| 10-2-51 |
Agusta |
Superseded by 11-17-1 |
| 10-2-2 |
Dassault |
Rivise the Limitations Section of the AFM concerning radio-altimeter lock-up conditions | Falcon 7X |
| 10-2-1 |
Turbomeca |
Replace the reduction gear box intermediate pinions as specified | Arriel 1B, 1D, 1D1 |
| 10-19-6 |
Turbomeca |
AD to prevent failure of gas generator second stage turbine disc | Arriel 1A,1A1, 1B, 1C,1C1,1C2, 1D,1D1, 1S1 |
| 10-19-51 |
Bell |
AD intended to detect corrosion or a nonconforming piston rod that could result in a failure of the servo actuator for the main rotor | 222, 222B, 222U, 230, 430 |
| 10-19-5 |
Eurocopter |
If equipped with fenestron tail rotor and applicable part number inspect for stainless steel ring separation from blade sleeve as specified | SA-365N1,N2,N3, EC155B,B1 |
| 10-19-1 |
Rolls-Royce |
Supersedes 09-8-51 | Perform and Eddy current or surface wave ultrasonic test inspection on each affected HPT stage 2 wheel | AE3007A |
| 10-18-9 |
Pratt & Whitney |
See AD regarding intercompressor bleed valve/servo valve malfunction | PW530A, PW545A, PW545B engines |
| 10-18-3 |
Dassault Falcon |
Superseded by 12-12-8 |
| 10-18-2 |
Thielert Engines |
Replace the clutch assembly as specified | TAE 125-01, TAE 125-02-99 |
| 10-17-9 |
Pilatus |
Inspect the power control lever reverse thrust latch handle for free movement as specified | PC12/47E |
| 10-17-6 |
Pratt & Whitney |
Replace the FOHE fuel filter bypass poppet valve with a larger fuel filter bypass poppet valve as specified | PW615F |
| 10-17-18 |
Air Tractor |
Supersedes 10-13-8 | Inspect wing spar caps as specified | 802A |
| 10-17-16 |
Sikorsky |
Inspect the vertical stabilizer aft spar assembly for a crack, loose or working fastner, or corrosion as specified | S-76A, B, C |
| 10-17-15 |
Hawker Beechcraft |
Inspect both starter generators for affected serial numbers and replace if specified | Premier 1 |
| 10-17-1 |
Pratt & Whitney |
Replace the FOHE fuel filter bypass poppet valve with a larger fuel filter bypass poppet valve as specified | PW617F-E |
| 10-16-51 |
Eurocopter |
Inspect for a gap between a fan rotor blade and the upper section of the guide vane bearing housing over the entire width of the blade. | SA330J |
| 10-16-2 |
Embraer |
Perfrom an external detailed inspection for corrosion of the APU | EMB-135BJ |
| 10-15-9 |
Embraer |
Supersedes 09-23-11 | See AD | Phenom 100 |
| 10-15-3 |
Eurocopter |
AD is to detect interference and prevent damage to an electrical harness by lower structure fairing attachment screw | EC 130 B4 |
