What was found
(CAN) DURING PRESSURIZATION CHECK, A 4 INCH CRACK WAS DETECTED IN THE FUSELAGE SKIN AT R1 DOOR, FORWARD GALLEY, LOWER AFT CORNER. REPAIRED IAW SRM 53-30-3.
- Difficulty date
- July 30, 1998
- 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
- Fuselage
- 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.