What was found
(CAN) DURING ROUTINE CHECK A 2.7500 INCH CRACK WAS FOUND ON THE OUTER FUSELAGE SKIN AT FS 847 STRINGER 24L. CRACK REPAIRED IAW SRM REV 85.53-30-3,FIG 48 SHT 33. TIMES 59257.06 CYCLES 55392.
- Difficulty date
- August 18, 2004
- Submitted
- February 3, 2005
- Operation
- General aviation
- Make and model
- Boeing 737201
- Aircraft time
- 57,685 hours, 49,371 cycles
- Engine
- Pwa JT8D9A
- System (JASC)
- 5330 · Fuselage Main, Plate/Skin
- Part
- Skin
- Condition
- Cracked
- Location
- Fuselage
- 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.