What was found
GRIPES ON SLAT SYS 2, WITH RESET OF SFCC2 SLAT CHANNEL CB CORRECTING THE PROBLEM. REPLACE THE SLAT FLAP CONTROL COMPUTER 2 IAW AMM. REPLACED PER LM CALL OUT & ACCOMPLISHED OPERATIONAL TEST OF FLAP AND SLAT SYSTEM, ALL TESTS PASS.
- Difficulty date
- August 27, 2011
- Submitted
- September 29, 2011
- Operation
- Air carrier
- Aircraft
- N810UA
- Make and model
- Airbus A319131
- Aircraft serial
- 843
- Aircraft time
- 45,471 hours, 18,053 cycles
- Engine
- Iae V2522A5
- System (JASC)
- 2780 · Leading Edge Slat Control System
- Part
- Computer
- Part number
- 4917011
- Part serial
- 72171
- Condition
- Faulty
- Location
- Nr 2
- Stage of operation
- NR
- How discovered
- O
- Nature of condition
- F
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.