N151RF

Substantial
Minor

OLIVER ROBERT K OLIVER SERIES 6S/N: S69912-006

Accident Details

Date
Friday, August 25, 2023
NTSB Number
ANC23LA070
Location
Big Delta, AK
Event ID
20230903192993
Coordinates
64.102592, -145.786930
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
2
Uninjured
0
Total Aboard
2

Probable Cause and Findings

A partial loss of engine power for undetermined reasons.

Aircraft Information

Registration
Make
OLIVER ROBERT K
Serial Number
S69912-006
Engine Type
Reciprocating
Year Built
2000
Model / ICAO
OLIVER SERIES 6
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
OLIVER SERIES 6

Registered Owner (Current)

Name
BURHANS WILLIAM M
Address
7025 SATURN CIR
City
ANCHORAGE
State / Zip Code
AK 99504-4564
Country
United States

Analysis

On August 24, 2023, about 1600 Alaska daylight time, a Kitfox Series 6 experimental airplane, N151RF, sustained substantial damage when it was involved in an accident near Delta Junction, Alaska. The pilot and passenger sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that he was flying around the Salcha River area and decided to fly to Charley River. About 10 to 15 minutes from his destination, the engine sustained a partial loss of power. To troubleshoot the loss of power, he pulled carburetor heat on but power was not restored. He moved the throttle control from idle to full power and the engine would only increase to about 25% with full throttle. The pilot decided to make a forced landing along a treeless mountain ridgeline. During landing, a strong gust of wind lifted the airplane’s right wing and subsequently the left wing and engine impacted terrain and the airplane nosed over. The airplane sustained substantial damage to the fuselage and wings.

The postaccident examination of the engine revealed no evidence of any preimpact mechanical malfunctions or anomalies that would have precluded normal operation. Control continuity was established between the cockpit and engine. Although both carburetor bowls were empty of fuel, when disconnected the fuel line had fuel drain from both sides of the disconnection. Thumb compression was established for all four cylinders. The top spark plugs all appeared to be normal; the lower spark plugs in the two right cylinders had oil in them, as did the forward right cylinder, which contained about a cup of oil. Small amounts of water were drained from the two left cylinders.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC23LA070