What was found
INSPECTION TYPE:C&SI #6 FLAP TRACK AFT O/B ATTACH POINT VERTICAL STIFFENER ON R/H FALSE S PAR CRACKED STIFFENER REMOVED IAW SRM 51-30-2. STIFFENER REPLACED IAW SRM 51-30 -02 & DRAWING 65-16216
- Difficulty date
- February 25, 2003
- Submitted
- March 14, 2003
- Operation
- Air carrier
- Aircraft
- N936UP
- Make and model
- Boeing 727108C
- Aircraft serial
- 19503
- Aircraft time
- 47,122 hours, 30,408 cycles
- System (JASC)
- 5753 · Trailing Edge Flaps
- Part
- Stiffener
- Condition
- Cracked
- Location
- #6 Flap Track
- Stage of operation
- IN
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.