| 01-8-14 |
Turbomeca |
Superseded by 13-11-9 |
| 01-8-13 |
Gulfstream |
Perform visual inspection of landing gear door control valve for specified part number; modify if identified | I,II,III,IV,V |
| 01-8-10 |
Aerostar |
Replace both landing gear lower side brace assemblies in main landing gear | |
| 01-8-1 |
JanAero Devices |
Superseded by 01-17-13 |
| 01-7-4 |
Cessna |
Inspect bulkhead web for round bulkhead web doubler; install new right & left bulkhead web doubler as specified | X |
| 01-7-3 |
Hartzell Propeller |
Disassemble, clean and inspect Y-shank series propellers | Various hub serial numbers |
| 01-7-11 |
Learjet |
Visually inspect main landing gear tires for damage, failure or irregularity | Various Lear models |
| 01-6-6 |
Cessna |
Inspect main landing gear pivot assemblies for cracks | Install new bushings on both landing gear pivot assemblies | 172RG |
| 01-6-5 |
Socata |
Relocate oil breather vent location as specified | TBM 700 |
| 01-6-17 |
Cessna |
Inspect for proper engine idle speed and fuel control mixture setting as specified; adjust fuel servo | Ammend AFM as directed | 172R,S |
| 01-6-1 |
New Piper |
Supersedes 70-26-6 & 80-2-15 | Inspect rudder and elevator spars and elevator butt ribs for cracks | Modify/repair as specified | PA-31,-300 |
| 01-5-9 |
Bell Helicopter |
Modify electrical system as specified | 430 |
| 01-5-6 |
Rolls Royce |
Superseded by 03-7-11 |
| 01-5-4 |
Piaggio |
Inspect flap actuators for incorrect maneuvering & evidence of grease/oxidation around gear box | P-180 |
| 01-5-3 |
Socata |
Superseded by 02-9-11 |
| 01-4-7 |
Socata |
Install thermal protection sleeve on propeller governor flexible cable | TBM 700 |
| 01-4-14 |
Eurocopter |
Supersedes 85-14-6 | Repetitively inspect fuselage-to-tailboom attachment bolts and frame as specified | AS350, 355 |
| 01-4-13 |
Eurocopter |
Supersedes 98-10-9 | Inspect each blade spar for crack by dye penetrant or eddy curent as specified | Clean each blade root as directed | SA-315B,316B |
| 01-4-12 |
Eurocopter |
Inspect main gear box in area of tube cylindrical casing on fitting; replace tube as specified | EC120B |
| 01-4-10 |
Pratt&Whitney Eng |
Remove stage 4 low pressure turbine disks as specified | Hawker 1000, Lear 60 |
