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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 |
| 78-4-1 |
Beech |
Replace flap control weld assembly | 23, 19, 24, 24R |
| 78-3-5 |
Mitsubishi |
Supersedes 76-16-5 | replace eng cowl latch links | all series thru MU-2N |
| 78-3-3 |
BAe |
Superseded by 80-12-10 |
| 78-3-1 |
Bell |
If STC SH357SW, inspect hopper brackett | 47 series |
| 78-26-9 |
Cessna |
Superseded by 79-10-14 |
| 78-26-8 |
Gen Elec |
Replace lube pumps | CT58-100-2; -110-1,-2; -140,-1,-2 |
| 78-26-6 |
Piper |
Dye check and/or replace vertical fin spar plate | PA-38-112 (all thru SN-78A0749) |
| 78-26-5 |
Piper |
Each 50 hrs inspect and/or replace elevator & aileron rod end bearings | PA-36 |
| 78-26-4 |
Hughes |
Inspect tail rotor hub | 369 series & 269 series thru 269C SN 0716 |
| 78-26-3 |
Grumman |
Inspect wing fittings for corrosion | G-164,A,B |
| 78-26-2 |
deHavilland |
Superseded by 97-23-9 |
| 78-26-12 |
Cessna |
Check fuel guage sys | 210G,H,J,M,N; T210G,H,J,M,N; P210N |
| 78-26-11 |
Piper |
Modify elevator control sys | PA-31-350 (SN -5001 thru -7852151) |
| 78-26-1 |
Allison |
Modify eng electrical system | 250-C28B eng |
| 78-25-8 |
AiResearch |
Revised 6/80 | modify fuel control drive gear prior to next 3100 hrs | TSE, TPE |
| 78-25-7 |
Cessna |
Replace vertical fin bracketts | A150, A152 (SN A1500654 thru -0833) |
| 78-25-5 |
Brackett |
Superseded by 81-51-3 |
| 78-25-4 |
Hughes |
Inspect input pinions SN 001 thru 5101 | 269A,B,C |
| 78-25-3 |
Piper |
Replace certain Deutsch hoses | PA-23-250; PA-28R-180,-200,-201; PA-28R-201T; PA-31,-300,-325,-350; PA-31P,T,TI; PA-34-200T; PA-44-180 |
| 78-25-2 |
Gates-Lear |
Periodically inspect or modify 36" door | 35 (SN 35-001 thru -167), 36 (SN 36-001 thru -038) |
Showing Results 3861 - 3880 of 5103
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190
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191
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194
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