| AD number |
Issue date |
TC Holder |
Type |
Subject |
| 2008-0036 |
2008-02-22 |
BAE SYSTEMS (OPERATIONS) LTD |
JETSTREAM4100 |
Landing Gear - Nose Landing Gear (NLG) Wheel Outer Cone - Inspection |
| 2008-0037 |
2008-02-22 |
BAE SYSTEMS (OPERATIONS) LTD |
HP 137 JETSTREAM MK 1, JETSTREAM200, JETSTREAM3100, JETSTREAM3200 |
Landing Gear - Nose Landing Gear (NLG) Wheel Outer Cone - Inspection |
| 2008-0016R1 |
2008-02-22 |
THIELERT AIRCRAFT ENGINES |
TAE125 |
Engine Oil System - Piston Cooling Nozzles - Inspection |
| 2008-0034 |
2008-02-21 |
AIRBUS |
A318, A319, A320, A321 |
[Corrected] Hydraulic Power - Auxiliary Hydraulic Power - Ram Air Turbine (RAT) Gerotor Pump - Replacement |
| 2008-0032 |
2008-02-21 |
AIRBUS |
A318, A319, A320, A321 |
Indicating Systems- Electronic Instrument System (EIS) -Display Management Computer (DMC) Software EIS2 Standard S7 / Installation |
| 2008-0035-E |
2008-02-21 |
EUROCOPTER |
AS 332 |
Fuselage - Outer Skin, Butt Strap & Frame 5295 - Check / Repair / Modification |
| 2008-0033 |
2008-02-19 |
DOWTY PROPELLERS |
R354/4-123-F/13, R354/4-123-F/20, R375/4-123-F/21, R389/4-123-F/25, R389/4-123-F/26, R390/4-123-F/27 |
Propellers - Blade Outer Sleeve - Inspection |
| 2008-0030 |
2008-02-15 |
SAAB AB, SAAB AEROSYSTEMS |
2000 |
Engine Oil - Air Cooled Oil Cooler (ACOC) Self-Sealing Couplings - Inspection / Replacement |
| 2008-0031 |
2008-02-15 |
SAAB AB, SAAB AEROSYSTEMS |
2000 |
Fuel - Wing Tank Fuel Pump Wiring Harness - Replacement; AND Fuel - Fuel Quantity Indication System (FQIS) Signal Conditioner 28 VDC Supply Wiring - Modification |
| 2008-0029 |
2008-02-14 |
EADS SOCATA |
TBM700 |
Equipment/Furnishings - Pilot's Operating Handbook procedure for crew and front passenger seats - Modification |
| 2008-0027-E |
2008-02-13 |
THIELERT AIRCRAFT ENGINES |
TAE125 |
Engine Fuel Injection System - High-Pressure Fuel Line Bracket - Installation |
| 2008-0028-E |
2008-02-13 |
TECNAM |
P92 |
Stabilizers - Vertical Fin Spar - Inspection |
| 2008-0024 |
2008-02-12 |
Rolls Royce Turbomeca |
RTM 322 |
Life Limits / Critical Parts - First Stage High Pressure Turbine Rotor Assembly - Service Life Limitations |
| 2008-0025 |
2008-02-12 |
Rolls Royce Turbomeca |
RTM 322 |
Life Limits / Critical Parts - Special Regular Inspections after Operation in Cold Weather Conditions and Low Altitude |
| 2008-0026 |
2008-02-12 |
AIRBUS |
A330, A340 |
Flight Controls - Flap Down Drive Shaft - Inspection |