N5793Z
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
7 reports on file, 1996-03-19 – 1997-04-01.
Part: ROD BEARING — CRACKED (T/R PITCH CONT)
PITCH CONTROL ROD CRACKED END BEARINGS.
Part: INDICATOR — ERRATIC (FUEL GAGE)
GAGE ERRATIC WITH 20% MORE FUEL.
Part: GYRO — DEFECTIVE (COCKPIT DG)
UNIT PRECESSING AND SLAVE METER WILL NOT SWING.
Part: TRANSCEIVER — INTERMITTENT (COCKPIT ATC)
INTERMITTENT TRANSMIT. VERIFIED UNIT TO HAVE LOW POWER OUT. TRIED ADJUSTING POWER TO SPECS. NO HELP. REPLACED CAVITY TUBE V101. REPAIRED. ADJUSTED FREQUENCY. COOKED UNIT UNDER HEAT LAMP, VIBRATED AND PUT IN FREEZER. FREQUENCY REMAINED STEADY. BENCH CHECK GOOD.
Part: VALVE — DEFECTIVE (FUEL SYS)
LEAKING FROM #2 TO #1 ENGINE.
Part: SHAFT — DEFECTIVE (ENG PT OUTER)
UPON INSPECTION OF NEW OUTER PT SHAFT NOTED THE FOLLOWING: ALSEAL COATING FLAKING ON SHAFT O.D. NEW PART INSTALLED.
Part: WHEEL — BLADE ERODED (1ST STAGE)
ENGINE REMOVED DUE TO #1 AND #2 WHEEL CYCLE RETIREMENT. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: 1ST STAGE WHEEL BLADES MINOR SULFIDATION AND ERODED LEADING EDGE. SCRAPPED 1ST STAGE WHEEL.