| 93-24-7 |
Corp Jets |
Deactivate APU until new sealant installed around over-temp sensor | BH/HS 125-600A; HS 125-800A, BAe 125-800A series equipped w/Sundstrand Turbomach APU |
| 93-24-3 |
Beech |
Supersedes 92-15-6 | replace cracked rudder forward spar assembly; modify rudder if cracked near center hinge; if intact, reinspect ev 500 hrs | 33;35;36,-TC series |
| 93-24-2 |
Piper |
Revised 2/94 | replace elevator control tube asmbly parts if damaged | PA31,-P,-T |
| 93-24-15 |
Cessna |
Replace existing rheostat w/improved one | 150, 172 & 180 series |
| 93-24-14 |
Piper |
Superseded by 05-13-16 |
| 93-24-13 |
Enstrom |
Replace failed trim sys parts; rewire sys & replace trim actuator circuit breaker | F28C,-2; F28F; 280-C,-F,-FX |
| 93-24-12 |
Piper |
Repetitively replace bolt btn upper drag link & nose gear trunnion | PA34 series |
| 93-24-10 |
Learjet |
Modify wiring in & btn left- & right-hand generator interface boxes | 55,-B,-C |
| 93-24-1 |
Raytheon |
Reposition or replace parts damaged from chafing of oxy pipe next to nose wheel steering control chain; ensure minimum clearance btn pipe & chain | Hawker 1000 |
| 93-23-9 |
Turbomeca |
Superseded by 95-11-1 |
| 93-23-8 |
Corp Jets |
Modify mounting of battery contactors & emerg contactors in rear equipment bay | DH/BH/HS/BAe 125 series except BAe 125-1000A series |
| 93-23-4 |
Eurocopter |
Install OAT & Vne limit placards; operate accordingly | SA315B,-316B,-319B w/STC'd main rotor blades |
| 93-23-13 |
Piper |
Supersedes 93-2-13 | Install thicker eng baffle seals | PA31 series |
| 93-23-12 |
Learjet |
Deactivate & placard auxiliary cabin & cockpit heating system | 60 |
| 93-23-1 |
Nordskog |
Replace or stop using specific water heaters & coffee makers w/discrepant pressure relief valves | Gulfstream G-1159 series, GIV; Falcon 50 & 900 series; Canadiar CL-600-1A11,-2A12,-2B16,-2B19 |
| 93-22-7 |
BAe |
Replace existing forward cabin door retainer catch assembly | 125-800A series |
| 93-22-5 |
Tele-Cont |
Replace cracked carb air intake housing assembly | O-200,-A; O-240; C85; C90 |
| 93-22-4 |
Canadair |
Superseded by 95-18-7 |
| 93-22-11 |
Bell Heli |
Superseded by 94-20-3 |
| 93-21-6 |
IAI |
Supersedes 92-12-7 | repetitively inspect outer lugs of horiz stabilizer hinge fitting; if cracked or within one year, replace w/titanium splice fitting | 1125 series |
