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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.
Showing Results 161 - 180 of 5103
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| AD No. |
MAKE |
Condensed description of ad note |
| 12-17-7 |
Diamond |
Inspect the adhesive joint between the center wing spars and upper wing skin | DA-42, 42NG, 42M-NG |
| 12-17-6 |
Piper |
Reported cracks developing in the stabilator horn assembly | PA-24, 24-250, 24-260 |
| 12-17-5 |
Honeywell |
Rim/web seperation of an LPT1 rotor assembly | TFE731-5,-5AR,-5BR,-4,-4R, |
| 12-17-3 |
Eurocopter |
Unprotected forward (pitch) servo-control hydraulic hoses, which could become damaged and leak fluid that could ignite during flight | AS350B,BA,D,B1,B2,B3 |
| 12-17-2 |
Eurocopter |
Regards cracked rotor mast nut | SA-356N,-N1, SA-366G1, AS365N2, AS365N3, EC155B, EC155B1 |
| 12-16-2 |
Eurocopter |
AD defines the unsafe condition as possible overloading of the seat structure at the attachment point during a hard landing | EC155B, B1 |
| 12-16-14 |
Honeywell |
Remove suspect LPT2 rotor blades from service as specified | TFE731-20R, -20AR,-20BR, -40,-40AR,-40R, -50R, -60 |
| 12-16-13 |
Rotax |
Fuel pump | 912 series |
| 12-15-8 |
Sikorsky |
Unsafe condition exists as an overheated Electric Rotor Brake can result in ignition of hydraulic fluid | S-76A |
| 12-15-6 |
Gulfstream |
Detect and correct chafing of fuel lines | Astra SPX, 1125, G100 |
| 12-15-4 |
Eurocopter |
Intermittent uncommanded roll oscillations during coupled instrument landing system and localizer approaches with the autopilot coupled | EC155B1 |
| 12-15-11 |
Dassault |
Passenger oxygen pipe at frame 10 | Falcon 7X |
| 12-14-7 |
Bell |
Supersedes 11-15-51 | AD is in regards to servos that may have a loose nut, shaft, and clevis assembly | 407, 427 |
| 12-14-6 |
Rolls-Royce |
AD due to released turbine blades and shrouds | 250-C20, -C20B, -C20R/2 |
| 12-14-14 |
Eurocopter |
Uncommanded cutting of the hoist cable | BK-117 series |
| 12-13-51 |
Gulfstream |
One-time detailed or borescope inspection of the left- and right-hand inboard vent holes for debris or obstructions, and repair if necessary | G150 |
| 12-13-4 |
Embraer |
Visually inspect the RH & LH aileron lower skin for the existence of required drain holes | Phenom 300 |
| 12-13-12 |
Gulfstream |
Detect and correct paint thickness on flight controls | GIV, GIV-X, GV, GVSP |
| 12-13-11 |
Eurocopter |
Improperly swaged spherical bearing on the pitch link | BK 117 Series |
| 12-12-21 |
Eurocopter |
Unsafe condition, complete electrical power system failure due to excessive high reverse current flow when switching off a generator in flight, causing other generator to fail | BK 117 C-2 |
Showing Results 161 - 180 of 5103
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