|
Number
|
Issued by
|
Issue date
|
Subject
|
Approval Holder / Type Designation
|
Effective date
|
Attachment |
|
2007-0310R1
|
|
2008-01-08
|
Engine - Low Pressure Turbine (LPT) Shaft - Inspection / Replacement
|
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
|
2008-01-02
|
|
|
2008-0001
|
|
2008-01-08
|
SUPERSEDED BY EASA AD 2013-0167
|
|
2008-01-17
|
|
|
US-2007-26-07
|
|
2008-01-07
|
Engine Core Cowls Flipper Door Assemblies - Inspection
|
|
2008-02-01
|
|
|
US-2007-26-20
|
|
2008-01-07
|
Low Pressure Turbine Stage 4 Discs - Identification / Removal from Service
|
|
2008-02-07
|
|
|
US-2007-26-16
|
|
2008-01-07
|
Lower Tail Cone Fairing Wire Bundle Assembly - Inspection
|
|
2008-01-18
|
|
|
US-2007-26-09
|
|
2008-01-07
|
Propeller Blades - Inspection / Rework
|
-
HARTZELL PROPELLER INC.
-
HC-C2Y
-
HC-C3Y
-
HC-E2Y
-
HC-E3YR
-
HC-F2Y
-
HC-F3Y
-
HC-H3Y
-
HC-I2Y
-
HC-I3YR
-
HC-J3Y
-
HC-M2YR
-
HC-M3Y
|
2008-01-30
|
|
|
CF-2007-35
|
|
2008-01-07
|
Fuel System Safety - Introduction of Critical Design Configuration Control Limitations
|
|
2008-01-10
|
|
|
CF-2007-34
|
|
2008-01-07
|
Fuel System Safety -Insufficient Electrical Bonding for Lightning Protection Inside Fuel Tanks
|
|
2008-01-10
|
|
|
CF-2007-36
|
|
2008-01-07
|
Fuel System Safety - Chafing of Fuel Quantity Gauging System Wiring
|
|
2008-01-11
|
|
|
2008-0002
|
|
2008-01-07
|
Wings - Wing Shroud Box Bottom Panel - Modification
|
|
2008-01-21
|
|
|
US-2007-25-20
|
|
2008-01-04
|
Thrust Reverser Wiring and Locking System - Modification / Installation
|
|
2008-01-22
|
|
|
US-2007-26-03
|
|
2008-01-04
|
Main Equipment Center Mounting Brackets, Support Angles, and Moisture Curtains - Installation
|
|
2008-01-22
|
|
|
CF-2007-24R1
|
|
2008-01-04
|
Engine Compressor Turbine Disk Inspection and Retaining Nut Replacement
|
|
2008-01-10
|
|
|
CF-2007-33
|
|
2008-01-04
|
Fuel System Safety - Introduction of Maintenance Tasks
|
-
DE HAVILLAND AIRCRAFT OF CANADA LTD.
|
2008-01-03
|
|
|
US-2007-26-06
|
|
2008-01-04
|
Oxygen Masks Identification / Inspection / Modification
|
|
2008-01-02
|
|
|
US-2007-25-16
|
|
2007-12-21
|
Forward Passenger Doorjam Upper Corners Fuselage Skin - Inspection / Reinforcement / Repair
|
|
2008-01-14
|
|
|
US-2007-23-10
|
|
2007-12-21
|
Main Landing Gear Wheel Well Receptacles Fillet Sealant - Inspection
|
|
2007-12-20
|
|
|
2007-52
|
|
2007-12-21
|
Rolls-Royce RB211-524 and -535E4, RB211 Trent 500, 700 and 800 series engines - Group A Parts - Non-compliance with required Magnetic Particle Inspection (MPI) instructions
|
-
Safety Information Bulletin
|
|
|
|
2007-0313
|
|
2007-12-21
|
SUPERSEDED BY EASA AD 2008-0064
|
-
AIRBUS HELICOPTERS DEUTSCHLAND
|
2008-01-04
|
|
|
2007-0315-E
|
|
2007-12-21
|
SUPERSEDED BY EASA EMERGENCY AD 2008-0053-E
|
|
2007-12-25
|
|
