| 08-14-3 |
Bell |
Determine if the correct number and type of washers are installed, the tailboom bolt is oriented in the correct direction and then correct number of bolt threads are exposed in accordance with the notes in the AD | 206A, 206B, 206L, L1, L3, L4 |
| 08-14-13 |
Cirrus |
If threaded sleeve is or is not installed at the cabin door rod end install the appropriate rod end kit | SR20, SR22 |
| 08-14-1 |
Bell |
Rewire the No. 1 and No. 2 engines' fuel valve switch as specified | 222, 222B, 222U, 230, 430 |
| 08-13-6 |
Cessna |
Inspect the left and right wing electrical wire bundles at the anchor attach points for loose and damaged wiring | 208, 208B |
| 08-13-51 |
Eclipse |
Superseded by 08-16-15 |
| 08-13-4 |
Dassault |
Determine whether any wing anti-ice flexible hose having P/N FAL1006 or ARM224A is installed and replace as sepcified | Falcon 20 |
| 08-13-31 |
Dassault |
Modify the existing engine cowls' locking system as specified if applicable | Falcon 2000 |
| 08-13-30 |
Gulfstream |
Inspect/replace fastner bolts used to attach the scissors to the horizontal and vertical stabilizers and update AFM as specified | Astra SPX, 1125 Westwind, G100 |
| 08-13-28 |
Hartzell Propeller |
Perform an initial ECI of the area around the lubrication holes of the hub blade sockets | Piper Seneca, Seminole, Beech 76 |
| 08-13-27 |
Turbomeca |
Replace the engine module 02 with a module that incorporates Turbomeca modification TF 12A as specified | Arrius 2F |
| 08-13-17 |
Beechcraft |
Replace all affected circuit breaker toggle switches on applicable models as specified | Various Bonanzas and Barons |
| 08-13-16 |
Pratt & Whitney |
Inspect low pressure compressor fan blades and replace as specified | PW305A, 305B |
| 08-13-15 |
Embraer |
Superseded by 11-1-1 |
| 08-13-11 |
DeHavilland |
Develop a schedule for doing the initial and repeat CTs required in the AD | DHC-6-200, -300 |
| 08-13-10 |
Dassault |
Revise the Limitations Section of the AFM to include the AD information | Falcon 7X |
| 08-12-7 |
Embraer |
Remove the sealant used to protect the LH and RH clear ice wiring conduits at the holes through the wing spars and install Teflon spiral as specified | Legacy |
| 08-12-19 |
Dassault |
Inspect for damage of the feeder cable bundle at the right side partition wall at frame 22/23 and repair as specified | Falcon 900, 900EX |
| 08-12-18 |
Dassault |
Check the integrity of the GP bus and IRS2 and repair them as applicable | 2000EX, 900EX |
| 08-12-15 |
Dassault |
Replace the passenger oxygen mask boxes as specified | Falcon 900EX and 2000EX |
| 08-12-14 |
Dassault |
Modify the electrical wiring of the wings' anti-ice system as specified | Falcon 2000EX |
