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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 29, 1993 · Cessna 185 · N80124

Bulchitna Lake, AK

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
May 29, 1993
Injury Outcomes
No injuries (3 uninjured)
Location
Bulchitna Lake, AK
Aircraft
Cessna 185
Tail Number
N80124
Operator
White Carl H
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ANC93LA071

THE PILOT-IN-COMMAND STATED HE EXPERIENCED A MODERATELY HARD LANDING AND THE RIGHT MAIN WHEEL SEPARATED FROM THE LANDING GEAR AT THE UPPER BOLT HOLES WHICH NORMALLY SECURE THE AXLE TO THE LANDING GEAR LEG. METALLURGICAL EXAMINATION OF THE GEAR LEG SHOWED THAT THE FAILURE STEMMED FROM AREA OF FATIGUE CRACKING THAT INITIATED FROM CROSSION PITTING IN THE BOLT HOLES AND EXTERIOR SURFACES OF THE LOWER PORTION OF THE GEAR LEG.

NTSB Probable Cause

THE FAILURE OF THE LANDING GEAR LEG DUE TO A FATIGUE FRACTURE CAUSED BY CORROSION.

Full Narrative

On May 28, 1993, at 1715 Alaska daylight time, a wheel equipped Cessna 185 airplane, N80124, registered to and operated by the Pilot-in-Command, experienced a hard landing and subsequant landing gear failure at Sigley's private Airstrip located near Bulchitna Lake, Alaska. The business flight, operating under 14 CFR Part 91, last departed Kenai, Alaska, and the destination was the accident site. Visual meteorological conditions prevailed and no flight plan was filed. The airplane was substantially damaged and the Commercially Certificated Pilot-in-Command and the two passengers were not injured. According to the Pilot-in-Command, he experienced a moderate hard landing and the right main gear broke away at the wheel axle upper bolt holes. The airplane settled onto the remaining gear leg, veered right, and nosed over. Metallurigical examination of the fractured gear leg showed that the separation of the landing gear leg stemmed from areas of fatigue cracking that initiated from corrosion pitting in the bolt holes and exterior surfaces of the lower portion of the leg. Further, the metallurgist stated that the gear leg was composed of high strength steel, a material that is susceptible to fracture in the presence of relatively small defects.

Flight

Event TypeAccident
Event Time17:15 AKDT
Nearest AirportSigley'S Pvt Airstrip (0nm)
Runway36
Runway Length1100 ft
Runway Width30 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftCessna 185
Tail NumberN80124
Aircraft CategoryAir
DamageSubstantial
OperatorWhite Carl H
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsContinental · IO-520-F · Reciprocating · 300
Seats4

People & Injuries

Injury SummaryNo injuries (3 uninjured)
Fatal0
Serious0
Minor0
Uninjured3
Total3
Crew 1Age 51 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind360°
Visibility70 sm
CeilingNone
Temperature / Dew Point70 F / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data