99-2-2 |
Robinson |
Supersedes 95-6-7 | Replace specified forward flexplates | R22 |
99-2-17 |
Bell |
Review records for yoke bending loads that could cause failure of tail rotor yoke. Replace as directed | 214B, -1 |
99-2-14 |
Raytheon |
Inspect engine stainless steel fuel line; modify power lever bracket if not within specified clearence; replace fuel line & modify power lever bracket as directed | 2000 |
99-2-13 |
Eurocopter |
Remove & replace main rotor hib spindles & flapping hinge pin as directed | Specified AS332C, L, L1 |
99-2-1 |
Bell |
Recurringly inspect tailboom skin and edges; replace tailboom if cracked | Specifield 206L,1,3,4 |
99-19-32 |
Pilatus |
Inspect all flap actuator internal gear systems for end play and backlash measurement; adjust as specified | PC-12 |
99-19-30 |
Sikorsky |
Recurringly inspect attachment angle on tail gearbox forward fairing for disbonding | S-76 A B C |
99-19-24 |
Dassault |
Replace elevator auxilary artificial feel unit (AFU) as specified | Falcon 900, 2000 |
99-19-22 |
Eurocopter |
Superseded by 00-17-8 |
99-19-13 |
Sabreliner |
Revise AFM regarding activation of ice protection system | 75A, 75, 65, 60, 40 |
99-19-1 |
Tele-Cont |
Supersedes 99-9-17 | Perform visual and ultrasonic inspection of crankshaft as specified; if crack found, replace | selected TCM models |
99-18-8 |
IAI |
Install independent circuit breaker and accessories for hydraulic low pressure warning lights | 1124 |
99-18-2 |
Bell |
Modify and inspect fin spar for cracks | Replace if detected | Repair disbonding or corrosion | 205 |
99-18-15 |
Beech |
Replace landing gear emergency hand pump as specified | C90A,B200,350 |
99-18-14 |
Cessna |
Inspect control pivot bolt for clearance with aileron cable | 172R |
99-18-13 |
DeHavilland |
Ammend AFM to prevent throttle levers being positioned below flight idle stop while in flight | DHC-6 |
99-17-8 |
Pilatus |
Superseded by 01-11-2 |
99-17-7 |
Eurocopter |
Create component log card for each tension-torsion strap | Review history | Replace as specified | BK 117 |
99-17-5 |
IAI |
Recurringly perform dye inspection of main fuel tube assemblies of pressure transmitter tubes on engines to detect cracking | 1125SPX |
99-17-3 |
Bell |
Modify vertical fin and inspect fin spar assembly for cracks | Replace as specified | Repair corrosion or disbonding if detected | 204B |