N86361

Substantial
None

AERONCA 11AC S/N: 11AC174

Accident Details

Date
Monday, August 16, 1993
NTSB Number
ANC93LA150
Location
GALENA, AK
Event ID
20001211X13037
Coordinates
64.740356, -156.849975
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

THE LOSS OF ENGINE POWER FOR UNDETERMINED REASONS. A FACTOR WAS THE LACK OF SUITABLE TERRAIN ON WHICH TO MAKE A FORCED LANDING.

Aircraft Information

Registration
Make
AERONCA
Serial Number
11AC174
Engine Type
Reciprocating
Year Built
1946
Model / ICAO
11AC AB11
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
11AC

Registered Owner (Current)

Name
BIAS CHRISTOPHER S
Address
4905 N FLYING CIRCUS CIR
City
WASILLA
State / Zip Code
AK 99654-4620
Country
United States

Analysis

On August 16, 1993, at 1145 Alaska daylight time, a wheel equipped Aeronca Chief 11AC aircraft, N86361, experienced a loss of engine power while at cruise flight resulting in a forced landing and nose over on muskeg tundra near Kalakette Creek, approximately eight miles west of Galena, Alaska. The pilot in command, who was also the registered owner/operator of the airplane, and his passenger were not injured and the airplane sustained substantial damage. The pleasure flight, operating under 14 CFR Part 91, departed Galena at approximately 1135 and the intended destination was Kalakette Creek. Visual meteorological conditions prevailed and no VFR flight plan had been filed.

During a telephone interview with the NTSB investigator in charge on August 16, 1993, the pilot stated that he performed a thorough preflight (including a check of the engine oil quantity and fuel sumps) and engine run up and found the airplane to be in good operating condition. The fuel on board the airplane consisted of two gallons in the rear tank and 10 gallons in the front (main) tank. The takeoff and flight was conducted with the fuel selector on the main tank. While cruising at 850 feet above the ground at an engine rpm setting of 2200, the sound from the engine changed pitch and he observed on the rpm gage a bleed off of approximately 100 rpm. Believing the engine throttle had crept back, he advanced the throttle and the engine stopped suddenly as if it had locked up. There were no metallic sounds associated with the engine stoppage. Post accident attempts by the pilot and passenger to rotate the engine by hand using the propeller were not successful. The pilot reported that he had flown the airplane about 65 hours since acquiring it and had not experienced any problems with the engine. The airplane received an annual inspection in October 1992, and the engine had accumulated approximately 220 hours since undergoing a major overhaul.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC93LA150