| 08-19-11 |
Turbomecca |
Identify and modify/replace listed EEC units as specified | Arrius 2B1, 2B1A, 2B2, 2K2 |
| 08-19-10 |
Socata |
Inspect the gap between the landing gear control button and the floor panel and proceed as specified | TBM 700 |
| 08-19-1 |
Harco Labs |
Inspect/replace pitot/AOA probe and adjust the AFM limitation section as specified | Eclipse 500 |
| 08-17-9 |
Socata |
Supersedes 08-10-13 | Inspect for oil leakage in the pulley drive assembly and repair as specified | TBM 700 |
| 08-17-5 |
Embraer |
Replace the metallic tubes enclosing the vent and pilot valve wires in the left and right wing fuel tanks as specified | EMB-135BJ |
| 08-17-18 |
Embraer |
Inspect the aileron control system inside the wings for possible absence of the cable guard pins as specified | EMB-135BJ |
| 08-16-8 |
Dassault |
Modify the GCU electrical wiring as specified | Falcon 2000EX |
| 08-16-4 |
Bell |
Adjust the rigging of the tail rotor pitch change mechanism as specified | 222, 222U |
| 08-16-20 |
Diamond |
Replace the specified aileron bellcrank and any bent rod ends | DA 42 |
| 08-16-2 |
Beechcraft |
This AD results from reports of the potential for unannunciated loss of the heating function in the left and right stall warning AOA transmitters | Premier 1 |
| 08-16-16 |
Bell |
Adjust the rigging of the tail rotor pitch change mechanism as specified | Bell 230 |
| 08-16-15 |
Eclipse |
Supersedes 08-13-51 | Do a one time pilot evaluation of the throttles as specified and insert temporary revisions into the emergency and normal procedures sections of the AFM | EA500 |
| 08-16-10 |
Gulfstream |
Inspect the clamping blocks for wear and for any loose or damaged hydraulic tubes and replace as specified | G200 |
| 08-15-6 |
Cessna |
Check/replace the engine mounting brackets as specified | 175, 175A |
| 08-15-4 |
Bell |
Adjust the rigging of the tail rotor pitch change mechanism as specified | Bell 430 |
| 08-15-3 |
MD Helicopter |
Inspect the abrasion strip-to-skin bond integrity on each T/R blade using a tap test method as specified | Multiple 369 models |
| 08-14-7 |
Lycoming |
Superseded by 11-26-4 |
| 08-14-6 |
Bell |
Access the horizontal stabilizer ID tag, if applicable inspect the horizontal stabilizer for a crack or deformation around the areas of the inserts as specified | 206L, 206L-1, L-3, L-4 |
| 08-14-5 |
Agusta |
Inspect for interference between the hydraulic lines and the tail rotor control rod assebmly as specified | A109E |
| 08-14-4 |
Eurocopter |
Install load limitation for the starter generator on the overhead instrument panel as specified | AS 355 N |
