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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 21, 1998 · Cessna A185F · N9620Q

Homer, AK

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
March 21, 1998
Injury Outcomes
No injuries (2 uninjured)
Location
Homer, AK
Aircraft
Cessna A185F
Tail Number
N9620Q
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ANC98LA027

The airplane bounced once during landing on the dry, paved runway. The pilot stated that as the airplane settled, the left wheel began to vibrate, and then the airplane ground looped to the left. Postaccident inspection revealed the inner tube inflation valve stem sheared off, and the wheel halves fractured. No preaccident mechanical anomalies were discovered during the inspection. The wheels had been installed 4.5 service hours, and 7 landings prior to the accident.

NTSB Probable Cause

The pilot's failure to maintain directional control. Factors in the accident are the sheared valve stem/deflation of the tire, and subsequent fracturing of the associated wheel.

Full Narrative

On March 21, 1998, at 1040 Alaska standard time, a Cessna A185F airplane, N9620Q, sustained substantial damage when it ground looped on landing at the Homer, Alaska, airport. The private pilot and the one passenger were uninjured. The airplane was operated by Fairweather, Inc., of Anchorage, Alaska. The flight was conducted under 14 CFR Part 91 as a personal flight. Visual meteorological conditions prevailed at the time of the accident, and a VFR flight plan was filed. The flight departed Anchorage at 1001, bound for Homer. The pilot stated during a telephone interview with the NTSB investigator-in-charge, and in his Pilot/Operator report, that during landing on the dry asphalt runway, the airplane bounced once, and after settling onto the runway, the left wheel began to vibrate. He indicated that as the airplane was decelerating, he retracted flaps and the airplane began drifting to the left. Application of right rudder did not stop the drift, the airplane ground looped to the left, and the right wing struck the runway. The airplane came to rest on the runway. The pilot, and the mechanics who repaired the airplane, said that the valve stem of the tire's inner tube was observed to be sheared off. Postaccident inspection of the wheel by the NTSB investigator revealed that both left wheel halves had fractured into numerous pieces. No preaccident anomalies were observed with the wheel or bearings. The Cleveland wheel assemblies with 8.50 inch by 6 inch tires had been installed October 3, 1997, 7 landings and about 4.5 hours prior to the accident.

Flight

Event TypeAccident
Event Time05:40 AKST
Nearest AirportHOMER (0nm)
Runway21
Runway Length7401 ft
Runway Width150 ft
Flight Plan FiledVFR
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftCessna A185F
Tail NumberN9620Q
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsContinental · IO-520-D · Reciprocating · 350
Seats4

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 48 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind110° @ 3 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point41 C / 36 C
Altimeter30.00 inHg
Observation Time14:53
Weather SourceWFAC

Appendix: Source Data