What was found
DIVERTED TO SLC DUE TO WING BODY OVERHEAT INDICATION. DISCREPANCY FOUND TO BE NR 2 ENGINE, STRUT CAVITY OVERHEAT DETECTOR ELEMENT FAULT. REPLACED OVERHEAT DETECTOR SENSING ELEMENT OF NR 2 ENGINE STRUT CAVITY .
- Difficulty date
- December 2, 2004
- Submitted
- December 29, 2004
- Operation
- Air carrier
- Aircraft
- N308UA
- Make and model
- Boeing 737322
- Aircraft serial
- 23669
- Aircraft time
- 51,063 hours, 30,150 cycles
- Engine
- Ge CFM56*
- System (JASC)
- 2613 · Overheat Detection
- Part
- Overheat Loop
- Part number
- 355574255
- Condition
- Failed
- Location
- Nr 2 Engine
- Stage of operation
- CR
- How discovered
- O
- Nature of condition
- N
- Precautionary procedure
- A
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.