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Aviation safety reports, made easier to study

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November 3, 2003 · Piper PA-20 · N1486A

Bethel, AK

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
November 3, 2003
Injury Outcomes
1 injury (1 minor injury), 1 uninjured
Location
Bethel, AK
Aircraft
Piper PA-20
Tail Number
N1486A
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
ANC04LA005

The commercial pilot was flying over mountainous terrain when he noted a rough running engine and a slight reduction in engine rpm. He applied full carburetor heat, which was followed by a rapid loss of engine power, and subsequent loss of altitude. Unable to restore adequate engine power to maintain level flight, the pilot selected an uphill portion of a mountainside as a forced landing site. During touchdown on the soft, tundra-covered terrain, the left main landing gear collapsed, and the left wing struck the ground. The airplane sustained structural damage to the left wing and fuselage. The pilot said that weather conditions at the time of the accident were, in part: Visibility, 10 statute miles in light rain and mist; clouds and sky condition, 3,000 feet overcast; temperature, 40 degrees F. The pilot reported that there were no preaccident mechanical anomalies with the airplane, and that the loss of engine power was due to carburetor icing.

NTSB Probable Cause

The pilot's delayed application of carburetor heat, which resulted in a loss of engine power, and subsequent forced landing. Factors associated with the accident were weather conditions conducive to carburetor icing, and the lack of suitable terrain for a forced landing.

Full Narrative

On November 2, 2003, about 1700 Alaska daylight time, a tundra tire-equipped Piper PA-20 airplane, N1486A, sustained substantial damage when the left main landing gear collapsed during a forced landing following a loss of engine power, about 65 miles east of Bethel, Alaska. The airplane was being operated as a visual flight rules (VFR) cross-country personal flight under Title 14, CFR Part 91, when the accident occurred. The commercial certificated pilot sustained minor injuries, and the sole passenger aboard was not injured. Visual meteorological conditions prevailed, and no flight plan was filed. The flight originated about 1545, from the Aniak Airport, Aniak, Alaska, and was returning to Aniak when the accident occurred. During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC), on November 5, the pilot related that the purpose of the flight was to view some Alaskan scenery, and added that two off airport landings were accomplished prior to the accident. He said that on the return flight to Aniak, while over mountainous terrain, he noted a rough running engine and a slight reduction in engine rpm. He applied full carburetor heat, which was followed by a rapid loss of engine power, and subsequent loss of altitude. The pilot said that he was unable to restore adequate engine power to maintain level flight, and he selected an uphill portion of a mountainside as a forced landing site. During touch down on the soft tundra-covered terrain, the left main landing gear collapsed, and the left wing struck the ground. The airplane sustained structural damage to the left wing and fuselage. The pilot reported that weather conditions at the time of the accident were, in part: Visibility, 10 statute miles in light rain and mist; clouds and sky condition, 3,000 feet overcast; temperature, 40 degrees F. The pilot reported that there were no preaccident mechanical anomalies with the airplane, and that the loss of engine power was due to carburetor icing. According to the pilot, Piper PA-20 airplanes with Lycoming O-290-D engines are highly susceptible to carburetor icing.

Flight

Event TypeAccident
Event Time16:00 AKST
Nearest Airport0nm
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-20
Tail NumberN1486A
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-290-D · Reciprocating · 125
Seats2

People & Injuries

Injury Summary1 injury (1 minor injury), 1 uninjured
Fatal0
Serious0
Minor1
Uninjured1
Total2
Crew 1Age 38 · Second Class · Minor

Conditions

ConditionsVMC
LightDaylight
Wind180°
Visibility10 sm
CeilingOvercast 3000 ft
Temperature / Dew Point39 C / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data