What was found
(CAN) DURING ROUTINE INSPECTION AME DISCOVERED A CRACK SURROUNDING ELEVATOR CONTROL SUPPORT (P/N 205-001-920-001) IN A FWD AND AFT SKIN OF TAILBOOM PANEL (205-032-819-3). PANEL REPLACED, A/C RETURNED TO SERVICE.
- Difficulty date
- September 29, 2004
- Submitted
- October 5, 2004
- Operation
- General aviation
- Make and model
- Bell 212
- Aircraft time
- 11,077 hours
- Engine
- Pwa PT6T3
- System (JASC)
- 5302 · Rotorcraft Tail Boom
- Part
- Panel
- Part number
- 2050328193
- Condition
- Cracked
- Location
- Tailboom
- 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.