What was found
(CAN) 2.34 CRACK IN FUSELAGE TOP OF S18L BETWEEN BS 727A AND BS 727B. REPAIRED IAW SRM 53-30-3,FIG 48, SHEET 33, DETAIL XI REFERENCE PROCEDURE IV AND VII. AIRCRAFT TIME 56,880:17 CYCLES52,484 C
- Difficulty date
- November 11, 2003
- Submitted
- January 5, 2004
- Operation
- General aviation
- Make and model
- Boeing 737296
- Aircraft time
- 54,706 hours, 48,128 cycles
- Engine
- Pwa JT8D9A
- System (JASC)
- 5330 · Fuselage Main, Plate/Skin
- Part
- Skin
- Condition
- Cracked
- Location
- Fuselage
- Stage of operation
- IN
- How discovered
- 9
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.