| 1 |
AD |
F-2005-079 |
2005-05-25 |
SUPERSEDED BY DGAC FRANCE AD F-2005-129 |
AIRBUS HELICOPTERS SA 330 / AS 332 / EC 225 |
2005-05-02 |
62 |
|
| 2 |
AD |
US-2009-07-53 |
2009-04-27 |
SUPERSEDED by FAA AD 2009-13-01 |
SIKORSKY S-92 |
2009-04-27 |
63 |
|
| 3 |
AD |
IT-1994-230 |
1994-09-29 |
Tail Rotor - Tail Rotor Blade - Inspection |
MECAER AVIATION GROUP SpA NH-500D |
1994-11-05 |
64 |
|
| 4 |
AD |
2017-0147 |
2017-08-10 |
Rotors Flight Control - Tail Rotor Controls - Modification |
AIRBUS HELICOPTERS DEUTSCHLAND EC135/635 |
2017-08-24 |
67 |
|
| 5 |
AD |
2012-0094 |
2012-05-31 |
SUPERSEDED BY EASA AD 2015-0214 |
AIRBUS S.A.S. A330 |
2012-06-14 |
71 |
|
| 6 |
AD |
2022-0139 |
2022-07-07 |
Engine - High Pressure Turbine Nozzle Assembly and Stator Stationary Seal - Inspection |
CFM INTERNATIONAL LEAP-1A/-1C |
2022-07-21 |
72 |
|
| 7 |
AD |
US-2017-19-20 |
2017-09-26 |
Turbine Engine - High-Pressure Compressor Impeller - Removal |
GENERAL ELECTRIC CT7-8 CT7-9 |
2017-10-27 |
72 |
|
| 8 |
AD |
2010-0242-CN |
2011-03-02 |
CANCELLED: Engine - High Pressure / Intermediate Pressure (HP/IP) Structure - Inspections |
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG RB211 TRENT 900 |
2011-03-02 |
72 |
|
| 9 |
AD |
G-2005-0016R1 |
2005-07-10 |
SUPERSEDED BY EASA AD 2005-0024 |
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG RB211 TRENT 700 |
2005-06-16 |
72 |
|
| 10 |
AD |
CF-2025-12 |
2025-03-10 |
Engine Fuel and Control - Electronic Engine Control (EEC) Software - Deficiency to Detect and Protect against Large Engine Bleed Duct Leak |
AIRBUS CANADA LP BD-500 (A220 Series) |
2025-03-18 |
73 |
|