| 01-3-8 |
Bombardier |
Revise AFM to include restrictions of altitude and airspeed under single or double hydraulic system failure | CL-600-2B19 |
| 01-3-6 |
Raytheon |
Perform visual inspection of bleed air supply tube assemblies for broken wire braiding on bellow assemblies or for rupturred, leaking bellow assemblies | 300,400 |
| 01-3-52 |
Bombardier |
Revise AFM Limitations and Abnormal Procedures regarding fuel migration in acceleration/climb | CL-600-2B16 |
| 01-3-51 |
Sikorsky |
Conduct fluorescent penetrant inspection in area above upper main rotor shaft output seal and below lower hub attachment flange; replace as specified | S-76B,C |
| 01-3-5 |
Bombardier |
Revise limitations section of AFM for flight into icing conditions | Inspect manifold assembly for missing pieces from spoiller vanes and amend maintenace program as specified | Lear 45 |
| 01-3-4 |
Bombardier |
Superseded by 01-12-24 |
| 01-3-3 |
Bell |
Replace main rotor blade strap fitting as specified | Create component log | 214 |
| 01-3-2 |
Pratt&Whitney Eng |
Replace specified compressor rotors, stage drum assemblies and impellers | Galaxy |
| 01-3-1 |
IAI |
Revise AFM Emergency Procedures main exit door as specified | Galaxy |
| 01-26-7 |
Gulfstream |
Perform visual inspection of electrical connections of fire extinguisher bottles for correct connection | G-IV |
| 01-26-6 |
CFE Engine |
Remove and replace fan rotor disks as specified | CFE 738-1-1B |
| 01-26-55 |
Eurocopter |
Daily inspect tail rotor blade for cracks as specified | As 350, 355 series |
| 01-26-54 |
Eurocopter |
Replace Smart Multifunction Display as specified; ammend RFM as specified | EC 155B |
| 01-26-53 |
Eurocopter |
Superseded by 03-22-11 |
| 01-26-52 |
Eurocopter |
Replace Smart Multifunction Display as specified; ammend RFM as specified | EC 135 |
| 01-26-13 |
Pilatus |
Inspect landing gear emergency extension cable | PC-12 |
| 01-25-6 |
Sikorsky |
Modify # 1 & 2 attitude heading reference signal (AHRS) circuits as specified | S76B |
| 01-25-52 |
Schweizer |
Superseded by 03-13-15 |
| 01-25-4 |
Honeywell Engine |
Remove and replace fuel control as specified | LTS & LTP series engines |
| 01-25-3 |
Cirrus Design |
Inspect for understrength rivets on elevator torque tube and rudder hinge; replace as specified | SR20,22 |
