTRIDGE 02749 LH2 26-25 MRB 26-25-01-07 000-26-310-762 DISCARD THE CARGO COMP. FIREX BOTTLE SQUIBS 1-Apr-04 120 MONTHS 30-Mar-14

30903870 CARGO SQUIB-CARTRIDGE 04939 RH1 26-25 MRB 26-25-01-07 000-26-310-762 DISCARD THE CARGO COMP. FIREX BOTTLE SQUIBS 1-Nov-08 120 MONTHS 30-Oct-18

30903870 CARGO SQUIB-CARTRIDGE 04927 RH2 26-25 MRB 26-25-01-07 000-26-310-762 DISCARD THE CARGO COMP. FIREX BOTTLE SQUIBS 1-Nov-08 120 MONTHS 30-Oct-18

852D100-21 ACTUATOR, INBD FLAP 6022 LH INBD 27-50 CMR* C27-50-111-11 000-27-580-700 FUNCTIONAL CHECK OF THE FLAP ACT. TORQUE LIMITER 20-Apr-07 9,422 10666C 0 7,857

853D100-23 ACTUATOR, INBD FLAP 2205 LH OUTBD 27-50 CMR* C27-50-111-11 000-27-580-700 FUNCTIONAL CHECK OF THE FLAP ACT. TORQUE LIMITER 18-Jun-09 13,228 10666C 0 11,663

853D100-24 ACTUATOR, INBD FLAP 1966 RH OUTBD 27-50 CMR* C27-50-111-11 000-27-680-700 FUNCTIONAL CHECK OF THE FLAP ACT. TORQUE LIMITER 6-Jul-09 13,288 10666C 0 11,723

852D100-25 ACTUATOR, INBD FLAP 3900 RH INBD 27-50 CMR* C27-50-111-11 000-27-680-700 FUNCTIONAL CHECK OF THE FLAP ACT. TORQUE LIMITER 5-May-09 13,228 10666C 0 11,663

852D100-21 ACTUATOR, OUTB FLAP 7207 LH INBD 27-50 CMR* C27-50-111-10 000-27-590-741 FUNCTIONAL CHECK OF THE FLAP ACT. TORQUE LIMITER 20-Apr-07 9,422 14000C 0 11,191

Task Orig.

Cycle C/W

Hrs atInstall

Cyc atInstall

25-62-01-01FAR 91.207

25-62-01-03FAR 91.207

Airframe HT StatusAirframe HT Status

of 158

MSN: 7707 A/C TSN: 15,685.59

MFG Date: A/C CSN: 12,231


Part Number Part Description S/N Pos. ATA Task No. Task Card No. Task Description Date C/W Hour C/W Interval Date Due REM HRS REM CYCTask Orig.

Cycle C/W

Hrs atInstall

Cyc atInstall

Airframe HT StatusAirframe HT Status

854D100-23 ACTUATOR, OUTB FLAP 3649 LH OUTBD 27-50 CMR* C27-50-111-10 000-27-590-741 FUNCTIONAL CHECK OF THE FLAP ACT. TORQUE LIMITER 18-Jun-09 13,228 14000C 0 14,997

852D100-21 ACTUATOR, OUTB FLAP 7205 RH INBD 27-50 CMR* C27-50-111-10 000-27-690-741 FUNCTIONAL CHECK OF THE FLAP ACT. TORQUE LIMITER 20-Apr-07 9,422 14000C 0 11,191

854D100-24 ACTUATOR, OUTB FLAP 2815 RH OUTBD 27-50 CMR* C27-50-111-10 000-27-690-741 FUNCTIONAL CHECK OF THE FLAP ACT. TORQUE LIMITER 18-Jun-09 13,228 14000C 0 14,997

853D100-23 ACTUATOR, OUTB FLAP 2205 LH INBD 27-50 SR R27−50−300−01 000-27-590-740 RESTORATION OF OUTBD FLAP ACTUATORS (N/A to 853D100-23) 20000C 0 N/A

854D100-23 ACTUATOR, OUTB FLAP 3649 LH OUTBD 27-50 SR R27−50−300−01 000-27-590-740 RESTORATION OF OUTBD FLAP ACTUATORS (N/A to 854D100-23) 20000C 0 N/A

853D100-24 ACTUATOR, OUTB FLAP 1966 RH INBD 27-50 SR R27−50−300−01 000-27-690-740 RESTORATION OF OUTBD FLAP ACTUATORS (N/A to 853D100-24) 20000C 0 N/A

854D100-24 ACTUATOR, OUTB FLAP 2815 RH OUTBD 27-50 SR R27−50−300−01 000-27-690-740 RESTORATION OF OUTBD FLAP ACTUATORS (N/A to 854D100-24) 20000C 0 N/A

1023100-7 AILERON FLUTTER DAMPER HAI2751 LH 27-70 MRB 27-15-05-03 000-27-590-720 FUNCTIONAL CHECK OF AILERON FLUTTER DAMPERS 25-May-09 15,679 8000H 0.00 7,993.41

1023100-7 AILERON FLUTTER DAMPER HAI0231 RH 27-70 MRB 27-15-05-03 000-27-690-720 FUNCTIONAL CHECK OF AILERON FLUTTER DAMPERS 25-May-09 15,679 8000H 0.00 7,993.41

1023100-7 ELEVATOR FLUTTER DAMPER HAI4073 LH OUTBD 27-70 MRB 27-34-05-05 000-27-330-720 FUNCTIONAL CHECK OF ELEVATOR FLUTTER DAMPERS 28-May-09 15,679 8000H 0.00 7,993.41

1023100-7 ELEVATOR FLUTTER DAMPER HAI1544 LH INBD 27-70 MRB 27-34-05-05 000-27-330-720 FUNCTIONAL CHECK OF ELEVATOR FLUTTER DAMPERS 28-May-09 15,679 8000H 0.00 7,993.41

1023100-7 ELEVATOR FLUTTER DAMPER HAI2178 RH INBD 27-70 MRB 27-34-05-05 000-27-340-720 FUNCTIONAL CHECK OF ELEVATOR FLUTTER DAMPERS 28-May-09 15,679 8000H 0.00 7,993.41

1023100-7 ELEVATOR FLUTTER DAMPER HAI0672 RH OUTBD 27-70 MRB 27-34-05-05 000-27-340-720 FUNCTIONAL CHECK OF ELEVATOR FLUTTER DAMPERS 28-May-09 15,679 8000H 0.00 7,993.41

228077-2/-3 APU FUEL PUMP N/A APU 28-24 MRB 28-24-00-05 000-28-160-700 RESTORE APU FUEL PUMP BRUSHES COMPONENT N/A TO MSN 7707 1500H

S800-3000-00 ULB, FLIGHT DATA RECORDER 000183169 FDR 31-31 MRB 31-31-03-01 000-31-360-720 FUNCTIONAL CHECK OF FDR ULB 27-Apr-07 36 MONTHS 26-Apr-10

DK120 BATTERY, FDR ULB DH6040 FDR 31-31 MRB 31-31-03-03 000-31-360-760 RESTORE FDR ULB 25-May-09 72 MONTHS 30-Oct-11

7-45502-1 HANDLE, LG CONTROL N/A ONLY 32-31 SR R32-31-828-02 000-32-220-701 RESTORE THE LG CONTROL HANDLE COMPONENT N/A TO MSN 7707 300C

7-45502-1/-3 HANDLE, LG CONTROL N/A ONLY 32-31 SR R32-31-828-03 000-32-220-702 RESTORE THE LG CONTROL HANDLE COMPONENT N/A TO MSN 7707 4000C

RPS1-B BATTERY, EMERGENCY LIGHT 18764 1 33-50 MRB 33-51-04-01 000-33-900-701 RESTORE EMERG. LIGHTING SYSTEM BATTERY PACK 31-May-09 18 MONTHS 29-Nov-10

RPS1-B BATTERY, EMERGENCY LIGHT 13739 2 33-50 MRB 33-51-04-01 000-33-900-701 RESTORE EMERG. LIGHTING SYSTEM BATTERY PACK 11-Jun-09 18 MONTHS 10-Dec-10

RPS1-B BATTERY, EMERGENCY LIGHT 22526 3 33-50 MRB 33-51-04-01 000-33-900-701 RESTORE EMERG. LIGHTING SYSTEM BATTERY PACK 5-Feb-09 18 MONTHS 6-Aug-10

RPS1-B BATTERY, EMERGENCY LIGHT 22546 4 33-50 MRB 33-51-04-01 000-33-900-701 RESTORE EMERG. LIGHTING SYSTEM BATTERY PACK 5-Feb-09 18 MONTHS 6-Aug-10

0856KV9 PITOT STATIC SYSTEM 229654 1 34-11 MRB FAR 91.411 000-34-900-122 FUNCTIONAL/LEAK CHECK OF PITOT-STATIC SYSTEMS 16-Dec-08 24 MONTHS 16-Dec-10

0856KV10 PITOT STATIC SYSTEM 232936 2 34-11 MRB FAR 91.411 000-34-900-122 FUNCTIONAL/LEAK CHECK OF PITOT-STATIC SYSTEMS 16-Dec-08 24 MONTHS 16-Dec-10

822-0372-445 AIR DATA COMPUTER GMCL 1 34-13 FAR FAR 91.411 000-34-220-723 CALIBRATE ADC 16-Dec-08 24 MONTHS 16-Dec-10

822-0372-445 AIR DATA COMPUTER DKFJ 2 34-13 FAR FAR 91.411 000-34-220-723 CALIBRATE ADC 16-Dec-08 24 MONTHS 16-Dec-10

WL102AMS5 INDICATOR STNDBY ALTITUDE AP527 ONLY 34-14 MRB 000-34-220-720 CALIBRATE STANDBY AIRSPEED/ALTIMETER INDICATOR 10-Jul-08 24 MONTHS 10-Jul-10

PAI700 COMPASS STANDBY 45905 ONLY 34-22 MRB 34-22-01-01 000-34-220-730 FUNCTIONAL CHECK OF STANDBY COMPASS 13-Dec-08 36 MONTHS 13-Dec-11

622-9210-004 ATC TRANSPONDER 10K9R 1 34-54 FAR FAR 91.413 CALIBRATE ATC TRANSPONDER 17-Dec-09 24 MONTHS 17-Dec-11

622-9210-004 ATC TRANSPONDER 10KBD 2 34-54 FAR FAR 91.413 CALIBRATE ATC TRANSPONDER 17-Dec-08 24 MONTHS 17-Dec-10

897-93050 CYLINDER, CREW OXYGEN ALT279-16149 ONLY 35-10 MRB 35-11-03-01 000-35-140-730 HYDROSTATIC TEST OF CREW OXYGEN CYLINDER 1-Feb-07 60 MONTHS 31-Jan-12

897-93050 CYLINDER, CREW OXYGEN ALT279-16149 ONLY 35-10 MRB 35-11-03-05 000-35-140-760 DISCARD CREW OXYGEN CYLINDER 1-Feb-07 180 MONTHS 28-Jan-22

803000-12 OXYGEN GENERATOR See OEM Book Several 35-23 MRB 35-23-13-03 000-35-900-760 DISCARD THE OXYGEN GENERATORS 1-May-02 144 MONTHS 28-Apr-14

803000-13 OXYGEN GENERATOR See OEM Book Several 35-23 MRB 35-23-13-03 000-35-900-760 DISCARD THE OXYGEN GENERATORS 1-Aug-02 144 MONTHS 29-Jul-14

176965-31 BOTTLE, PORTABLE OXYGEN 760301 FWD 35-30 MRB 35-31-05-01 000-35-900-750 HYDRO TEST OF PORTABLE OXYGEN CYLINDER 4-Jun-06 60 MONTHS 3-Jun-11

176965-31 BOTTLE, PORTABLE OXYGEN 794933 AFT 35-30 MRB 35-31-05-01 000-35-900-750 HYDRO TEST OF PORTABLE OXYGEN CYLINDER 22-Mar-09 60 MONTHS 21-Mar-14

MR-10037N PBE E0603769 FWD 35-30 MRB 35-31-07-03 000-35-900-761 DISCARD THE PBE 31-Jul-05 126 MONTHS 25-Jan-16

MR-10037N PBE E0603764 AFT 35-30 MRB 35-31-07-03 000-35-900-761 DISCARD THE PBE 31-Jul-05 126 MONTHS 25-Jan-16

MR-10037N PBE E0604159 COCKPIT 35-30 MRB 35-31-07-03 000-35-900-761 DISCARD THE PBE 31-Jul-05 126 MONTHS 25-Jan-16

3800488-3 APU P-1150 ONLY 49-20 MRB 49-20-00-01 000-49-310-706 APU RESTORATION PER VENDOR CMM 3500AH -6,343.00

34-12-01-01FAR 91.411


Status Date: 8-Apr-23 LG CSN: 12,231

Description Part Number Serial NoCurrent Cycles Cycles @ Instl Cycles Remaining Cycle Limits Calendar

Since New Since O/H Since New Since O/H A/C Cycles Life Limit Restore Restore Life Limit Restore Date Limit (Days) Restore Due Date

NOSE LANDING GEARNose Gear Assy 16040-117 DCL750/02 12,231 12,231 0 0 0 120,385 N/A 132,616NLG Uplock Assy 16600-103 CDWW106902 12,231 12,231 0 0 0 94,436 7,769 20,000 106,667 20-Nov-02 3650 17-Nov-12NLG Drag Brace Assy 16400-105 DCL759/02 12,231 12,231 0 0 0 45,666 7,769 20,000 57,897 20-Nov-02 3650 17-Nov-12NLG Shock Strut Assy 16050-115 DCL750/02 12,231 12,231 0 0 0 7,769 20,000 N/A 20-Nov-02 3650 17-Nov-12NLG Actuator 16520-101 DAY0651 12,231 12,231 0 0 0 7,769 20,000 N/A 20-Nov-02 3650 17-Nov-12NLG Axle/Nut 16122-101 WHM1242 12,231 12,231 0 0 0 7,769 20,000 N/A 20-Nov-02 3650 17-Nov-12

MAIN LANDING GEAR - LEFTMain Landing Gear Assy 17002-113 DCL738/02 see sub assysMain Gear Fitting 17064-105 WHM1860 12,231 12,231 0 0 0 107,769 7,769 20,000 120,000 20-Nov-02 3650 17-Nov-12Axle 17050-101 EXC1230 15,013 3,807 11,206 0 9,424 104,987 16,193 20,000 120,000 23-Aug-06 3650 20-Aug-16Pin, Pintle 17040-1 DCL1703 12,231 12,231 0 0 0 52,376 N/A 64,607Trailing Arm 17084-111 PLT3087 12,231 12,231 0 0 0 51,638 7,769 20,000 63,869 20-Nov-02 3650 17-Nov-12Pin, Pivot 17041-3 DCL1662 12,231 12,231 0 0 0 107,769 N/A 120,000Uplock Assy 17051-101 CWDD210302 12,231 12,231 0 0 0 75,769 7,769 20,000 88,000 20-Nov-02 3650 17-Nov-12Main Gear Shock Absorber 17100-105 DCL1575/02 12,231 12,231 0 0 0 7,769 20,000 see sub assys 20-Nov-02 3650 17-Nov-12Cylinder 17105-105 DCL897 12,231 12,231 0 0 0 107,769 N/A 120,000Piston 17115-101 DCL1504 12,231 12,231 0 0 0 107,769 N/A 120,000Pin, Shock Absorber Piston 17207-1 EXC3012 12,231 12,231 0 0 0 107,769 N/A 120,000Pin, Shock Absorber Cylinder 17207-1 EXC2988 12,231 12,231 0 0 0 107,769 N/A 120,000Side Stay Actuator 17008-113 01603 12,231 12,231 0 0 0 7,769 20,000 see sub assys 20-Nov-02 3650 17-Nov-12Cylinder 17027-7 248C 12,231 12,231 0 0 0 107,769 N/A 120,000Piston 17014-3 2209 12,231 12,231 0 0 0 101,124 N/A 113,355Rod End 17028-3 1603 12,231 12,231 0 0 0 101,124 N/A 113,355Pin, Side Stay 17076-1 DCL1695 12,231 12,231 0 0 0 107,769 N/A 120,000

MAIN LANDING GEAR - RIGHTMain Landing Gear Assy 17002-114 DCL730/02 see sub assysMain Gear Fitting 17064-106 WHM1789 12,231 12,231 0 0 0 107,769 7,769 20,000 120,000 20-Nov-02 3650 17-Nov-12Axle 17050-101 EXC1989 12,231 12,231 0 0 0 107,769 7,769 20,000 120,000 20-Nov-02 3650 17-Nov-12Pin, Pintle 17040-1 DCL1705 12,231 12,231 0 0 0 52,376 N/A 64,607Trailing Arm 17084-111 MBM1848 12,231 12,231 0 0 0 51,638 7,769 20,000 63,869 20-Nov-02 3650 17-Nov-12Pin, Pivot 17041-3 DCL1625 12,231 12,231 0 0 0 107,769 N/A 120,000Uplock Assy 17051-101 CWDD203801 12,231 12,231 0 0 0 75,769 7,769 20,000 88,000 20-Nov-02 3650 17-Nov-12Main Gear Shock Absorber 17100-105 DCL1565/02 12,231 12,231 0 0 0 7,769 20,000 see sub assys 20-Nov-02 3650 17-Nov-12Cylinder 17105-105 DCL888 12,231 12,231 0 0 0 107,769 N/A 120,000Piston 17115-101 DCL1490 12,231 12,231 0 0 0 107,769 N/A 120,000Pin, Shock Absorber Piston 17207-1 EXC3003 12,231 12,231 0 0 0 107,769 N/A 120,000Pin, Shock Absorber Cylinder 17207-1 EXC2985 12,231 12,231 0 0 0 107,769 N/A 120,000Side Stay Actuator 17008-113 01495 12,231 12,231 0 0 0 7,769 20,000 see sub assys 20-Nov-02 3650 17-Nov-12Cylinder 17027-7 126C 12,231 12,231 0 0 0 107,769 N/A 120,000Piston 17014-3 2057 12,231 12,231 0 0 0 101,124 N/A 113,355Rod End 17028-3 1467 12,231 12,231 0 0 0 101,124 N/A 113,355Pin, Side Stay 17076-1 DCL1640 12,231 12,231 0 0 0 107,769 N/A 120,000

Landing Gear LLP & HT StatusLanding Gear LLP & HT Status

of 158

MSN: 7707 A/C TSN: 14287.54MFG Date: 20-Nov-02 A/C CSN: 12231.00


TASK CARD TITLE INTERVAL STATUSLAST ACCOMPLISHMENT NEXT DUE

DATE FH FC INT DATE FH

000-21-280-700 C21−50−115−01 10000 FH C/W 17-Jun-09 15679 10000 25679

000-24-220-701 C24−20−129−01 4000 FH C/W 27-May-09 15676 4000 19676

000-24-900-701 C24−10−129−01 4000 FH C/W 23-Jun-09 15679 4000 19679

000-26-900-701 C26−10−131−01 10000 FH C/W 8-Dec-06 10698 10000 20698

000-27-220-122 C27−31−102−01 10000 FH C/W 23-Apr-07 10706 10000 20706

000-27-330-100 C27−30−102−05 10000 FH C/W 19-Apr-07 10706 10000 20706

000-27-340-100 C27−30−102−05 10000 FH C/W 19-Apr-07 10706 10000 20706

000-27-580-700 C27−50−111−11 10666 FC 10666

000-27-590-741 C27−50−111−10 14000 FC 14000

000-27-680-700 C27−50−111−11 10666 FC 10666

000-27-690-741 C27−50−111−10 14000 FC 14000

000-27-900-108 C27−30−102−05 10000 FH C/W 19-Apr-07 10706 10000 20706

000-27-900-700 C27−20−108−01 10000 FH C/W 8-Dec-06 10698 10000 20698

000-27-900-706 C27−30−102−01 10000 FH C/W 29-Nov-06 10698 10000 20698

000-27-900-720 C27−10−105−03 10000 FH C/W 27-May-09 15676 10000 25676

000-30-900-700 C30−10−141−01 4000 FH C/W 28-Nov-08 14578 4000 18578

000-34-900-124 C34−40−107−01 10000 FH CW 29-Nov-06 10698 10000 20698

000-05-900-992 Routine Check 100 FH WORKSCOPE 100 100

000-22-220-100 C27−35−112−01 5000 FH CW 23-May-09 15676 5000 20676

000-24-900-702 C24−20−129−01 4000 FH

000-25-220-701 C25−17−152−01 5000 FH CW 27-May-09 15676 5000 20676

000-27-130-100 C27-35-300-01 Functional Check of the Stick-Pusher Capstan Shaft 5000 FH CW 14-Apr-09 15548 5000 20548

TASK CARDNUMBER

TASKNUMBER

Visual Check of the DecompressionEqualizer Rubber−Diaphragm

Functional Check (In−FlightDeployment) of the Air DrivenGenerator (ADG)

Operational Test of the GCUOvervoltage Protection

Operational Check of the APU FireDiode

Functional Check of the Pitch FeelSimulator Pilot Input Lever

Detailed Inspection of the LeftElevator Flutter Dampers

Detailed Inspection of the RightElevator Flutter Dampers

Functional Check of the Left WingInboard Flap Actuator Torque LimiterEFFECTIVITY:IB Flap Actuators:P/N 601 R93101 −1 9(P/N 852D100−19) and subsNOTE:Replace the following components:1. Pinion seals.2. Retaining ring (snap ring).3. Needle bearings.

Functional Check of the Left WingOutboard Flap Actuator TorqueLimiterEFFECTIVITY:OB Flap Actuators:P/N 601 R93103−19, −20(P/N 853D100−19, −20) and subsP/N 601 R93104−19, −20(P/N 854D100−19, −20) and subs

Functional Check of the Right WingInboard Flap Actuator Torque LimiterEFFECTIVITY:IB Flap Actuators:P/N 601 R93101 −1 9(P/N 852D100−19) and subsNOTE:Replace the following components:1. Pinion seals.2. Retaining ring (snap ring).3. Needle bearings.

Functional Check of the Right WingOutboard Flap Actuator TorqueLimiterEFFECTIVITY:OB Flap Actuators:P/N 601 R93103−19, −20(P/N 853D100−19, −20) and subsP/N 601 R93104−19, −20(P/N 854D100−19, −20) and subs

Operational Check of the ElevatorFlutter−Damper Fluid−LevelTransmitter−Switch

Operational Test of the Rudder LoadLimiters

Operational Test of the PitchDisconnect System

Functional Check of the AileronBreakout Bungee and BreakoutSwitch

Functional Check of the WingAnti−Ice Overheat Sensors andStandby Overheat Switches

Functional Check of the WindshearWarning System (A/C with EGPWS)

C26−20−131−02C26−20−131−03C27−40−113−01C27−50−111−12C28−00−142−01C30−10−141−02

Operational Check of the AP/SPDisconnect Switch, LH and RH

Functional Check (On−Ground) ofthe Dry Air Driven Generator (ADG)

N/A - TC 000-24-220-701

WAS USED

Functional Check of the FlightCompartment Reinforced DoorDecompression LatchEFFECTIVITY:Post− Modsum TC601R101329

CMR StatusCMR Status

of 158




DATE FH FC INT DATE FHTASK CARD

NUMBERTASK

NUMBER


000-27-140-101 C27−50−111−05 5000 FH CW23-May-09 15676

5000 20676

000-27-220-004 C27−35−112−02 500 FH NOT APPLICABLE

000-27-320-102 C27−42−103−01 5000 FH CW 18-Jun-09 15679 4000 19679

000-27-580-002 C27−50−111−07 1000 FH 1000 1000

000-27-580-004 C27−50−111−01 1000 FH

000-27-580-005 C27−50−111−03 500 FH

000-27-580-006 C27−50−111−09 1000 FH 1000

000-27-580-007 C27-50-300-01 2000 FC 2000

000-27-580-701 C27−50−111−06 4000 FH

000-27-590-002 C27−50−111−07 1000 FH 1000 1000

Functional Check of the FlapElectronic Control Unit

Operational Check of the StallProtection Computer (Flap PositionTransmitter Interface)EFFECTIVITY:Post− Modsum TC601 R15984

Detailed Inspection of the HSTASecondary Load Path IndicatorPHASE−IN:1. For aircraft with 4500 HSTA FH or less,2. For aircraft with more than 4500 HSTA

Detailed Inspection of the Left WingInboard Flap Actuators for StructuralIntegrity and External DisconnectEFFECTIVITY:IB Flap Actuators:P/N 601 R93101−19(P/N 852D100−19) and subs

Functional Check (Backlash) of theLeft Wing Inboard Flap ActuatorsEFFECTIVITY:IB Flap Actuators:P/N 601 R93101−9(P/N 852D100−11) or lowerPHASE−IN:Do the initial functional check within500 Flight Hours from January 19,2007.

N/A - COMPONENT NOT INSTALLED

Detailed Inspection of the Left WingInboard Flap Actuator Fittings andTrunnion HousingsEFFECTIVITY: IB Flap Actuators:P/N 601 R93101−9(P/N 852D100−11) or lowerPHASE−IN:Do the initial detailed inspectionwithin 500 Flight Hours from January19, 2007.


Functional Check of the Left WingInboard Flap Actuators for InternalDisconnectEFFECTIVITY:IB Flap Actuators:P/N 601 R93101−19(P/N 852D100−19) and subs

Functional Check of the LeftInboard-Flap Actuators forLinear-EndplayEFFECTIVITY:IB Flap Actuators:P/N 601R93101-19(P/N 852D100-19)PHASE-IN:Do the initial functional check within2000 Flight Cycles from the issuedate of this TR.

Discard of the Left Wing InboardFlap ActuatorsEFFECTIVITY:IB Flap Actuators:P/N 601 R93101 − 9(P/N 852D100−11) or lowerPHASE−IN:Do the discard within 4000 FlightHours from January 19, 2007 or,before March 31, 2008, whichevercomes first.


Detailed Inspection of the Left WingOutboard Flap Actuators forStructural Integrity and ExternalDisconnectEFFECTIVITY:OB Flap Actuators:P/N 601 R93103−19, −20(P/N 853D100−19, −20) and subsP/N 601 R93104−19, −20(P/N 854D100−19, −20) and subs

of 158





NUMBERTASK

NUMBER


000-27-590-004 C27−50−111−01 1000 FH

000-27-590-005 C27−50−111−03 500 FH

000-27-590-006 C27−50−111−09 1000 FH 1000 1000

000-27-900-711 C27−10−105−07 5000 FH CW 29-May-09 15676 5000 20676

000-27-590-742 C27−50−111−06 4000 FH

000-27-680-002 C27−50−111−07 1000 FH 1000 1000

000-27-680-004 C27−50−111−01 1000 FH

000-27-680-005 C27−50−111−03 500 FH

000-27-680-006 C27−50−111−09 1000 FH 1000 1000

Functional Check (Backlash) of theLeft Wing Outboard Flap ActuatorsEFFECTIVITY:OB Flap Actuators:P/N 601 R93103−18(P/N 853D100−18) or lowerP/N 601 R93104−10(P/N 854D100−12) or lowerPHASE−IN:Do the initial functional check within500 Flight Hours from January 19,2007.


Detailed Inspection of the Left WingOutboard Flap Actuator Fittings andTrunnion HousingsEFFECTIVITY:OB Flap Actuators:P/N 601 R93103−18(P/N 853D100−18) or lowerP/N 601 R93104−10(P/N 854D100−12) or lowerPHASE−IN:Do the initial detailed inspectionwithin 500 Flight Hours from January19, 2007.


Functional Check of the Left WingOutboard Flap Actuators for InternalDisconnectEFFECTIVITY:OB Flap Actuators:P/N 601 R93103−19, −20(P/N 853D100−19, −20) and subsP/N 601 R93104−19, −20(P/N 854D100−19, −20) and subs

Detailed Inspection of the LeftAileron Flutter Damper

Discard of the Left Wing OutboardFlap ActuatorsEFFECTIVITY:OB Flap Actuators:P/N 601 R93103−18(P/N 853D100−18) or lowerP/N 601 R93104−10(P/N 854D100−12) or lowerPHASE−IN:Do the discard within 4000 FlightHours from January 19, 2007 or,before March 31, 2008, whichevercomes first.


Detailed Inspection of the Right WingInboard Flap Actuators for StructuralIntegrity and External DisconnectEFFECTIVITY:IB Flap Actuators:P/N 601 R93101−19(P/N 852D100−19) and subs

Functional Check (Backlash) of theRight Wing Inboard Flap ActuatorsEFFECTIVITY:IB Flap Actuators:P/N 601 R93101−9(P/N 852D100−11) or lowerPHASE−IN:Do the initial functional check within500 Flight Hours from January 19,2007.


Detailed Inspection of the Right WingInboard Flap Actuator Fittings andTrunnion HousingsEFFECTIVITY: IB Flap Actuators:P/N 601 R93101−9(P/N 852D100−11) or lowerPHASE−IN:Do the initial detailed inspectionwithin 500 Flight Hours from January19, 2007.


Functional Check of the Right WingInboard Flap Actuators for InternalDisconnectEFFECTIVITY:IB Flap Actuators:P/N 601 R93101−19(P/N 852D100−19) and subs

of 158





NUMBERTASK

NUMBER


000-27-680-007 C27-50-300-01 2000 FC

000-27-680-701 C27−50−111−06 4000 FH

000-27-690-002 C27−50−111−07 1000 FH 1000 1000

000-27-690-004 C27−50−111−01 1000 FH

000-27-690-005 C27−50−111−03 500 FH

000-27-690-006 C27−50−111−09 1000 FH 1000 1000

000-27-690-711 C27−10−105−07 5000 FH CW 29-May-09 15676 5000 20676

000-27-690-742 C27−50−111−06 4000 FH

000-27-900-001 C27−10−105−01 500 FH CW 27-May-09 15676 500 16176

000-27-900-003 500 FH CW 27-May-09 15676 500 16176

Functional Check of the RightInboard-Flap Actuators forLinear-EndplayEFFECTIVITY:IB Flap Actuators:P/N 601R93101-19(P/N 852D100-19)PHASE-IN:Do the initial functional check within2000 Flight Cycles from the issuedate of this TR.


Discard of the Right Wing InboardFlap ActuatorsEFFECTIVITY:IB Flap Actuators:P/N 601 R93101 − 9(P/N 852D100−11) or lowerPHASE−IN:Do the discard within 4000 FlightHours from January 19, 2007 or,before March 31, 2008, whichevercomes first.


Detailed Inspection of the Right WingOutboard Flap Actuators forStructural Integrity and ExternalDisconnectEFFECTIVITY:OB Flap Actuators:P/N 601 R93103−19, −20(P/N 853D100−19, −20) and subsP/N 601 R93104−19, −20(P/N 854D100−19, −20) and subs

Functional Check (Backlash) of theRight Wing Outboard Flap ActuatorsEFFECTIVITY:OB Flap Actuators:P/N 601 R93103−18(P/N 853D100−18) or lowerP/N 601 R93104−10(P/N 854D100−12) or lowerPHASE−IN:Do the initial functional check within500 Flight Hours from January 19,2007.


Detailed Inspection of the Right WingOutboard Flap Actuator Fittings andTrunnion HousingsEFFECTIVITY:OB Flap Actuators:P/N 601 R93103−18(P/N 853D100−18) or lowerP/N 601 R93104−10(P/N 854D100−12) or lowerPHASE−IN:Do the initial detailed inspectionwithin 500 Flight Hours from January19, 2007.


Functional Check of the Right WingOutboard Flap Actuators for InternalDisconnectEFFECTIVITY:OB Flap Actuators:P/N 601 R93103−19, −20(P/N 853D100−19, −20) and subsP/N 601 R93104−19, −20(P/N 854D100−19, −20) and subs

Detailed Inspection of the RightAileron Flutter Damper

Discard of the Right Wing OutboardFlap ActuatorsEFFECTIVITY:OB Flap Actuators:P/N 601 R93103−18(P/N 853D100−18) or lowerP/N 601 R93104−10(P/N 854D100−12) or lowerPHASE−IN:Do the discard within 4000 FlightHours from January 19, 2007 or,before March 31, 2008, whichevercomes first.


Operational Check of the AileronDisconnect System

C27−10−105−01C27−60−106−01

Operational Check of the ManualRoll Priority System

of 158





NUMBERTASK

NUMBER


000-27-900-007 C27−50−111−08 500 FH CW 24-May-09 15676 500 16176

000-27-900-150 C27−10−105−06 5000 FH CW 27-Jan-09 15047 5000 20047

000-27-900-701 C27−30−102−03 5000 FH CW 25-May-09 15676 5000 20676

000-27-900-711 C27−10−105−07 5000 FH CW 24-May-09 15676 5000 20676

000-27-900-712 C27−10−105−05 5000 FH CW 2-Jun-09 15676 5000 20676

000-27-900-714 C27−10−105−05 5000 FH CW 3-Jun-09 15676 5000 20676

000-28-900-702 C28−20−131−01 5000 FH CW 25-May-09 15676 5000 20676

000-31-220-102 C31−40−158−01 5000 FH CW 9-Jun-09 15676 5000 20676

000-34-220-723 C34−10−141−01 24 Months CW 17-Jun-09 15679 730 17-Jun-11

000-34-220-731 C34−10−141−03 8 Months NOT APPLICABLE

000-34-900-123 C34−40−107−01 10000 FH

000-35-900-702 C35−10−128−01 500 FH CW 28-May-09 15676 500 16176

000-36-220-700 500 FH CW 27-May-09 15676 500 16176

000-49-310-120 C26−20−131−01 10000 FH CW 6-Dec-06 10698 10000 20698

Operational Test of the SkewDetection System (IBIT)EFFECTIVITY:Post− Modsum TC601 R15480ORPost−SB 601 R−27−116

Functional Check of Each AileronPCU for Internal Leakage

Operational Check of the ElevatorLoad Limiters

Operational Check of the AileronFlutter−Damper Fluid−LevelTransmitter−Switch

Functional Check (Backlash) of theElevator Control System

Functional Check (Backlash) of theRudder Control System

Leak Check of the APU Fuel−FeedShutoff−Valve

Operational Check of the DataConcentrator Unit (DCU 1 and DCU2)EFFECTIVITY:2 DCU configuration only

Functional Check of the AltimeterScale ErrorEFFECTIVITY:Post−SB 601 R−34−080ORCR34−365With ADC−850AP/N 822−0372−143/−445Post−VSB Rockwell CollinsADC−850()−34−63 or, all otherADC−850A part numbersNOTE:The time interval refers to ADCcomponent time and is counted fromthe date of the last ADC test.

Functional Check of the AltimeterScale ErrorEFFECTIVITY:Post−SB 601 R−34−080ORCR34−365With ADC−850AP/N 822−0372−143/−445Pre−VSB Rockwell CollinsADC−850()−34−63NOTE:The time interval refers to ADCcomponent time and is counted fromthe date of the last ADC test.

Functional Check of the WindshearWarning System (A/C with GPWS)

N/A - EGPWS INSTALLED

Visual Check of the CrewOxygen−Bottle Pressure−Gauge

C36−20−133−01C36−20−133−02

Operational Check of the Bleed−AirLeak Detection System

General Visual Inspection of the APUFirex Tubing

of 158

NEXT DUE

FC

10666

14000

10666

14000

of 158

NEXT DUE

FC

1000

2000

of 158

NEXT DUE

FC

of 158



Location Description Approval Document Compliance Document Date C/W C/W By Status

1 Fuselage Removed scratch on fuselage at FS 260 above LH side windshield. SRM 51-12-00 Air Canada 57 1-Dec-03 Atlantic Coast Airlines CLOSED

2 Windows Scuff found on service door window to be within limits. SRM 56-00-00 271239 25-Jun-04 Atlantic Coast Airlines CLOSED3 Doors Removed gouges on LH overwing emergency exit. SRM 51-12-00 Air Canada 92 12-Feb-03 Atlantic Coast Airlines CLOSED4 Fuselage Scratches removed from FS 685.0 Str 3R. SRM 51-12-00 Air Canada 52 1-Dec-03 Atlantic Coast Airlines CLOSED5 Fuselage Scratch found within limits - Blended per SRM. SRM 53-00-31 Reebaire 18 14-Aug-05 Atlantic Coast Airlines CLOSED

6 Vertical Stabilizer SRM 51-12-00 17-Aug-05 Atlantic Coast Airlines CLOSED

7 Doors 17-Aug-05 Atlantic Coast Airlines CLOSED

8 Wings Dent to RH wing L/E within limits. SRM 57-31-51 FL 322944 1-Sep-05 Atlantic Coast Airlines CLOSED9 Flap Vane Repair to leading edge skin - Inboard flap vane. REO 601R-57-52-004 Reebaire 131 17-Aug-05 Atlantic Coast Airlines CLOSED

10 Flap REO 601R-57-51-143 Reebaire 145 18-Aug-05 Atlantic Coast Airlines CLOSED

11 Wings R&R rivet Otbd L/E of RH wing. SRM 51-40-00 405851-1 21-Oct-05 Atlantic Coast Airlines CLOSED12 Wings Replacement of rivets, wing LE ribs WS50.54 - WS389.0. REO-601R-57-41-001 FL 358805 18-Feb-04 Atlantic Coast Airlines CLOSED13 Wings Dent to LH wing L/E within limits. SRM 57-41-31 1494124-1 28-May-04 Atlantic Coast Airlines CLOSED14 Wings Repair to leading edge skin dent at WS 225.00. SRM 57-41-31 Air Canada 36 1-Dec-03 Atlantic Coast Airlines CLOSED

15 Wings Atlantic Coast Airlines CLOSED

16 Nacelles Delamination repair to Nose inlet cowl SRS053. CMM 71-61-01 Air Canada 98 3-Dec-03 Atlantic Coast Airlines CLOSED17 Nacelles Erosion repair to Nose inlet cowl SRS053. CMM 71-61-01 Air Canada 68 2-Dec-03 Atlantic Coast Airlines CLOSED18 Nacelles Lower core cowl hole repair to honeycomb. CMM 71-12-01 SRS046 379266-05 3-Jul-05 Atlantic Coast Airlines CLOSED19 Nacelles Erosion repair to Nose inlet cowl SRS053. CMM 71-61-01 396965 1-Sep-05 Atlantic Coast Airlines CLOSED20 Nacelles Delamination repair to Nose inlet cowl SRS012. CMM 71-61-01 Air Canada 89 2-Dec-03 Atlantic Coast Airlines CLOSED21 Nacelles Erosion repair to Nose inlet cowl SRS053. CMM 71-61-01 Air Canada 73 12-Dec-03 Atlantic Coast Airlines CLOSED

22 Nacelles REO 601R-71-14-2053 191178 4-Dec-03 Atlantic Coast Airlines CLOSED

23 Nacelles Gouge repaired access cowl internal skin SRS011. CMM 71-61-01 Air Canada 87 2-Dec-03 Atlantic Coast Airlines CLOSED24 Nacelles RH Eng inlet cowl dent 2.25x1.40x.085 SRM 54-11-31 BBD 3 27-Jul-06 Bombardier CLOSED25 Nacelles LH lower trans cowl dent .5x.5x.009 CMM 78-30-00 BBD 4 27-Jul-06 Bombardier CLOSED26 Fuselage Dent 1.2x1.2x.035 left fuselage sta. 365 stringers 14L and 15L SRM 53-00-31 BBD 6 2-Aug-06 Bombardier CLOSED27 Fuselage Fuselage between NLG door and ADG door 2 small dents SRM 53-00-31 BBD 113 2-Aug-06 Bombardier CLOSED28 Fuselage Dent FS 574.00 above right pylon SRM 53-00-31 BBD 29 6-Aug-06 Bombardier CLOSED29 Wings Panel 620AT dent repair REO 601R-57-9654 BBD 27 7-Aug-06 Bombardier CLOSED

30 Flap Vane REO 601R-57-52-004 31-Jul-06 Bombardier CLOSED

31 Flap Vane REO 601R-57-52-004 31-Jul-06 Bombardier CLOSED

32 Wings REO 601R-57-21-030 BBD 75 31-Jul-06 Bombardier

33 Radome Radome has one dead spot on fwd section under boot SRM 51-74-04 BBD 102 28-Mar-08 Bombardier CLOSED34 Fuselage Dent within limits on fuselage skin FS 672 between STR 19L-20L SRM 53-00-31 BBD 111 19-Mar-08 Bombardier CLOSED35 Nacelles RH Exhaust nozzle fairing dent below panel 446BL REO 601R-78-14-770 BBD 112 23-Mar-08 Bombardier CLOSED36 Nacelles Fan Cowl 442AT aft edge is chaffed CMM 71-14-01 SRS090 BBD 114 24-Mar-08 Bombardier CLOSED

Repair No.

Access panel damage - 325BL scratch repair.Access panel damage - 325CL gouge repair.Access panel damage - 325DL gouge repair.Access panel damage - 325AR gouge repair.Access panel damage - 325CR gouge repair.Access panel damage - 325DR gouge repair.Access panel damage - 325ER scratch repair.

Reebaire 157Reebaire 158Reebaire 159Reebaire 160Reebaire 161Reebaire 162Reebaire 163

Allowable damage limits for chafing on LH/RH MLG doors. LHAllowable damage limits for chafing on LH/RH MLG doors. RH

SRM 51-12-00REO 601R-52-82-033

Reebaire 143Reebaire 141

Generic repair for wear damage on outboard flap alignment fitting LH/RH.

R&R rivet Otbd L/E of LH wing.Replacement of rivets, wing LE ribs WS50.54 - WS389.0. Wing leading edge rivets missing - Temporary repair.

SRM 51-42-00601R-57-41-001601R-57-41-037

364026-7Multiple

FL 15822

27-Apr-05Multiple2-Jan-03

Chafing damage on LH/RH upper and LH/RH lower access cowl Aft edge strips. Temporary until 2 inspections then becomes permanent.

RH Inbd Flap Vane L/E chafed at inbd endRH Inbd Flap Vane L/E chafed at mid stop contact pointRH Inbd Flap Vane L/E chafed at outbd stop contact point

BBD 52BBD 53BBD 54

LH Inbd Flap Vane L/E chafed at inbd endLH Inbd Flap Vane L/E chafed at mid stop contact pointLH Inbd Flap Vane L/E chafed at outbd stop contact point

BBD 55BBD 56BBD 57

LH Wing lower plank fuel tank access cutout at WS 12.245 with corrosion

SUBJECT TO INSPECTIONS(1)

Structural Repairs Summary - External RepairsStructural Repairs Summary - External Repairs

of 158



Location Description Approval Document Compliance Document Date C/W C/W By StatusRepair No.

Structural Repairs Summary - External RepairsStructural Repairs Summary - External Repairs

37 Nacelles Core Cowl 445AB is chaffed by hinge latch REO 601R-71-12-2326 BBD 115 29-Mar-08 Bombardier CLOSED

38 Nacelles EO 601R-71-14978 BBD 116 25-Mar-08 Bombardier CLOSED

39 Nacelles REO 601R-71-12-2812 BBD 117 29-Mar-08 Bombardier CLOSED

40 Wings Refueling Door has erosion. Repaired. REO 601R-53-82-009 BBD140 18-Mar-08 Bombardier CLOSED

41 Nacelles RH Engine Inlet Cowl lip skin has 3 gouges CMM 71-61-01 25-Mar-08 Bombardier CLOSED

42 Nacelles EO 601R-71-14792 21-Mar-08 Bombardier CLOSED

43 Wings EO 601R-57-0080 23-Mar-08 Bombardier CLOSED

44 Wings RH Wing Outbd LE Panel disbonded on upper and lower trailing edge EO 601R-57-0080 BBD 234 24-Mar-08 Bombardier CLOSED

45 Nacelles RH Engine Inlet Cowl lip skin repair at 11 o'clock position EO 601R-71-14971 BBD 259 27-Mar-08 Bombardier CLOSED

46 Nacelles RH Engine Inlet Cowl lip skin dent at 5 o'clock position. Within limits. CMM 71-61-01 BBD 260 21-Mar-08 Bombardier CLOSED

47 Nacelles RH Engine core cowl has a dent CMM 71-12-01 Alma OT 947 7-May-07 Alma CLOSED

48 Nacelles REO 601R-78-11-3099 Alma OT 1584 11-Jun-07 Alma CLOSED

49 Fuselage SRM 53-00-31 Alma OT 1600 27-Jul-07 Alma CLOSED

(1) See Structural Deviations Inspections Requirements Book for Details of Airworthiness Limitations

Core Cowl 445AB has a dent approx. 10" frm FWD edge and 20" from outbd side. Repaired.

Core Cowl 445AB has a chafe on second rib on the inner side. Repaired.

BBD 190BBD 274

RH Engine Inlet Cowl lip skin is eroded on upper, lower, inboard and outboard areas

BBD 191BBD 192BBD 193BBD 194

RH Wing LE Panel 630JL disbonded on lower and upper outbd trailing edge

BBD 232BBD 255

RH Engine Exhaust Nozzle Fairing cracked at 6 o'clock position, 2" from fwd edge

Two scratches on fuselage skin at FS 227 between STR 13LH and STR 14LH

of 158



Location Description Approval Document Compliance Document Date C/W C/W By Status

1 Doors Temporary disposition to passenger door seal retainer. 601R-52-11-772 2145109-1 2-Aug-05 Atlantic Coast Airlines CLOSED2 Pylons Generic temporary repair for missing engine pylon seals. LH. 601R-54-63-016 3544204-1 19-Dec-04 Atlantic Coast Airlines CLOSED3 Pylons Generic temporary repair for missing engine pylon seals. RH. 601R-54-63-016 193974 11-Dec-03 Atlantic Coast Airlines CLOSED4 Doors Generic temporary repair for ADG door. 601R-52-44-043 148833 22-Aug-03 Atlantic Coast Airlines CLOSED

5 Fuselage REO 601R-53-61-366 18-Aug-05 Atlantic Coast Airlines

6 Nacelles RH bottom TR chafe repair. CMM 78-30-00 Reebaire 98 17-Aug-05 Atlantic Coast Airlines CLOSED

7 Nacelles 601R-71-61-3003 Reebaire 33 18-Aug-05 Atlantic Coast Airlines CLOSED

8 Doors Repair to passenger door edge member. Aft. 601R-52-11-279 Reebaire 50 16-Aug-05 Atlantic Coast Airlines CLOSED

9 Nacelles RH engine thrust reverser - Chafe damage support fitting blend repair. 601R-78-34-2355 Air Canada 94 2-Dec-03 Atlantic Coast Airlines TEMPORARY

10 Nacelles Thrust reverser blocker door blend repair. LH 1,2,3,4,5,6,7, and 10. 601R-78-30-H0267 Reebaire 123 17-Aug-05 Atlantic Coast Airlines CLOSED

11 Fuselage 601R-53-61-117 17-Aug-05 Atlantic Coast Airlines CLOSED

12 Cargo Cargo door opening panel 281DLW crack repair. AMM 25-00-00-340-806 Air Canada 64 2-Dec-03 Atlantic Coast Airlines CLOSED13 Cargo Cargo door opening panel 281DLW composite repair. SRM 51-25-36 Reebaire 108 16-Aug-05 Atlantic Coast Airlines CLOSED

14 Fuselage 601R-53-61-422 18-Aug-05 Atlantic Coast Airlines CLOSED

15 Fuselage Repair to FS 621 bulkhead Aft vertical stiffner, BL 0.00. 601R-53-61-1495 Reebaire 11 19-Aug-05 Atlantic Coast Airlines CLOSED16 Ram Air Exhaust Repair to ACM ram air exhaust duct vane. 601R-21-52-003 386270-01 27-Jul-05 Atlantic Coast Airlines CLOSED

17 Cargo Repair to liner & caps installation - Cargo compartment. 601R-25-53-005 14-Feb-03 Atlantic Coast Airlines CLOSED

18 Cargo Cargo bay wall panel permaglass repair. AMM 25-00-00-340-806 399047-02 19-Sep-05 Atlantic Coast Airlines CLOSED19 Cargo Repair cargo bay cover 282AZ composite damage. SRM 51-74-16 Reebaire 187 19-Aug-05 Atlantic Coast Airlines CLOSED20 Cargo Cargo bay wall panel damage repair. CMM 25-52-01 Multiple Multiple Atlantic Coast Airlines CLOSED21 Vertical Stabilizer Repair to vertical stabilizer drag angle diaphragm. 601R-55-32-075 Air Canada 91 2-Dec-03 Atlantic Coast Airlines CLOSED22 Engines Repair all eroded fan blade leading edges of RH engine AMM 72-20-00-300-801 Air Canada 70 2-Dec-03 Atlantic Coast Airlines CLOSED

23 Fuselage Repair to pressure bulkhead web FS 621.00, Lintel installation REO 601R-53-61-1230 BBD 27 26-Mar-08 Bombardier

24 APU APU access door cracked at top center REO 601R-49-11-070 BBD 83 19-Mar-08 Bombardier CLOSED25 Doors Pax Door handrail has loose rivets REO 601R-52-11-018 BBD 135 20-Mar-08 Bombardier CLOSED

26 Wings LH Wing-to-Fuselage fitting at STA 473.15 have migrated bushing REO 601R-57-21-407 BBD 218 26-Mar-08 Bombardier

27 APU APU access door chafed in 3 places REO 601R-49-11-070 BBD 219 20-Mar-08 Bombardier CLOSED28 Fuselage Fwd face of rear pressure bulkhead chafed at RBL 8 EO 601R-53-14797 BBD 262 29-Mar-08 Bombardier CLOSED29 Fuselage Fwd face of rear pressure bulkhead chafed at LBL 8 EO 601R-53-14797 BBD 263 29-Mar-08 Bombardier CLOSED

(1) See Structural Deviations Inspections Requirements Book for Details of Airworthiness Limitations(2) Inspect per AWL 57-21-123 at the required MRM threshold

Repair No.

Repair to engine support beam lower web. LH.Repair to engine support beam lower web. RH

391773EO 04-53-042


Repair to chafe damage on ballscrew actuator support assembly - Nose cowl.

Repair to floor support angle FS 621. LHRepair to floor support angle FS 621. RH


Fastener substitute for intercostals at FS 621-625 Str 14. LHFastener substitute for intercostals at FS 621-625 Str 14. RH


65278-1465278-13



Structural Repairs SummaryStructural Repairs SummaryStructural Repairs Summary - Other RepairsStructural Repairs Summary - Other Repairs

Engine Installed on Aircraft MSN: 7707 MFG Date: 4-Jan-02Model: GE34-3B1 TSN: 17,373.41

ESN: GE-E-873331 CSN: 14,795Position: 1 (LH) Status Date: 8-Apr-23

Module Description Partnumber Serial number Cycle Limit (Note 1) Current Cycles Cycles remainingFAN ROTOR

211 Shaft, Forward Fan 6078T51P02 GATH738G 25,000 14,795 10,205212 Disk, Fan 6078T57G05 GEE1FFA3 24,300 14,795 9,505602 Shaft, Fan Drive 6036T78P02 BCM74446 25,000 14,795 10,205

COMPRESSOR ROTOR321 Shaft, Compressor Forward 5037T01P04 PAMBW314 30,000 14,795 15,205322 Blisk, Stage 1 Compressor Rotor 5087T84P01 GLHTF307 22,200 14,795 7,405323 Disk, Stage 2 Compressor Rotor 6036T91P02 GATH7J89 25,000 14,795 10,205324 6078T56P04 GATH77N3 22,000 14,795 7,205325 Disk, Stage 9 Compressor Rotor 6087T01P03 HAAJ6377 25,000 14,795 10,205326 Spool, Stage 10-14 Compressor Rotor 5087T46P02 GATH7EG7 25,000 14,795 10,205327 Shaft, Compressor Rotor Rear 6087T03P03 GEE1FFAA 25,000 14,795 10,205328 Seal, Compressor Discharge Rotating 4019T38P01 PAMCD203 30,000 14,795 15,205

HIGH-PRESSURE TURBINE ROTOR521 Shaft, HPT Rotor 5079T62P02 GWN049T4 30,000 14,795 15,205522 Seal, Balance Piston Air 5079T63P02 NCE3431P 18,000 14,795 3,205523 Plate, Stage 1 Front Cooling 5079T65P06 BSLH8355 30,000 14,795 15,205524 Disk, Stage 1 Turbine 5079T52P09 GATH7LL0 18,000 14,795 3,205526 Plate, Stage 1 Aft Cooling 5123T02P01 BSLN4315 18,000 14,795 3,205528 Coupling, Outer Torque 5079T64P05 NCE7546N 30,000 14,795 15,205529 Plate, Stage 2 Front Cooling 5079T55P04 BSLJ9275 30,000 14,795 15,205530 Disk, Stage 2 Turbine 5079T73P02 GATH7KWA 18,000 14,795 3,205532 Plate, Stage 2 Rear Cooling 5079T56P02 BSLG7354 30,000 14,795 15,205

LOW-PRESSURE TURBINE ROTOR631 Shaft, Turbine Rear 6030T72P02 NCE0029R 25,000 14,795 10,205632 Disk, Stage 3 Turbine 6078T91P01 GATH8AAK 25,000 14,795 10,205634 Seal, Stage 3 and 4 Turbine 5023T59P02 WESE0189 23,000 14,795 8,205635 6078T02P03 GATH87TR 22,000 14,795 7,205637 Seal, Stage 4 and 5 Turbine 5023T67P01 WESD0122 25,000 14,795 10,205638 Cone, Turbine Drive 5023T40P03 BCM75549 25,000 14,795 10,205639 6078T92P01 GATH8A35 25,000 14,795 10,205641 Seal, Stage 5 and 6 Turbine 5023T64P02 WES36092 25,000 14,795 10,205642 6078T89P01 GATH8AA6 25,000 14,795 10,205

Average Rem.: 9,698

NOTE 1: Engine Manual Rev. 44, 31 Mar 2008

NOTE 2:

NOTE 3:

Spool, Stage 3-8 Compressor Rotor (Note 2)

Disk, Stage 4 Turbine



HPC Fwd Spool - EMM states 27,000 CSN limit reduced to 22,000 CSN IAW AD 2004-26-02

#1 Engine - Disk Sheet#1 Engine - Disk Sheet

Engine Installed on Aircraft MSN: 7707 MFG Date: 4-Jan-02

Model: GE34-3B1 TSN: 17,373.41

ESN: GE-E-873331 CSN: 14,795

Position: 1 (LH) Status Date: 8-Apr-23

AD NO. SUBJECT/TITLE

NEXT DUE ORIGINAL COMPLIANCE

Date Hours Cycles DATE TSN CSN Comments

99-11-08 Main Fuel Control Flange Vent Rework X N/A N/A N/A Superseded Superseded By AD 99-23-26 R1

X N/A N/A N/A CLOSED 4-Jan-02 0 0 Complied at OEM

2000-03-03R1 Mandatory Critical Inspection-NDT LCF X N/A N/A N/A FAA A.D. 2000-03-03 Superseded Superseded By AD 2002-05-02

2001-10-03 Removed/Inspect Fan Disk for ARC out X N/A N/A N/A Superseded Superseded By AD 2006-05-04

X N/A N/A N/A CLOSED 4-Jan-02 0 0 Complied at OEM

2001-19-02 B-Sump inspection and cleaning for coking X N/A N/A N/A Superseded Superseded By AD 2003-05-10

Mandatory Inspection Requirements X N/A N/A N/A CLOSED

X N/A N/A N/A CLOSED 1-Sep-02 1260 1299 C/W SB 79-A016 Rev 3

2004-15-03R1 X N/A N/A N/A Superseded Superseded By AD 2006-04-12

X N/A N/A 22000 CF34RJ SB 72-A0165 REV 01 OPEN

X N/A N/A N/A CF34RJ SB 72-A0173 Not Applicable N/A by Disk S/N

2006-05-04 Inspect fan disks to prevent failure of the fan disk X N/A N/A N/A Superseded Superseded By AD 2007-07-07

2007-04-51 X N/A N/A N/A Superseded Superseded By AD 2007-05-16

X N/A N/A N/A CF34RJ SB 72-A0232 Not Applicable N/A by Disk S/N

X N/A N/A N/A CF34RJ SB 72-A0231 REV 01 Not Applicable N/A by Disk S/N

X N/A N/A N/A CF34RJ SB 72-A0233 REV 03 Not Applicable N/A by Disk S/N

X Next piece-part exposure CF34RJ SB 72-A0238 OPEN

ONE TIME

ON GOING

GE S/B REMARKSMETHOD OF COMPLIANCE COMPLIANCE

STATUS

BJ SB A73-32 A73-33RJ SB A73-18 A73-19

99-23-26 R117-Feb-00

Replace BUNA-N-O' Ring in Main Fuel Control & Vent Groove MOD

BJ SB A73-33 A73-40 A73-41RJ SB A73-19 A73-26 A73-25

BJ SB 72-A0088RJ SB 72-A0103

2001-12-0620-Jul-01

New NO. 5 Bearing Rotating Air Seal Repl with P/N 4019T60G03

BJ SB 72-093RJ SB 72-109

RJ Alert SB 79-A014 R1BJ Alert SB 79-A015 R1

2002-05-02 C12-Apr-02

Chapter 05-21-00SEI-756 Manual

CF34-3B1 Engine Manual Rev 42 Dated 30-Sep-2007 has all

requirements of the AD Incorporated

2003-05-10 R118-Nov-03

Install new screenless fittings or fittings rwkd to remove screens in B-Sump oil Scavange System

Comair EO 79-022RJ Alert SB 79-A016

Prevent LCF failure of S5 Lpt Disk P/N 6078T92P01 & S6 Lpt Disk P/N 6078T89P01 with certain SN'S

RJ Alert SB 72-A0173 R3RJ Alert SB 72-A0178 R0

2004-26-0226-Jan-05

Rmv from service Hpc Fwd Spool at first piece part level exposure after 6000 CSN but not later than 22000 CSN.

2006-04-1230-Mar-06

To prevent low cycle fatigue (LCF) failure of LPT stages 5 and 6 Disks

Fan Disks - Perform one time visual and tactile inspection of the bore area

2007-05-1612-Mar-07

Shop Level Inspection for Fan Disk Arc-Out Indications

2007-07-07 R112-Sep-07


2009-07-127-May-09

Combustion Liner and Stage 1 Nozzle - Rework of the Air Balance Piston Stationary Seal

#1 Engine - AD Status#1 Engine - AD Status

150 of 158



SB No. DESCRIPTION STATUSLAST COMPLIANCE

INTERVALTET TEC DATE

72-0085 R00 17-Nov-98 - - - N/A N/A N/A

72-0103 R03 13-Mar-07 - - - N/A N/A N/A

72-0121 R00 03-Jul-01 - - - N/A N/A N/A

72-0161 R02 18-Aug-04 OPEN N/A N/A N/A

72-0165 R01 15-Jun-04 OPEN - - - 22,000 22,000 7,205

72-0173 R05 02-Apr-04 - - - N/A N/A N/A

72-A0178 R04 24-May-05 - - - N/A N/A N/A

EFFECTIVE DATE

THRESHOLD&

INTERVAL

ACCOMPLISHMENTDOCUMENTATION

NEXT DUE

TIME REMAINING

All CF34-3A1 turbofan ESN 807226 through 807557, except SN 807519, 807520, 807535, 807537, 807540, and 807555. All CF34-3B1 turbofan ESN 872001 through 872444, except SN 872339, 872388, 872391, 872393 through 872398, 872404, 872409, 872412, 872415 through 872422, 872433, 872434, and 872439 through 872442. The visual (bright light) inspection must be complied with within the next 50 FH of operation after receipt of this SB. The torque check of the total temperature and pressure boss cap must be complied with within the next 400 FH of operation after receipt of this SB.

One-Time Visual and Torque Inspection of the Total Temperature and

Pressure Boss Cap

N/A Per Engine Serial Number

NOT APPLICABLE

Information only. GE recommends you no longer do this Alert Service Bulletin. This Alert Service Bulletin is superseded by CF34-AL S/B 72-A0233.

Fan Disk Field Management Plan

Superseded byS/B 72-A0233

NOT APPLICABLE

CF34-3A1 ESN 807001 through 807239. This SB is applicable to any HPT bayonet-style borescope plugs PN 5071T39G03 that are in inventory as spares. Within the next 400 hours of engine operation. If CF34 Turbofan SB (CF34-BJ) 72-A0097, (Business Jet application), has been complied with, the intent of this Service Bulletin has been accomplished

One-Time Inspection of HPT Borescope Plugs

N/A Per Engine Serial Number. The requirements of this SB are only ONE TIME

NOT APPLICABLE

CF34-3A1 ESN 807007 through 807661. CF34-3B1 ESN 872001 through 873878, 873880, and 873881. As soon as the borescope plug is removed, but before 4,000 FH. If the engine has more than 4,000 FH, ompliance the next time the cowl is opened.

Relocation of Axis K Lanyard & Plug Assy for

Higher Visibility for CF34-3A1/-3B1 Engines

All CF34-3A1 and CF34-3B1 turbofan engines that have any of these compressor rotor spool stages 3 thru 8, part numbers installed: PN 6078T56P03 or PN 6078T56P04. If greater than 6,000 accumulated cycles, at piece part exposure for compressor rotor spool stages 3 thru 8, but prior to accumulating 22,000 part operating cycles-since-new (CSN).

Compressor Rotor Spool Stages 3 thru 8, Field

Management Plan.

OPEN. The requirements of this SB are only ONE TIME

Do this SB at the next piece part exposure of affected stg 5 and/or stage 6 LPT disks. June 1, 2005 and later, consistent with SB 72-A0178, LPT stage 5 and stage 6 disk listed in Appendix (figure 3 only), may be reinspected in accordance with this SB 72-A0173 provided the stg 5 or stg 6 disk was initially inspected prior to June 1, 2005 in accordance with this SB 72-A0173 and the disk(s) are reinstalled in the engine or LPT module they were removed from. Disk not inspected prior to June 1, 2005 in accordance with this SB 72-A0173 must be replaced with disk not listed in the Appendix (figure 3 or figure 4). June 1, 2005 and later, the replacement engine or module contains a stg 5 and/or stg 6 LPT disk listed in Appendix (figure 3 only) and initially inspected prior to June 1, 2005 and are in compliance with the interval inspection requirement in SB 72-A0178. Replacement engine or LPT modules containing a stg 5 or stg 6 disks listed in Appendix (figure 3 only) and not inspected prior to June 1, 2005, the suspect disk must be replaced with disk not listed in Appendix (figure 3 or figure 4) of this SB 72-A0173 prior to service.

Replacement or Inspection of Stg 5 and 6 LPT Rotor

Disks, and Insp. of Stages 3 and 4 LPT

Disk Arms for Arc Out.

Disk installed on subject engine are not affected.

The requirements of this SB are only ONE TIME

NOT APPLICABLE

Remove within the following intervals or performance of the LPT disk inspections in SB 72-A0173: Disks greater than or equal to 14,750 CSN on the effective date of this SB & which have not been inspected (FPI) at a prior piece part exposure, prior to accumulating an additional 250 CIS since the effective date of this SB. Disks greater than or equal to 14,750 CSN on the effective date of this SB & which have been inspected (FPI) at a prior piece part exposure, prior to accumulating an additional 500 CIS since the effective date of this SB. Disks greater than or equal to 14,500 CSN and less than 14,750 CSN, on the effective date of this SB, at piece part exposure, but prior to accumulating an additional 500 CIS since the effective date of this SB. Disks greater than or equal to 14,250 CSN and less than 14,500 CSN, on the effective date of this SB, at piece part exposure, but prior to accumulating an additional 750 CIS since the effective date of this SB. Disks greater than or equal to 13,000 CSN and less than 14,250 CSN, on the effective date of this SB, at piece part exposure, but prior to accumulating an additional 1,000 CIS since the effective date of this SB.

Removal Plan to Replace or Inspect LPT Disks for Arc-

out Indications



NOT APPLICABLE

#1 Engine - Alert SB Status#1 Engine - Alert SB Status

151 of 158





EFFECTIVE DATE

THRESHOLD&

INTERVAL


NEXT DUE

TIME REMAINING


72-A0222 R02 21-Feb-07 Inspection of LPT Modules CLOSED 12,367.00 11,124 19-Dec-06 N/A N/A CLOSED

72-A0231 R01 07-Mar-07 - - - N/A N/A N/A

72-0232 R01 27-Feb-07 - - - N/A N/A N/A

72-0233 R04 27-Jun-07 - - - N/A N/A N/A

72-0252 27-Oct-08 - - - N/A N/A N/A

72-0253 27-Oct-08 - - - N/A N/A N/A

73-0019 R05 02-Dec-04 - - - N/A N/A N/A

73-0022 R00 19-Jan-99 - - - N/A N/A N/A

73-0024 R01 26-Mar-99 - - - N/A N/A N/A

73-0025 R00 07-Jul-99 CLOSED 0.00 0 04-Jan-02 N/A N/A N/A

CF34-3 LPT module, SN GED872001 and up, GED873001 and up, GED950001 and up. For LPT modules installed on wing: FPI inspection of the LPT case shell at the 3 o'clock and 9 o'clock locations (figure 1) approximately 1 inch (25.4 mm) aft of the LPT case forward flange based on - Under 6,000 Hours: FPI inspection not to exceed 5,000 additional LPT module operating hours from the issue date of this SB. 6,000 - 10,000 Hours: FPI Inspection notto exceed 11,000 LPT Module operating hours TSN. > 10,000 Hours: Spot FPI inspection not to exceed 1,000 additional LPT module operating hours from the issue date of this SB.

Delta TechOps Accomplished SB 72-0223

Fan Disk Identified on Table 1 of this SB. Within 500 engine FH from the issue date of this Alert Service Bulletin. If SB 72-A0233 has been complied with, compliance with this SB is not required. Fan disks listed in Table 1, without an asterisk, that have already had a shop inspection per 72-21-00 ECI and FPI, compliance with this SB is not required.

Tactile and Enhanced Visual On Wing Inspection

N/A Per Fan Disk SN The requeriments of this SB are

only ONE TIME

NOT APPLICABLE

Fan disks with SNs identified in Table 1 of this SB. Do this Alert Service Bulletin within 20 engine FH from the issue date of this Alert Service Bulletin.

Fan Disk Bore Tactile and Visual Inspection


only ONE TIME

NOT APPLICABLE

Fan disks with disk SNs identified in Table 1 or Table 2 of this SB. Do this SB within 5000 FH after the issuance date of this SB and no later than March 19, 2012. If a fan disk had inspections per SEI-756 72-21-00 prior to the issuance of this SB and has accumulated less than 100 cycles since the inspection, then performing the inspection requirements in SB 72-A0231 will meet the intent of SB 72-A0233.

Shop Level Inspection for Fan Disk Arc-Out

Indications


only ONE TIME

NOT APPLICABLE

This Alert Service Bulletin at intervals not to exceed 3,000 cycles of operation, and remove the affected parts from service no later than September 30, 2018. For affected fan disks P/N 6078T57G04, P/N 6078T57G05, and P/N 6078T57G06, remove from service prior to reaching 24,300 total accumulated cycles.For parts with 2,500 cycles of operation or more (as of the issue date of this Alert Service Bulletin) from compliance with CF34-AL S/B 72-A0233, GE recommends that you do this Alert Service Bulletin as soon as possible without effect on revenue service but within 500 additional cycles of operation.

Shop Level Repetitive Eddy Current Inspection

for Fan Disk Arc-Out Indications


only ONE TIME

NOT APPLICABLE

GE recommends that you do this Alert Service Bulletin at the next shop visit. For affected fan disks P/N 6078T57G04, P/N 6078T57G05, and P/N 6078T57G06 remove from service prior to reaching 24,300 total accumulated cycles.Compliance with the inspection requirements in CF34-AL S/B 72-A0233, Revision 4 or greater will meet the intent of CF34-AL S/B 72-A0253. The inspectors completing the requirements of CF34-AL S/B 72-A0253 must have completed the course on the CF34 fan disk TEV

Shop Level Eddy Current and Redundant Tactile

Enhanced Visual Inspection for Fan Disk Arc-Out

Indications


only ONE TIME

NOT APPLICABLE

All CF34-3A1 ESN 807001 through 807461, and 807463 through 807518. All CF34-3B1 ESN 872001 through 872278 and 872280. Within the next 4,000 engine operating hours after receipt of this SB, but not to exceed 24 months from the issue date of this Alert Service Bulletin.

Rework of Main Fuel Control for

Overspeed Protection

N/A Per Engine SN. The requirements of this SB are

only ONE TIME

NOT APPLICABLE

MFC listed in tables 1 and 2 of this SB. Prior to the next flight, and on the other engine within the next 400 FH from the date of receipt of this SB. If CF34 Operator’s Wire 99-01 has been complied with, then the intent of this SB has been accomplished.

Replacement of Selected CF34 Main Fuel Controls

N/A Per Main Fuel Control Part Number The

requeriments of this SB are only ONE TIME

NOT APPLICABLE

Main fuel filter PN 4106T62P01 with one of the main fuel filter serial numbers in table 1 of this SB. Replace the main fuel filter at the next exposure, but not later than the next replacement of the filter element. If SB (CF34-BJ) A73-39, Inspection and Replacement of Main Fuel Filter PN 4106T62P01, has been complied with, the intent of this SB has been accomplished

Inspection and Replacement of Main Fuel Filter PN

4106T62P01



NOT APPLICABLE

All CF34-3A1/-3B1 turbofan engines that may have Buna-N material preformed packings PN R1307P020 and PN R1307P141 installed. As soon as possible without effect on revenue service, but within 120 days from the issue date of this Service Bulletin (no later than November 4, 1999). If SB (CF34-AL) 73-20, latest revision, has been complied with, the intent of this bulletin has been accomplished. If SB (CF34-BJ) 73-A0040, latest revision, has been complied with, the intent of this bulletin has been accomplished.

Replacement of Buna-N Material

Preformed Packing

MANUFACTURE ACCOMPLISHED

152 of 158





EFFECTIVE DATE

THRESHOLD&

INTERVAL


NEXT DUE

TIME REMAINING


73-0035 R03 25-Apr-08 OPEN 0.00 0 30-Dec-99 N/A N/A

79-0014 R03 31-Jan-03 CLOSED - - - N/A N/A N/A

79-0016 R00 17-Jun-02 CLOSED 1,260.00 1,299 01-Sep-02 N/A N/A N/A

All CF34-3 turbofan engine MFCs & MFPs. Asia (1): 4,000 hours. China (2,3): Shop visit. India (2,3): Shop visit. Japan: 1,500 hours. Africa (2): 10,000 hours. N America (2,3): Shop visit. S. America (2): 10,000 hours. Europe (2): 10,000 hours. Australia (2): 10,000 hours. Unknown: 1,500 hours. (1) Exceptions for the Asian region include China, India, and Japan. (2) If the aircraft is re-fueled in the Asian region more than 50 % of the time since the initial SB inspection, re-inspect per the Asian region inspection intervals. (3) If the aircraft is re-fueled outside this region since the initial SB inspection, and has not been operated in the Asian region, re-inspect every 10,000 hours.

Inspection of MFC Input Drive Shaft Spline, Main Fuel Pump Control Drive

Shaft Spline, and Main Fuel Pump Secondary Drive

Shaft Spline


Next Shop Visit

All CF34-3A1 & CF34-3B1 Engines. Initial and follow-on inspections or checks directed by this Alert Service Bulletin be accomplished within the operating intervals specified by paragraph 4 Table 1 of this SB. If SB (CF34-AL) 79-A0016, has been complied with, the intent of this SB has been accomplished. If (CF34-BJ) 79-A0015, has been complied with, the intent of this SB has been accomplished. If SB (CF34-BJ) 79-A0017, has been complied with, the intent of this SB has been accomplished.

Field Management Program to Prevent B-sump Oil

Release Events

SB 79-0016A complied by Comair Airlines.


All CF34-3A1 engines, CF34-3B1 ESN 872001 through 873520. Next A-check interval on engines with more than 4000 hours TSN or within 1000 hours since last overhaul. If SB (CF34-BJ) 79-A0017, has been complied with, the intent of this SB has been accomplished.

B-Sump Scavenge Screenless Fittings - Field

Rework Program

SB 79-0016A complied by Comair Airlines.



ESN: GE-E-873333 CSN: 14,795Position: 2 (RH) Status Date: 8-Apr-23

Module Description Partnumber Serial number Cycle Limit (Note 1) Current Cycles Cycles remainingFAN ROTOR

211 Shaft, Forward Fan 6078T51P02 GWN042FN 25,000 14,795 10,205212 Disk, Fan 6078T57G05 GEE1FF95 24,300 14,795 9,505602 Shaft, Fan Drive 6036T78P02 BCM74056 25,000 14,795 10,205

COMPRESSOR ROTOR321 Shaft, Compressor Forward 5037T01P04 PAMBW316 30,000 14,795 15,205322 Blisk, Stage 1 Compressor Rotor 5087T84P01 GLHTF29K 22,200 14,795 7,405323 Disk, Stage 2 Compressor Rotor 6036T91P02 GATH7FWC 25,000 14,795 10,205324 Spool, Stage 3-8 Compressor Rotor (Note 2) 6078T56P04 GATH77N7 22,000 14,795 7,205325 Disk, Stage 9 Compressor Rotor 6087T01P03 HAAJ6379 25,000 14,795 10,205326 Spool, Stage 10-14 Compressor Rotor 5087T46P02 GATH7EG5 25,000 14,795 10,205327 Shaft, Compressor Rotor Rear 6087T03P03 GEE1FFK7 25,000 14,795 10,205328 Seal, Compressor Discharge Rotating 4019T38P01 PAMCD177 30,000 14,795 15,205

HIGH-PRESSURE TURBINE ROTOR521 Shaft, HPT Rotor 5079T62P02 GEE1FFG4 30,000 14,795 15,205522 Seal, Balance Piston Air 5079T63P02 NCE8438N 18,000 14,795 3,205523 Plate, Stage 1 Front Cooling 5079T65P06 BSLH8368 30,000 14,795 15,205524 Disk, Stage 1 Turbine 5079T52P09 GATH7L3L 18,000 14,795 3,205526 Plate, Stage 1 Aft Cooling 5123T02P01 NCE6981P 18,000 14,795 3,205528 Coupling, Outer Torque 5079T64P05 NCE7548N 30,000 14,795 15,205529 Plate, Stage 2 Front Cooling 5079T55P04 BSLJ9298 30,000 14,795 15,205530 Disk, Stage 2 Turbine 5079T73P02 GATH7KTM 18,000 14,795 3,205532 Plate, Stage 2 Rear Cooling 5079T56P02 BSLG7359 30,000 14,795 15,205

LOW-PRESSURE TURBINE ROTOR631 Shaft, Turbine Rear 6030T72P02 NCE8975N 25,000 14,795 10,205632 Disk, Stage 3 Turbine 6078T91P01 GATH7FP1 25,000 14,795 10,205634 Seal, Stage 3 and 4 Turbine 5023T59P02 WESE0022 23,000 14,795 8,205635 6078T02P03 GATH7D52 22,000 14,795 7,205637 Seal, Stage 4 and 5 Turbine 5023T67P01 WESD0005 25,000 14,795 10,205638 Cone, Turbine Drive 5023T40P03 BCM73898 25,000 14,795 10,205639 6078T92P01 GATH7EHF 25,000 14,795 10,205641 Seal, Stage 5 and 6 Turbine 5023T64P02 WESF0065 25,000 14,795 10,205642 6078T89P01 GATH7GFN 25,000 14,795 10,205

Average Rem.: 9,698

NOTE 1: Engine Manual Rev. 44, 31 Mar 2008

NOTE 2:

NOTE 3:




HPC Fwd Spool - EMM states 27,000 CSN limit reduced to 22,000 CSN IAW AD 2004-26-02

#2 Engine - Disk Sheet#2 Engine - Disk Sheet

Engine Installed on Aircraft MSN: 7707 MFG Date: 4-Jan-02

Model: GE34-3B1 TSN: 17,373.41

ESN: GE-E-873333 CSN: 14,795

Position: 2 (RH) Status Date: 8-Apr-23

AD NO. SUBJECT/TITLE

NEXT DUE ORIGINAL COMPLIANCE

Date Hours Cycles DATE TSN CSN

99-11-08 Main Fuel Control Flange Vent Rework X N/A N/A N/A Superseded

X N/A N/A N/A CLOSED 4-Jan-02 0 0

2000-03-03R1 Mandatory Critical Inspection-NDT LCF X N/A N/A N/A FAA A.D. 2000-03-03 Superseded

2001-10-03 Removed/Inspect Fan Disk for ARC out X N/A N/A N/A Superseded

X N/A N/A N/A CLOSED 4-Jan-02 0 0

2001-19-02 B-Sump inspection and cleaning for coking X N/A N/A N/A Superseded

Mandatory Inspection Requirements X N/A N/A N/A CLOSED

X N/A N/A N/A CLOSED 1-Sep-02 1260 1299

2004-15-03R1 X N/A N/A N/A Superseded

X N/A N/A 22000 CF34RJ SB 72-A0165 REV 01 OPEN

X N/A N/A N/A CF34RJ SB 72-A0173 Not Applicable

2006-05-04 Inspect fan disks to prevent failure of the fan disk X N/A N/A N/A Superseded

2007-04-51 X N/A N/A N/A Superseded

X N/A N/A N/A CF34RJ SB 72-A0232 Not Applicable

ONE TIME

ON GOING

GE S/B REMARKSMETHOD OF COMPLIANCE COMPLIANCE

STATUS

BJ SB A73-32 A73-33RJ SB A73-18 A73-19

99-23-26 R117-Feb-00

Replace BUNA-N-O' Ring in Main Fuel Control & Vent Groove MOD

BJ SB A73-33 A73-40 A73-41RJ SB A73-19 A73-26 A73-25

BJ SB 72-A0088RJ SB 72-A0103

2001-12-0620-Jul-01

New NO. 5 Bearing Rotating Air Seal Repl with P/N 4019T60G03

BJ SB 72-093RJ SB 72-109

RJ Alert SB 79-A014 R1BJ Alert SB 79-A015 R1

2002-05-02 C12-Apr-02

Chapter 05-21-00SEI-756 Manual

2003-05-10 R118-Nov-03

Install new screenless fittings or fittings rwkd to remove screens in B-Sump oil Scavange System

Comair EO 79-022RJ Alert SB 79-A016

Prevent LCF failure of S5 Lpt Disk P/N 6078T92P01 & S6 Lpt Disk P/N 6078T89P01 with certain SN'S

RJ Alert SB 72-A0173 R3RJ Alert SB 72-A0178 R0

2004-26-0226-Jan-05

Rmv from service Hpc Fwd Spool at first piece part level exposure after 6000 CSN but not later than 22000 CSN.

2006-04-1230-Mar-06

To prevent low cycle fatigue (LCF) failure of LPT stages 5 and 6 Disks

Fan Disks - Perform one time visual and tactile inspection of the bore area

2007-05-1612-Mar-07


#2 Engine - AD Status#2 Engine - AD Status

X N/A N/A N/A CF34RJ SB 72-A0231 REV 01 Not Applicable

X N/A N/A N/A CF34RJ SB 72-A0233 REV 03 Not Applicable

X Next piece-part exposure CF34RJ SB 72-A0238 OPEN

FOR REFERENCE ONLY

2007-07-07 R112-Sep-07


2009-07-127-May-09

Combustion Liner and Stage 1 Nozzle - Rework of the Air Balance Piston Stationary Seal

156 of 158





72-0085 R00 17-Nov-98 - - - N/A N/A N/A

72-0103 R03 13-Mar-07 Superseded by S/B 72-A0233 - - - N/A N/A N/A

72-0121 R00 03-Jul-01 - - - N/A N/A N/A

72-0161 R02 18-Aug-04 OPEN N/A N/A N/A

72-0165 R01 15-Jun-04 OPEN - - - 22,000 22,000 7,205

72-0173 R05 02-Apr-04 - - - N/A N/A N/A

72-A0178 R04 24-May-05 - - - N/A N/A N/A

EFFECTIVE DATE

THRESHOLD&

INTERVAL


NEXT DUE

TIME REMAINING

All CF34-3A1 turbofan ESN 807226 through 807557, except SN 807519, 807520, 807535, 807537, 807540, and 807555. All CF34-3B1 turbofan ESN 872001 through 872444, except SN 872339, 872388, 872391, 872393 through 872398, 872404, 872409, 872412, 872415 through 872422, 872433, 872434, and 872439 through 872442. The visual (bright light) inspection must be complied with within the next 50 FH of operation after receipt of this SB. The torque check of the total temperature and pressure boss cap must be complied with within the next 400 FH of operation after receipt of this SB.

One-Time Visual and Torque Inspection of the Total Temperature and

Pressure Boss Cap

N/A Per Engine Serial Number

NOT APPLICABLE

Information only. GE recommends you no longer do this Alert Service Bulletin. This Alert Service Bulletin is superseded by CF34-AL S/B 72-A0233.

Fan Disk Field Management Plan

NOT APPLICABLE

CF34-3A1 ESN 807001 through 807239. This SB is applicable to any HPT bayonet-style borescope plugsPN 5071T39G03 that are in inventory as spares. Within the next 400 hours of engine operation. If CF34 Turbofan SB (CF34-BJ) 72-A0097, (Business Jet application), has been complied with, the intent of this Service Bulletin has been accomplished

One-Time Inspection of HPT Borescope Plugs


NOT APPLICABLE

CF34-3A1 ESN 807007 through 807661. CF34-3B1 ESN 872001 through 873878, 873880, and 873881. As soon as the borescope plug is removed, but before 4,000 FH. If the engine has more than 4,000 FH, ompliance the next time the cowl is opened.

Relocation of Axis K Lanyard & Plug Assy for

Higher Visibility for CF34-3A1/-3B1 Engines

With SB 72-0161AR02. The requirements of this SB are

only ONE TIME

All CF34-3A1 and CF34-3B1 turbofan engines that have any of these compressor rotor spool stages 3 thru 8, part numbers installed: PN 6078T56P03 or PN 6078T56P04. If greater than 6,000 accumulated cycles, at piece part exposure for compressor rotor spool stages 3 thru 8, but prior to accumulating 22,000 part operating cycles-since-new (CSN).

Compressor Rotor Spool Stages 3 thru 8, Field

Management Plan.


Do this SB at the next piece part exposure of affected stg 5 and/or stage 6 LPT disks. June 1, 2005 and later, consistent with SB 72-A0178, LPT stage 5 and stage 6 disk listed in Appendix (figure 3 only), may be reinspected in accordance with this SB 72-A0173 provided the stg 5 or stg 6 disk was initially inspected prior to June 1, 2005 in accordance with this SB 72-A0173 and the disk(s) are reinstalled in the engine or LPT module they were removed from. Disk not inspected prior to June 1, 2005 in accordance with this SB 72-A0173 must be replaced with disk not listed in the Appendix (figure 3 or figure 4). June 1, 2005 and later, the replacement engine or module contains a stg 5 and/or stg 6 LPT disk listed in Appendix (figure 3 only) and initially inspected prior to June 1, 2005 and are in compliance with the interval inspection requirement in SB 72-A0178. Replacement engine or LPT modules containing a stg 5 or stg 6 disks listed in Appendix (figure 3 only) and not inspected prior to June 1, 2005, the suspect disk must be replaced with disk not listed in Appendix (figure 3 or figure 4) of this SB 72-A0173 prior to service.

Replacement or Inspection of Stg 5 and 6 LPT Rotor

Disks, and Insp. of Stages 3 and 4 LPT

Disk Arms for Arc Out.



NOT APPLICABLE

Remove within the following intervals or performance of the LPT disk inspections in SB 72-A0173: Disks greater than or equal to 14,750 CSN on the effective date of this SB & which have not been inspected (FPI) at a prior piece part exposure, prior to accumulating an additional 250 CIS since the effective date of this SB. Disks greater than or equal to 14,750 CSN on the effective date of this SB & which have been inspected (FPI) at a prior piece part exposure, prior to accumulating an additional 500 CIS since the effective date of this SB. Disks greater than or equal to 14,500 CSN and less than 14,750 CSN, on the effective date of this SB, at piece part exposure, but prior to accumulating an additional 500 CIS since the effective date of this SB. Disks greater than or equal to 14,250 CSN and less than 14,500 CSN, on the effective date of this SB, at piece part exposure, but prior to accumulating an additional 750 CIS since the effective date of this SB. Disks greater than or equal to 13,000 CSN and less than 14,250 CSN, on the effective date of this SB, at piece part exposure, but prior to accumulating an additional 1,000 CIS since the effective date of this SB.

Removal Plan to Replace or Inspect LPT Disks for Arc-

out Indications



NOT APPLICABLE


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EFFECTIVE DATE

THRESHOLD&

INTERVAL


NEXT DUE

TIME REMAINING


72-A0222 R02 21-Feb-07 Inspection of LPT Modules CLOSED 12370.40 11,125 13-Mar-07 N/A N/A N/A

72-A0231 R01 07-Mar-07 - - - N/A N/A N/A

72-0232 R01 27-Feb-07 - - - N/A N/A N/A

72-0233 R04 27-Jun-07 - - - N/A N/A N/A

72-0252 27-Oct-08 - - - N/A N/A N/A

72-0253 27-Oct-08 - - - N/A N/A N/A

73-0019 R05 02-Dec-04 - - - N/A N/A N/A

73-0022 R00 19-Jan-99 - - - N/A N/A N/A

73-0024 R01 26-Mar-99 - - - N/A N/A N/A

73-0025 R00 07-Jul-99 - - - N/A N/A N/A

CF34-3 LPT module, SN GED872001 and up, GED873001 and up, GED950001 and up. For LPT modules installed on wing: FPI inspection of the LPT case shell at the 3 o'clock and 9 o'clock locations (figure 1) approximately 1 inch (25.4 mm) aft of the LPT case forward flange based on - Under 6,000 Hours: FPI inspection not to exceed 5,000 additional LPT module operating hours from the issue date of this SB. 6,000 - 10,000 Hours: FPI Inspection notto exceed 11,000 LPT Module operating hours TSN. > 10,000 Hours: Spot FPI inspection not to exceed 1,000 additional LPT module operating hours from the issue date of this SB.

GE-Aviation Complied With SB 72-223 Rev 1

Fan Disk Identified on Table 1 of this SB. Within 500 engine FH from the issue date of this Alert Service Bulletin. If SB 72-A0233 has been complied with, compliance with this SB is not required. Fan disks listed in Table 1, without an asterisk, that have already had a shop inspection per 72-21-00 ECI and FPI, compliance with this SB is not required.

Tactile and Enhanced Visual On Wing Inspection


only ONE TIME

NOT APPLICABLE

Fan disks with SNs identified in Table 1 of this SB. Do this Alert Service Bulletin within 20 engine FH from the issue date of this Alert Service Bulletin.

Fan Disk Bore Tactile and Visual Inspection


only ONE TIME

NOT APPLICABLE

Fan disks with disk SNs identified in Table 1 or Table 2 of this SB. Do this SB within 5000 FH after the issuance date of this SB and no later than March 19, 2012. If a fan disk had inspections per SEI-756 72-21-00 prior to the issuance of this SB and has accumulated less than 100 cycles since the inspection, then performing the inspection requirements in SB 72-A0231 will meet the intent of SB 72-A0233.

Shop Level Inspection for Fan Disk Arc-Out

Indications


only ONE TIME

NOT APPLICABLE

This Alert Service Bulletin at intervals not to exceed 3,000 cycles of operation, and remove the affected parts from service no later than September 30, 2018. For affected fan disks P/N 6078T57G04, P/N 6078T57G05, and P/N 6078T57G06, remove from service prior to reaching 24,300 total accumulated cycles.For parts with 2,500 cycles of operation or more (as of the issue date of this Alert Service Bulletin) from compliance with CF34-AL S/B 72-A0233, GE recommends that you do this Alert Service Bulletin as soon as possible without effect on revenue service but within 500 additional cycles of operation.

Shop Level Repetitive Eddy Current Inspection

for Fan Disk Arc-Out Indications


only ONE TIME

NOT APPLICABLE

GE recommends that you do this Alert Service Bulletin at the next shop visit. For affected fan disks P/N 6078T57G04, P/N 6078T57G05, and P/N 6078T57G06 remove from service prior to reaching 24,300 total accumulated cycles.Compliance with the inspection requirements in CF34-AL S/B 72-A0233, Revision 4 or greater will meet the intent of CF34-AL S/B 72-A0253. The inspectors completing the requirements of CF34-AL S/B 72-A0253 must have completed the course on the CF34 fan disk TEV

Shop Level Eddy Current and Redundant Tactile

Enhanced Visual Inspection for Fan Disk Arc-Out

Indications


only ONE TIME

NOT APPLICABLE

All CF34-3A1 ESN 807001 through 807461, and 807463 through 807518. All CF34-3B1 ESN 872001 through 872278 and 872280. Within the next 4,000 engine operating hours after receipt of this SB, but not to exceed 24 months from the issue date of this Alert Service Bulletin.

Rework of Main Fuel Control for

Overspeed Protection

N/A Per Engine SN. The requirements of this SB are

only ONE TIME

NOT APPLICABLE

MFC listed in tables 1 and 2 of this SB. Prior to the next flight, and on the other engine within the next 400 FH from the date of receipt of this SB. If CF34 Operator’s Wire 99-01 has been complied with, then the intent of this SB has been accomplished.

Replacement of Selected CF34 Main Fuel Controls



NOT APPLICABLE

Main fuel filter PN 4106T62P01 with one of the main fuel filter serial numbers in table 1 of this SB. Replace the main fuel filter at the next exposure, but not later than the next replacement of the filter element. If SB (CF34-BJ) A73-39, Inspection and Replacement of Main Fuel Filter PN 4106T62P01, has been complied with, the intent of this SB has been accomplished

Inspection and Replacement of Main Fuel Filter PN

4106T62P01



NOT APPLICABLE

All CF34-3A1/-3B1 turbofan engines that may have Buna-N material preformed packings PN R1307P020 and PN R1307P141 installed. As soon as possible without effect on revenue service, but within 120 days from the issue date of this Service Bulletin (no later than November 4, 1999). If SB (CF34-AL) 73-20, latest revision, has been complied with, the intent of this bulletin has been accomplished. If SB (CF34-BJ) 73-A0040, latest revision, has been complied with, the intent of this bulletin has been accomplished.

Replacement of Buna-N Material

Preformed Packing


NOT APPLICABLE

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EFFECTIVE DATE

THRESHOLD&

INTERVAL


NEXT DUE

TIME REMAINING


73-0035 R03 25-Apr-08 Shop Level Inspection OPEN N/A N/A

79-0014 R03 31-Jan-03 CLOSED 0.00 0 01-Sep-02 N/A N/A N/A

79-0016 R00 17-Jun-02 CLOSED 0.00 0 01-Sep-02 N/A N/A N/A

All CF34-3 turbofan engine MFCs & MFPs. Asia (1): 4,000 hours. China (2,3): Shop visit. India (2,3): Shop visit. Japan: 1,500 hours. Africa (2): 10,000 hours. N America (2,3): Shop visit. S. America (2): 10,000 hours. Europe (2): 10,000 hours. Australia (2): 10,000 hours. Unknown: 1,500 hours. (1) Exceptions for the Asian region include China, India, and Japan. (2) If the aircraft is re-fueled in the Asian region more than 50 % of the time since the initial SB inspection, re-inspect per the Asian region inspection intervals. (3) If the aircraft is re-fueled outside this region since the initial SB inspection, and has not been operated in the Asian region, re-inspect every 10,000 hours.

Inspection of MFC Input Drive Shaft Spline, Main Fuel Pump Control Drive

Shaft Spline, and Main Fuel Pump Secondary Drive

Shaft Spline

Next Shop Visit

All CF34-3A1 & CF34-3B1 Engines. Initial and follow-on inspections or checks directed by this Alert Service Bulletin be accomplished within the operating intervals specified by paragraph 4 Table 1 of this SB. If SB (CF34-AL) 79-A0016, has been complied with, the intent of this SB has been accomplished. If (CF34-BJ) 79-A0015, has been complied with, the intent of this SB has been accomplished. If SB (CF34-BJ) 79-A0017, has been complied with, the intent of this SB has been accomplished.

Field Management Program to Prevent B-sump Oil

Release Events

SB 72-0016A complied at OEM. The requirements of this SB are only ONE TIME

All CF34-3A1 engines, CF34-3B1 ESN 872001 through 873520. Next A-check interval on engines with more than 4000 hours TSN or within 1000 hours since last overhaul. If SB (CF34-BJ) 79-A0017, has been complied with, the intent of this SB has been accomplished.

B-Sump Scavenge Screenless Fittings - Field

Rework Program

SB 72-0016A complied at OEM. The requirements of this SB are only ONE TIME

msn 7707 reports - 11-25-09

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