NCFBBW
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.
4 reports on file, 2010-10-27 – 2011-05-28.
Part: LONGERON — CRACKED (ZONE 400) · airframe 35,412 hrs · 47,581 cycles
RT ENGINE NACELLE OTBD LONGERON CRACKED. FOUND ON ROUTINE INSPECTION, REMOVED AND REPLACED RIGHT NACELLE OTBD LONGERON. FOUND ON ROUTINE INSPECTION.
Part: DOUBLER — CORRODED (RT EXHAUST) · corrosion level 2 · airframe 35,412 hrs · 47,581 cycles
RT EXHAUST TRAIL DOUBLER CORRODED WS 131 AND WS 90.6 IS THE CENTER OF THE CORROSION. REPAIRED IAW EO-CFBBW-5-31-11, SRM 57-30, AND RD-57-213.
Part: SCREEN — OBSTRUCTED (RT ENGINE SCAV) · airframe 35,271 hrs · 47,103 cycles
IN-FLIGHT SHUTDOWN OF RT ENGINE DUE TO TORQUE FLUCTUATION BETWEEN 45 TO 40, OIL PRESSURE COMING DOWN FAST AND T5 RISING TO 900C AT IDLE. R & R RT ENGINE IAW WC 72-00 LEAK CHECK AND GROUND RUNS NORMAL. THE ENGINE IN-FLIGHT SHUT DOWN ROOT CAUSE DETECTED AS THE OIL LEAKED OUT FROM THE COMPRESSOR DUE TO THE AGB INTERNAL SCAVENGE PUMP INLET SCREEN BLOCKED BY THE BROWNISH AND ASH COLORED FLAKES FROM THE AGB INTERNAL COATING
Part: LONGERON — CRACKED (LT NACELLE) · airframe 34,627 hrs · 45,057 cycles
(CLOSED) LT INBD LONGERON CRACKED AT NACELLE STA 47. (THIS WAS FOUND ON AS ROUTINE INSP)