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Aviation safety reports, made easier to study

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NTSB Report

July 19, 1997 · De Havilland DHC-2 · N68084

Alagnak River, AK

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
July 19, 1997
Injury Outcomes
No injuries (2 uninjured)
Location
Alagnak River, AK
Aircraft
De Havilland DHC-2
Tail Number
N68084
Operator
Lakeside Industries
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ANC97LA106

The pilot was making a no-wind takeoff downstream from a 4,000-foot slow flowing river. The takeoff water run for the conditions was calculated at 1,300 feet. The pilot and passenger both reported a partial loss of engine RPM just prior to lift-off from the water. According to the pilot, there was insufficient stopping distance before reaching a river bank. The pilot rotated the airplane off the water below flying speed, cleared the bank, and settled back into the tundra. The pilot stated that a similar loss of engine RPM had happened before, but was considered transient.

NTSB Probable Cause

A partial loss of engine power for an undetermined reason, and the pilot's intentional operation of the airplane with known deficiencies.

Full Narrative

On July 19, 1997, at 0845 Alaska daylight time, an amphibious float equipped DeHavilland DHC-2 airplane, N68084, sustained substantial damage when it impacted tundra during a takeoff from the Alagnak River, twenty-eight miles northwest of King Salmon, Alaska. The airline transport certificated pilot and single passenger were not injured. The airplane was operated by Lakeside Industries of Bellevue, Washington, to transport company employees to a fishing lodge. The flight was being conducted under 14 CFR Part 91 in visual meteorological conditions from the Alagnak River to King Salmon. The pilot and passenger stated to the NTSB investigator that they were attempting to takeoff downstream on the slow flowing Alagnak River. Just prior to lifting off the water, they sensed a loss in engine RPM and no loss in manifold pressure. The pilot said he did not have room to abort the takeoff on the water, and rotated the airplane to clear the riverbank. The airplane impacted the tundra, remaining upright. Both wings and floats sustained substantial damage. The pilot stated that there had been two previous RPM drops on takeoff from the King Salmon runway, which self corrected, and were not considered significant. He stated he did not perform magneto checks on the day of the accident. The pilot and passenger estimated 500 pounds of luggage on board. The pilot weighed 173 pounds, according to his second class medical dated May 5, 1997. The passenger weight was estimated at 180 pounds. The pilot stated there was sixty gallons of fuel on board (360 pounds). The empty weight of a representative amphibian DHC-2 on Wipline 2000 floats is 3,890 pounds. The seaplane takeoff distance given in the DHC-2 and U-6A(military DHC-2) operators manuals for the conditions is 1,300 feet. The pilot and passenger estimated the takeoff area to be 4,000 feet long, and downstream. Both occupants stated that the airplane made an uneventful takeoff from the same location one hour earlier.

Flight

Event TypeAccident
Event Time08:45 AKDT
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftDe Havilland DHC-2
Tail NumberN68084
Aircraft CategoryAir
DamageSubstantial
OperatorLakeside Industries
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsP&W · R-985 · Reciprocating · 450
Seats2

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 62 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind180° @ 10 kt
Visibility7 sm
CeilingBroken clouds 600 ft
Temperature / Dew Point54 / 50
Altimeter29.00 inHg
Observation Time11:51
Weather SourceWFAC

Appendix: Source Data