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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 |
| 96-8-4 |
Eurocopter |
Recurringly inspect switch-over sys linkage & test tandem hydraulic sys; perform required maintenance as needed | BO-105,C,LS A-1 |
| 96-8-3 |
Flight Trails Heli |
Replace specific hardpoint assembly | modified MDHS 369D,E,F; 500N |
| 96-7-3 |
Eurocopter |
Inspect cyclic pitch control rod; replace if rod end fittings are not safetied | AS350B, BA, B1, B2, D; AS355E, F, F1, F2, N |
| 96-7-12 |
Bell |
Recurringly inspect tailboom assembly; modify if cracked | 214ST (SN -1 thru -32) |
| 96-7-11 |
Raytheon |
Inspect specified hydraulic pipes; replace if chafed; adjust clearance | Hawker 1000,A |
| 96-6-4 |
Bell |
Supersedes 81-4-8 | recurringly inspect main transmission driveshaft until specified parts are replaced | 206A,B |
| 96-6-3 |
Enstrom |
Supersedes 89-4-9 | recurringly inspect main rotor transmission clutch assmbly | F28,-A,-C,-C-2,-F,-FX |
| 96-6-2 |
Enstrom |
Supersedes 76-6-11 | recurringly inspect upper swashplate bearing; replace if corroded; replace upper & lower swashplate bearing at 1200 hr or more TIS | F-28A,-C,-C-2; 280,-C |
| 96-6-12 |
Bell |
Recurringly inspect blade; replace if corroded or damaged | 47G,-2,-2A,-2A1; -3,-3B,-3B1,-3B2,-3B2A; -4,-4A; -5,-5A; 47J,-2,-2A |
| 96-6-11 |
Allied Signal |
Initiate life limited part log card for main shouldered shafts; remove from service accordingly | TPE331-14A, -14B |
| 96-6-10 |
Allied Signal |
Install improved power turbine retention sys mod | LTS101 engs on Eurocopter |
| 96-5-3 |
Allied Signal |
Supersedes 91-8-13 | replace cracked fan rotor discs | TFE 731-2,-3 & -4R series |
| 96-4-8 |
Air Tractor |
Replace main landing gear legs | AT 802,-A |
| 96-4-2 |
Allied Signal |
Remove stage 1 & 3-7 compressor disks & stage 2 turbine disks per new life limits | ALF502L,-2,-2A,-2C,-3 |
| 96-4-1 |
Allied Signal |
Supersedes 93-25-16 | replace specified fan disks if cracked | TFE731-2,-2A,-3,-3R |
| 96-3-7 |
Beech |
Superseded by 09-7-2 |
| 96-3-3 |
Fairchild |
Replace nuts on lever attach point clevis | SA226-T,-TC; SA227-TT,-AC |
| 96-3-13 |
Beech |
Assure roll pin holes penetrate both walls of landing gear drag leg lock link | F90; 99,-A; B99; 100; A100; 200,-T,-C; B200,-T,-C |
| 96-3-11 |
Am Champ |
Superseded by 96-18-2 |
| 96-25-3 |
Raytheon |
Supersedes 94-14-6 | remove specified washers, tab washers & flat washers from roller attach bolts of left & right flaps; replace w/specified new washers | 400A |
Showing Results 2041 - 2060 of 5103
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< Previous |
98
|
99
|
100
|
101
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102
|
103
|
104
|
105
|
106
|
107
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|
