What was found
DURING ROUTINE INSPECTION, RIGHT I/B MIDFLAP REAR SPAR UPPER CHORD FOUND CRACKED AT WING BUTT LINE 120 UPPER ROW FWD FASTENER HOLE. REMOVED AND REPLACED PER IAW MM 27-51-1. RIG AND OP CHECK FLAP PER IAW MM 27-51-0.
- Difficulty date
- June 5, 2000
- Submitted
- June 7, 2000
- Operation
- Air carrier
- Aircraft
- N101FE
- Make and model
- Boeing 72722C
- Aircraft serial
- 19197
- Aircraft time
- 50,425 hours, 36,789 cycles
- System (JASC)
- 5753 · Trailing Edge Flaps
- Part
- Spar
- Condition
- Cracked
- Location
- Te Flap
- 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.