| 09-15-15 |
Bell Helicopter |
Remove the vertical fin and visiually inspect the inboard and outboard surfaces where it attaches to the tail rotor gearbox support for cracks, elongated bolt hole, fretting, distortion and corrosion | Bell 427 |
| 09-15-13 |
Honeywell |
Insepect the CT disc bore area for damage as specified | Multiple models |
| 09-15-1 |
Beechcraft |
Inspect for improper installation of the P60 / J60 electrical connector, associated wiring, and fuel line as specified | G36 |
| 09-14-9 |
Dassault |
Inspect and rework/replace the web of the LH stringer 13 between frames 7 and 8 as specified | Falcon 200EX |
| 09-14-7 |
Dassault |
Verify that seals with correct temperature rating have been installed to prevent hot air leaks when operating wing anti-icing system | Falcon 20-5 series |
| 09-14-3 |
Bombardier |
Revise the Normal Procedures section of the applicable airplane flight manual regarding the stick pusher as specified | 600;601,-3A,3R;604 |
| 09-14-13 |
Pilatus |
Superseded by 12-26-16 |
| 09-14-12 |
Pratt & Whitney |
Within 500 hours after effective date of AD, borescope-inspect the interiors of affected HPC rotor assemblies for cracks, replace as required | PW305A,B |
| 09-14-11 |
Turbomeca |
Superseded by 12-7-9 |
| 09-14-1 |
Turbomeca |
Supersedes 05-17-17 | Inspect the O-ring on the check valve piston in the lubrication unit as specified | Arrius 2F |
| 09-13-6 |
Piper |
Detect and correct damaged, worn, corroded, or non-conforming nose baggage door components | Multiple Piper aircraft |
| 09-13-5 |
Socata |
Insert POH temporary revision 03 into the Emergency Procedures section of the Limitations section of the POH | TBM 700 |
| 09-12-7 |
Agusta |
Before each cargo hook operation, visually inspect the cargo hook lever for any crack as specified | A109E |
| 09-12-51 |
Turbomeca |
Superseded by 09-26-7 |
| 09-11-5 |
Air Tractor |
Supersedes 08-10-12 | Inspect/repair the lower engine mount tube where it is welded to the engine mount ring | AT-400,A; -402,A,B; -502,A,B; -503A; -602; -802,A |
| 09-11-13 |
Learjet |
Superseded by 11-13-10 |
| 09-11-10 |
Eurocopter |
Measure clearance between the outer race and the transmission housing at four positions offset by 90 degrees if unusual vibrations are detected during the start or shutdown phase as specified | EC135 |
| 09-11-1 |
Eurocopter |
Supersedes 95-21-12 | Inspect specified upper/lower surface of main rotor blades on reoccuring basis; replace if bulging | MBB-BK117 A-1,-3,-4; B-1,-2; C-1 |
| 09-10-9 |
Cessna |
Inspect/install rudder stop as specified | Multiple 150 & 152 models |
| 09-10-4 |
Diamond |
Supersedes 07-17-6 | Inspect the nose gear landing leg as specified | DA40, 40F |
