|
Number
|
Issued by
|
Issue date
|
Subject
|
Approval Holder / Type Designation
|
Effective date
|
Attachment |
|
2009-0085
|
|
2009-04-14
|
Fuselage – Reinforcement of Fuselage Frame 19
|
-
GENERAL ATOMICS AeroTec Systems GmbH
|
2009-04-28
|
|
|
2009-0071
|
|
2009-04-14
|
CORRECTED: Engine – High Pressure (HP) / Intermediate Pressure (IP) Turbine Bearing Oil Vent Tube – Inspection / Cleaning / Replacement
|
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
|
2009-04-22
|
|
|
2009-0087-E
|
|
2009-04-11
|
SUPERSEDED BY EASA EMERGENCY AD 2009-0099-E
|
|
2009-04-11
|
|
|
2009-0084
|
|
2009-04-09
|
SUPERSEDED BY EASA AD 2010-0070
|
-
AIRBUS S.A.S.
-
A300-600
-
A300-600ST (Beluga)
-
A310
|
2009-04-23
|
|
|
US-2009-07-12
|
|
2009-04-07
|
High Pressure Rotor 4-step Air Balance Piston Stationary Seals - Removal / Modification / Replacement
|
|
2009-05-07
|
|
|
2009-0082
|
|
2009-04-07
|
SUPERSEDED BY EASA AD 2010-0169
|
|
2009-04-21
|
|
|
2007-0136R1
|
|
2009-04-07
|
Engine - IP Compressor Shaft - Inspection
|
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
|
2007-05-29
|
|
|
US-2009-07-10
|
|
2009-04-06
|
High-Pressure Turbine Rotor (HPTR) Stage 1 Disk Part Number 9367M45G06. New Reduced Life Limit / Removal.
|
|
2009-05-06
|
|
|
US-2009-07-07
|
|
2009-04-06
|
Wiring of the Auxiliary Hydraulic Pump in the Right MLG Wheel Well - Modification.
|
|
2009-05-05
|
|
|
US-2009-07-04
|
|
2009-04-06
|
SUPERSEDED BY FAA AD 2010-21-16
|
|
2009-05-05
|
|
|
2009-0075
|
|
2009-04-06
|
Engine / Engine Fuel and Control – Intermediate Pressure Turbine Over Speed (IPTOS) Protection - Function Activation
|
|
2009-04-20
|
|
|
2009-0077
|
|
2009-04-06
|
Electric and Electronic Common Installation – Hat-rack Connectors – Modification
|
|
2009-04-20
|
|
|
2009-0076
|
|
2009-04-06
|
Electric and Electronic Common Installation – Routing – Installation / Modification
|
|
2009-04-20
|
|
|
2009-0080-E
|
|
2009-04-03
|
SUPERSEDED BY EASA AD 2009-0249 DATED 20 NOVEMBER 2009
|
|
2009-04-07
|
|
|
US-2006-08-08R1
|
|
2009-04-02
|
Wing Lower Spar Cap - Eddy Current Inspections / Safe Life Limit
|
-
AIR TRACTOR
-
AT-250/-300/-400
-
AT-401/-402/-500
|
2009-05-05
|
|
|
US-2009-05-09
|
|
2009-04-01
|
SUPERSEDED BY FAA AD 2013-20-18
|
|
2009-03-31
|
|
|
US-2009-04-05
|
|
2009-04-01
|
Intercooler and inlet and outlet hoses - Replacement / Inspections
|
-
SMA AERO ENGINES GmbH
-
FAA STC SA03302AT
-
STC EASA IM.A.S.02857
-
TEXTRON AVIATION INC.
|
2009-03-27
|
|
|
2009-0079
|
|
2009-04-01
|
SUPERSEDED BY EASA AD 2010-0049
|
-
AIRBUS HELICOPTERS DEUTSCHLAND
|
2009-04-15
|
|
|
CF-2009-07
|
|
2009-03-31
|
Tailboom – Skin Cracking
|
-
BELL TEXTRON CANADA LTD (BTCL)
|
2009-04-06
|
|
|
2009-0074
|
|
2009-03-31
|
Structures – New and Revised Inspections for Fatigue and Environmental Damage – Implementation
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
2009-04-14
|
|