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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 |
| 90-8-14 |
Beech |
Inspect wing forward spar carry-thru structure | 55, 56TC, 58, 95 series |
| 90-8-12 |
Rolls-Royce |
Remove low torque switch | Dart 529, 511 |
| 90-7-8 |
SELA |
Replace failed lamps; inspect cabin fluorescent lighting sys | Falcon 10,20,50,900; PA-42; BE 2000 |
| 90-7-10 |
Cessna |
Inspect elev & rudder cable; replace a/c mount hardware | 500,501,550,551,S550 |
| 90-6-3 |
Cessna |
Revised 3/91 | supersedes 58-8-2 | test exhaust heater | SN 36216 up on 172 |
| 90-6-13 |
Honeywell |
Supersedes 90-3-2 | replace defective liquid level tilt switch on vertical gyros | 550/551, S550, 560, 650, KA300, KA200 |
| 90-6-10 |
Schweizer |
Inspect & replace throttle cable assemblies | 269 series |
| 90-5-9 |
Tracor |
Install placard: "Deselect 58 prior to each flight" | Jetstar, KA200, C-441, Falcon 20, PA-42, HS-125, SA226T(B) |
| 90-5-6 |
Fairchild |
Revised 8/90 | inspect & rework MLG door to nacelle skin gap | SA226, SA227 |
| 90-5-4 |
Cessna |
Inspect eng mount ring lower attach pts;replace nose gear shimmy dampener | 208 |
| 90-5-1 |
Cessna |
Inspect right flap bellcrank | 208, 208A, 208B |
| 90-4-7 |
Commander |
Supersedes 87-14-3 | inspect MLG brace fittings for cracks | 112, 114 |
| 90-4-6 |
Textron Lyc Eng |
Revised 5/91 | inspect prop governor oil line installation; replace aluminum attachment | Textron Lycoming 4-cyl piston engs mfgd before 1/1/90 |
| 90-4-4 |
Beech |
Superseded by 92-15-13 | supersedes 77-5-1 |
| 90-3-9 |
Bell |
Inspect T/R trunnion bearing housing assembly; within 150 hrs, remove T/R hub & blade assembly | 412, 205A, 205A-1, 212 |
| 90-3-7 |
Falcon |
Revised 4/90 | modify thrust reverser electrical control system, reinforce T/R actuating mechanism; replace hydraulic actuator end fitting | 900 |
| 90-3-6 |
BAe |
Repetitively inspect fuselage keel skin panels & local keel structures | BAe/DH/BH/HS 125-1A, -3A, -400A, -600A |
| 90-3-5 |
Falcon |
Repetitively test main landing gear door manual release system; replace door's manual release system bell crank | 50, 900 |
| 90-3-4 |
Garrett |
Remove suspect high pressure turbine rotor discs | TFE731-3, -3A, -3AR, -3R |
| 90-3-2 |
Honeywell |
Superseded by 90-6-13 |
Showing Results 2621 - 2640 of 5103
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