N7507P

Substantial
Minor

PIPER PA-24-250 S/N: 24-2708

Accident Details

Date
Thursday, September 2, 1993
NTSB Number
BFO93LA150
Location
CARIBOU, ME
Event ID
20001211X13327
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
2
Uninjured
0
Total Aboard
2

Probable Cause and Findings

LOSS OF ENGINE POWER FOR UNDETERMINED REASONS. CONTRIBUTING TO THE ACCIDENT WAS THE UNSUITABLE TERRAIN.

Aircraft Information

Registration
N7507P
Make
PIPER
Serial Number
24-2708
Engine Type
Reciprocating
Model / ICAO
PA-24-250 PA24
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
DORAN DONALD W
Address
723 TIMBER RIDGE TRL SW
Status
Deregistered
City
VERO BEACH
State / Zip Code
FL 32962
Country
United States

Analysis

On Thursday, September 2, 1993, at 1000 eastern daylight time, N7507P, a Piper PA-24-250, owned and operated by Donald Doran of Vero Beach, Florida, lost engine power shortly after takeoff and collided with the ground in a field at Caribou, Maine. Visual meteorological conditions prevailed and a flight plan was not filed. The certificated commercial pilot and his passenger received minor injuries. The airplane was substantially damaged. The personal flight was being operated under 14 CFR 91 and was destined for Auburn-Lewiston, Maine.

According to the pilot, he had completed his pretakeoff checks and run-up successfully. He stated that after departing runway 29 at about 200 feet above the ground, the engine lost power. The pilot stated that the fuel selector was on the left tank and that he tried switching tanks to restart the engine, but he was unsuccessful. He made a forced landing in a field about a quarter mile from the airport.

According to the FAA Inspector who examined the wreckage, both auxiliary fuel tanks and the left main fuel tank were full and the right main fuel tank was empty. A witness at the accident site stated that he turned the fuel selector off after he smelled fuel, but he does not recall which tank the selector was on. The pilot had reported to the FAA that the tanks were topped off about a week prior to the accident, and that he had flown about 2.12 hours since the refuelling. The airplane's main tanks capacity is 30 gallons per tank, and the fuel consumption according to the FAA is 14.3 gph.

The engine was examined after the accident under the supervision of an FAA inspector. The engine was installed with a test club propeller and a slave carburetor in order to test run the engine. The engine was started and operated without difficulty. According to the FAA there was no evidence of mechanical malfunction that would have prevented the engine from operating.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# BFO93LA150