What was found
(CAN) WEB P/N 205-030-163-395 FOUND CRACKED AT INDUCTION BAFFLE SUPPORT WL 80.13. THE CRACK WAS APPROX 1 INCH IN LENGTH AND .5 INCH DOWN . REPAIR SCHEME IN PROGRESS THROUGH MFG. (TC NR 20070321008)
- Difficulty date
- March 21, 2007
- Submitted
- May 1, 2007
- Operation
- General aviation
- Make and model
- Bell 205A1
- Aircraft time
- 11,658 hours, 3,646 cycles
- Engine
- Lyc T5313B
- System (JASC)
- 5310 · Fuselage Main, Structure
- Part
- Beam
- Part number
- 205030163395
- Condition
- Cracked
- Location
- Fuselage
- Part time
- 1,231 hours
- Stage of operation
- NR
- How discovered
- 9
- Nature of condition
- O
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.