What was found
(CAN)POWER LOSS IN THE CLIMB FOLLOWED BY IMMEDIATE LANDING. #6 CYLINDER FAILED DUE TO INGESTION OF METAL DEBRIS WHICH HAD REMAINED IN THE INDUCTION SYSTEM AFTER THE FAILURE OF #2 CYLINDER EXHAUST VALVE ON THE PREVIOUS DAY.
- Difficulty date
- April 5, 1996
- Submitted
- March 26, 2000
- Operation
- Air carrier
- Make and model
- Dhav DHC3
- Engine
- Pwa R134059
- System (JASC)
- 8530 · Reciprocating Engine Cylinder Section
- Part
- Piston
- Part number
- 15373CAI
- Condition
- Pounded
- Location
- #6 Cylinder
- Component
- Pwa
- Stage of operation
- CL
- Nature of condition
- E, R
- Precautionary procedure
- A
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.