| 02-11-7 |
Raytheon |
Inspect instrument subpanel electroluminescent panel for specified switch near eledctroluminescent panel retaining screw; replace retaining screw as specified | E55,A56TC,58,58P,58TC |
| 02-11-5 |
Air Tractor |
Eddy current inspect lower spar cap as specified | Ammend aircraft records to reflect reduced safe life for wing lower spar cap and safe life limit for winglet usage | 400, 401, 402, 501, 802 |
| 02-11-3 |
Air Tractor |
Eddy current inspect lower spar cap as specified | Ammend aircraft records to reflect reduced safe life for wing lower spar cap and safe life limit for winglet usage | 502 & 503 series |
| 02-11-1 |
Eurocopter |
Modify FADEC software; modify collective linear transducers as specified | EC 135 |
| 02-10-9 |
Gulfstream |
Visually inspect for fuel accumulation inside aft service compartment; perform fuel leak test if evidence found; accomplish modification as specified | G200 |
| 02-10-5 |
MD Helicopter |
Inspect main rotor hub drive plate attach flange and components; replace as specified | 900 |
| 02-10-13 |
Raytheon |
Attach placard modifying exterior door operating procedures as specified | 58P, 60, 65-88 |
| 02-1-9 |
Pilatus |
Superseded by 04-4-1 |
| 02-1-8 |
Gulfstream |
Disable baggage compartment heating blanket system as specified | G-200 |
| 02-1-7 |
Bell |
Perform requirements of Bell Helicopter SB 430-01-19 dated 2-22-01 | 430 |
| 02-1-30 |
Eurocopter |
Inspect main gear box magnet plug for particles as specified | SA 315, 316 |
| 02-1-26 |
Gulfstream |
Inspect bolts on engine inlet cowl and aft nacelle attachment flange as specified | 1124 & 1125 |
| 02-1-23 |
Raytheon |
Perform fluorescent penetrant inspection of engine mount and assemblies | 400, MU300 |
| 02-1-2 |
Turbomeca Engine |
Replace fuel injectors as specified | Eurocopter AS355N, 555UN |
| 02-1-16 |
Fairchild |
Supersedes 86-25-4 & 86-24-11 | Install torque sensing system kit for auto igniters; modify POH | Merlin & Metro |
| 02-1-10 |
Raytheon |
Inspect MLG upper and lower torque knee for cracks | King Air 90 series |
| 01-9-6 |
Cessna |
Visually inspect right and left horizontal stabilizer attachment reinforcement brackets for seam welds along lower inboard and outboard wall/flange; replace as specified | 206,T206 |
| 01-9-11 |
Bell Helicopter |
Supersedes 98-7-3 | Review yoke assembly records for yoke bending loads | modify airspeed indicators; revise RFM | 412 |
| 01-8-8 |
Raytheon |
Repetitively replace V-band exhaust clamp as specified | 33,35,36 |
| 01-8-4 |
Bell Helicopter |
Supersedes 00-25-3 | Inspect the tab on the locking washer on each actuator piston for twisting, damage or unthreading from rod | 205, 212, 412 |
