N95410

Substantial
None

PIPER PA28S/N: 28-25930

Accident Details

Date
Sunday, May 27, 2018
NTSB Number
GAA18CA307
Location
Butler, KY
Event ID
20180529X72300
Coordinates
38.728889, -84.394996
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The pilot’s improper fuel management, which resulted in fuel starvation.

Aircraft Information

Registration
N95410
Make
PIPER
Serial Number
28-25930
Engine Type
Reciprocating
Model / ICAO
PA28P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
BIEHL EDGAR A
Address
2816 BUXTON LN
Status
Deregistered
City
GROVE CITY
State / Zip Code
OH 43123-3531
Country
United States

Analysis

The pilot reported that, while enroute, the airplane's engine began to run rough and lose power. He immediately turned toward the nearest airport and slowed the airplane to 100 knots. He added that he pushed the mixture to full rich, which caused a short burst of power that lasted just a few seconds. He then pumped the throttle and applied carburetor heat, but then realized he did not have enough altitude to make the airport and began to look for an alternate landing site.

He further added, that after locating a ridge top field, he slowed the airplane to 75 knots and pulled one notch of flaps and trimmed for landing. As he lined the airplane up with the field he pulled full flaps at about 300 ft above the ground. The touchdown was smooth and the airplane continued the landing roll in wheat that was approximately 3 ft tall. Subsequently, the right wing struck an industrial irrigation nozzle and the right wing separated from the fuselage.

The airplane sustained substantial damage to the right wing and stabilator.

The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation.

The pilot added that, during the engine failure, he did not attempt to change fuel tanks from the empty right wing fuel tank, and as a recommendation to make the fuel selector check the first part of the restart procedure.

The Federal Aviation Administration inspector reported that, while on scene, he was able to run the engine. He added, the left tank was approximately ½ full of fuel. He switched the fuel selector to the left tank and started the engine normally. The oil pressure was fine; fuel pressure normal on both the electric pump and engine driven pump; and the magnetos checked fine.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# GAA18CA307