What was found
(CAN) CRACKS FOUND AT FUSELAGE FRAME RIVETS FOR VENTRAL FIN POSSIBLE REASON RIVET SPACING TO SMALL CRACKS AT RIVETS WHERE FRAME AND VENTRAL FIN JOIN.
- Difficulty date
- January 20, 2003
- Submitted
- February 10, 2003
- Operation
- Air carrier
- Make and model
- Cessna 208B
- Engine
- Pwa PT6A114A
- System (JASC)
- 5500 · Empennage Structure
- Part
- Frame
- Condition
- Cracked
- Location
- Empennage
- 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.