What was found
(CAN) IN THE TASK OF CHANGING THE LONGERON, IT WAS VISUALLY NOTED THAT THIS FRAME WAS CRACKED IN TWO PLACES. THE CRACKS WERE NEAR THE UPPER TWO ATTACHMENT POINTS OUT OF THE 4 ATTACHMENT POINTS.
- Difficulty date
- October 4, 2004
- Submitted
- March 3, 2005
- Operation
- General aviation
- Make and model
- Bell 206L1
- Aircraft time
- 7,580 hours
- Engine
- Allsn 250C28B
- System (JASC)
- 5313 · Fuselage Main, Longeron/Stringer
- Part
- Longeron
- Part number
- 206032308003
- Condition
- Cracked
- Location
- Fuselage
- 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.