What was found
UPON INSTALLATION OF VANE NOTED: TWO STUD WELDS BROKEN AS MARKED DURING TORQUE. REPLACED DISCREPANT PART.
- Difficulty date
- September 12, 1996
- Submitted
- March 26, 2000
- Operation
- Air carrier
- Aircraft
- N1073W
- Make and model
- Bell 206L1
- Aircraft serial
- 45386
- Engine
- Allsn 250C28B
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Diffuser Vane
- Part number
- 23007208
- Condition
- Weld Broken
- Location
- Engine
- Component
- 23033191
- 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.