What was found
(CAN) HOT END INSPECTION REVEALED THE FIRST STAGE NOZZLE BURNT BEYOND ACCEPTABLE LIMITS.
- Difficulty date
- November 22, 2001
- Submitted
- April 26, 2002
- Operation
- General aviation
- Make and model
- Bell 206L1
- Aircraft time
- 4,169 hours, 12 cycles
- Engine
- Allsn 250C28B
- System (JASC)
- 7250 · Turbine Section
- Part
- Nozzle
- Part number
- 23008593
- Condition
- Burned
- Location
- Turbine Section
- 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.