N123RA

DASSAULT/SUD FAN JET FALCON · 1966 · Fixed-wing multi-engine · 2 engines · 12 seats · Valid Registration

Registered owner: ROYAL AIR FREIGHT INC, MI (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
Royal Air Freight, Inc. (BUHA)Certificate holder—Matched by certificate designator

Accident & incident history

Cessna 310R Fatal injury Part 91 — operator not named in the NTSB record
Source: NTSB case NYC01FA064

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.

5 reports on file, 1996-04-30 – 2000-02-03.

OTHER · 2000-02-03 Matched by certificate designator
ATA 2140

Part: PUMP — FAILED (HEATER)

PILOT REPORTED THE HEATER WAS INOPERATIVE. TROUBLESHOOTING FOUND THE HEATER FUEL PUMP HAD FAILED, AND THAT IT WAS PUMPING FUEL OUT AROUND THE PUMP SHAFT. (X)

Source: SDR 2000ZZZX640
OTHER · 1997-08-13 Matched by certificate designator
ATA 2562

Part: ELT — WEAK (OUTPUT)

DURING ROUTINE ELT CHECK, FOUND THE ELT HAD A WEAK SIGNAL. ELT WAS REPAIRED, RECERTIFIED, AND NEW BATTERY BY NARCO ON 12-21-95. BATTERY DUE OFF DATE IS JANUARY 17, 1998. A REPLACEMENT BATTERY WAS TRIED, BUT DID NOT FIX THE PROBLEM.

Source: SDR 97ZZZX4032
FLUID LOSS · 1997-05-29 Matched by certificate designator
ATA 2140

Part: COIL — SHORTED (HEATER IGNITOR)

THE FIRST COIL EXPLODED BREAKING OFF THE TOP OF THE IGNITOR AND BREAKING WIRES IN THE IGNITION UNIT SPEWING 'OIL' FROM INSIDE THE COIL THROUGHOUT THE HEATER BAY. THE REPLACEMENT COIL SHORTED OUT, LEAKED OIL, AND THE COVER CAME LOOSE.

Source: SDR 97ZZZX2883
OTHER · 1997-04-16 Matched by certificate designator
ATA 2140

Part: COIL — EXPLODED (HEATER)

HEATER FOUND INOPERABLE. FOUND THE IGNITION COIL HAD EXPLODED. THE END CAP HAD COME OFF WITH ENOUGH FORCE THAT IT BENT THE IGNITER OVER; THE OPPOSITE REACTION CAUSED THE COIL CAN TO GO AFT AND BREAK WIRES OFF MISCELLANEOUS PARTS IN THE COIL COVER. THE MOST SIGNIFICANT POINT WAS THAT FUEL WAS STILL BEING PUMPED INTO THE HEATER, BUT NOT BEING IGNITED.

Source: SDR 97ZZZX1972
OTHER · 1996-04-30 Matched by certificate designator
ATA 6114

Part: STUD — OVER TORQUE (PROPELLER)

THESE MCCAULEY PROPELLERS COME PLACARDED TO LUBE TORQUE TO 40-45 FEET/POUNDS. THE CESSNA MM SPECIFIES 80-85 FEET/POUNDS DRY TORQUE. THE CESSNA TECH SAID BOTH ARE ACCEPTABLE, BUT DO NOT MIX THE TWO. TECH SAID 80 POUNDS LUBE TORQUE WILL PULL THE STUD OUT OF THE HUB. THIS COULD BE CONFUSING, AND HAS CAUSED EXPENSIVE PROBLEMS.

Source: SDR 96ZZZX2565