SEA85FA034

NTSB accident investigation · de Havilland DHC-3 Turbo · West Seattle, WA · December 19, 1984

Accident · Serious injuriesField investigationFinal report
Date
December 19, 1984, 11:08 local (19:08 UTC)
Place
West Seattle, WA
Injuries
1 serious, 2 minor
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N4247Ade Havilland DHC-3 Turbo
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19841219014769A
Case key
40024

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Analysis

Acft was performing test flt maneuvers when problems with the modified fuel system occurred. Ice blocking a fuel vent line caused a partial collapse of the main (engine feed) fuel cell which produced an errouneous fuel quantity reading. In addition, the main tank overflow shutoff valve was leaking, so tank overflow occurred. The fuel overflow caution light illuminated and auxiliary tank fuel pump feed to main automatically shut down. Due to miscalibration, this system overrode plt attempts to restart aux fuel pumps. Plt remained in test area troubleshooting rather than immediate return to base, finally noted main tank gage continuing to read 'full.' En route to Boeing field, fuel starvation occurred. Pltopted to attempt forced lndg in small athletic field in residential area rather than ditch in puget sound. The acft touched down in intended lndg area, then bounced across an adjacent street. The arresting action of telephone wires on the vertical fin brought the acft to rest in a residential backyard.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Airframe/component/system failure/malfunctionManeuvering
Fuel system,vent - blocked(total)Cause
Fuel system,tank - distortedFactor
Engine instruments,fuel quantity gage - false indicationFactor
Fuel system,fuel shutoff - leakFactor
Airframe/component/system failure/malfunctionManeuvering
Fuel system,pump - switched off
Remedial action - not possible
Loss of engine power(total) - nonmechanicalCruise
Precautionary landing - delayedPilot in commandFactor
Fuel supply - misjudgedPilot in commandFactor
Fluid,fuel - starvationCause
Forced landingDescent - emergency
In flight collision with terrain/waterLanding
Terrain condition - none suitableFactor

Aircraft

Registration
N4247A
Reported as
de Havilland DHC-3 Turbo (DHC-3 TURB)
Category
Airplane
Serial number
421
Airframe hours
7,445
Engine
P&W PT-6A-135, 787 horsepower, turbo prop
Damage
Substantial damage
Flight
Part 91
Registered owner
Cox Aircraft Corporation
Airworthiness certificate
Special, Experimental (Special)
Last inspection
100 hour · November 21, 1984 · 11 hours before
Departed
BFI · Seattle, WA
Airport
Boeing Field

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
61
Certificates
Airline transport, Flight instructor, Commercial
Airplane ratings
Multi-engine sea, Single-engine sea, Multi-engine land, Single-engine land
Instrument ratings
Helicopter, Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
8,500 total · 15 in this make and model · 7,500 as pilot in command · 15 in the last 90 days · 15 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
30° at 3 knots
Visibility
60 statute miles
Lowest ceiling
10,000 ft broken
Temperature
25 °F, dew point 18 °F
Altimeter
30.00 inHg
Observed at
BFI, 5 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.