| 00-25-54 |
Agusta |
Daily check both sides of each tail rotor blade for crack as specified | A109E |
| 00-25-52 |
MD Helicopter |
Supersedes 00-24-51 | Perform tap inspection of each upper and lower blade spar bonded surface for void | 500D,E,F,500C,500 |
| 00-25-4 |
Raytheon |
Perform visual inspection for hydraulic fluid leakage in B-nut area of anti-skid valve assembly and tube | MU-300,400,A |
| 00-25-3 |
Bell |
Superseded by 01-8-4 |
| 00-25-2 |
American Champion |
R1 2001-12 | Inspect wood wing spars for cracks and loose or missing rib nails as specified | Various models |
| 00-25-1 |
New Piper |
Inspect main landing gear inboard door hinge as specified | Various PA-31 models |
| 00-24-51 |
MD Helicopter |
Superseded by 00-25-52 |
| 00-24-5 |
Partenavia |
Inspect by magnetic particle method, nose landing gear upper strut for cracking | P68 |
| 00-24-4 |
Raytheon |
Inspect for misrouted rudder control cable and assembly as specified | A36,B36TC,58 |
| 00-24-25 |
Raytheon |
Inspect as specified drag stay arm of nose landing gear at stop bolt for clearance | 800 |
| 00-24-21 |
Hiller |
Replace undrilled-shank bolts at pivoting joints in control system linkage as specified | UH-12E,L4 |
| 00-24-19 |
Learjet |
Revise AFM as specified on Emergency Decent to include use of masks and oxygen select | 35,A, 36,A |
| 00-24-1 |
Bombardier |
Install protection shields in wheel bay of main landing gear as specified | CL-600 series |
| 00-23-52 |
Sikorsky |
Superseded by 01-10-6 |
| 00-23-51 |
Sikorsky |
Superseded by 00-23-52 |
| 00-23-21 |
TCM Engine |
Supersedes 00-8-51 | Perform crankshaft material inspection as specified | Various engines |
| 00-23-2 |
Bombardier |
Visually inspect inboard flap actuator beam assembly and gaps between vane brackets and skin as specified | CL-604 |
| 00-23-18 |
Learjet |
Visually inspect oxygen tubing for adequate clamping and clearance from electrical wiring and electrical contacts | 60 |
| 00-23-13 |
Galaxy/IAI |
Visually inspect tie rod installation to dust shield and jackscrew assemblies on horizontal stabilizer trim actuator as specified | 1121, Westwind |
| 00-23-12 |
CFE Engine |
Remove and replace specified stage 4 and 5 blisks and impeller aft shafts prior to cycle life | Falcon 2000 |
