| 00-2-25 |
Mitsubishi |
Revise AFM as specified on operation of deicing boots | MU-2B |
| 00-2-15 |
Raytheon |
Suspend operation if equipped with specified Walter turboprop engine and Avia-Hamilton propeller modification | Select Queen & King Air models |
| 00-2-14 |
Cessna |
Supersedes 98-13-10. Fabricate placard for inspection of exhaust muffler end plates with copy to AFM. Inspect engine exhaust muffler as specified | 182S |
| 00-2-12 |
Bell |
Superseded by 02-6-52 |
| 00-19-1 |
Bombardier |
Modify main landing gear brake units and inboard main landing gear wheels as specified; revise AFM as specified to include brake cooling times for modification | CL-600 |
| 00-18-9 |
Bell |
Inspect tail boom cap angle and adjacent structure for crack with magnifying glass as specified | 412 |
| 00-18-6 |
Allison Engine |
Inspect and replace as applicable Full Authority Digital Electronic Controls, FADEC's, as specified | Citation X |
| 00-18-53 |
Lycoming Engine |
Inspect oil filter converter plate gasket for leaks or displacement as specified; replace if defective | Various models |
| 00-18-51 |
Bell |
Inspect main rotor blade grip with liquid penetrant or eddy current for cracks in threads; repeat inspection as specified | 47 series models |
| 00-18-2 |
Raytheon |
Inspect elevator skin assemblies for separation; replace as specified | Various models |
| 00-18-13 |
Eurocopter |
Supersedes 99-20-13 | Create component log for each tension-torsion strap; review and replace as specified | BO 105LS A-3 |
| 00-18-12 |
Melex |
Inspect with magnetic particles center wing to outboard wing attach joints for cracks in lugs; corrosion and ovalization of main holes | M18 |
| 00-18-11 |
Galaxy/IAI |
Superseded by 04-9-20 |
| 00-17-8 |
Eurocopter |
Supersedes 99-19-22 | Create component card for each rotor tension-torsion strap; review history; replace as specified | BO-105,105CBS-4 |
| 00-17-7 |
Eurocopter |
Superseded by 01-24-8 |
| 00-17-52 |
Agusta |
Inspect rotating scissors assembly for correct installation; replace any described unworthy part as directed | 109E |
| 00-17-11 |
Fairchild |
Inspect main landing gear brace assemblies with dye penetrant for cracks | Merlin III,IV,300,Metro |
| 00-17-1 |
Fairchild |
Supersedes 92-1-2 | Modify B.F. Goodrich landing gear system as specified; repetitively inspect as directed | Merlin III,IV,300,Metro |
| 00-16-6 |
Bell |
Remove and replace arm clamp screws in yaw, roll, pitch and collective syncro resolvers; install guard bracket as specified | 430 |
| 00-16-52 |
Eurocopter |
Daily inspect fairing at left and right side heat shield attachement areas for cracks | AS350B-3 |
