What was found
(CAN) #2 ENGINE HAD A UNCOMMANDED SHUTDOWN IN CRUISE. POST FLIGHT INSPECTION FOUND THE CAUSE OF THE FAILURE WAS A FRACTURE OF THE ANGLE BEVEL DRIVE GEAR.
- Difficulty date
- February 12, 1997
- Submitted
- March 26, 2000
- Operation
- General aviation
- Engine
- Pwa PW120A
- System (JASC)
- 7260 · Turbine Engine Accessory Drive
- Part
- Bevel Drive Gear
- Condition
- Fractured
- Location
- Accessory Gearbx
- Part time
- 11,567 hours
- Stage of operation
- CR
- Nature of condition
- E
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.