What was found
(CAN) DURING DESCENT, STABILIZER TRIM AND MACH TRIM CAUTION MESSAGES GOT POSTED, COULD NOT RE-ENGAGED EITHER HORIZONTAL STABILIZER CHANNELS. LANDING SUCCESSFULLY WITH FLAPS AT 20. AIRCRAFT RELEASED BY REFERRING TO AOM254.
- Difficulty date
- May 2, 2005
- Submitted
- June 2, 2005
- Operation
- General aviation
- Make and model
- Cndair CL6002C10
- Engine
- Ge CF348C1
- System (JASC)
- 2740 · Stabilizer Control System
- Part
- Control Unit
- Part number
- C13045BA03
- Condition
- Inoperative
- Location
- Horizontal Stab
- Stage of operation
- DE
- How discovered
- O
- Nature of condition
- F
- Precautionary procedure
- B
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.