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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

September 7, 1998 · Cessna 140 · N81045

Fairbanks, AK

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
September 7, 1998
Injury Outcomes
No injuries (2 uninjured)
Location
Fairbanks, AK
Aircraft
Cessna 140
Tail Number
N81045
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ANC98LA140

While in cruise flight the pilot heard a 'clunk' and engine rpm immediately began to decrease. The engine noise and rpm decrease continued, the pilot performed a forced landing in tundra, and the airplane nosed over onto its back. Postaccident inspection revealed that the exhaust valve stem of the number two cylinder had separated, and the valve was ingested into the cylinder. The engine had accumulated 4,555 hours since new, and 1,089 hours since overhaul.

NTSB Probable Cause

The loss of engine power due to an in-flight fracture of an engine exhaust valve stem assembly. A factor associated with the accident was the lack of suitable terrain for a forced landing.

Full Narrative

On September 6, 1998, at 1707 Alaska daylight time, a Cessna 140 airplane, N81045, sustained substantial damage when it nosed over during an emergency landing seven miles southeast of the Fairbanks International Airport, Fairbanks, Alaska. The private pilot owner and the sole passenger were not injured. The flight was conducted under 14 CFR Part 91 as a personal flight. The flight departed the Fairbanks/Clear Creek airstrip at 1615, and was returning to Fairbanks International Airport, from a camping trip. Visual meteorological conditions prevailed at the time of the accident, and no flight plan was filed. The pilot told the NTSB investigator-in-charge during a telephone interview on September 6, and in his NTSB Pilot / Operator report, that while in cruise at 1,500 feet msl, he heard a "clunk" and the engine rpm began to decrease. He stated that application of carburetor heat, and changing fuel tanks did not improve the engine performance. The engine noise continued, and engine rpm continued to decrease. The pilot notified the Fairbanks Air Traffic Control Tower of his emergency, and made a forced landing on tundra. The airplane nosed over during the landing. Postaccident inspection of the Teledyne Continental Motors C-85-6-12 engine revealed the exhaust valve stem of the number two cylinder had separated, allowing the valve to be ingested into the cylinder. Metal pieces up to 1/2 inch in diameter, were recovered from the cylinder and exhaust manifold. The engine had accumulated 4,555 hours in service at the time of the accident, and 1,089 hours since overhaul.

Flight

Event TypeAccident
Event Time17:07 AKDT
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftCessna 140
Tail NumberN81045
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsContinental · C-85-12 · Reciprocating · 85
Seats2

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 29 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind200° @ 5 kt
Visibility10 sm
CeilingBroken clouds 8000 ft
Temperature / Dew Point57 / 39 C
Altimeter29.00 inHg
Observation Time19:53
Weather SourceWFAC

Appendix: Source Data