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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 2201 - 2220 of 5103
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| AD No. |
MAKE |
Condensed description of ad note |
| 95-18-7 |
Canadair |
Supersedes 93-22-4 | inspect inside root radius of spigot rudder; modify if cracked | CL600 SN1004 thru-85; CL601 SN3001 thru -66; CL601-3A SN5001 thru -5147 |
| 95-18-5 |
Fairchild |
Replace aluminum cargo dr receptacles w/steel receptacles | SA226-AT |
| 95-18-4 |
Beechcraft |
Install autopilot & rudder boost improvement kit | 400 (SN 61), -A |
| 95-18-12 |
Mooney |
Replace Gerdes fuel selector valve w/Airight brand | M20K (SN -0001 thru -0091) |
| 95-18-11 |
DeHavilland |
Supersedes 81-10-11 | replace cracked wing spar attachment caps or incorporate mod 6/1301; until mod accomplished, reinspect at specified intervals | DHC-6-300 |
| 95-18-10 |
DeHavilland |
Supersedes 73-5-3 | replace cracked elevator root rib or incorporate mod 6/1769; reinspect ev 600 hrs until mod is incorporated | DHC-6-300 |
| 95-17-9 |
Fairchild |
Revised 4/96 | relocate left & right essential bus current limiters | SA-226 & -227 |
| 95-17-7 |
Fairchild |
Remove specified bolts from MLG door stop; service fluid servicing | SA226-T,-TC |
| 95-17-6 |
Mooney |
Replace cracked exhaust sys parts; reinspect ev 25 hrs if not cracked | M20K |
| 95-17-14 |
Bombardier |
Replace unserviceable horizontal stabilizer trim control unit | CL-600,-601 |
| 95-16-8 |
Allied Signal |
Replace specified eng parts | TPE331-25,-43,-1,-2,-3,-5,-8,-10,-11,-12 repaired/modified/altered by Fliteline Maintenance in Wharton, Tex. |
| 95-16-4 |
Allied Signal |
Replace specified axial compressor rotors & parts | LTS101, LTP101 |
| 95-15-4 |
Raytheon |
Remove corrosion on wing leading edges, anti-ice fluid distribution panel & landing/taxi lamp assembly; apply enhanced protectant | BAe 125-800A, -1000A |
| 95-14-9 |
Lear |
Superseded by 03-19-11 |
| 95-13-3 |
Beech |
Install circuit breaker per SB | F90; 99,-A; B99; A-,B-,100; 200,-C; B200,-C; A100 |
| 95-13-2 |
Twin Cmdr |
Inspect vert stabilizer ev 500 hrs TIS; if damaged or cracked, modify or replace | 685; 690,-A,-B,-C,-D; 695,-A |
| 95-13-10 |
Agusta |
Inspect/modify tail boom vert fin; reinspect ev 300 hrs for cracks | A109A,- AII,-C |
| 95-12-23 |
Twin Cmdr |
Recurringly inspect wing; if cracked, replace/modify per SB | 690C, 695 |
| 95-12-2 |
Hiller |
Recurringly inspect alignment of outboard T-T bar pin; inspect for cracks; install shims btn inboard end of drag strut & outboard T-T bar pin | UH-12,-A,-B,-C,-D,-E |
| 95-12-1 |
Piper |
Supersedes 93-21-12 | repetitively inspect wing forward spar fuselage attachment assembly; replace cracked/corroded parts | PA-25-150,-235,-260 |
Showing Results 2201 - 2220 of 5103
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