What was found
(CAN) CRACK IS FROM THE FORWARD I/B SPAR CAP TO FITTING RIVET AND GOES TO THE EDGE OF THE FITTING. THE CRACK WAS DISCOVERED DURING A SCHEDULED WING INSPECTION. CRACK WAS VERIFIED USING LEVEL 2 PENETRANT.
- Difficulty date
- October 16, 2000
- Submitted
- January 19, 2001
- Operation
- Air carrier
- Make and model
- Beech A100
- Aircraft time
- 19,583 hours
- Engine
- Pwa PT6A28
- System (JASC)
- 5740 · Wing, Attach Fittings
- Part
- Fitting
- Part number
- 351150582
- Condition
- Cracked
- Location
- Wing
- 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.