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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 3021 - 3040 of 5103
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| AD No. |
MAKE |
Condensed description of ad note |
| 86-10-3 |
Mitsubishi & Beech |
Replace starter relay & modify manual | MU-300,-10 (all thru SN A1011SA) |
| 86-10-2 |
Canadair |
Check aileron/elevator dampers each 100 hrs or 3 months | CL600-1A11,- 2A12 |
| 86-10-12 |
PZL-Melex |
Revised 3/88 | inspect crankshaft & counterweight each 300 hrs | PZL-3S engs |
| 86-1-6 |
Airborne |
Replace dry air pumps installed after 9-1-85 | various aircraft (see AD) |
| 86-1-4 |
Hughes |
Supersedes 85-18-8 | modify tail rotor blades | 369 (500 series) |
| 86-1-2 |
Cessna |
Superseded by 88-13-3 |
| 86-1-1 |
Cessna |
Revised 7/87 | prohibits flight in icing conditions unless proper optional equipment installed | T303 |
| 85-9-4 |
Bell |
Inspect/repair main rotor trim tabs | 206L, L-1, L-3 |
| 85-9-1 |
Airotech |
Inspect rip cord cable housing | Model Force I (A) |
| 85-8-8 |
McCauley |
Modify prop hub models D2A32C90, -A, -B, -C, -J, -K, -L, -M, -BLM, -CLM, -JLM, -KLM, -LM | on but not limited to Bellanca 17-30,-A; Cessna A185E, F; A188B; P206A, TP, U206A thru -F; TU206A thru -F; 207, A; T207; Navion A thru H |
| 85-8-6 |
Partenavia |
Inspect & rework aileron cable assemblies | P68, B, C, TC, Observer (001 thru 335,XXX-01TC thru XXX-26TC) |
| 85-8-5 |
Piper |
Rework main & nose landing gear struts | PA31,-300,-325 (SN 31-2 thru -831201), PA31-350 (31-5001 thru -8352042), T1020 (-8153001 thru -8353007), PA31P (31P-1 thru 7730012), PA31T (-7400002 thru -8120104), PA31T1 (-7804001 thru -1104006), PA31T II XL (-8166001 thru -8166076) |
| 85-8-4 |
Partenavia |
Modify wing spar prior to 2100 hrs | P68, B, C, -TC (SN 001 thru 328) |
| 85-8-3 |
Bell |
Replace tail rotor blades P/N 47-642-117-1 | all 47 series |
| 85-8-2 |
Cont Eng |
Replace exhaust valves in cylinder assembly P/N 646680A4 & 646680A5 | O-470G, -K, -L, -M, -R, -S; IO-470-C |
| 85-8-1 |
MBB |
Modify gearbox mount & upper fin | BO-105 (S1 thru S350) |
| 85-7-8 |
BAe |
Modify power supply | HS/BH/DH-125 series |
| 85-7-7 |
Aerospatiale |
Modify tail rotor gearbox control rod | SA318B, C; SA315B |
| 85-7-3 |
Sperry |
Placard SPZ-7000 with FZ-700 computer | S-76, SA-365N |
| 85-7-1 |
Bell |
Check rotor pitch horn each 20 hrs | 412 (SN 33001 thru 33110) |
Showing Results 3021 - 3040 of 5103
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< Previous |
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148
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149
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152
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153
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154
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155
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