What was found
(CAN) CRACKED IN "O" RING GROOVE, IMPROPER FITTING OF "O" RING OR IMPROPER "O" RING FITTED TO THE CAP. POTENTIAL LOSS OF SEALING OF OIL TANK AND LOSS OF OIL OUT OF FILLER DURING FLIGHT.
- Difficulty date
- December 5, 1997
- Submitted
- March 26, 2000
- Operation
- General aviation
- Engine
- Pwa PW120A
- System (JASC)
- 7261 · Turbine Engine Oil System
- Part
- Oil Filler Cap
- Part number
- 3006084
- Condition
- Cracked
- Location
- O-Ring Groove
- 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.