| 10-6-13 |
Bombardier |
Perform a general visual inspection for cracked or missing ballscrew assembly sleeves of the flap actuator as specified | Lear 45 |
| 10-6-12 |
Thielert |
Replace existing rail pressure control valve with P/N 05-7320-E000702 and modify the Vrail plug to make it compatible with the replacement rail pressure control valve | TAE 125-1 |
| 10-6-11 |
Honeywell |
Inspect to prevent an uncontained failure of a second stage LPCR disc and/or a third stage LPCR disc due to cracks in the bore, see AD for specific engines | Mutiple TFE731 series |
| 10-5-51 |
Eurocopter |
To prevent failure of the main rotor hub, excessive vibrations, loss of main rotor blade, see AD | EC120B |
| 10-5-2 |
Pilatus |
Supersedes 09-8-10 | Insert "Maximum bank angle during climb must not exceed 30 degrees into the Limitations section of the POH as specified | PC12/47E |
| 10-5-10 |
Beechcraft |
This AD is issued to detect and correct the installation of an incorrect bus bar, which could result in failure of the pitot heat annunciators to illuminate. | B300, B300C |
| 10-4-7 |
Turbomeca |
Perform an upgrade of the digital electronic control unit software to version 11.01, to implement modification TU 109 as specified | Arriel 2S1 |
| 10-4-6 |
Thielert |
Modify the engine oil system by installing a filter adaptor to the catch tank as specified | TAE 125-01 |
| 10-4-5 |
McCauley |
Supersedes 03-12-5 | Inspect propeller | 1A103/TCM series |
| 10-4-16 |
SICLI |
Replace all H1-10 AIR Halon 1211 (BCF) portable fire extinguishers manufactured by SICLI, having P/N 1708337B4 and having serial number listed in AD table | Various Aircraft |
| 10-4-14 |
Varga |
Visually inspect the vertical stabilizer front spar for cracks and other damage as specified | 2150, 2180 |
| 10-4-1 |
Dassault |
Inspect RH oxygen line routing for interference from the structure as specified | Falcon 900 EX |
| 10-3-9 |
Piaggio |
This AD mandates a non-destructive inspection and reinforcement-by installation doublers-of the "0" pressure bulkhead | P180 |
| 10-3-6 |
Turbomeca |
Superseded by 12-3-11 |
| 10-3-4 |
Piaggio |
Inspect for minimum clearance and insulation damage to the generator power cables as specified | P180 |
| 10-3-3 |
Bell Helicopter |
Superseded by 11-23-2 |
| 10-26-9 |
Sikorsky |
Affects models with LITREF LCR-100 Attitude Heading and Reference System (AHRS) Unit, See AD for Details | S76A, B, C models |
| 10-26-54 |
Cessna |
Supersedes 10-26-53 | Obtain written approval to operate the airplane from the Manager, Wichita Aircraft Certification Office (ACO) as specified | LC41-550FG and LC42-550FG |
| 10-26-53 |
Cessna |
Superseded by 10-26-54 |
| 10-26-52 |
Bell |
Supersedes 07-19-53 | Remove & replace any affected tail rotor blade as specified | 205, 412, 210, 212 series |
