| 07-4-18 |
Learjet |
Modify the left and right-hand standby fuel pump switches as specified | 23,24,24B/C/D/E/F,25,25B/C/D,28,29,31,31A,35,35A,36,36A,55,55B/C |
| 07-4-13 |
Socata |
Inspect main landing gear cylinders for cracks and reapir as specified | TBM 700 |
| 07-3-6 |
Pilatus |
Inspect/replace pedestal legs of executive seats | PC-12 and PC-12/45 |
| 07-3-5 |
Gulfstream |
Superseded by 10-11-2 |
| 07-3-20 |
Turbomeca |
Replace LPG board of the ECU housing | Makila 1A and 1A1 |
| 07-3-17 |
Socata |
Inspect and replace loose rivets on frames C18 BIS and C19 to prevent reduced structural integrity of the tail area | TBM 700 |
| 07-3-16 |
Socata |
Verify no lateral play for both elevator trim tabs and correct as specified if necessary | TBM 700 |
| 07-3-14 |
Turbomeca |
Superseded by 07-19-9 |
| 07-26-9 |
Hartzell |
Inspect for cracks as specified on models HC-, Y, compact series constant speed or feathering props with Hartzell manufactured Y shank aluminum blades | Multiple aircraft see AD |
| 07-26-52 |
Agusta |
Supersedes 01-24-7 | Perform tap inspection of blade tip cap as specified | A109C,E, K2 |
| 07-26-51 |
Eurocopter |
Inspect the tail rotor control rod and adjoining ball pivot and replace any unairworthy parts as specified | EC 135 |
| 07-26-19 |
Rolls-Royce |
Supersedes 04-5-22 | Inspect ice-panels as specified |
| 07-26-16 |
Cessna |
Inspect the routing of the aft fairing wire bundle assembly for adequate separation between the wiring and the hydraulic line and for chafing or damage of the wire assembly | 680 |
| 07-26-12 |
Robinson |
Superseded by 11-12-10 |
| 07-26-11 |
Intertechnique Zodiac AC Sys |
Remove any affected oxygen cylinders as specified | Falcon 900, 20, 200, 50, Eurocopter AS350, SA315 |
| 07-26-10 |
Bell |
Replace affected bolts on helicopters with a servo actuator-to-actuator support attachment bolt as specified | Model 430 |
| 07-26-1 |
Thrush |
Inspect empennage for cracks and repair as specified | S2R series |
| 07-25-8 |
Eurocopter |
Supersedes 06-9-10 | Inspect tail rotor pitch control rod assembly double bearing as specified | 365/155 series |
| 07-25-7 |
Bell |
Inspect the vertical fin and fin support bracket for paint and attaching hardware for proper torque as specified | 206A/B |
| 07-25-10 |
Dassault |
Verify the correct assembly of the flap rotating rods and associated retaining brackets installed in the LH and RH wing root compartment and main gear compartment, inspect and replace if necessary as specified | Falcon 50, 900/EX, 2000/EX |
