| 07-24-3 |
Embraer |
Add two reinforcements to the forward fuselage skin on the LH and RH sides as specified | EMB-135BJ |
| 07-24-15 |
Piaggio |
Inspect fuselage drain holes and the passenger evaporator drain line for propper operation and do all necessary corrective actions | P-180 |
| 07-24-14 |
Hartzell Propeller |
Perform a one time eddy current inspection of the propeller mounting holes and replace the propeller hub if any crack is found as specified | Various Hartzell models |
| 07-24-13 |
Cirrus |
Install a drain hole in the left and right outboard wing tips as specified | SR22 |
| 07-24-12 |
Eclipse |
Inspect the right and left fuel filler adapters for application of primer and/or paint and remove as specified | EA500 |
| 07-24-10 |
Turbomeca |
Replace the fuel filter drain screw with a new one and tighten it to an effective torque of 6.5Nm as specified | Arriel 2S1/2 |
| 07-24-1 |
Beechcraft |
Inspect and replace wiring within galley cabinet as specified | 400A |
| 07-23-7 |
Socata |
Inspect main landing gear wheel axels to determine the batch number, if number is listed in AD then comply as specified | TBM 700 |
| 07-23-17 |
Bell |
Remove and replace each main rotor latch bolt that has a part number that is included in the applicability of this AD | 206A/B |
| 07-23-16 |
Cessna |
Incorporate electrical power relay circuit protection kit part number SB525-24-02 as specified | 525B |
| 07-23-14 |
Diamond |
Modify the engine electrical system by installing additional engine control unit backup batteries following Diamond Aircraft specifications, update aircraft records to show compliance and update the AFM | DA 42 |
| 07-23-13 |
Cessna |
Superseded by 08-26-4 |
| 07-22-2 |
Bell |
Supersedes 02-9-4 | Inspect tip weight retention block and aft tip closure as specified | 205, 212, 412 |
| 07-22-1 |
Bell |
Check for affected serial numbered transmission pylon support spindle, replace as required | 206A/B series |
| 07-21-8 |
Beechcraft |
Inspect panel DA wiring for clearance and for signs of chafing or exposed conductors, replace as specified | 800XP |
| 07-21-12 |
Embraer |
Install heat shrinkable sleeves on the inspection and refueling panel illumination lights wiring, and install nipples on the terminal lugs | EMB-135BJ |
| 07-21-11 |
Pilatus |
Supersedes 00-21-14 | Inspect/repair torque oil-pressure tubes and py pressure pipe assemblies for abrasion damage or distortion | PC-12 |
| 07-21-10 |
Socata |
Inspect and follow instructions in regards to imperfect locking on ground of the upper access door opening interior handle | TBM 700 |
| 07-20-7 |
Beechcraft |
Inspect the left-hand and right-hand starter-generators | 390 |
| 07-2-8 |
Socata |
Inspect/Replace master cylinder yoke of brake system | TBM 700 |
