| 10-23-1 |
Piaggio |
Inspect the elevator hinge fittings for corrosion and the stabilizer for delamination, repair as specified | P180 |
| 10-22-8 |
Eurocopter |
Replace each installed servo control that has a serial number listed in AD as specified | AS350B,BA,B1,B2,B3,D; AS355E,F,F1,F2,N |
| 10-22-7 |
Eurocopter |
Supersedes 06-26-51 | Inspect tail rotor control lever if affected | MBB-BK-117 |
| 10-21-9 |
Piaggio |
Inspect the LH and RH engine mounted fuel heater for wear damage and minimum clearance as specified | P180 |
| 10-21-8 |
Piaggio |
Repetitive visual checks of oil levels and inspections of the oil dipsticks to detect faulty units | P180 |
| 10-21-7 |
Eurocopter |
Inspect for the proper operation of contactors 53Ka and 53Kb as specified | AS350B3, EC130B4 |
| 10-21-19 |
Bombardier |
Replace the aluminum fire extinguisher discharge tubes with new, improved stainless steel tubes as specified | Lear 45 |
| 10-21-18 |
Cessna |
Perform a general and focused inspection of the wing for internal and external damage from wing station 23 to the wing tip as specified | 336 and 337 models |
| 10-21-15 |
Embraer |
Rework the elevators, elevator trim tabs, and aileron surfaces by drilling additional drain holes as specified | Phenom 100 |
| 10-21-14 |
Piaggio |
Replace as required rivets of the joint brackets on the RH and LH beam with "Hi-Lok" fasteners | P180 |
| 10-20-5 |
Turbomeca |
Check the fuel metering system and perform maintenance procedures; repeat as specified every 210 operating hours | Arriel 2B |
| 10-20-4 |
Gulfstream |
Revise the Limitations section of the AFM regarding maximum air brakes operation/extended speed | G200 |
| 10-20-3 |
Bombardier |
See AD regarding balance washer screw failure on ADG/ram air turbines | CL604 / CL605 |
| 10-20-24 |
Eclipse |
Issued to correct uncommanded changes to Com frequency, altitude preselect and transponder codes | EA500 |
| 10-20-21 |
Agusta |
If applicable by part number, modify the fuselage electrical and overhead panel electrical installation with a BATT BUS circuit breaker mod kit | A109E |
| 10-20-20 |
Eurocopter |
Issued to detect a crack in the web of the planet gear carrier, borescope as specified | EC155B,B1; SA360C; SA365C,C1,C2,N,N1,N2,N3; SA366G1 |
| 10-20-2 |
Eurocopter |
Replace each affected hydraulic pump as specified | AS332C, L, L1, L2 |
| 10-20-10 |
Cessna |
Supersedes 06-23-5 | Inspect elevator inboard-hinge brackets as specified | 750 |
| 10-2-8 |
Turbomeca |
Visually inspect for absence of oil leakage or seepage from both unions of the intermediate bearing return flexible pipes | Turmo IV A and IV C |
| 10-2-7 |
Eurocpoter |
Tap and visually inspect each blade in the root doublers for a void and in the forward and aft edges for a paint crack in the areas depicted | SA315B, SA319B |
