What was found
ENGINE REMOVED DUE TO N2 DRAG. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: LIFTING AND FLAKING PLASMA IN 4TH STAGE NOZZLE #4 TIP PATH. INSTALLED SERVICEABLE 4TH STAGE NOZZLE.
- Difficulty date
- February 23, 1995
- Submitted
- March 26, 2000
- Operation
- General aviation
- Aircraft
- N6160Z
- Make and model
- Bell 206L3
- Aircraft serial
- 51610
- Engine
- Allsn 250C30P
- System (JASC)
- 7250 · Turbine Section
- Part
- Nozzle
- Part number
- 23031426
- Condition
- Defective
- Location
- 4th Stage
- Component
- 23035128
- Stage of operation
- IN
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.