Aircraft Bluebook The Premier Resource
for Aircraft Values
Your Aircraft
Sales Report

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:

Showing Results 241 - 260 of 5103 | View All
< Previous | 8 | 9 | 10 | 11 | 12 | 13 | 14 | 15 | 16 | 17 | Next >

AD No. MAKE Condensed description of ad note
11-22-5 Bell Supersedes 11-22-6, 03-22-6 | Inspect tail rotor rod contrl bearings | AS350, AS355 series
11-22-3 Rolls Royce Issued to prevent uncontained failure of the 6th-through-13th stage compressor wheel | AE 3007A, A1/1, A1, A1/3, A1E, A1P, A3
11-22-1 Rolls Royce AD issued to prevent failure of high-energy, life-limited parts, uncontained engine failure, and damage to the airplane | BR700-710A1-10; 710A2-20
11-21-51 Cessna AD prompted by a report of a battery fire that resulted after an energized GPU was connected to an airplane equipped with a lithium-ion battery as the main battery | 525C
11-21-18 Eurocopter To prevent jamming of a pilot cyclic control stick and subsequent loss of control of the helicopter | EC 120B
11-21-10 Diamond See AD regarding aircraft equipped with vapor cycle system a/c | DA 40
11-20-51 Pratt & Whitney Prompted by failures of certain first stage reduction sun gears manufactured by Timken Alcor Aerospace Technologies, Inc, | PT6A-15AG, -27,-28,-34,-34AG,-36
11-20-4 Gulfstream Cracked nuts found in multiple locations could result in failure of affected locations and consequent reduced controllability or reduced structural capability of the airplane | 200
11-2-2 Socata Supersedes 08-19-6 | Inspect/replace the pulley drive assembly as specified | TBM 700
11-18-9 Lycoming AD prompted by the failure of a crankshaft due to incorrect pasrts installed | IO-720-A1B
11-18-51 Honeywell Prompted by an excessive failure rate of PMA main shaft bearings, see AD for details | TPE331
11-18-19 Austro Engine Supersedes 10-23-9 | Inspect the fuel pressure supply for excessive oscillations using the inspection schedule in the AD as specified | Austro Engine
11-18-12 Eurocopter Supersedes 82-13-5 | dye check upper vertical fin | AS350B,B1,B2,B3,BA,D; AS355E,F,F1,F2,N
11-17-7 M7 Aerospace Repetitive replacement of specific flight control cables on affected serial number model SA226 airplanes | SA226-T, TC, AT
11-17-6 Socata Elevator trim tab actuator jamming, affects batch or part numbers, check for S/N inclusion | TBM 700
11-17-15 Embraer Regarding moisture that may accumulate and freeze in the gap between the AOA vanebase assembly and the stationary ring of the sensor body | Phenom 100
11-17-14 Agusta To detect an improperly torqued hub plug that could lead to tail rotor failure and subsequent loss of control | A109A, AII
11-17-13 Eurocopter To prevent nonisolation of electrical equipment creating the risk of uncontrolled electrical fire | EC120B
11-17-1 Agusta Supersedes 10-2-51 | Inspect the main scissor fitting assembly to determine if there are 2 washers installed under the head of each fixing bolt | A109A, AII, 109C, 109K2
11-16-5 Eurocopter To prevent exposure of the electrical wires, which could lead to a short circuit and activation of the indicator light without the high fuel level actually being reached | SA-365N, N1

Showing Results 241 - 260 of 5103 | View All
< Previous | 8 | 9 | 10 | 11 | 12 | 13 | 14 | 15 | 16 | 17 | Next >

In order to deliver a personalized, responsive service and to improve the site, we remember and store information about how you use it. This is done using simple text files called cookies which sit on your computer. By continuing to use this site and access its features, you are consenting to our use of cookies. To find out more about the way Informa uses cookies please go to our Cookie Policy page.