| 02-8-8 |
Bombardier |
Inspect intergrated drive generator cables; install teflon tubing and clamps | 601, 604 series |
| 02-8-54 |
Bell |
Visually inspect main rotor grips for cracks as specified | 222 series, 230 |
| 02-8-53 |
Bell |
Superseded by 02-9-51 |
| 02-8-4 |
Piaggio |
Replace horizontal stabalizer hinge bushings as specified | P-180 |
| 02-8-3 |
Enstrom |
Replace main rotor gearbox and shaft as specified | 28 & 280 series |
| 02-8-2 |
Fairchild |
Supersedes 01-20-14 | Replace brake shuttle valve as specified; install shield over hydraulic lines; replace rubber fuel hose as specified | Merlin, Metro |
| 02-8-16 |
Eurocopter |
Supersedes 01-19-51 | Replace each main rotor torsion tie bar as specified | SA 341G, SA 342J, SA360C |
| 02-8-1 |
Fairchild |
Replace brake master cylinders as specified | Merlin series, Metro |
| 02-7-2 |
Gulfstream |
Visually inspect main landing gear and components as specified | G200 |
| 02-7-1 |
Cessna |
Replace left and right horizontal stabalizer attachment brackets as specified | 206,207&210 series |
| 02-6-8 |
Rolls-Royce Engine |
Remove from service third stage turbine wheels as specified | 250-C28 series |
| 02-6-6 |
Rockwell Collins |
Modify Mode S transponders as specified | TDR94 (D) |
| 02-6-52 |
Bell |
Superseded by 04-10-7 |
| 02-6-5 |
Rockwell Collins |
Perform pulse test on transport category aircraft with Mode C 621 A-3 ATC transponder | various aircraft |
| 02-6-4 |
Eurocopter |
Replace tail rotor hub pitch change plate bearing as specified | AS350 & 355 series |
| 02-6-12 |
Dassault |
Perform feeder tank leak test as specified | 50 |
| 02-6-10 |
Pilatus |
Replace oxygen tubing and attachments as specified | PC-12 |
| 02-5-6 |
Sikorsky |
Supersedes 86-9-11 | Replace landing gear components as specified | S76A |
| 02-5-5 |
Cirrus Design |
Install cable clamp external to cone adapter on CAP activation cable | Revise AFM as specified | SR20, SR22 |
| 02-5-2 |
GE Engine |
Modify mandatory inspection requirments as specified | CF 34 series |
