| 96-20-8 |
Fairchild |
Supersedes 93-19-6 | repetitively inspect acrylic cabin & cockpit windows; replace if cracked | SA26-T,-AT; SA226-T,-AT,-TC; SA227-AT,-AC |
| 96-20-7 |
Janitrol |
Superseded by 04-21-5 |
| 96-2-4 |
Franklin |
Supersedes 94-14-11 | replace certain parts on engs using 80-91+ octane avgas | 6A4-150-B3,-165-B3 |
| 96-19-5 |
Fairchild |
Supersedes 95-19-7 | recurringly clean & inspect main /nose landing gear yokes; replace if cracked | SA226-T,-AT,-TC; SA227-AT,-AC,-TT |
| 96-19-2 |
Piaggio |
Modify passenger seat cushion | P-180 (SN1002,1004 thru 1022) |
| 96-19-18 |
Socata |
Install rivets on rudder right side; drill drainage holes in area of elevators & rudder | specified TBM 700 |
| 96-19-15 |
Bombardier |
Replace spring bungee assembly of nose landing gear if improper collar torque or if clearance between collar & body of bugee is incorrect | CL-601-3A, -3R (SN5100 thru 5166) |
| 96-19-13 |
Learjet |
Permanently reduce max operating Mach limit by accomplishing specified actions, or remove Raisbeck STC SA766NW mod & return aircraft to original or "Softflight" config | specified 35,-A; 36,-A |
| 96-19-1 |
Allison |
Recurringly inspect eng filters for metal particles; if necessary, replace parts; replace bearing at specified time | various engs w/Superior Air Parts bearings |
| 96-18-9 |
Raytheon |
Modify TKS metering pump in airframe ice protection sys | Hawker 800,A; 1000,A |
| 96-18-7 |
Bellanca |
Recurringly inspect nose landing gear sys; replace cracked/bent brackets & corroded/worn bolts; adjust discrepancies; replace cylinder internal stroke limiting sleeve if out of tolerance | 17-30,A; 17-31,A,TC,ATC |
| 96-18-5 |
Bell |
Supersedes 96-14-10 | recurringly inspect tailboom; replace if cracked or corroded beyond limits | 206L,L-1,L-3 |
| 96-18-22 |
Robinson |
Disassemble & inspect gearbox; replace if needed | specified R44 |
| 96-18-20 |
Piaggio |
Replace outflow/safety valve | P-180 |
| 96-18-2 |
Am Champ |
Supersedes 96-3-11 | install removable inspection hole openings; repetitively inspect wing front strut attach fittings until replaced | specified 8KCAB, 8GCBC, 7GCBC, 7ECA |
| 96-18-15 |
Bell |
Supersedes 96-1-8 | recurringly inspect tail rotor blade; replace if cracked | specified 222,B,U; 230 |
| 96-18-14 |
Hartzell |
Correction BW 2002-18 | Replace specified prop hubs; replace cracked blades & blade clamps | various aircraft |
| 96-18-13 |
Honeywell |
Superseded by 01-23-9 |
| 96-18-1 |
Learjet |
Modify aft core cowl nozzle of eng nacelles | 60 |
| 96-17-9 |
Raytheon |
Supersedes 95-10-1 | recurringly inspect fuel feed hose assembly on APU; correct any discrepancy; replace conduit | Hawker 1000,A |
