What was found
ENGINE EXHIBITED HIGH VIBRATION IN SERVICE. DISASSEMBLY INSPECTION REVEALED T-2 BLADE FAILURE AND CONSEQUENTIAL DAMAGE TO THE 2ND, 3RD, AND 4TH AIRFOILS. THE CAUSE OF FAILURE IS UNDER INVESTIGATION.
- Difficulty date
- September 12, 1996
- Submitted
- March 26, 2000
- Operation
- General aviation
- Engine
- Pwa JT8D9A
- System (JASC)
- 7250 · Turbine Section
- Part
- Blade
- Part number
- 834401
- Condition
- Failure
- Location
- N2 Turbo T1
- Stage of operation
- IN
- Nature of condition
- E
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.