N81MR
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, 1995-02-07 – 2012-04-17.
Part: FUEL CONTROL — ERRATIC (LT ENGINE) · airframe 14,750 hrs · 12,902 cycles
SUPPLEMENTAL RECORD - THE LEFT FUEL CONTROL UNIT WAS REPLACED WITH A OVERHAULED UNIT. OPS CHECK NORMAL AND FLIGHT CHECK NORMAL.
Part: PUMP — INOPERATIVE (RT ENGINE) · airframe 12,239 hrs · 10,945 cycles
DEPARTING BFI EXPERIENCE A UNCONTROLLED SHUT DOWN ON THE RIGHT ENGINE. THIS HAPPENED ON CLIMBOUT AT APPROXIMATELY 2000 FEET. THE FLIGHT CREW WITH MEDICS (NO PATIENT) RETURNED TO BFI WITHOUT FURTHER INCIDENT. GALVIN FLYING SERVICE WAS CONTACTED TO TROUBLESHOOT THE PROBLEM. DISCOVERED THE ENGINE DRIVEN FUEL PUMP HAD NO OUTPUT.
Part: SHUTOFF VALVE — LEAKING (BLEED AIR)
MAINTENANCE PERSONNEL DETECTED BLEED AIR LEAK IN TAILCONE DURING GROUND OPERATION. TRACED SOURCE TO CENTER MATING SURFACES OF WINDSHIELD ANTI-ICE SHUTOFF VALVE. REPLACED VALVE WITH OVERHAULED UNIT. PROBABLE CAUSE: BLOWN GASKET IN VALVE.
Part: LINE — CHAFED (BRAKE PRESS)
LINES WERE CHAFING ON CLAMP ATTACHED TO GEAR DOOR ACTUATOR. LINE NEEDS SMALL BEND AT THIS AREA FOR PROPER CLEARANCE. (LINES WERE .50 INCH TO .75 INCH CHAFED THROUGH WALL THICKNESS.) LINES LOCATED IN AT WHEELWELL.