| 08-22-18 |
Cessna |
Applicable to Cessna 150s and 152s with a ballistic parachute with S/N range of 50001 - 50006 via STC SA64CH; See AD | 150 models, 152 and A152 |
| 08-22-15 |
Dassault |
Supersedes 07-2-1 | Perform an engine fire detection integrity check as specified | Falcon 200EX |
| 08-22-11 |
Beechcraft |
Inspect/replace engine hydraulic pump pressure output hose assemblies if applicable by S/N as specified | Premier 1 |
| 08-21-9 |
Bombardier |
Supersedes 08-8-6 | Inspect wing leading edges or forward upper wing surfaces for forst, ice, or snow | CL-600, -601, -601-3A,-3R, 604 |
| 08-21-8 |
Air Tractor |
Visually inspect the rudder and vertical fin hinge attachment for loose fasteners; and inspect the rudder or vertical fin skins, spars, hinges, and brackets for cracks and/or corrosion | AT-402, -402A, -402B |
| 08-21-4 |
Beechcraft |
Modify the cabin barometric pressure switch and cabin altitude high switch installations as specified | Premier 1 |
| 08-21-1 |
Beechcraft |
Inspect the MLG upper casing for applicable serial numbers and replace as required | 125 series, 800A, 800XP |
| 08-2-6 |
Garmin |
Inspect Garmin GSM 85 servo gearbox units as specified | Various Aircraft see AD |
| 08-2-4 |
Eclipse |
Supersedes 07-13-11 | Change Limitations section of AFM to operate only in VFR as specified | EA500 |
| 08-2-3 |
Pilatus |
Inspect special bolts that attach MLG retraction actuators and the shock absorbers to the MLG assemblies and proceed as specified | PC-12 |
| 08-2-19 |
Honeywell |
Inspect applicable high pressure turbine rotor discs and assemblies as specified | Multiple models |
| 08-2-18 |
Cessna |
If equipped with BRS-172 or -182 parachute system, remove and replace the pick-up collar support and two retaining screws as specified | 172 and 182 series |
| 08-2-10 |
Eurocopter |
Inspect to identify the load compensator lever and the hydraulic actuator assembly and replace as specified | AS 355 F2, AS 355 N |
| 08-2-1 |
Embraer |
Inspect the interior of center-passenger cabin furnishings for cotton adhesive tape and replace as specified | EMB 135BJ |
| 08-19-8 |
Dassault |
Supersedes 07-18-8 | Revise the limitations section of the Falcon 10 AFM and install a placard in the flight deck concerning icing as specified | Falcon 10 |
| 08-19-6 |
Socata |
Superseded by 11-2-2 |
| 08-19-51 |
Rolls-Royce |
Perform an eddy current inspection (ECI) on the HPT stage 2 wheel as specified | AE3007A series |
| 08-19-5 |
Lycoming |
Superseded by 09-26-12 |
| 08-19-2 |
Bell |
Supersedes 01-1-51 | Visually inspect main rotor hydraulic actuator support for all dowl pins and sealant between support and transmission | 222,B,U,230,430 |
| 08-19-12 |
Honeywell |
Replace the affected ITT ducts listed by part number in the AD | TFE731-4, -4R, -5, -5AR, -5BR, -5R |
