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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 501 - 520 of 5103 | View All
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AD No. MAKE Condensed description of ad note
09-10-14 Hartzell Applies to Hartzell steel hub turbine props listed, see AD | Multiple aircraft
09-1-11 Turbomeca Perform a one-time inspection of the HMU as specified | Arriel 2B and 2B1 series
08-9-3 Agusta Inspect the four grooved clamps that attach the engine exhaust ducts and replace if required | A109A, AII, C
08-9-21 Dassault Inspect for damage of the electrical feeder bundle under the circuit breaker panel and repair/modify as specified | Falcon 50
08-9-18 Taylorcraft Inspect the left and right wing lift strut attach fittings for corrosion or cracking and replace as specified | F-19, F-21,-A,-B, F-22,-A,-B,-C
08-9-10 Air Tractor Supersedes 03-6-1 | Replace wing lower spar cap | 300, 301, 302, 400 series
08-8-6 Bombardier Superseded by 08-21-9
08-8-3 Pacific Aerospace Replace certain pitot heat sensor circuit breakers and add a cooling fan circuit as specified | 750XL
08-8-20 Dassault Remove and modify affected wing anti-ice telescopic tubes P/N 5035-400 and 5035-500 ball joints as specified | Falcon 2000
08-8-19 Gulfstream Inspect the feeder cable, terminal lug 123P/2, and ground point 803GND installed within the left DC power box for chafing and arcing damage as specified | G150
08-8-16 Turbomeca Supersedes 02-15-5 | Replace electronic control unit (ECU) and comparator/selector circuit board as specified | Eurocopter 332 series
08-8-14 Continental/Lycoming Supersedes 08-6-51 | See AD concerning TSIO-360-RB and IO-360 engines with certain Precision Airmotive fuel injection servos | Various 360 models
08-7-8 Pacific Aerospace Inspect/replace to ensure that 1/8-inch rivets are not installed in place of the correct 5/32-inch rivets that secure the horizontal tail surface load transfer angles to the rearmost fuselage frame as specified | 750XL
08-7-11 Pilatus Insert updated documents into the airworthiness limitations section of the AFM as sepcified | PC-12,/45,/47
08-7-10 Beechcraft Superseded by 10-26-3
08-7-1 Turbomeca Superseded by 10-10-9
08-6-51 Continental/Lycoming Superseded by 08-8-14
08-6-28 Avidyne Corp Perform a logbook inspection to determine if any PFD serial numbers are affected by this AD and then proceed as specified | Various Aircraft
08-6-19 Honeywell Using the compliance schedule in the AD, remove and replace the LPC aft shaft as specified | ATF3-6-4C, AT3-6A-3C, -4C
08-6-17 Pilatus Superseded by 09-5-7

Showing Results 501 - 520 of 5103 | View All
< Previous | 21 | 22 | 23 | 24 | 25 | 26 | 27 | 28 | 29 | 30 | Next >

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