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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 |
69-8-11 |
Cessna |
Modify fuel boost pump | 205, 206, U206, P206, 210 |
69-8-10 |
IAI |
Modify horizontal stabilizer trim system | all Model 1121 |
69-6-6 |
Beech |
Revised 6/71 | inspect rudder spar web ev 300 hours | 80,90,99 series |
69-6-4 |
Piper |
Inspect elevator control sys | PA-31 & PA-31-300 (SN 31-2 thru -334) |
69-6-2 |
Gen Elec |
Superseded by 69-20-8 |
69-5-3 |
Mooney |
Superseded by 76-15-1 |
69-5-1 |
deHavilland |
Revised 7/80 | 100-hour inspect or replace control column assembly | DHC-6 |
69-4-2 |
Cessna |
Replace throttle control bellcrank | A188 300hp IO-520-D thru SN 0478 |
69-26-7 |
Cont Eng |
Superseded by 71-11-4 |
69-26-5 |
Rockwell |
Superseded by 70-12-6 |
69-26-4 |
Beech |
Superseded by 77-11-3 |
69-25-8 |
Lyc Eng |
Reduction gear asmbly | GO-435-C2A;GO-,GSO-,IGSO-480;IGO-,IGSO-540 |
69-24-5 |
Kollsman |
Modify A4 series altimeters |
69-24-4 |
Piper |
Revised 8/77 | Vmc limit placard: 90 MPH | PA-30 |
69-24-3 |
Marvel |
Rework MA- and HA- series carburetor |
69-24-2 |
Beech |
Revised 4/83 | supersedes 69-18-6 | check/rerig elevator control | 99 |
69-23-7 |
Beech |
Rescinded by 71-12-2 |
69-23-6 |
P&W Eng |
Install snap ring fuel pump coupling | PT6A-6,-6B;PT6B-9;PT6A-20, -27,-28 |
69-23-3 |
Piper |
Inspect for inferior steel in the lower longerons | model PA-18-150 |
69-23-1 |
Piper |
Superseded by 72-14-5 |
Showing Results 4681 - 4700 of 5103
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< Previous |
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231
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233
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234
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235
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236
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237
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238
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239
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