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Airworthiness Directives
NOTE - This AD note listing is intended as a guide only and
should not be relied upon as conclusive evidence of AD applicability on
any particular aircraft. Entire Airworthiness Directives may be accessed
at: http://rgl.faa.gov.
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| AD No. |
MAKE |
Condensed description of ad note |
| 09-24-13 |
Cessna |
Superseded by 10-12-1 |
| 09-24-12 |
Honeywell |
See AD regarding engineering drawing change for the gas generator turbine disk | LTS101-600, -650, -750 series |
| 09-24-11 |
GE Engines |
Superseded by 10-1-4 |
| 09-23-9 |
Bombardier |
Inspect ADG power harness as specified | Challenger 600, 601, 601-3A |
| 09-23-12 |
Socata |
Superseded by 10-23-28 |
| 09-22-4 |
Eurocopter |
Amend the flight manual concerning FMS as specified | EC155B, B1 |
| 09-22-3 |
Hartzell Propeller |
Supersedes 06-18-15 | Inspect propeller hub | Various models |
| 09-22-2 |
American Champion |
Check and correct cracking of rear seat back hinge area and excessive elongation of the rear seat hinge bolt hole | 7ECA, 7GCAA, 7KCAB, 8KCAB, 8GCBC |
| 09-22-11 |
Bell |
Inspect the swashplate link assembly bearing as specified | 407, 427 |
| 09-22-10 |
Eurocopter |
Inspect the main rotor de-icing system distributor retaining clamp | AS332 and SA330 series |
| 09-21-8 |
Piaggio |
Perform a functional test of the nose landing gear steering manifold as specified | P-180 |
| 09-21-11 |
Turbomeca |
Removal of engines with balancing pistons before 16,000 CSN | Arrius 1A series |
| 09-21-10 |
AVOX Systems |
AD applies to the oxygen cylinder assemblies | Gulfstream GIV |
| 09-2-3 |
Lycoming/Cont |
Applies to engines with a Precision Airmotive LLC, RSA-5 or RSA-10 series or Bendix, RSA-5 or RSA-10 series, fuel injection servo, see AD for details | Multiple Lycoming and Continental |
| 09-19-7 |
Teledyne Continental |
Visual inspection of cylinders | O470, IO470, TSIO470, TSIO520, IO550 |
| 09-18-4 |
Air Tractor |
Secure any items stowed in the baggage compartment using tie down straps and/or a cargo net | AT-802, -802A |
| 09-17-5 |
Honeywell |
Remove first stage turbine disks from service as specified if applicable | TPE331-10 and TPE331-11 |
| 09-17-1 |
Gulfstream |
Results from notification from manufacturer that an improper flammable sealant was used on the interior and exterior of the APU enclosure; see AD | G300,400,GIV,G350,G450,GV,G500,G550 |
| 09-16-3 |
Superior Air parts |
Applies to Teledyne Continental Motors IO-520, TSIO-520 and IO-550, see AD for details | Multiple aircraft |
| 09-15-5 |
Cessna |
Measure and adjust as necessary, the roll bridle cable tension and yaw bridle cable tension, and torque the 12 bridle cable clamp screws | 208, 208B |
Showing Results 461 - 480 of 5103
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