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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

March 30, 1996 · Stinson 108-3 · N6443M

Soldotna, AK

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
March 30, 1996
Injury Outcomes
No injuries (2 uninjured)
Location
Soldotna, AK
Aircraft
Stinson 108-3
Tail Number
N6443M
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ANC96LA048

The pilot landed a tundra tire and tail-wheel equipped airplane in a westerly direction and was slowing to begin taxiing to a parking area. At about that time, the airplane encountered a gust of wind from the right and went off the right side of the runway. The airplane received damage to the left wing tip, fuselage, and the left main gear attach point. The pilot estimated the wind was from the north at 16 gusting 22 knots.

NTSB Probable Cause

The pilot's inadequate compensation for wind conditions. The gusty/crosswind condition was a related factor.

Full Narrative

On March 30, 1996, about 1530 Alaska standard time, a tundra tire equipped Stinson 108-3, N6443M, ground looped while taxiing from landing at the Soldotna airport, Soldotna, Alaska. The airplane was being operated as a visual flight rules (VFR) cross-country personal flight when the accident occurred. The airplane, registered to and operated by the pilot, sustained substantial damage. The certificated private pilot, and the sole passenger, were not injured. Visual meteorological conditions prevailed. The flight departed Lake Clark, Alaska, about 1315. The pilot reported that he landed on runway 25 and was slowing to begin taxiing to a parking spot. A gust of wind from the right produced a ground loop and the airplane slid off the right side of the runway. The pilot initially reported minor damage to the left wing. Further inspection on April 17, 1996, confirmed structural damage to the fuselage at the left main gear attach point. At 1546, a surface observation at Kenai, Alaska, 8 miles northwest of the accident site was reporting, in part: Sky conditions and ceiling, clear; visibility, 70 miles; temperature, 40 degrees F; dew point, 34 degrees F; wind, 020 degrees at 13 knots; altimeter, 30.27 inHg. After landing, the pilot estimated the winds from the north at 16 knots with gusts to 22 knots.

Flight

Event TypeAccident
Event Time10:30 AKST
Nearest AirportSOLDOTNA (0nm)
Runway25
Runway Length4973 ft
Runway Width130 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftStinson 108-3
Tail NumberN6443M
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsFranklin · 6A4-165-B3 · Reciprocating · 165
Seats4

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 56 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind20° @ 13 kt
Visibility70 sm
CeilingNone
Temperature / Dew Point39 C / 34 C
Altimeter30.00 inHg
Observation Time19:46
Weather SourceWFAC

Appendix: Source Data