| 1 |
AD |
G-008-03-89 |
1989-03-01 |
Electrical Power - Introduction of auto transfer from centre busbar to starboard busbar of power supply to No. 2 inverter when undervoltage protection system operates. |
BAE SYSTEMS (OPERATIONS) LTD HS748 |
1989-03-01 |
00 |
|
| 2 |
AD |
F-1986-125-048R1 |
1986-10-15 |
Behaviour of the helicopter on the ground with rotor turning |
AIRBUS HELICOPTERS AS 350 / EC 130 |
1986-10-15 |
00 |
|
| 3 |
AD |
G-005-01-84 |
1984-01-01 |
Flight Controls - Introduction of a once only inspection to ensure correct installation of intermediate cross shaft in the centre console. |
BAE SYSTEMS (OPERATIONS) LTD HS748 |
1984-01-01 |
00 |
|
| 4 |
AD |
G-2070-PRE80 |
1980-01-01 |
Wings - Mainplanes - Repair Scheme No BE.03.10169 to mainplanes not having Mod. BE 214 embodied |
ORPHANED (No TC Holder) BEAGLE |
1980-01-01 |
00 |
|
| 5 |
AD |
G-0070-PRE80 |
1980-01-01 |
Landing Gear - Introduction of baulking device to ensure the nose leg to aircraft attachment pin is installed correctly. |
BAE SYSTEMS (OPERATIONS) LTD HS748 |
1980-01-01 |
00 |
|
| 6 |
AD |
F-1976-037 |
1976-03-02 |
Fuel Tap Control |
ORPHANED (No TC Holder) CERVA |
1976-03-10 |
00 |
|
| 7 |
AD |
F-1966-040 |
1966-12-30 |
Engine Air Intake Unit - Repetitive Inspections |
ORPHANED (No TC Holder) SOCATA (Gardan) |
1966-12-30 |
00 |
|
| 8 |
AD |
2016-0001 |
2016-01-04 |
Air Conditioning - Air Inlet Cover Ring - Inspection / Modification |
AIRBUS HELICOPTERS DEUTSCHLAND MBB-BK 117 |
2016-01-18 |
21 |
|
| 9 |
AD |
2023-0050 |
2023-03-09 |
SUPERSEDED BY EASA AD 2023-0126 |
SONACA AIRCRAFT S.A. |
2023-03-16 |
24 |
|
| 10 |
AD |
US-2003-08-16 |
2003-04-25 |
Electrical Power - RDB Wire Bundle - Inspection / Modification |
BOEING MD-90 |
2003-05-30 |
24 |
|