N940AK

Substantial
Serious

Curtiss-Wright P-40E S/N: 15321

Accident Details

Date
Thursday, May 11, 1995
NTSB Number
BFO95LA052
Location
PHELPS, NY
Event ID
20001207X03415
Coordinates
42.950729, -77.060523
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

Loss of engine power for undetermined reasons. A factor related to the accident was the lack of suitable terrain for the forced landing.

Aircraft Information

Registration
Make
CURTISS-WRIGHT
Serial Number
15321
Engine Type
Reciprocating
Year Built
1941
Model / ICAO
P-40E P40
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
1
FAA Model
P-40E

Registered Owner (Current)

Name
P40 KITTYHAWK LLC
Address
9800 SW NIMBUS AVE
City
BEAVERTON
State / Zip Code
OR 97008-7197
Country
United States

Analysis

On May 11, 1995, at 1940 eastern daylight time, N940AK, a Curtiss Wright Kittyhawk P-40E experimental airplane, lost engine power during cruise flight and crashed in a freshly plowed corn field in Phelps, New York. The certificated commercial pilot was seriously injured and the airplane sustained substantial damage. Visual meteorological conditions prevailed and a flight plan was not filed. The personal flight was conducted under 14 CFR 91. The flight originated in Fulton, New York, about 1930, with an intended destination was Geneseo, New York.

According to an FAA Aviation Safety Inspector, the pilot stated that the aircraft was in storage all winter, and had just received an annual inspection. The pilot stated that the preflight inspection, engine run up, takeoff and climb out were all normal. He stated that the airplane was in cruise flight at 1600 feet MSL about 10 minutes into the flight when the engine "...backfire violently twice...[then] the engine stopped dead." The pilot stated that he completed the emergency checklist, but all attempts to restart the engine were unsuccessful. The pilot reported that he "...did not have the opportunity of gliding to a more suitable landing area." A forced landing was made in a freshly plowed corn field, and the landing gear collapsed.

The airplane was examined at the accident site by the FAA Inspector. The examination included checking the fuel lines, carburetor, gascolator, the engine and electric driven fuel pumps. The fuel lines separated during the impact sequence. The examination also revealed that there was no fuel in the carburetor nor the fuel lines leading from the electric fuel pump to the engine driven fuel pump . The engine driven fuel pump, and the electric driven fuel pump were removed and bench checked at a test facility. Both pumps operated satisfactory when tested.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# BFO95LA052