What was found
(CAN) 0.5 INCH CRACK AT BS 801 3 INCHES ABOVE STRINGER 24L ORIGINATING FROM SMALL GRAVEL DENT IN FUSELAGE. REPAIRED IN ACCORDANCE WITH SRM.
- Difficulty date
- December 16, 1996
- Submitted
- March 26, 2000
- Operation
- Air carrier
- Make and model
- Boeing 737210C
- Engine
- Pwa JT8D9A
- System (JASC)
- 5330 · Fuselage Main, Plate/Skin
- Part
- Skin
- Condition
- Cracked
- Location
- Bs801 Str 24l
- 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.