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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

September 8, 1996 · Stinson 108 · N97337

Quincy, CA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
September 8, 1996
Injury Outcomes
1 injury (1 minor injury)
Location
Quincy, CA
Aircraft
Stinson 108
Tail Number
N97337
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
LAX96LA329

The pilot leaned the engine before takeoff, but as the aircraft reached about 50 feet agl, the engine lost power. He switched tanks, enriched the mixture, pumped the throttle, and attempted to restart the engine. The engine started, but it ran for only a few seconds before quitting again. When his second attempted restart was unsuccessful, he executed a forced landing. During the forced landing, the airplane hit a log and was damaged. The pilot said he could have induced the problem by over leaning the engine. He also said he could have restricted the fuel flow when he inadvertently moved the fuel selector beyond the tank detent. The aircraft was fueled with a mixture of aviation fuel and auto gas, but it did not have an STC for auto gas. The aircraft had not had an annual inspection within the previous 12 months, and the pilot's medical certificate had expired.

NTSB Probable Cause

the pilot's over leaning of the fuel mixture, which resulted in the initial loss of engine power; and continued fuel starvation, resulting from the pilot's inadvertent mispositioning of the fuel selector valve during an attempted restart of the engine.

Full Narrative

On September 8, 1996, at 0909 hours Pacific daylight time, a Stinson 108, N97337, experienced a power loss and forced landing after takeoff from Gansner Field, Quincy, California. The aircraft sustained substantial damage and the private pilot received minor injuries. The aircraft was operated as a personal flight by the pilot/owner when the accident occurred. The flight originated in McCall, Idaho, the day before the accident with an overnight stop in Denio, Nevada. The flight resumed at 0600 on the morning of the accident. The pilot landed at Gansner Field and was on departure when the accident occurred. Visual meteorological conditions prevailed and no flight plan had been filed. The pilot reported he leaned the engine prior to taking off on runway 24. The engine performed normally during the run-up and takeoff roll, but quit as the aircraft reached about 50 feet agl. He switched tanks, moved the mixture control to the full rich position, and pumped the throttle twice before attempting to restart the engine. On his first attempt, the engine started but ran only for a few seconds before quitting again. A second attempted restart was unsuccessful. He executed a forced landing in an open field on the opposite side of state highway 70. During the landing roll the aircraft struck a log with the right main gear. Damage to the aircraft included a collapsed right main gear, fuselage buckling aft of the main wings, and bent propeller blades. The pilot told FAA inspectors that he could have induced the problem initially by over leaning the engine. He also said that he could have restricted the fuel flow when he inadvertently moved the fuel selector beyond the tank detent position. During their postaccident examination, inspectors found no discrepancies in the fuel system, with fuel available in both tanks as well as in the carburetor. An inspection of the aircraft logbooks revealed that the aircraft had not undergone an annual inspection within the last 12 calendar months. In addition, the pilot reported that he was using a mixture of aviation fuel and auto gas. The aircraft did not have an STC authorizing the use of auto gas. The pilot was flying with an expired medical certificate.

Flight

Event TypeAccident
Event Time09:09 PDT
Nearest AirportGansner Field (0nm ENE)
Runway24
Runway Length4100 ft
Runway Width60 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftStinson 108
Tail NumberN97337
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsFranklin · 6A4-165-B3 · Reciprocating · 165
Seats4

People & Injuries

Injury Summary1 injury (1 minor injury)
Fatal0
Serious0
Minor1
Uninjured0
Total1
Crew 1Age 51 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind340° @ 5 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point39 C
Altimeter29.00 inHg
Observation Time15:55
Weather SourceWFAC

Appendix: Source Data