| 01-14-16 |
Gulfstream |
Replace nose wheel steering actuator as specified | G-V |
| 01-13-51 |
Bell Helicopter |
Inspect each main rotor driveshaft for crack, loose bolt, nut or red powder residue; replace as specified | 206L-4,407,427 |
| 01-13-5 |
Raytheon |
Remove specified hardware from air turbine discharge duct and water seperator and replace with approved components | 1000,800/XP |
| 01-13-4 |
Eurocopter |
Visually check each cabin sliding door in open position for proper roller tracking | EC 155B |
| 01-13-2 |
Bell Helicopter |
Remove and replace warning horns and install specified terminal junctions | 407 |
| 01-13-11 |
Dassault |
Inspect for proper installation of pins in the dual non-return valves of fire extinguishing system for engines | 10 |
| 01-13-1 |
Bell Helicopter |
Replace retention nuts retaining the tail rotor counterweight bellcrank as specified | 205,212,412 |
| 01-12-9 |
Dassault |
Remove and replace specified protective screens in structure boxes at frame 25 | 900,EX |
| 01-12-6 |
GE Engine |
Check magnetic chip detector indicators on No. 5 bearing rotating air seal as specified | Candadair CL-601 |
| 01-12-24 |
Bombardier |
Supersedes 01-3-4 | Perform ultrasonic inspection of flight spoiler actuator lugs on both center hinge fittings | Canadair CL-600-2B19 |
| 01-12-2 |
Lear |
Replace brake valve lever stop switch and valve adjustment screws as specified | 55,60 |
| 01-12-19 |
Turbomeca Engine |
Limit operating cycle to two hours total time until modification TU 24 is installed | Eurocopter SA 316,315 |
| 01-12-17 |
Raytheon |
Perform one time inspection as specified to confirm installation of rivets at fuselage stations | 800XP |
| 01-12-1 |
Piper |
Inspect left and right inboard flap drive bellcrank assemblies for welding as specified | PA-46-301P,350P,500TP |
| 01-11-4 |
Raytheon |
Inspect main landing gear hydraulic actuators for specified end caps; replace as directed | 99 |
| 01-11-3 |
Raytheon |
Modify KA-33 cooling blower as specified | F33A, A36, B36TC,58/A,C90A,B200 |
| 01-11-2 |
Pilatus |
Supersedes 99-17-8 | Modify generator 2 excitation as specified | PC-12 |
| 01-10-9 |
Honeywell |
Inspect model KC 225 automatic flight control system for computer modifications; perform correction as specified |
| 01-10-6 |
Sikorsky |
Supersedes 00-23-52 | Replace, serial number specific, main rotor shaft | S76A,B,C |
| 01-10-4 |
Air Tractor |
R1 2001-12 | Supersedes 00-14-51 | Modify specified records to show reduced safe life for wing lower spar cap; ammend AFM | Replace wing lower spar cap as specified | 400,401,402,501,503,802 |
