|
|
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 2581 - 2600 of 5103
| View All
< Previous |
125
|
126
|
127
|
128
|
129
|
130
|
131
|
132
|
133
|
134
| Next >
| AD No. |
MAKE |
Condensed description of ad note |
| 91-2-7 |
Cessna |
Change take-off info in airplane flight manual & owner's manual | C-411,-A |
| 91-2-6 |
Piper |
Superseded by 91-21-9 |
| 91-19-6 |
Piaggio |
Endoscopically inspect vertical stabilizer attachment spar; modify if cracked | P180 |
| 91-19-5 |
BAe |
Correct fire extinguish sys crossed/loose/misidentified wires, supports & connectors | 125-800A,HS.125-700A,DH/BH/HS 125 retrofit w/pre-mod 253274A Garrett engs |
| 91-19-3 |
Tele-Cont |
Inspect & replace specified eng oil filters | IO-360; L/TSIO-360; IO-346; L/I/O-470; TSIO-470; IO-520; L/TSIO-520,6-285; IO-550,G; TSIO-520 |
| 91-19-2 |
Sikorsky |
Superseded by 96-15-3 |
| 91-19-1 |
Canadair |
Repair/modify chafed air drive generator wiring harness | CL600-1A11,-2A12,-2B16 |
| 91-18-19 |
Beech |
Superseded by 09-25-01 |
| 91-18-12 |
PZL Eng |
Superseded by 94-2-6 | supersedes 91-15-12 |
| 91-18-11 |
Beech |
Superseded by 92-10-12 |
| 91-17-4 |
MDHC |
Superseded by 95-3-13 |
| 91-17-2 |
Canadair |
Superseded by 92-20-4 |
| 91-17-1 |
Beech |
Paint contrasting colors on horiz. stabilizer rear spars, actuator housing & inspection hole ledges | 33, 34, 35, 36, 45, 55, 56, 58, 95 series |
| 91-15-4 |
McCauley Prop |
Supersedes 77-17-9 & 77-20-3 & 77-23-1 & 77-24-4 & 78-20-1 | replace cracked assembly of 2-bladed, c/s prop w/threaded retention hubs; modify prop hub assembly | Beech A23, 24, 58, 55; Bellanca 17-30,-A; Cessna 180, 182, 185, 188, 206, 207, 210, 305, 310, 336, 337; Mooney M20; Navion A,B,D-H |
| 91-15-20 |
Beech |
Reinforce/repair cracked eng mounts; inspect recurringly | 95, 55, 58 series |
| 91-15-2 |
P&W Eng |
Repetitively perform borescope inspection of gas generator case on JT15D-4B turbofan engine; replace case if cracked | Cessna S550 series |
| 91-15-12 |
PZL Eng |
Superseded by 91-18-12 |
| 91-15-10 |
Aerospatiale |
Supersedes 91-12-19 | modify horiz stabilizer balance weight | TB9,-10,-20,-21 |
| 91-14-5 |
Avco Lyc |
Remove corroded, cracked 3rd stage high compressor rotor disc bore | ALF 502L |
| 91-14-22 |
Textron Lyc Eng |
Superseded by 04-10-14 |
Showing Results 2581 - 2600 of 5103
| View All
< Previous |
125
|
126
|
127
|
128
|
129
|
130
|
131
|
132
|
133
|
134
| Next >
|
