| 11-16-1 |
Dassault |
Supersedes 11-12-51 | AD offers resolution to the emergency grounding of Falcon 7X aircraft from runaway trim | Falcon 7X |
| 11-15-51 |
Bell |
Superseded by 12-14-7 |
| 11-15-5 |
Beechcraft |
Insert Hawker Beechcraft Corporation Log of Temporary Changes dated Feb 2011 as specified | B300 and B300C |
| 11-15-11 |
Cessna |
AD to detect and correct damage in the wings and prevent overload failure of the wing due to the installation of STC SA5090NM from Flint Aero, Inc. | 337 Series |
| 11-15-10 |
Lycoming |
Superseded by 12-3-6 |
| 11-14-9 |
Rotax |
Supersedes 11-11-3 | Replace defective washers that are part of the magneto ring flywheel hub as specified | DA20-A1 |
| 11-13-7 |
Dassault |
Supersedes 10-2-2 | Revise the Limitations Section of the AFM concerning the radio-altimeter lock-up conditions | Falcon 7X |
| 11-13-5 |
Turbomeca |
Accomplish TU166 modification as specified | Arriel 2B and 2B1 |
| 11-13-3 |
Lycoming and Teledyne Cont |
AD prompted by a trubocharger failure due to machining debris, see AD for details and applicability | Multiple engines |
| 11-13-10 |
Bombardier |
Supersedes 09-11-13 | Perform a detailed inspection for chafing and damage of the case drain tube from the hydraulic pump case installed on the left-hand engine as specified by applicable S/N | Larjet 45 |
| 11-12-8 |
Bell |
AD to detect corrosion or pitting in the forward spar area of a T/R blade to prevent a crack in the T/R blade or loss of the T/R blade | 205A, A-1, B, 212, 412, 412CF, EP |
| 11-12-7 |
Eurocopter |
Visually inspect the adhesive bead between the bushing and the starflex arm for a crack, a gap or loss of the adhesive bead and inspect the starflex arms as specified | SA-365C, C1, C2, N, N1, N2, N3 |
| 11-12-51 |
Dassault |
Superseded by 11-16-1 |
| 11-12-4 |
Rotax |
Replace the magneto ring flywheel hub washer as specified | 912F3, 912 |
| 11-12-16 |
Schweizer |
Supersedes 11-1-52 | Remove locknut MS21043-3 from tailboom aft cluster and re-install as specified | 269A, A-1, B, C, C-1 |
| 11-12-10 |
Robinson |
Supersedes 07-26-12 | Visually inspect for skin seperation along the leading edge of any exposed blade skin aft of the skin-to-spar bond line on the lower surface of each blade as specified | R22, -Alpha, -Beta, -Mariner, R44 |
| 11-11-7 |
Diamond |
AD due to cracks found on DA42 Main Landing Gear damper-to-trailing arm joints, see AD for details | DA42 |
| 11-11-3 |
Rotax |
Superseded by 11-14-9 |
| 11-10-9 |
Cessna |
Supersedes 87-20-3 | Inspect/repair seat rails & seat assembly | various Cessna models |
| 11-10-14 |
Dassault |
Supersedes 10-24-8 | Perform a visual inspection for correct installation of the emergency brake system number 2 as specified | Falcon 50 |
