What was found
DURING MAINTENANCE AFTER FLT 247 IN EWR, THE NR 1 SLAT FLAP SYSTEM FAULTED. REMOVED AND REPLACED THE NR 1 SLAT FLAP CONTROL COMPUTER (SFCC) IAW 27-51-34-000-001, TESTED OK IAW 27-54-00-710-002. AIRCRAFT RETURNED TO SERVICE.
- Difficulty date
- April 4, 2003
- Submitted
- April 7, 2003
- Operation
- Air carrier
- Aircraft
- N261AV
- Make and model
- Airbus A320214
- Aircraft serial
- 1615
- Aircraft time
- 4,198 hours, 1,261 cycles
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Computer
- Part number
- 4917011
- Part serial
- 04140
- Condition
- Faulty
- Location
- Zone 120
- Stage of operation
- IN
- How discovered
- V
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.