| 95-11-9 |
Robinson |
Low G pushovers prohibited | R-22 |
| 95-11-8 |
Hartzell |
Supersedes 73-2-1 | inspect blade clamp screws | 95 Beech; Cessna 172, 175,-A; Mooney M20A; Piper PA-23, PA-24, PA-25; Lake LA-4 |
| 95-11-6 |
Eurocopter |
Remove and replace main gearbox oil pressure switch | AS 350 series |
| 95-11-5 |
Eurocopter |
Remove and replace main gearbox oil pressure switch | AS 355 series |
| 95-11-16 |
Aerospatiale |
Install pneumatic deicers on the leading edges of the elevator horn | TBM 700 |
| 95-11-14 |
Bell |
Replace non-airworthy crosstubes with airworthy crosstubes | 206 series |
| 95-11-10 |
Robinson |
Low G pushovers prohibited | R-44 |
| 95-11-1 |
Turbomeca |
Superseded by 03-16-3 |
| 95-10-7 |
Bell |
Inspect 42-degree gear box for cracks near gear teeth on pinion | 206 series |
| 95-10-6 |
Bombardier |
Inspect/replace air-driven generator uplock latch per SB A601R-24-019 Rev A | CL 600 series |
| 95-10-4 |
Text-Lyc |
Conduct a revised centrifugal compressor impellor operating cycle count per SB T5313B/17-0020 rev 4 | Bell 205 |
| 95-10-1 |
Hawker |
Superseded by 96-17-9 |
| 95-1-7 |
Fairchild |
Supersedes 83-12-1 | inspect lower wing skin panel; if cracked, install reinforcement doublers; if not cracked, reinspect ev 50 hrs | SA227-AC, -AT |
| 95-1-3 |
Dassault |
Reroute & clamp elec bundles in left-hand cabinet & counterbalancing actuator of passenger door if outside specified limits | Falcon 50 SN 2 thru 232 |
| 95-1-2 |
Hartzell |
Supersedes 93-1-9 & 93-9-4 & 93-12-1 | replace specific blades & hub | MU-2B |
| 95-1-1 |
Terra Corp |
Replace specified transponder | TRT 250 w/specified parts & serial numbers |
| 94-9-8 |
Garrett Eng |
Inspect/replace 3rd stage turbine stator assemblies per cycle schedule | TPE-331-1, -2,-2UA,-3U,-3UW,-5,-5A,-6,-6A |
| 94-9-7 |
Tele-Cont |
Superseded by 95-3-14 |
| 94-9-11 |
Raytheon |
Rescinded 9-3-2002 | Recurringly inspect thrust reverser drive mechanism for wear, abrasion & security of attachments; correct discrepancies | BAe 125-100A & Hawker 1000 series |
| 94-8-15 |
Canadair |
Reinstall improperly installed shoulder bolts; replace adjacent flap actuator housings parts if damaged | specified CL-600-2A12 and -2B16 |
