What was found
(AUS) NR 2 ENGINE CONSTANT SPEED DRIVE (CSD) INTERNAL FAILURE. INVESTIGATION FOUND THAT THE OIL PRESSURE RELIEF VALVE HAD BLOWNOUT AND THE ATTACHMENT BOLTS HAD SHEARED. OIL LOSS THEN CAUSED CSD FAILURE.
- Difficulty date
- December 29, 2000
- Submitted
- March 20, 2001
- Operation
- General aviation
- Make and model
- Boeing 737376
- Engine
- Cfmint CFM563C
- System (JASC)
- 2410 · Alternator-Generator Drive
- Part
- Relief Valve
- Part number
- 735511A
- Condition
- Failed
- Location
- Alternator
- Part time
- 14,949 cycles
- Stage of operation
- CR
- How discovered
- O
- Nature of condition
- J
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.