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20111 ADs
| AD Number | Status | Subject | Effective Date | Superseded By |
|---|---|---|---|---|
| 2006-21-09 | Active |
Identification plate of torque box
|
2006-11-03 | — |
| 2006-20-02 | Active |
Longitudinal rows of fasteners in the bonded skin panels
|
2006-11-02 | — |
| 2006-20-04 | Active |
Inspection of chain assemblies of elevator trim system
|
2006-11-02 | — |
| 2006-20-05 | Active |
Inspect chafing in skin of wing-to-fuselage fairing
|
2006-11-02 | — |
| 2006-17-07R1 | Active |
High pressure compressor (HPC) front hubs and HPC disk
|
2006-11-02 | — |
| 2006-20-01 | Active |
Incorporate restrictions for high altitude operations.
|
2006-11-02 | — |
| 2006-20-07 | Active |
Adds an additional life limit for third- and fourth-stage turbine wheels
|
2006-11-02 | — |
| 2006-20-03 | Active |
Girt bar position of forward passenger doors
|
2006-11-02 | — |
| 2006-19-12 | Superseded |
Engine struts investigation
|
2006-10-30 |
2016-23-02
|
| 2006-19-11 | Active |
Seat stop relocation
|
2006-10-25 | — |
| 2006-21-02 | Active |
Operating Limitations, Abnormal Procedures, and Normal Procedures
|
2006-10-25 | — |
| 2006-19-07 | Active |
Attachment landing assemblies of blow- down panels of wing
leading edges
|
2006-10-24 | — |
| 2006-19-10 | Active |
Adjust crew seat break-over bolts
|
2006-10-24 | — |
| 2006-19-09 | Active |
Passenger seat mod kit
|
2006-10-24 | — |
| 2006-19-02 | Active |
Cracking of the fuselage outer skin at frames 28A and 30A above stringer 30
|
2006-10-17 | — |
| 2006-19-03 | Active |
Fabrication and installation of a wire harness guard in the right wheel well of the main \n landing gear (MLG)
|
2006-10-17 | — |
| 2006-19-04 | Active |
Honeywell COM unit and Mode S transponder
|
2006-10-17 | — |
| 2006-20-51 | Superseded |
Airplane Flight Manual to prohibit takeoffs at less than full-rated thrust
|
2006-10-16 |
2006-20-51 R1
|
| 2006-20-06 | Superseded |
Main fuel pump (MFP) inlet strainer
|
2006-10-16 |
2007-12-15
|
| 2006-19-05 | Active |
Tail rotor (T/R) slider
|
2006-10-16 | — |
| 2006-18-13 | Active |
Hardover prevention system (HOPS) in the roll axis due to a short circuit in the wiring harness
|
2006-10-13 | — |
| 2006-18-17 | Superseded |
Yaw damper actuator portion of the upper and lower rudder power control modules (PCMs)
|
2006-10-13 |
2008-13-03
|
| 2006-18-12 | Active |
Hot detection system of the tail pipe harness of the engine nacelles
|
2006-10-13 | — |
| 2006-18-14 | Superseded |
Cyclic life of stage 1 HPT discs, and stage 1 LPT discs
|
2006-10-13 |
2016-17-01
|
| 2006-18-16 | Active |
Wing spigot bearing retainer kit
|
2006-10-13 | — |
| 2006-18-07 | Active |
Replacing the very high frequency (VHF) antenna located in position 1 of the fuselage with a new,
improved VHF antenna
|
2006-10-11 | — |
| 2006-18-05 | Active |
Disconnect panel
|
2006-10-11 | — |
| 2006-18-06 | Active |
Stainless steel ribs left- and right-hand engine
pylons
|
2006-10-11 | — |
| 2006-18-08 | Active |
Nosewheel tires
|
2006-10-11 | — |
| 2006-19-08 | Active |
Exhaust bends in curvature bend area
|
2006-10-10 | — |
| 2006-17-07 | Superseded |
Fretting and fluorescent magnetic particle inspections (FMPI) for cracking in the area of the tierod holes on the HPC front hubs
|
2006-10-04 |
2006-17-07R1
|
| 2006-18-02 | Active |
Replacing the clamp bases for the fuel vent pipe
|
2006-10-04 | — |
| 2006-18-03 | Active |
Flap system interface wiring
|
2006-10-04 | — |
| 2006-18-01 | Active |
Notar fan system tension-torsion (TT)
straps.
|
2006-10-03 | — |
| 97-06-13R1 | Active |
Rescinds AD 97-06-13.
|
2006-10-02 | — |
| 2006-17-16 | Active |
Wing rear spar lower girder
|
2006-09-29 | — |
| 2006-17-15 | Active |
Replacing the clamp bases for the fuel vent pipe with improved clamp bases
|
2006-09-29 | — |
| 2006-19-06 | Active |
Propeller shaft
|
2006-09-29 | — |
| 2006-17-17 | Active |
Rivets on left and right control column torque tube assemblies
|
2006-09-29 | — |
| 2006-18-11 | Active |
Auxiliary fuel system
|
2006-09-27 | — |
| 2006-17-11 | Active |
Fill and safety fittings of the cargo fire extinguishing bottles
|
2006-09-27 | — |
| 2006-17-10 | Active |
Fluorescent light tube assemblies of the cabin, lavatory, and sidewall
|
2006-09-27 | — |
| 2006-17-12 | Active |
High pressure (HP) turbine discs
|
2006-09-27 | — |
| 2006-19-01 | Active |
Tapered housing of each main servo-control (MSC)
|
2006-09-27 | — |
| 2006-17-08 | Superseded |
HPC exit inner and outer brush seal assembly
|
2006-09-27 |
2007-04-26
|
| 2006-17-13 | Active |
Replacing the existing attachment bolts for the seat belts with longer attachment bolts
|
2006-09-27 | — |
| 2006-18-15 | Superseded |
Front cylinder half of the propeller hub
|
2006-09-25 |
2009-22-03
|
| 2006-16-18 | Superseded |
Installing a warning placard on the TAWS/RMI and
revising the Limitations section of the airplane flight manual (AFM)
|
2006-09-25 |
2006-16-18 R1
|
| 2006-16-17 | Active |
Torque values of the screws that attach the seat tracks
|
2006-09-25 | — |
| 2006-17-01 | Superseded |
Airplane Flight Manual (AFM)
|
2006-09-22 |
2010-10-17
|