| 09-10-14 |
Hartzell |
Applies to Hartzell steel hub turbine props listed, see AD | Multiple aircraft |
| 09-1-11 |
Turbomeca |
Perform a one-time inspection of the HMU as specified | Arriel 2B and 2B1 series |
| 08-9-3 |
Agusta |
Inspect the four grooved clamps that attach the engine exhaust ducts and replace if required | A109A, AII, C |
| 08-9-21 |
Dassault |
Inspect for damage of the electrical feeder bundle under the circuit breaker panel and repair/modify as specified | Falcon 50 |
| 08-9-18 |
Taylorcraft |
Inspect the left and right wing lift strut attach fittings for corrosion or cracking and replace as specified | F-19, F-21,-A,-B, F-22,-A,-B,-C |
| 08-9-10 |
Air Tractor |
Supersedes 03-6-1 | Replace wing lower spar cap | 300, 301, 302, 400 series |
| 08-8-6 |
Bombardier |
Superseded by 08-21-9 |
| 08-8-3 |
Pacific Aerospace |
Replace certain pitot heat sensor circuit breakers and add a cooling fan circuit as specified | 750XL |
| 08-8-20 |
Dassault |
Remove and modify affected wing anti-ice telescopic tubes P/N 5035-400 and 5035-500 ball joints as specified | Falcon 2000 |
| 08-8-19 |
Gulfstream |
Inspect the feeder cable, terminal lug 123P/2, and ground point 803GND installed within the left DC power box for chafing and arcing damage as specified | G150 |
| 08-8-16 |
Turbomeca |
Supersedes 02-15-5 | Replace electronic control unit (ECU) and comparator/selector circuit board as specified | Eurocopter 332 series |
| 08-8-14 |
Continental/Lycoming |
Supersedes 08-6-51 | See AD concerning TSIO-360-RB and IO-360 engines with certain Precision Airmotive fuel injection servos | Various 360 models |
| 08-7-8 |
Pacific Aerospace |
Inspect/replace to ensure that 1/8-inch rivets are not installed in place of the correct 5/32-inch rivets that secure the horizontal tail surface load transfer angles to the rearmost fuselage frame as specified | 750XL |
| 08-7-11 |
Pilatus |
Insert updated documents into the airworthiness limitations section of the AFM as sepcified | PC-12,/45,/47 |
| 08-7-10 |
Beechcraft |
Superseded by 10-26-3 |
| 08-7-1 |
Turbomeca |
Superseded by 10-10-9 |
| 08-6-51 |
Continental/Lycoming |
Superseded by 08-8-14 |
| 08-6-28 |
Avidyne Corp |
Perform a logbook inspection to determine if any PFD serial numbers are affected by this AD and then proceed as specified | Various Aircraft |
| 08-6-19 |
Honeywell |
Using the compliance schedule in the AD, remove and replace the LPC aft shaft as specified | ATF3-6-4C, AT3-6A-3C, -4C |
| 08-6-17 |
Pilatus |
Superseded by 09-5-7 |
