What was found
(CAN) DURING C-CHECK A CRACK WAS FOUND IN THE ENGINE SUPPORT BEAM LOWER WEB BETWEEN FS 625.30 AND FS 640.00 NEAR LBL 36.20. THE CRACK WAS LOCATED IN THE CORNER OF ACCESS PANEL (P/N 601-35006-39) LANDING AND ENDED NEAR THE PANEL EDGE.
- Difficulty date
- March 13, 2001
- Submitted
- April 12, 2001
- Operation
- General aviation
- Make and model
- Cndair CL6002B19
- Engine
- Ge CF341A
- System (JASC)
- 5340 · Fuselage Main, Attach Fittings
- Part
- Beam
- Part number
- 601350061
- Condition
- Cracked
- Location
- Fuselage
- Component
- 60135006
- 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.