| 09-8-11 |
Pilatus |
Install an overboard vent for the airfoil deice system pressure regulator | PC12 and PC12/45 |
| 09-8-10 |
Pilatus |
Superseded by 10-5-2 |
| 09-8-1 |
Honeywell |
Supersedes 07-7-12 | Inspect NZ-2000 nav computer for affected serial numbers and comply as specified | Various aircraft |
| 09-7-8 |
Piper |
Insert "operate only under day VFR rules" into the AFM until inspection of the 35-amp and 250-amp current limiters are done as specified | Pa-46-350P and 46R-350T |
| 09-7-52 |
Bell Helicopter |
Supersedes 09-7-51 | Inspect the cyclic control lever assembly and determine if affected bearing SN is installed correctly as specified on assemblies less then 50 hours TIS | 206A,-B,-L, 407, 427 |
| 09-7-51 |
Bell Helicopter |
Superseded by 09-7-52 |
| 09-7-2 |
Hawker Beechcraft |
Supersedes 96-3-7 | Install adjustment mechanism on crew seats; replace aluminum assemblies | 400,-A; MU-300-10 |
| 09-7-14 |
Diamond |
Inspect the adhesive joint between the wing main spar caps and the upper wing skin for adhesive voids as specified | DA40 |
| 09-6-5 |
Bombardier |
This AD is in regards to cracking of the wing anti-ice piccolo ducts and their inspection/prevention as specified | CL-600,-601,-6013A,-6013R,-604 |
| 09-6-1 |
Eurocopter |
Determine the orientation of the fixed connector "24 Delta" and if the large contacts are not oriented "aft," re-orient the fixed connector so that they are facing "aft" as specified | EC 155B, B1 |
| 09-5-9 |
Bell Helicopter |
Superseded by 13-20-51 |
| 09-5-7 |
Pilatus |
Supersedes 08-6-17 | Inspect the stick-pusher servo-cables for correct installation, position, and tension as specified | PC12/45, /47, /47E |
| 09-5-5 |
Avidyne |
Inspect PFD for affected serial numbers listed in the AD and do the required actions as specified | Multiple aircraft |
| 09-5-12 |
Cessna |
Modify the aileron carry-through cable attachment to the aileron upper quadrant with parts of improved design as specified | 208 & 208B |
| 09-4-9 |
DeHavilland |
Supersedes 08-11-10 | Install inspection holes in the left and right lower wing skins and inspect front spar adapter assemblies for cracks as specified | DHC-6-200, -300 |
| 09-4-4 |
Cessna |
Using Cessna SB MEB08-8, inspect the auxiliary wing spar near the location where the main landing gear trunnion is mounted for cracks as specified | 401/A/B, 402/A/B |
| 09-4-3 |
Rolls-Royce |
AD issued to prevent low-cycle fatigue of the parts listed, see AD | AE 3007A1E and AE 1107C |
| 09-4-14 |
Pilatus |
Superseded by 09-8-10 |
| 09-3-5 |
Pratt & Whitney |
Inspect the CT disc bore area for damage and replace as specified | PW206A - E, PW207C - E |
| 09-3-4 |
Turbomeca |
Superseded by 12-23-12 |
