N7254R
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
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.
3 reports on file, 1995-10-24 – 2005-01-14.
Part: SENSOR — DEFECTIVE (OIL TEMP)
(MRR NR 01-011405) LOSS OF NR 1 ENGINE OIL PRESSURE. LOOSE AND LEAKING OIL TEMPERATURE SENSOR. LOOSE BUT IN SERVICEABLE CONDITION. REMOVED TEMPERATURE SENSOR, INSPECTED, AND REINSTALLED. RAN ENGINE AND FOUND NO FURTHER DEFECTS. (NM05200502782) (K)
Part: TRUSS — CRACKED (RT ENGINE) · airframe 1,700 hrs
GJT - RIGHT ENGINE TRUSS MOUNT CRACKED NEAR WELD AT UPPER OUTBOARD ATTACH POINT. AREA ''A''. CRACKED AT TYPICAL LOCATION AS IDENTIFIED IN AD 95-02-18, BEECH SB NR 2255 R6. REMOVED AND REPLACED THE TRUSS ASSEMBLY. THE REPETATIVE INSPECTIONS REQUIRED BY AD 95-02-18 ARE NOW TERMINATED BY INSTALLATION OF TRUSS P/N 129-910047-17. THE NEW TRUSS WILL BE DUE MAGNETIC PARTICLE INSPECTIONS AT 8,000 HOUR INTERVALS. (X)
Part: BEARING — FAILED (LT START/GEN)
DEN - FLT 7536 - DURING CLIMB-OUT, LEFT GENERATOR FAILED. PILOT RETURNED TO BASE WITH NO FURTHER INCIDENT. AFT BEARING, PN 03-6009-18, WAS FOUND TO HAVE FAILED. REMOVED AND REPLACED START/GENERATOR WITH OVERHAULED UNITS. SYSTEM OPS CHECK COMPLETED WITH NO FURTHER DEFECTS.