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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 |
| 97-10-16 |
Hiller |
Supersedes 77-7-5 | Inspect blade spar tube for corrosion or cracks at 100 hour intervals. | UH-12,A,B,C,D UH-12C,D,E CH-112 H-23A,B,C,D,F HTE-1,2 OH-23G |
| 97-10-13 |
Fairchild |
Supersedes 96-21-5 | Inspect inside of elevator torque tube for corrosion; replace if damaged. | SA226-T,-T(B),-AT,-TC; SA227-AT,-AC,-BC |
| 97-1-5 |
Williams Int'l |
Replace HPT disks by 7/1/97 | FJ44-1A |
| 97-1-4 |
Textron-Lyc |
Repetitively inspect cylinder assemblies; replace if cracked | TIO-,LTIO-,IO-540 engs w/Superior Air Parts parts |
| 97-1-3 |
Textron-Lyc |
Superseded by 97-15-11 |
| 97-1-2 |
Cessna |
Repetitively inspect MLG trunnion pins; if not properly installed, replace existing bearing w/sealed, self-lubricating bearing | 525 (SN 1 thru 153) |
| 97-1-13 |
Cessna |
Replace P/N S51-10 (fuel, oil or hydraulic hose) that has diagonal or spiral pattern external reinforcement wrap w/hose that has criss-cross pattern external wrap | 150,172,175,177,180,182,185,188,206,207,208,210,303,310,335,336, 337,340,401,402,404,411,414,421 & 425 |
| 97-1-12 |
Airtel Int'l |
Replace Centaurus C3-100 GPWS | Beech 200, Falcon 200, Embraer EMB-110, Fairchild SA226-TC & SA227-AT |
| 97-1-1 |
New Piper |
Recurringly inspect main gear sidebrace stud; if cracked, replace or install new stud bracket assembly or modify existing bushings to install 5/8-inch stud in specified models | PA-28R-180,-200,-201-201T; PA 32R-300; PA-34,-200,-200T |
| 96-9-9 |
Piaggio |
Modify nacelle | P180 (SN1,2,4,6 thru 33) |
| 96-9-6 |
Brackett |
Supersedes 95-3-2 | repetitively inspect air filter assembly; replace if damaged | various aircraft |
| 96-9-5 |
Diamond |
To prevent jamming, visually inspect aileron pushrod clearance in accordance with service bulletin. | DA20-A1 |
| 96-9-3 |
Eurocopter |
Inspect passenger door jettison sys; replace & add second spring pin | SA-365N,N1,N2 |
| 96-9-29 |
Robinson |
Replace upper V-belt sheave | R22 |
| 96-9-16 |
Fairchild |
Revise AFM on operating in severe icing cond | SA226-T,-AT,-TC; SA227-TT,-AC,-AT |
| 96-9-15 |
Cessna |
Revise AFM on operating in severe icing cond | 208, 208B |
| 96-9-13 |
Beech |
Revise AFM on operating in severe icing cond | 99,-A; A99A; B99; C99; B200,-C |
| 96-9-12 |
Embraer |
Revise AFM on operating in severe icing cond | EMB-110P1,-110P2 |
| 96-9-11 |
DeHavilland |
Revise AFM on operating in severe icing cond | DHC-6-1,-100,-200,-300 |
| 96-9-10 |
Text-Lyc |
Supersedes 81-18-4 | replace oil pump impeller & shaft | 235, 290, 320, 340, 360, 540 series |
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99
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