NTSB CAROL · Event
Event ANC93IA188
Aircraft involved
Probable cause & findings
FOREIGN OBJECT DAMAGE TO THE COMPRESSOR FORWARD FAN ASSEMBLY AS A RESULT OF THE INGESTION OF A BIRD.
Factual narrative
On September 25, 1993, at 0835, Alaska daylight time, a Boeing 747-200, N629US, experienced a partial power loss after it had ingested 28 ounce Gadwell duck into its number one engine during takeoff rotation at Anchorage International Airport. The pilot in command shut down the affected engine, dumped fuel and landed without further incident at 0911. The airplane was operated by Northwest Airlines on a regularly scheduled cargo flight to Tokyo as NW Flight 905, under 14 CFR Part 121, on an international IFR flight plan. Visual meteorological conditions existed. A flight crew of 3 were the only persons on board, and they were uninjured. Damage was limited to the number one engine and the event was classified as incident damage. The pilot told NTSB and FAA investigators that while he noticed waterfowl in the area on taxi out, he did not see birds at the time he experienced the engine failure. The airplane reportedly weighed 752,000 pounds at takeoff and dumped 84,300 pounds of fuel while orbiting at the direction of ATC. The landing gross weight was approximately 628,000 pounds. Investigators found blood and material resembling feather parts in the number one engine inlet. Damage was seen to the rotor blades of the fan, inside and outside of the inlet cowl. The fiberglass spinner cone was destroyed. No wing or fuselage damage was seen. The engine damage was examined by Northwest Airlines with the assistance of Pratt & Whitney. The NTSB was advised that failure was due to downstream ingestion of fiberglass spinner parts and pieces of first stage fan blades. The NTSB investigator contacted Pratt & Whitney at East Hartford Connecticut. The powerplant investigator at P&W told the NTSB that there "were a limited amount of 10 ply fiberglass spinners out there." He said that "P&W was aware of about one inflight failure per year with these thin spinners from bird strikes." He also said that he and the FAA had discussed it and didn't feel that an AD (Airworthiness Directive) was necessary, but that they were watching the numbers (as an in-house study). He also said that these were being replaced with a newer model spinner that had 20 plys, and there were no known instances of inflight failure known. The findings of the investigation were forwarded to the NTSB's Engineering Division ((AS-40). On October 4, 1993, the NTSB NW Field Office was advised that the Engineering Division was reviewing the information for possible safety recommendation activity. A 28 OUNCE DUCK WAS INGESTED INTO A JT9 TURBOFAN ENGINE OF A B747 ON TAKEOFF, IMPACTING AND BREAKING THE 10 PLY FIBERGLASS FAN SPINNER. DOWNSTREAM ENGINE DESTRUCTION FOLLOWED. ENGINE MANUFACTURE AND FAA WAS AWARE OF A NUMBER OF PREVIOUS BIRD-STRIKE FAILURES WITH THIS SPINNER. NEW AND STRONGER 20 PLY SPINNERS ARE BEING PHASED IN; HOWEVER, THIN SPINNERS ARE STILL IN USE ON JT9 ENGINES IN COMMERCIAL SERVICE. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1993_ANC93IA188.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (engine failure). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- arXiv 2022 · arXiv preprint
Multi-level Adaptation for Automatic Landing with Engine Failure under Turbulent Weather
This paper addresses efficient feasibility evaluation of possible emergency landing sites, online navigation, and path following for automatic landing under engine-out failure subject to turbulent wea…
- NASA NTRS 2019 · Conference Paper
Simulation of Liquid Rocket Engine Failure Propagation Using Self-Evolving Scenarios
Traditional probabilistic risk assessment approaches often require failure scenarios to be explicitly defined through event sequences that are then quantified as part of the integrated analysis.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techiques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techniques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Technical Memorandum (TM)
A simulator investigation of engine failure compensation for powered-lift STOL aircraft
A piloted simulator investigation of various engine failure compensation concepts for powered-lift STOL aircraft was carried out at the Ames Research Center.
- Semantic Scholar 2019 · Article (AIAA Scitech 2019 Forum)
Impact of Engine Failure Constraints on the Initial Sizing of Hybrid-Electric GA Aircraft
Potential advantages of hybrid-electric aircraft are fuel savings, lower emissions, and reduced noise. Since these aircraft generally apply multiple power sources, they can also be designed to sustain…
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