96-17-13 |
Raytheon |
Inspect elevator control circuit for correct sleeve lengths & elevator pulley assembly; correct any discrepancy | Hawker 1000,A |
96-17-10 |
Beech |
Superseded by 98-6-30 |
96-17-1 |
Text-Lyc |
Supersedes 96-15-7 | replace suspect second stage power turbine disks | T5313B |
96-15-7 |
Allied Signal |
Superseded by 96-17-1 |
96-15-4 |
Hartzell |
Replace prop blade shanks if flawed or cracked | various aircraft |
96-15-3 |
Sikorsky |
Supersedes 93-11-5 & 91-19-2 | recurringly inspect drive shaft & balance weights; replace if cracked or loose | specified S-76B |
96-15-2 |
P&W Eng |
Recurringly inspect crankshaft counterweights; replace if cracked; replace at next o'haul | R1340-AN1 |
96-14-10 |
Bell |
Superseded by 96-18-5 |
96-12-9 |
PTC Seating |
Convert seat footrest assembly per SB25-1330 | various aircraft |
96-12-8 |
Twin Cmdr |
Superseded by 98-8-25 |
96-12-7 |
Tel-Cont |
Superseded by 05-12-6 |
96-12-6 |
Tele-Cont & Rolls-Royce |
Supersedes 77-13-3 & 78-19-2 | reset engine timing | Tele-Cont O-200A,B & Rolls-Royce O-200A,B,C |
96-12-5 |
Allied Signal |
Replace specified power turbine rotors | LTS101 & LTP101 series |
96-12-4 |
Sup. Air Parts |
Replace specified pistons | Tele-Cont O-470-K,-L,-R |
96-12-27 |
Allied Signal |
Inspect disk tenon area of gas generator turbine disk; remove suspect disks | LTS-,LTP-101 series |
96-12-25 |
Bell |
Recurringly inspect t/r blade along bond lines; replace blade if corroded | 204B (SN -1 thru -70; -2196 thru -2199) |
96-12-23 |
Cessna |
Replace wing stall fence exceeding 1.28 inches in height | 150 & 152 series w/Bush STOL |
96-12-22 |
Cessna |
Recurringly inspect eng oil filter adapter assembly; replace if damaged | various aircraft |
96-12-17 |
Raytheon |
Remake specified diode soldered connection or replace if not sound | Hawker 800,A; 1000,A |
96-12-16 |
Raytheon |
Modify airframe in lower fuselage aft of wing rear spar; repair if bolt fouls flap control sys | Hawker 800,A |