UA328
2021-FEB-20 · Broomfield, Colorado

United Airlines — Flight UA328

United Airlines Flight 328 suffered a contained right engine failure shortly after departing Denver, resulting in a massive debris field over residential Broomfield, Colorado. A fan blade in the Pratt & Whitney PW4077 engine fractured due to metal fatigue, leading to the separation of the engine's inlet and cowling and sparking an in-flight fire. Despite the severe damage and falling debris hitting homes and vehicles, the flight crew successfully returned the aircraft to Denver International Airport with no injuries to the 239 people on board or those on the ground.

Aircraft
Boeing 777-222
Registration
N772UA
Phase
Initial climb
Cause
Mechanical Failure
Souls on Board
239
Fatalities
0
Origin → Dest
Denver International Airport, CO → Daniel K. Inouye International Airport, Honolulu, HI
Report
Final Report

Investigation Summary

The investigation centered on the failure of fan blade #11, which experienced a full-length separation due to a fatigue crack. This crack had been present during a 2016 inspection but was misidentified as a low-level indication and allowed to remain in service. The failure was the fourth such event involving PW4000-series engines on Boeing 777s. The incident was particularly severe because the engine inlet, made of carbon fiber reinforced plastic (CFRP), could not dissipate the energy of the fan blade out (FBO) event as effectively as traditional aluminum structures, leading to the total separation of the inlet and fan cowls. Furthermore, the high dynamic loads caused the 'K' flange bolts to fail, allowing hot gases to escape the engine core and ignite a fire that was fed by leaking fuel and hydraulic fluid.

Final Conclusions

The NTSB determined the probable cause was the fatigue failure of the right engine fan blade, exacerbated by inadequate inspections and insufficient inspection intervals by the manufacturer. Contributing factors included the engine inlet design, which failed to limit damage during a fan blade out event, and the failure of the 'K' flange, which allowed an unextinguishable fire to propagate into the thrust reversers. Additionally, a contaminated hydraulic shutoff valve failed to close, providing further fuel to the fire.

Photographic Evidence (1)

© Wikimedia Commons

Video Analysis

UNITED 328 Engine Failure! WHAT CHECKLISTS did the Pilots use? — A detailed breakdown of the United 328 engine failure, the mechanics of the fan blade out event, and the emergency procedures followed by the crew.

If playback is blocked, the owner has disabled embedding — use the link above.

Airframe & Maintenance

Airframe Hours
96,814
Engines
Pratt & Whitney PW4077

Systems & Failure Modes

i

Pratt & Whitney PW4077

The turbofan engine that suffered a fan blade out event due to metal fatigue.

i

Engine Inlet (CFRP)

The carbon fiber reinforced plastic structure that failed to dissipate energy and separated from the aircraft.

i

K Flange

A structural connection between the main gearbox and the engine core that failed, allowing hot gases to ignite a fire.

i

Hydraulic Shutoff Valve

A safety valve that failed to close due to electrical contact contamination, allowing hydraulic fluid to feed the fire.

Interesting Facts

  • 01The aircraft was the fifth Boeing 777 ever produced, manufactured in 1995.
  • 02Debris damaged a residential roof and a parked pickup truck, but caused no injuries on the ground.
  • 03The engine fire was fed by high-pressure fuel after the 'K' flange failure caused a servo fuel heater to fracture.
  • 04The hydraulic pump supply shutoff valve failed to close due to silicone lubricant contamination.
  • 05The fan blade fatigue crack had been visible in Thermal Acoustic Imaging (TAI) records from 2016 but was not caught.

Safety Actions & Advisories

Emergency Airworthiness Directive

The FAA issued an emergency AD requiring immediate thermal acoustic imaging (TAI) inspections of all PW4000-series fan blades before further flight.

Inlet Structural Modifications

Boeing developed modifications to add metallic structure and increase the strength and ductility of the 777 engine inlets to prevent separation during FBO events.

K Flange Redesign

Pratt & Whitney began evaluating actions to improve the strength of the 'K' flange to prevent core gas leakage during high-vibration events.

Location

Broomfield, Colorado · 39.9290, -105.0550

Case File History

  1. CorrectionUpdated event timeline.

Related Cases

Case ID · ua328-2021Last updated · Filed

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