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NTSB Report

June 16, 1998 · Cessna A185F · N185DG

Talkeetna, AK

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
June 16, 1998
Injury Outcomes
No injuries (3 uninjured)
Location
Talkeetna, AK
Aircraft
Cessna A185F
Tail Number
N185DG
Operator
Douglas Geeting Aviation
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ANC98LA074

During takeoff from a glacier off airport landing site, the right landing gear leg and ski separated from the airplane and both wings contacted the snow. Postaccident inspection revealed multiple site fatigue cracks at both upper wheel attachment bolt holes on the right landing gear leg. The airplane was routinely used for off airport landings on both wheels and skis. The airplane had accumulated 6,561 hours in operation at the time of the accident. No life limit (hours or cycles) exists for Cessna 185 landing gear legs. The only inspection for cracks is a visual inspection for general condition performed at 100 hour and annual intervals. This inspection does not require removal of the wheels/skis, nor does it require removal of any paint coatings prior to inspection.

NTSB Probable Cause

The failure of the right main landing gear leg due to fatigue cracking. A factor associated with this accident is the inadequate inspection procedure specified by the manufacturer.

Full Narrative

On June 16, 1998, at 1215 Alaska daylight time, a wheel/ski equipped Cessna A185F airplane, N185DG, sustained substantial damage during takeoff from the 6,900 feet msl level of the Kahiltna Glacier, 50 miles northwest of Talkeetna, Alaska. The commercial pilot and the two passengers were not injured. The flight was operated under 14 CFR Part 135 by Douglas Geeting Aviation, Inc., of Talkeetna, as an on demand charter transporting mountain climbers from the Kahiltna Glacier to Talkeetna. Visual meteorological conditions prevailed at the time of the accident, and a VFR flight plan was filed. The pilot reported to the NTSB Investigator-In-Charge during a telephone interview that during his landing roll on the glacier he heard a "bang." He stated that he inspected the airplane and skis, and found no damage. During acceleration for takeoff from the glacier, after reaching 45 knots, the right ski separated from the airplane, the airplane swerved right, and both wings contacted the snow. Inspection of the fractured landing gear leg at the NTSB metallurgical laboratory on July 13, 1998, revealed multiple site fatigue cracking at the location of both landing gear attachment bolt holes. The airplane had accumulated 6,561 hours of operation at the time of the accident. There is no established life limit (hours or cycles) for Cessna 185 landing gear legs. There is no inspection requirement or procedure to detect fatigue cracks in the landing gear legs except for a visual inspection conducted during 100 hour and annual inspections. No nondestructive inspection technique requiring removal of wheels or skis, or removal of paint coatings to facilitate crack detection, had been specified by the manufacturer or FAA at the time of the accident.

Flight

Event TypeAccident
Event Time12:15 AKDT
Nearest Airport0nm
Runway0
Flight Plan FiledVFR
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftCessna A185F
Tail NumberN185DG
Aircraft CategoryAir
DamageSubstantial
OperatorDouglas Geeting Aviation
Operating RulePart 135
Engines1
Engine TypeReciprocating
Engine DetailsContinental · IO-520D · Reciprocating · 300
Seats6

People & Injuries

Injury SummaryNo injuries (3 uninjured)
Fatal0
Serious0
Minor0
Uninjured3
Total3
Crew 1Age 57 · Second Class

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility50 sm
CeilingNone
Temperature / Dew Point50 / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data