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Aviation safety reports, made easier to study

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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NTSB Report

May 23, 1998 · Piper PA-18 · N8578D

Glennallen, AK

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
May 23, 1998
Injury Outcomes
2 injuries (2 minor injuries)
Location
Glennallen, AK
Aircraft
Piper PA-18
Tail Number
N8578D
Operator
Tundra
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
ANC98LA054

The certificated commercial pilot was conducting an aerial moose survey for the State of Alaska. The passenger was a wildlife biologist employed by the State of Alaska. The pilot said that while in cruise flight, about 500 feet above the ground, all engine power was lost. Attempts to restore engine power were unsuccessful, and he turned the airplane to avoid rising terrain. During the subsequent forced landing, the airplane collided with trees. The airplane received substantial damage to the wings and fuselage. A Federal Aviation Administration (FAA) airworthiness inspector inspected the airplane wreckage and obtained a fluid sample from the fuel system gascolator. The sample exhibited two obvious layers of separated liquid. The top layer consisted of a bluish liquid, consistent with the color of 100LL aviation fuel. The lower layer consisted of a clear liquid which appeared to be water. The NTSB investigator-in-charge tested the clear fluid with water finding paste. The sample tested positive for water.

NTSB Probable Cause

The pilot's inadequate preflight of the airplane's fuel system, and presence of water in the fuel system.

Full Narrative

On May 23, 1998, about 0900 Alaska daylight time, a tundra tire equipped Piper PA-18 airplane, N8578D, sustained substantial damage during a forced landing, about 40 miles west of Glennallen, Alaska. The airplane was being operated as a civil government flight under Title 14 CFR Part 135 when the accident occurred. The certificated commercial pilot, and the sole passenger aboard, received minor injuries. Visual meteorological conditions prevailed, and company flight following procedures were in effect. The flight originated from a private airfield about 35 miles west of Glennallen about 0800. During a telephone conversation with the National Transportation Safety Board investigator-in-charge, on May 27, 1998, at 1000, the pilot reported that he was conducting an aerial moose survey for the State of Alaska. The passenger was a wildlife biologist employed by the State of Alaska. The pilot said that while in cruise flight, about 500 feet above the ground, all engine power was lost. Attempts to restore engine power were unsuccessful, and he turned the airplane to avoid rising terrain. During the subsequent forced landing, the airplane collided with trees. The airplane received substantial damage to the wings, and fuselage. The pilot related he was not sure why the engine lost power, but he suspected the fuel may have been contaminated with water. He said it had been raining hard the day before the accident flight, and that during the preflight inspection preceding the accident flight, he noticed some water in one of fuel samples taken from a wing sump. A Federal Aviation Administration (FAA) airworthiness inspector, inspected the airplane wreckage, and obtained a fluid sample from the fuel system gascolator. The sample exhibited two obvious layers of separated liquid. The top layer consisted of a bluish liquid, consistent with the color of 100LL aviation fuel. The lower layer consisted of a clear liquid which appeared to be water. The NTSB investigator-in-charge tested the clear fluid with water finding paste. The sample tested positive for water.

Flight

Event TypeAccident
Event Time09:00 AKDT
Nearest Airport0nm
Runway0
Flight Plan FiledCvfr
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-18
Tail NumberN8578D
Aircraft CategoryAir
DamageSubstantial
OperatorTundra
Operating RulePart 135
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-320-A2B · Reciprocating · 150
Seats2

People & Injuries

Injury Summary2 injuries (2 minor injuries)
Fatal0
Serious0
Minor2
Uninjured0
Total2
Crew 1Age 43 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind120° @ 5 kt
Visibility50 sm
CeilingNone
Temperature / Dew Point50 / 30 C
Altimeter29.00 inHg
Weather SourcePILO

Appendix: Source Data