N226JK

Substantial
Minor

CUB CRAFTERS PA18 150S/N: 9965CC

Accident Details

Date
Wednesday, March 21, 2018
NTSB Number
CEN18LA125
Location
Beggs, OK
Event ID
20180322X14941
Coordinates
35.793609, -96.029724
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
1
Total Aboard
2

Probable Cause and Findings

The pilot's failure to verify that the fuel selector was properly set before takeoff, which resulted in a total loss of engine power due to fuel starvation.

Aircraft Information

Registration
Make
CUB CRAFTERS
Serial Number
9965CC
Engine Type
Reciprocating
Year Built
2004
Model / ICAO
PA18 150
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
PA18-150

Registered Owner (Current)

Name
SMITH DAVID C
Address
343 MONSE RIVER RD
City
BREWSTER
State / Zip Code
WA 98812-9553
Country
United States

Analysis

On March 21, 2018, about 1745 central daylight time, a Cub Crafters PA18-150 airplane, N226JK, experienced a loss of engine power after takeoff from runway 36 (1,800 ft by 50 ft, turf) at the Eagle Creek Airport (51OK), Beggs, Oklahoma. The pilot sustained a minor injury; the passenger was not injured. The airplane was substantially damaged. The airplane was registered to and operated by the pilot as a Title 14 Code of Federal Regulations Part 91 flight. Day visual meteorological conditions prevailed. The flight was not operated on a flight plan. The local flight was originating at the time of the accident.The pilot stated that the pre-takeoff engine run up was normal. The accident takeoff was uneventful until the airplane reached about 50 ft above ground level when the engine lost power. The engine regained power momentarily, but then lost power again. The pilot executed a forced landing to an open grass area near the approach end of runway 8. The airplane impacted a ditch during the landing which caused the landing gear to collapse.

The airplane came to rest upright. The left wing struts were buckled, and both wings were deformed near midspan. The lower portion of the engine cowling exhibited upward crushing damage. The engine was displaced upward and to the left. The firewall and lower fuselage were deformed. The left side of the fuselage exhibited damage to the structural tubing along the cabin and baggage compartment.

A postrecovery examination of the airframe and engine did not reveal any anomalies consistent with a loss of engine power. A detailed summary of the examination is included in the docket associated with this accident investigation.

The pilot reported that about 30 gallons of fuel were on-board before takeoff. He stated that the fuel selector may not have been fully in the both position detent at the time of the accident takeoff, and as a result, the engine might have lost power due to fuel starvation.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN18LA125