LAX92LA282

NTSB accident investigation · Stinson 108-3 · Montague, CA · July 5, 1992

Accident · No injuriesLimited investigationFinal report
Date
July 5, 1992, 11:00 local (18:00 UTC)
Place
Montague, CA
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N592CStinson 108-3
Weather
Visual (VMC) · Day
Status
Completed · report September 28, 1993
Report
Approved by Office Director
FAA report
19920705023569A
Case key
27678

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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Probable cause

The disintegration of the left wheel during the landing roll out and the resultant inability of the pilot to maintain directional control of the aircraft. A factor in the accident was the soft nature of the terrain encountered by the aircraft after leaving the runway surface.

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/malfunctionLanding - roll
Landing gear,wheel - crackedCause
Landing gear,wheel - disintegratedCause
Directional control - not possiblePilot in commandCause
Ground loop/swerve - inadvertentCause
Nose overLanding - roll
Terrain condition - softFactor
On ground/water encounter with terrain/waterLanding - roll

Analysis

According to the pilot, the left main wheel disintegrated just after touchdown and he could not prevent the aircraft from veering off the runway. As the aircraft entered the grassy dirt area next to the runway, the left axle dug into the soil and the aircraft nosed over. The pilot reported that the wheel assembly was an original equipment item on the aircraft, which was manufactured in 1948 and has accrued a total time in service of 1,407 hours. The pilot said he had removed and inspected the wheel the day before the accident and that it appeared normal. Post accident inspection of the wheel pieces by the pilot revealed evidence of a small fairly recent crack in the wheel casting near the axle. The pilot further said the crack was in the inside part of the wheel and under the tire where it couldn't have been observed unless the wheel had been completely disassembled.

Aircraft

Registration
N592C
Reported as
Stinson 108-3
Category
Airplane
Serial number
108-3592
Airframe hours
1,407
Engine
Franklin 6A4-165-B3, 165 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Talmadge Westmoreland
Registered owner
Talmadge Westmoreland
Airworthiness certificate
Standard, Normal
Last inspection
Annual · July 21, 1991 · 21 hours before
Departed
CCR · Concord, CA
Destination
YVR · Vancover
Flight plan
VFR
Airport
105 · Rohrer Field, runway 32, 3,600 × 50 ft, asphalt

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
70
Certificate
Commercial
Airplane ratings
Multi-engine land, Single-engine land
Medical
Class 3, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
8,000 total · 750 in this make and model · 7,800 as pilot in command · 10 in the last 90 days · 10 in the last 30 days · 3 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
30 statute miles
Lowest ceiling
4,000 ft broken
Temperature
63 °F, dew point 48 °F
Altimeter
30.00 inHg

FAA reports on this event · 1

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