What was found
ABORTED TAKEOFF AT 110 KNOTS DUE TO NR 1 ENGINE AUTO-RETARDED TO 82 PERCENT. REPLACED THE MAIN ENGINE CONTROL. THE CAUSE OF THE POWER REDUCTION IS ATTRIBUTED TO A FAILED ROTABLE VARIABLE DIGITAL TRANSDUCER.
- Difficulty date
- September 22, 1995
- Submitted
- March 26, 2000
- Operation
- Air carrier
- Aircraft
- N948UA
- Make and model
- Boeing 737522
- Aircraft serial
- 26691
- Engine
- Ge CFM56*
- System (JASC)
- 7321 · Fuel Control/Turbine Engines
- Part
- Mec
- Part number
- 1680654
- Condition
- Failed
- Location
- Nr 1 Engine
- Stage of operation
- TO
- Nature of condition
- R
- Precautionary procedure
- C, D
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.