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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 2241 - 2260 of 5103
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| AD No. |
MAKE |
Condensed description of ad note |
| 94-8-14 |
Corp Jets |
Install amber annunciator screen for standby electric power | 1000A series |
| 94-8-10 |
DeHavilland |
Supersedes 88-13-11 | inspect wing main spar & lower spar cap extensions; replace corroded parts; reprotect reworked areas | DHC-6-200,-300 |
| 94-7-3 |
Allied Signal |
Supersedes 92-12-9 | revise AFM limits sect; monitor eng & flite data; replace cracked A5 seal | TFE731-2A;-3,-3A,-3R,-3AR,-3B,-3BR w/1st stage lo press nozzle |
| 94-7-10 |
Fairchild |
Revised 3/96 | repair/modify upper wing skin at battery box if cracked | specific SA226, SA227 |
| 94-6-9 |
Tele-Cont |
Replace specified capacitors | new/rebuilt mags/capacitors bought after 10/27/93 |
| 94-6-4 |
Eros |
Replace face piece & mask shell screw | Falcon 20,BAe 125-600,Piper PA31T,-42 |
| 94-5-9 |
Beech |
Weld or reinforce cabin seat frame if cracked | 400A (SN RK1 thru -40 & RK-45) |
| 94-5-5 |
Tele-Cont |
Revised 3/96 | replace cracked cyl rocker shft bosses | C75,-85,-90-,125,145;O-200,-300;GO-300 |
| 94-4-7 |
Beech |
Replace MLG hubcaps or rework existing hubcaps | 400A (SN RK-1 thru RK-23) |
| 94-4-17 |
Twin Cmdr |
Superseded by 98-7-17 |
| 94-4-16 |
Mitsubishi |
Superseded by 07-17-9 |
| 94-4-15 |
Twin Cmdr |
Inspect wing front spar lower cap; clear any interference btn firewall & spar flanges; repair corrosion; replace cap if cracked | 500, 560A,-E; 680,-E; 720 |
| 94-4-14 |
Twin Cmdr |
Supersedes 91-8-9 | recurringly inspect wing front spar lower cap; if corroded past service limits, replace cap | 500U,-S; 680FL,-FLP,-W; 681; 685; 690,-A,-B |
| 94-4-13 |
Twin Cmdr |
Supersedes 65-6-1 | recurringly inspect wing front lower spar cap at l & r wing station 24; replace if cracked | 500,-A,-B,-S,-U; 520; 560,-A,-E,-F; 680,-E,-F,-FL,-FL(P),-T,-V,-W; 681; 720 |
| 94-4-12 |
Twin Cmdr |
Modify specified wing rib per SB 211; replace wing front lower spar cap & lower wing stringer if cracked and/or corroded | 685 & 690,-A,-B |
| 94-4-11 |
Twin Cmdr |
Replace wing front spar lower cap if metallurgical exam reveals fine equi-axed grain structure | 500S (SN 3314 thru 3323), 690B (SN 11480 thru 11566) |
| 94-4-1 |
de Havilland |
Repetitively inspect left & right upper wing fuselage fairings; if cracked, replace fittings w/new front steel adapter fittings | DHC-6-300 |
| 94-3-11 |
Hartzell Prop |
Rework specified hub arm assemblies | HC-B4 series |
| 94-26-7 |
AlliedSignal |
Revise AFM; inspect fuel control drive shaft splines | TPE 331,-3,-5,-6,-10,-11U,-12 |
| 94-26-12 |
Raytheon |
Superseded by 97-3-7 |
Showing Results 2241 - 2260 of 5103
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