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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 31, 1993 · Cessna 310 · N5847M

Kodiak, AK

Overview

Report Status
Final with probable cause
Event Type
Incident
Date
May 31, 1993
Injury Outcomes
No injuries (2 uninjured)
Location
Kodiak, AK
Aircraft
Cessna 310
Tail Number
N5847M
Operator
Main Robert
Injuries
None
Aircraft Damage
Minor
NTSB Number
ANC93IA076

THE AIRPLANE JUST COMPLETED AN ANNUAL INSPECTION AND WAS ON A MAINTENANCE TEST FLIGHT. UPON GEAR RETRACTION THE NOSE GEAR MADE A LOUD NOISE AND THEN WOULD NOT LOCK IN THE DOWN POSITION OF THE SUBSEQUENT EXTENSION. EXAMINATION OF THE SYSTEM SHOWED THE LANDING MECHANISM WAS IN RIG AND THE NOSE GEAR CENTERING MECHANISM WAS OPERATIONAL. METALLURGICAL EXAMINATION SHOWED THAT THE FRACTURES REVEALED FEATURES TYPICAL OF OVERSTRESS SEPARATIONS.

NTSB Probable Cause

THE FAILURE OF THE NOSE GEAR IDLER BELL CRANK DUE TO OVERSTRESS BY AN UNDETERMINED SOURCE.

Full Narrative

On May 31, 1993, at 1315 Alaska daylight time, a retractable wheel equipped Cessna 310 airplane, N5847M, registered to and operated by the Pilot-in-Command, experienced a collapse of the nose gear upon landing at the Kodiak Airport, Kodiak, Alaska. The personal flight, operating under 14 CFR Part 91, departed Kodiak for a local maintenance test flight. Visual meteorological conditions prevailed and no flight plan was filed. The Airline Transport Pilot-in-Command and the mechanic/passenger were not injured and the airplane received only minor damage. According to the Pilot-in-Command, the nose gear made a loud noise upon retraction and then would not lock down during the subsequent extension. Examination of the system showed a failure of the nose gear idler bell crank. Metallurgical examination of the idler bell crank by use of the bench binocular microscope showed that the fractures revealed features typical of over stress separations. According to the Pilot-in-Command/owner and the mechanic, after the mishap, they simply replaced the idler bell crank and performed a gear extension and retraction check while the airplane was on jacks. The gear performed perfectly and they were not able to duplicate the problem. The nose wheel centering mechanism was examined and no anomalies were noted. According to the mechanic, the landing gear was rigged properly.

Flight

Event TypeIncident
Event Time13:15 AKDT
Nearest AirportKODIAK (0nm)
Runway28
Runway Length5400 ft
Runway Width150 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftCessna 310
Tail NumberN5847M
Aircraft CategoryAir
DamageMinor
OperatorMain Robert
Operating RulePart 91
Engines2
Engine TypeReciprocating
Engine DetailsContinental · IO-520-C · Reciprocating · 300
Seats6

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 39 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind80° @ 4 kt
Visibility20 sm
CeilingNone
Temperature / Dew Point55 / 50
Altimeter29.00 inHg
Weather SourcePILO

Appendix: Source Data