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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 2301 - 2320 of 5103
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| AD No. |
MAKE |
Condensed description of ad note |
| 94-14-8 |
Canadair |
Inspect wiring harness of air-driven generator; modify if chafing | CL-600-2B16 |
| 94-14-6 |
Beech |
Superseded by 96-25-3 |
| 94-14-3 |
Nordskog |
Install improved NUPRO pressure relief value in coffeepot/water heater | Gulfstream G-1159, G-IV; Falcon 50, 200, 900 series; Canadair CL-600, 601 |
| 94-14-22 |
DeHavilland |
Recurringly inspect center hinge bracket for cracks | DHC-6-1,-100,-200,-300 |
| 94-14-20 |
Sikorsky |
R1 BW 2001-10 | Supersedes 84-6-2 | inspect blades centering plug for disbonding of filler | S-76A |
| 94-14-15 |
Falcon |
Replace attachment clamps on eng exhaust ducts | 50 (SN 2 thru 216) |
| 94-14-14 |
Piper |
Modify nose landing gear | 28R-180,-200,-201,-201T;28RT-201,-201T;44-180,-T |
| 94-14-13 |
Text-Lyc |
Superseded by 95-26-2 |
| 94-14-12 |
Tele-Cont |
Superseded by 95-21-15 |
| 94-14-11 |
Franklin Eng |
Superseded by 96-2-4 |
| 94-13-9 |
Falcon |
Check pressure & torque of nose landing gear shock absorber; recharge/retorque if needed & until relay in right side of electrical rack is installed | 900 series |
| 94-13-4 |
Schweizer |
Replace clevis pins in the spring assembly with bolts | 269A, A-1, 269B, 269C |
| 94-13-3 |
Enstrom |
Recurringly inspect tail rotor spindle for cracks; replace within 100 hrs | F28C, 28C-2, 28F, 280C, -FX |
| 94-13-11 |
Piper |
Replace MLG trunnions w/improved unit | PA34-200,-T; PA34-220T; PA44-180,-T |
| 94-13-10 |
Piper |
Supersedes 74-12-1 | Install hi-shear rivet replacement kit if stabilator torque tube bearing support fittings are loose | PA24-180,-250,-260,-400; PA30; PA39 |
| 94-12-8 |
Cessna |
Calibrate & label fuel quantity indicating sys at empty | 210, P210, T210 |
| 94-12-6 |
Hughes |
Supersedes 80-2-14 | inspect/replace lower belt drive pulley bearings | 269A, 269A-1, 269B, 269C |
| 94-11-9 |
Beech |
Modify damaged wire harness in main landing gear wheel well if damaged | 400A |
| 94-11-4 |
Mitsubishi |
Adjust underspd governor minimum stop; modify airframe condition control linkage & tachometer marks; placard eng idle spd at 76.5% | MU-2B-26A,-36A,-40,-60,-36 |
| 94-11-3 |
Corp Jets |
Superseded by 06-1-4 |
Showing Results 2301 - 2320 of 5103
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< Previous |
111
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112
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113
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114
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115
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116
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117
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118
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119
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120
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