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Boeing 747-451 — registry & accident history

Compiled from FAA & NTSB records · as of Jul 18, 2026

There are 18 Boeing 747-451 airframes on record (built 1988–2002), 1 currently registered. 5 have one or more NTSB accident records (5 records total). Data as of Jul 18, 2026.

18
Airframes
1
Registered
1988–2002
Years
5
NTSB records

Recent Boeing 747-451 accidents

  1. N668USJun 7, 2017No injuries

    The PW4056 engine lost power due to the fatigue fracture of a 5th stage compressor blade. The cause of the fatigue fracture could not be determined.

  2. N662USOct 2, 2015No injuries

    The PW4056 engine experienced an in-flight loss of power because of damage to the low-pressure turbine (LPT) because of the inadequate overhaul inspection and repair instructions that existed at the time of the LPT module's last overhaul. A vane hook in the LPT case wore to the point to allow a 3rd stage turbine vane cluster to disengage and eventually fall into the path of the 3rd stage turbine blades causing extensive downstream damage to the LPT module.

  3. N669USSep 21, 2014No injuries

    Turbine Overhaul Service's aggressive grit blasting and incomplete masking of the blade root neck that allowed the no grit blast area being exposed during the overhaul of the blade resulting in blasting media being embedded in the blade root from which a fatigue crack developed. The fatigue crack propagated until separation of the blade occurred that resulted in a complete loss of engine power. The fire was caused by the B-nut on the hydraulic line from the fuel pump and pulsation damper loosening from engine vibration after the compressor blade separated spraying high pressure fluid into the engine compartment that ignited on the hot engine cases.

  4. N661USOct 23, 2011No injuries

    The penetration of turbine blade fragments through the rear turbine case, which punctured the No. 4 bearing oil pressure supply tube, allowing misted oil to contact the hot engine case and ignite the undercowl fire. Contributing to the incident was the installation of approved (but not preferred) stage 3 low pressure turbine outer transition duct segments with the riveted rear seal configuration and the failure of the engine design to comply with the engine debris containment requirements of 14 Code of Federal Regulations 33.13 and 33.75.

  5. N676NWFeb 20, 2009Serious

Boeing 747-451 aircraft