What was found
VERTICAL STIFFENER ON AFT SIDE OF BS 621 BULKHEAD AT BL 0 TOWARDS TOP IS CHAFED. BLENDED DAMAGE ON VERTICAL STIFFENER AND FOUND TO BE WITHIN LIMITS. MAX DEPTH O DAMAGE 0.009" MAX LENGTH OF DAMAGE 0.025 IN IAW REO 601R-53-61-1523.
- Difficulty date
- October 12, 2011
- Submitted
- December 23, 2011
- Operation
- Air carrier
- Aircraft
- N467AW
- Make and model
- Cndair CL6002B19
- Aircraft serial
- 7900
- Aircraft time
- 18,477 hours, 17,813 cycles
- System (JASC)
- 5320 · Fuselage Miscellaneous Structure
- Part
- Stiffener
- Condition
- Chafed
- Location
- Bs 621
- 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.