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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 |
| 79-10-8 |
Cessna |
Superseded by 80-2-17 |
| 79-10-7 |
deHavilland |
Superseded by 80-3-8 |
| 79-10-6 |
Enstrom |
Revised 3/82 | check tail rotor blade grips | F28C, 280C |
| 79-10-3 |
Lyc Eng |
Revised 7/80 | check eng mount bolts | PA-44 & Cessna 172N |
| 79-10-15 |
Cessna |
Superseded by 05-12-12 |
| 79-10-14 |
Cessna |
Revised 5/88 | supersedes 78-26-9 | install vented fuel cap | several models |
| 79-10-11 |
Embraer |
Check bearings in elevator, rudder, aileron each 500 yrs | EMP-110P1 |
| 79-10-10 |
Ayres |
Inspect rudder single upper hinge ea 100 hrs or replace w/3 hinges | S-2D,S-2R |
| 79-10-1 |
Bell |
Modify ASC external load device if pop-out floats | 206A,B |
| 79-1-7 |
Piper |
Superseded by 81-23-7 |
| 79-1-5 |
Piper |
Revised 12/79 | supersedes 77-26-4 | prevent improper fuel flow | 600,601,601P |
| 79-1-4 |
Piper |
Superseded by 98-9-18 |
| 79-1-3 |
Piper |
Inspect wing spar assembly prior to 2000 hrs | PA-36-285 (SN 36-7360001 thru -7560003) |
| 79-1-2 |
Beech |
Revised 9/80 | supersedes 72-18-7 & 72-18-8 & 73-23-4 & 75-25-4 & 76-13-3 & 77-25-1 |
| 79-1-1 |
Beech |
Supersedes 74-13-2 | (unless 74-13-2 complied) replace various screws in control sys | F33A, C;C33,A; V35B; A36; D55,A,E55,A; 56TC; 58,A,P,TC; B80; 70; B90; C90; E90; A55,B55,C55,A; 99,A99,B99; 100; 200 series |
| 78-9-7 |
Bendix |
Superseded by 96-12-7 |
| 78-9-5 |
Cessna |
Supersedes 76-10-11 | inspect wing spar caps at 3000 hrs, then ea 500 hrs | 337 series |
| 78-9-2 |
Bell |
Modify exit if emergency float kit installed | 212 |
| 78-8-9 |
Schweizer |
Superseded by 08-22-21 |
| 78-8-8 |
Bell |
Modify tail boom & fin | 214B,-1 (SN 28001 thru 28036) |
Showing Results 3821 - 3840 of 5103
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