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NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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March 22, 1998 · Hughes 369E · N5245P

Seattle, WA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
March 22, 1998
Injury Outcomes
2 injuries (2 minor injuries), 2 uninjured
Location
Seattle, WA
Aircraft
Hughes 369E
Tail Number
N5245P
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
SEA98LA050

The pilot stated that he was making a normal approach until about 30 feet in the air on short final, when he experienced a loss of power. After the resulting hard landing, the engine was still running and shut down by the pilot. Pressure and vacuum checks were performed on the engine fuel system and the engine was run successfully. Upon reassembly of the helicopter, the airframe mounted anti-ice fuel filter element was found to be restricted and the bypass switch was inoperative.

NTSB Probable Cause

Loss of engine power due to a restricted fuel system filter.

Full Narrative

On March 21, 1998, approximately 1745 Pacific standard time, a Hughes 369E, N5245P, registered to and operated by Trident Seafoods Corporation, was substantially damaged during a hard landing at Boeing Field, Seattle, WA. The pilot and one passenger received minor injuries. The two remaining passengers received no injuries. Visual meteorological conditions prevailed and no flight plan had been filed. The flight, which was for personal purposes, was operated under 14CFR91, and originated from Barnes Island, WA approximately 40 minutes prior to the accident. During an interview, the pilot stated that everything was normal until he was about 30 feet in the air on short final. At that point he experienced a loss of power but the engine did not quit. After the resulting hard landing, the engine was still running and shut down by the pilot. The helicopter was examined on March 23, 1998 after it had been moved to a hanger. Pressure and vacuum checks were performed on the engine fuel system. Fuel screens were also examined. No discrepancies were noted. The engine was later transported by the insurance company to ACRO Aerospace in Vancouver, BC, Canada. The Allison representative who observed the testing there reported that the engine started and ran normally during the tests except for a discrepancy about 40 minutes into the test when the engine failed to accelerate from idle. The scroll to PC filter tube B-nuts were found to be loose and the engine again performed normally after tightening. This line had previously been removed as part of the system pressure tests.

Flight

Event TypeAccident
Event Time17:45 PST
Nearest AirportBoeing Field (0nm)
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHughes 369E
Tail NumberN5245P
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · A250-C20B · Turboshaft · 420
Seats5

People & Injuries

Injury Summary2 injuries (2 minor injuries), 2 uninjured
Fatal0
Serious0
Minor2
Uninjured2
Total4
Crew 1Age 51 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind360° @ 5 kt
Visibility10 sm
CeilingBroken clouds 5000 ft
Temperature / Dew Point55 / 50
Altimeter29.00 inHg
Observation Time01:45
Weather SourceWFAC

Appendix: Source Data