What was found
SLAT SYS 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. - F -CTL REPLACED THE EXTEND SOLENOID ON 25CV POWER CONTROL UNIT REF AMM. PERFORMED OPS CHECKS PER AMM 27-84-00-710. NO DEFECTS OR LEAKS NOTED. SYSTEM CHECKS OK
- Difficulty date
- November 6, 2013
- Submitted
- November 8, 2013
- Operation
- Air carrier
- Aircraft
- N460UA
- Make and model
- Airbus A320232
- Aircraft serial
- 1248
- Aircraft time
- 41,808 hours, 17,830 cycles
- Engine
- Iae V2527A5
- System (JASC)
- 2780 · Leading Edge Slat Control System
- Part
- Solenoid
- Condition
- Faulty
- Location
- Le Slat
- Stage of operation
- IN
- How discovered
- O
- Nature of condition
- J
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.