What was found
(CAN) IN COMPLIANCE WITH CF-2006-12 THE VERTICAL FIN WAS INSPECTED WITH 10X MAGNAFLYING GLASS AND THEN WAS LPI INSPECTED AND A CRACK WAS FOUND ON ONE OF THE INSERTS. THE FIN WAS SENT OUT FOR REPAIR. (TC NR 20061004007)
- Difficulty date
- October 2, 2006
- Submitted
- December 4, 2006
- Operation
- General aviation
- Make and model
- Bell 206B
- Aircraft time
- 12,113 hours
- Engine
- Allsn 250C20B
- System (JASC)
- 5302 · Rotorcraft Tail Boom
- Part
- Insert
- Part number
- 206020113
- Condition
- Cracked
- Location
- Vertical Stab
- Part time
- 13,000 hours
- Stage of operation
- IN
- How discovered
- 9
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.