|
Number
|
Issued by
|
Issue date
|
Subject
|
Approval Holder / Type Designation
|
Effective date
|
Attachment |
|
F-2002-075R1
|
|
2005-03-16
|
SUPERSEDED BY EASA AD 2011-0024
|
|
2005-03-26
|
|
|
F-2005-029R1
|
|
2005-03-16
|
SUPERSEDED BY EASA AD 2007-0217
|
|
2005-03-26
|
|
|
F-2004-170R1
|
|
2005-03-16
|
Equipments/Furnishings - Hoist Hook - Operational Procedures/Restriction
|
-
AIRBUS HELICOPTERS
-
AS 350 / EC 130
-
AS 355
-
SA 330 / AS 332 / EC 225
-
SA 341/342
|
2005-03-26
|
|
|
F-2005-046
|
|
2005-03-16
|
SUPERSEDED BY EASA AD 2010-0148
|
|
2005-03-26
|
|
|
F-2005-045
|
|
2005-03-16
|
Engine - Icing Conditions - Ground Ice Shedding Procedure
|
|
2005-03-16
|
|
|
F-2005-044
|
|
2005-03-16
|
Landing Gear - MLG Wiring from LGCIU 2 to the EBCU - Modification
|
|
2005-03-26
|
|
|
F-2005-043
|
|
2005-03-16
|
SUPERSEDED BY EASA AD 2006-0081
|
|
2005-03-26
|
|
|
F-2005-042
|
|
2005-03-16
|
Rotor Flight Controls - Ball-type Yaw Controls - Replacement
|
|
2005-03-26
|
|
|
F-2005-047
|
|
2005-03-16
|
CANCELLED BY EASA AD CANCELLATION NOTICE 2009-0118-CN
|
-
SAFRAN HELICOPTER ENGINES
|
2005-03-26
|
|
|
D-2005-115
|
|
2005-03-15
|
Main Rotor System - Introduction of a Life Limit for Main Rotor Blades with Bolted Lead Inner Weights
|
-
AIRBUS HELICOPTERS DEUTSCHLAND
|
2005-03-15
|
|
|
D-2004-299R2
|
|
2005-03-15
|
Landing Gear Up-Lock Hook Replacement
|
|
2005-03-15
|
|
|
US-2005-05-18
|
|
2005-03-14
|
SUPERSEDED BY FAA AD 2021-21-09
|
|
2005-04-18
|
|
|
US-2005-05-15
|
|
2005-03-14
|
Low Pressure Turbine (LPT) Stage 1 Nozzle Assembly - Inspection / Rework / Replacement
|
-
HONEYWELL INTERNATIONAL INC.
|
2005-04-18
|
|
|
US-2005-03-11
|
|
2005-03-11
|
[Correction] Aft Pressure Bulkhead - Inspection / Repair
|
|
2005-03-18
|
|
|
US-2005-05-07
|
|
2005-03-11
|
Engine (PW JT9D) Nacelle Bulkhead Web - Inspection / Repair
|
|
2005-04-15
|
|
|
US-2005-05-08
|
|
2005-03-11
|
Fuselage Frame to Tension Tie Joints - Inspection
|
|
2005-04-15
|
|
|
D-2000-348R6
|
|
2005-03-11
|
Engine - LP Compressor Fan Disk Cracks
|
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
|
2005-03-31
|
|
|
US-2005-05-13
|
|
2005-03-10
|
HPT Second Stage Airseal - Replacement / 2nd Stage HPT Vane Cluster Assembly and 1st Stage Retaining Blade HPT Plate Assembly - Modification
|
-
PRATT & WHITNEY
-
JT9D-59A
-
JT9D-70A
-
JT9D-7Q
|
2005-04-14
|
|
|
G-2005-0009
|
|
2005-03-09
|
SUPERSEDED BY EASA AD 2020-0254
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
2005-04-29
|
|
|
G-2005-0008
|
|
2005-03-08
|
Engine Compressor Section- Intermediate Pressure Compressor - Inspection
|
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
|
2005-03-18
|
|