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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 |
96-25-2 |
Mitsubishi |
Revise AFM on operating in severe icing conditions | MU2B series |
96-25-12 |
Sundstrand |
Replace compressor wheels w/serviceable parts | AS332 Super Puma; Cessna 650 series; Falcon 20, 50, 200 series; Gulfstream 159, 1159 & G-III series; HS 125-700A; Sabre NA-265 series; Lockheed 1329 series |
96-24-9 |
Bell |
Supersedes 96-21-12 | replace eng main electrical harness assembly; disable overspeed solenoid; replace unserviceable ECU; placard appropriately & revise RFM | 407 |
96-24-8 |
Air Tractor |
Replace specified parking brake valve | AT-300,-301,-302,-400,-400A, -401,-402,-501,-502 series |
96-24-6 |
Cessna |
Superseded by 00-3-9 |
96-24-17 |
Luscombe |
Install 2 additional wing inspection holes & modify wing tip fairing in metal wings; replace spar extrusions if intergranular corrosion is evident | 8,-A,-B,-C,-D,-E,-F |
96-24-16 |
Raytheon |
Superseded by 00-8-7 |
96-24-13 |
New Piper |
Supersedes 75-26-18 | modify landing gear selector cable attach pin assembly | PA31 series |
96-24-11 |
IAI |
Recurringly inspect aileron push-pull tubes & guide rollers; replace if worn beyond limits or rollers do not rotate smoothly | 1124,-A; 1123 |
96-23-3 |
Text-Lyc |
Repair/replace specified high pressure fuel pumps | IO-320,-360,-540; LIO-320,-360,-540; AEIO-320,-360,-540; HIO-360; TO-360; O-540-L; |
96-23-19 |
Air Tractor |
Install new flap actuator stop & roll pin | AT-301,-302,-400,-401,-402,-501,-502,-503 series |
96-23-1 |
Bell |
Replace Kratos turbine outlet temp indicator | 206L-1 |
96-22-3 |
Raytheon |
Modify thrust reversers | Hawker 1000,A |
96-22-12 |
Raytheon |
Inspect fuel filter assemblies; replace if bypass valve is glued shut | 2000 |
96-21-5 |
Fairchild |
Superseded by 97-10-13 |
96-21-4 |
New Piper |
Supersedes 86-17-7 | replace specified hydraulic hoses installed after 2-1-85 | PA23 series; PA31,31P,31T series; PA42 series; Mojave |
96-21-3 |
New Piper |
Recurringly inspect aileron hinge bracket on aileron spar; replace if cracked or 1000 TIS after intial inspection | PA-31 series & PA-42 series |
96-21-13 |
LITEF GmbH |
Placard specified primary attitude indicator or modify attitude & heading reference sys | various aircraft |
96-21-12 |
Bell |
Superseded by 96-24-9 |
96-21-11 |
New Piper |
Supersedes 93-25-8 | replace specified main landing gear actuator reinforcement bracket | PA31 series |
Showing Results 2061 - 2080 of 5103
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< Previous |
99
|
100
|
101
|
102
|
103
|
104
|
105
|
106
|
107
|
108
| Next >
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