|
Number
|
Issued by
|
Issue date
|
Subject
|
Approval Holder / Type Designation
|
Effective date
|
Attachment |
|
US-2005-20-30
|
|
2005-10-12
|
SUPERSEDED BY FAA AD 2009-18-07
|
|
2005-11-16
|
|
|
F-2005-160
|
|
2005-10-12
|
Fuel - Fuel Quantity Indicators - Identification
|
|
2005-09-08
|
|
|
F-2002-424R3
|
|
2005-10-12
|
[Correction] Main Gearbox - Bevel Gear - Inspection
|
|
2005-04-09
|
|
|
CF-2005-37
|
|
2005-10-11
|
Cracking of the Outer Wing Fuel Access Panel
|
-
DE HAVILLAND AIRCRAFT OF CANADA LTD.
|
2005-10-31
|
|
|
US-2005-20-15
|
|
2005-10-06
|
Flight Controls - Rudder Pedal Torque Tube Assembly - Inspection / Replacement
|
|
2005-11-10
|
|
|
CF-2005-13R1
|
|
2005-10-06
|
SUPERSEDED BY TRANSPORT CANADA AD CF-2011-30
|
|
2005-11-07
|
|
|
US-2005-20-13
|
|
2005-10-05
|
Fuselage - Section 43 Lower Lobe Frames - Inspection
|
|
2005-11-09
|
|
|
US-2005-20-16
|
|
2005-10-05
|
Wing L/E Slat Tracks Inboard Attach Fittings - Inspection / Replacement
|
|
2005-11-09
|
|
|
US-2005-20-31
|
|
2005-10-05
|
CANCELLATION OF FAA AD 91-08-51
|
|
2005-10-05
|
|
|
US-2004-19-06R1
|
|
2005-10-05
|
SUPERSEDED BY FAA AD 2012-09-04
|
|
2004-11-01
|
|
|
F-2004-066R1
|
|
2005-10-05
|
Doors - Lateral Cargo Hold Doors - Pre-Flight Locking
|
|
2005-10-22
|
|
|
US-2005-20-18
|
|
2005-10-04
|
Flap Actuator Attachment Fittings - Inspection / Repair / Replacement
|
|
2005-11-08
|
|
|
G-2005-0029
|
|
2005-10-04
|
[Corrected] Engine - IP Turbine Bearing Oil Vent & Bearing Chamber - Inspection
|
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
|
2005-09-30
|
|
|
US-2003-17-07R1
|
|
2005-10-03
|
Engine and Auxiliary Power Unit Fire Extinguishers - Test / Trouble-Shooting
|
-
BOEING
-
DC-10
-
DC-8
-
DC-9
-
MD-11
-
MD-88
-
MD-90
|
2003-09-24
|
|
|
US-2005-20-11
|
|
2005-10-03
|
Engine - Third Stage Turbine Wheels Hub/Shroud Seal Joints - Inspection
|
-
ROLLS-ROYCE CORPORATION (USA)
|
2005-10-18
|
|
|
BR-2001-12-02R1
|
|
2005-09-30
|
Static Pressure Port Positioning / Airframe Skin Rework / Inspection
|
|
2005-09-30
|
|
|
US-2005-19-06
|
|
2005-09-30
|
SUPERSEDED BY FAA AD 2006-09-01
|
|
2005-09-30
|
|
|
IT-2005-406
|
|
2005-09-29
|
Main Rotor - M/R Blades P/N 206-010-200-All - Inspection/Rework
|
-
LEONARDO S.p.A. HELICOPTERS
|
2005-10-14
|
|
|
CF-2004-26R1
|
|
2005-09-28
|
Fluorescent Lighting System – Lamp Holder Overheating
|
-
DE HAVILLAND AIRCRAFT OF CANADA LTD.
|
2005-11-10
|
|
|
CF-2005-36
|
|
2005-09-28
|
Structural Life Limit
|
|
2005-12-29
|
|