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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 2161 - 2180 of 5103
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| AD No. |
MAKE |
Condensed description of ad note |
| 95-26-4 |
Robinson |
Supersedes 95-4-14 | revise AFM limits on flight under specific wind conditions | R-22 |
| 95-26-2 |
Text-Lyc |
Supersedes 94-14-13 | replace parts on engs burning 80-91+ octane avgas | O-235, -320,-360,-540; IO-320,-360,-540; LO-320,-360; LIO-360; TIO-360,-540; TVO-435 |
| 95-26-18 |
Maule |
Inspect wing lift struts; replace if corroded, treat internally if not | M-4,-5,-6,-7; MX-7; MXT-7; MT-7-235; M-8-235 |
| 95-26-16 |
Mooney |
Revised 5/96 | modify alternate air door assembly | M20J |
| 95-26-15 |
Allied Signal |
Revised 12/96 | revise limits section of AFM on TCAS operation | CAS-81 TCAS on Gulfstream G-I,-IV |
| 95-26-13 |
New Piper |
Supersedes 76-25-6 | recurringly inspect oil cooler hoses; replace if needed | PA28-, PA28R-, PA32, PA32R-, PA32RT- series |
| 95-26-1 |
Allied Signal |
Install improved power turbine rotor | LTS101-eng on Bell 222 & MBB BK117 |
| 95-25-7 |
Fairchild |
Replace main landing gear door actuator tangs & hardware | SA226-T,-AT,-TC |
| 95-25-6 |
Beech |
Modify stdby instrument lighting sys | 400 (SN RJ-61); 400A (SN RK-1 thru -80) |
| 95-25-5 |
Beech |
If needed, repair rivet & jam nut on ends of control push rod of spoiler flight control sys | 400A (SN RK1 thru -96) |
| 95-25-3 |
Learjet |
Superseded by 05-16-9 |
| 95-25-10 |
Cessna |
Replace outflow/safety valve | 441, 500, 550, 560 |
| 95-24-6 |
Bell |
Supersedes 91-23-15 | revise limitations section of STC-RFMS per Soloy SB 02-680| 206B,206L w/ Allison 250-C20R eng power-out warning sensors |
| 95-24-5 |
McCauley |
Revised 5/96 | recurringly inspect prop hub; if cracked, replace | specified hubs on C35, C72, C74, C75, C80, C86, C87, C92, C93 series props |
| 95-24-10 |
Michelin |
Replace P/N 028-520-1 tires | Cessna 650 (Citation III, VI, VII) |
| 95-23-5 |
Robinson |
Supersedes 94-17-07 | inspect tail rotor (t/r) blade alignment in each preflight; verify input & output shaft keys installed; replace t/r gearbox if misaligned | R22 with specified gearbox |
| 95-23-2 |
Bell |
Superseded by 96-1-8 |
| 95-23-12 |
Piper |
Install a placard that specifies manifold pressure limits | PA 46-350P |
| 95-23-11 |
Aerostar |
Replace cracked fittings on upr/lower horiz. flanges | PA 60-600,601,601P; 602P |
| 95-22-7 |
DeHavilland |
Supersedes 83-26-5 | recurringly inspect horiz. stabilizer forward/rear attachment fittings; replace if cracked | DHC-6 series |
Showing Results 2161 - 2180 of 5103
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< Previous |
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105
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109
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112
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113
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