| No | AD Class | Class Number | Issue Date | Subject | Approval Holder Type/Designation | Effective Date | ATA Chapter | Actions |
|---|---|---|---|---|---|---|---|---|
| 1 | AD | CF-2002-33 | 2002-07-04 | Main Rotor Pendulum Weight Support | BELL TEXTRON CANADA LTD (BTCL) 222 230 | 2002-08-02 | 62 | |
| 2 | EAD | F-2005-179 | 2005-11-23 | Engine Indicating - Tests of Torquemeter Printed Circuit Boards (PCBs) | AIRBUS HELICOPTERS SA 330 / AS 332 / EC 225 | 2005-10-28 | 63 | |
| 3 | AD | D-1978-295-2 | 1980-01-21 | Tail Rotor Blades and Tail Rotor Heads | AIRBUS HELICOPTERS DEUTSCHLAND BO 105 | 1980-01-21 | 64 | |
| 4 | AD | 2014-0129 | 2014-05-16 | Rotors Flight Control - Tail Rotor Control Turnbuckle - Inspection / Replacement | AIRBUS HELICOPTERS SA 330 / AS 332 / EC 225 | 2014-05-30 | 67 | |
| 5 | AD | 2009-0204 | 2009-09-30 | Power Plant - Engine Mount Link Pin Retention Bolts - Inspection / Replacement | AIRBUS S.A.S. A330 A340 | 2009-10-14 | 71 | |
| 6 | AD | US-2022-08-06 | 2022-04-27 | Engine - Compressor Inlet Guide Vane Outer Shroud Bushing and Vane Spindle Bushing - Inspection / Replacement | GENERAL ELECTRIC CF34-8 | 2022-04-29 | 72 | |
| 7 | AD | US-2017-07-04 | 2017-04-18 | SUPERSEDED BY FAA AD 2018-20-23 | GENERAL ELECTRIC GE90 | 2017-04-21 | 72 | |
| 8 | SIB | NE-10-37 | 2010-08-02 | General Electric - CF6-80C2 FADEC Fuel Metering Valve Resolver Feedback Faults | Safety Information Bulletin Airworthiness | 72 | ||
| 9 | AD | G-2005-0008 | 2005-03-08 | Engine Compressor Section- Intermediate Pressure Compressor - Inspection | ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG RB211-524 | 2005-03-18 | 72 | |
| 10 | AD | 2021-0284 | 2021-12-17 | Engine Fuel & Control - Electronic Engine Control Software - Update | AIRBUS S.A.S. A380 | 2021-12-31 | 73 |