N741FE
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.
6 reports on file, 1996-06-03 – 2005-10-03.
Part: INVERTER — INOPERATIVE (LT AC)
DEPARTURE, ENROUTE, NR 1 INVERTER WENT OFF LINE AND WOULD NOT COME BACK ON. CREW REPORTED A STRONG BURNING ODOR BUT NO SMOKE. AIRCRAFT DIVERTED. THE NR 1 INVERTER CB WAS POPPED. THE NR 1 INVERTER WAS REMOVED AND REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE. (K)
Part: WIRE HARNESS — INOPERATIVE (RT NACELLE)
NR 2 TGT FLUCUTATED BETWEEN 0 AND 600 DEGREES IN FLIGHT. AIRCRAFT RETURNED TO AIRPORT. NO EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. FOUND BROKEN WIRE ON CONNECTOR PLUG BACKSHELL AT FIREWALL. ENTIRE HARNESS WAS REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. (K)
Part: CONTROL PANEL — FAILED (LT GENERATOR)
AFTER TAKEOFF, LEFT ENGINE GENERATOR WOULD NOT CARRY A LOAD. CREW TURNED BACK WHERE MAINTNANCE WAS AVAILABLE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LT GENERATOR CONTROL PANEL. AIRCRAFT WAS RETURNED TO SERVICE.
Part: COOLING FAN — BURNED OUT (RADIO RACK)
EN ROUTE TO YVR, PILOT REPORTED A FAINT ODOR OF SOMETHING BURNING. HE TURNED ON COCKPIT LIGHT AND SAW A LIGHT HAZE OF SMOKE IN THE COCKIT. AT APPROX THE SAME TIME, CAPT STATED THE NR 1 INVERTED FAILED, HE SHUT THE SWITCH OFF AND TRIED NR 2 INVERTER, IT WAS ALSO INOP. THE EMERG INVERTER SELECTED AND FUNCTIONED NORMALLY. CAPT DECLARED AN EMERGENCY AND ELECTED TO LAND AT MFR. ACFT LANDED WITHOUT FURTHER PROBLEMS. MX TROUBLESHOT ACFT A/C ELECTRICAL SYSTEM. MECHANIC FOUND RADIO RACK COOLING FAN SEIZED AND THE NR 1 STATIC INVERTER INOP. MX REPLACED NR 1 INVERTER, DEFERRED RADIO COOLING FAN. ACFT RUN FOR A SYSTEMS CHECK, ALL SYSTEMS FUNCTION CHECKED GOOD. ACFT RETURNED TO SERVICE. (X)
Part: SKIN — CRACKED (BS 407-581)
FUSELAGE STATION 407 TO STATION 581 INCHES WL 30.5 BL RIGHT OML, NUMEROUS CRACKS ALONG THIS SECTION OF SKIN. THE LONGEST IS 17 INCHES. THERE ARE TWO PREVIOUS SMALL REPAIRS IN WHICH THE CRACKS PROCEEDED PAST THE REPAIR. THE ENTIRE LENGTH OF SKIN WAS REMOVED STATION 407 TO 581 STRINGER 44 TO 45 WAS REPLACED IAW FOKKER SRM 53-01-02, FIGURE 22. (M)
Part: SKIN — CRACKED (BS 407-546)
FUSELAGE STATION 407 INCHES TO STATION 546 INCHES WL 30.5 STRINGER 44 TO 45 BL LEFT OML, NUMEROUS CRACKS ALONG THE CHINE LINE FASTENER HOLES WITH PREVIOUS REPAIRS. THE ENTIRE LENGTH OF SKIN FUSELAGE STATION 407-546 INCHES WAS REMOVED AND REPLACED IAW FOKKER SRM 53-01-02, FIGURE 22. (M)