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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 1981 - 2000 of 5103
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| AD No. |
MAKE |
Condensed description of ad note |
| 97-21-16 |
Dassault |
Superseded by 00-4-19 |
| 97-20-4 |
Enstrom |
Conduct tests of voltage regulator and over-voltage relay. Replace if not to spec in accordance with service bulletin. Specified F-28A,280,F-28C,280C. |
| 97-2-2 |
Fairchild |
Apply torque to control column pitch bearing attaching nuts; if movement, replace pitch control column roller bearing & attaching nut; inspect elevator control rod end bearing retainer/dust seals; if creased, replace; install new washer & replace bolt on elevator control rod end bearing assembly at the walking beam connections | SA26, SA226, SA 227-AC,-AT,-BC,-TT |
| 97-2-15 |
Robinson |
Supersedes 96-11-9 | adjust RPM warning unit to activate when M/R RPM is between 96% & 97% | R44 |
| 97-2-14 |
Robinson |
Supersedes 96-11-8 | adjust low-RPM warning unit to activate when M/R RPM is between 96% & 97%; install governor (KI-67-2) if not so equipped, or upgrade governor in models w/ throttle/collective governor | R22 |
| 97-2-1 |
New Piper |
Reroute landing gear emergency extension air line | PA32T2 w/Parker Hannifin wheel & brake conversion kit |
| 97-19-7 |
Dassault |
Revise abnormal procedures section of the flight manual concerning rapid throttle reduction. Falcon 2000. |
| 97-18-7 |
Raytheon |
Modify rudder in accordance with Raytheon service bulletin. | 125-800A, 800, 800XP |
| 97-18-2 |
Hartzell |
Supersedes 77-14-7 | Revision 97-18-2R1 BW 2003-13 | Repetitively perform dye and eddy current inspection on specified prop blades, internal bearing bore, hub and blade clamps. | Various aircraft. |
| 97-18-11 |
Bell |
Modify tailboom vertical fin spar. | 204B,205A-1 |
| 97-17-6 |
Bell |
Replace solenoid valves with specified replacement parts to prevent inadvertent inflation of emergency float kit. | Bell 214ST |
| 97-17-3 |
Ayres |
Superseded by 00-11-16 |
| 97-16-5 |
Gulfstream |
Supersedes 67-4-1 | Inspect under wing fairings for corrosion. If corrosion detected, repair, then install protective paint system. | G-1 |
| 97-16-2 |
Robinson |
Inspect up-limit switches for proper operation. Replace if malfunctioning. | R44 |
| 97-16-10 |
Rapco |
Remove and replace specified Rapco in-line pressure filter to prevent flight instrument failure. | Beech 33,35,36,55,58,70,80, Cessna 310R, T310R, Piper PA-31-300, PA-31-325,PA-31P,PA-31P-350,PA-31T,PA-34-200T. |
| 97-15-4 |
Bell |
Supersedes 94-02-05 | Create new component history card for the carrier. Implement new RIN calculation methods. | 214B,214ST. |
| 97-15-16 |
Bell |
Superseded by 00-16-4 |
| 97-15-15 |
Eurocopter |
Superseded by 99-11-11 |
| 97-15-14 |
Piaggio |
Inspect torque tube bottom flange assembly of rudder for cracks. If cracks found, replace according to service bulletin. | P-180 |
| 97-15-11 |
Text-Lyc |
Supersedes 97-1-3 | Replace specified piston pins on specified engines. | O,IO,LIO, AIO,AEIO,VO,IVO,HO,HIO,LHIO,TIO,TO,LTO,LTIO,GO,IGO,GSO,IGSO,TVO,TIVO, TIGO series engines. |
Showing Results 1981 - 2000 of 5103
| View All
< Previous |
95
|
96
|
97
|
98
|
99
|
100
|
101
|
102
|
103
|
104
| Next >
|
