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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 |
| 97-15-10 |
AlliedSignal |
To correct non-responsive power lever, replace Pt2 sensor orifice fittings in accordance with service bulletin. | TPE331-3,-5,-6,-10,-11,-12. |
| 97-15-1 |
Tele-Cont |
Replace cylinders and cylinder pins on specified engines. | E-165,E-185,E-225,0-470, IO-470 series engines. |
| 97-14-9 |
Gulfstream |
Supersedes 72-24-04 | Repetitively inspect elvator trim actuator mounting lugs for cracks. Replace if cracks found. | G-1 |
| 97-14-8 |
Gulfstream |
Supersedes 66-10-03 | Conduct dye inspection to detect cracks in main landing gear uplock beam forward brackets. Replace brackets if cracks found. | G-1. |
| 97-14-5 |
Air Tractor |
Supersedes 95-20-6 | Repetitively inspect the fin front spar attachment fittings for cracking. Repair if cracked. | AT-301,302,400,400A,401,402, 501,502. |
| 97-14-15 |
Raytheon |
Check door handles for proper locking. If lock release button is inoperable, replace in accordance with service bulletin. 33,36,50,95,55,56,58 series. |
| 97-14-14 |
Piaggio |
Inspect baggage compartment for stringer or by-pass duct damage. If damage found, repair in accordance with service bulletin. | P-180 thru s/n 1030. |
| 97-14-13 |
Gulfstream |
Supersedes 67-17-05 | Repetitively inspect for chafe wear on diagonal engine mount tubes. Replace if wear detected. | G-1 |
| 97-14-12 |
Bell |
Create new component history cards for mast and trunion. Record new RIN's using specified guidelines. | 204B,205A-1,205,212 |
| 97-14-10 |
Gulfstream |
Supersedes 67-31-8 | Repetitively inspect main landing gear retract cylinder attachment fittings for cracks. Replace if cracks found. | G-1 |
| 97-13-2 |
Diamond |
Install spin restriction placard. | DA20-A1 |
| 97-13-11 |
Ayres |
Superseded by 97-17-3 |
| 97-13-10 |
Genl Elect |
Replace fan guards with new design within 2 years of AD issuance. | Falcon 20, Sabreliner NA265 Series with GE CF700 engines. |
| 97-12-6 |
Cessna |
Check clearance between the gascolator & tailpipe against cowling. If rubbing, modify in accordance with service bulletin. | 172R |
| 97-12-2 |
MDHC |
To prevent failure of link assembly, furthur flight or ground operations are prohibited. | MD 900 |
| 97-12-1 |
Cessna |
Visually inspect wire bundle in accordance with service bulletin. Replace if damaged. | Specified Citation 650's |
| 97-11-5 |
Allied Signal |
Superseded by 09-26-6 |
| 97-11-4 |
Bell |
Create new component history card for main rotor mast & main rotor spline plate. Record RIN's (retirement index numbers) using new specified guidelines. | 412, 412EP |
| 97-11-13 |
Fairchild |
Replace generator fault transformer wiring. | Specified SA226-T,-T(B),-AT,-TC; SA-227-TT,-AT,-AC |
| 97-10-6 |
IAI |
Repetitively inspect for loose or fretted rivets that fasten support beam to fuselage at sta. 452.000 | Specified 1125 Westwinds. |
Showing Results 2001 - 2020 of 5103
| View All
< Previous |
96
|
97
|
98
|
99
|
100
|
101
|
102
|
103
|
104
|
105
| Next >
|
