N705AP

Substantial
None

PFOUTS ALFRED L SENIOR AERO SPT D260S/N: 7

Accident Details

Date
Wednesday, May 4, 2011
NTSB Number
ERA11LA282
Location
Palm Coast, FL
Event ID
20110505X81116
Coordinates
29.474166, -81.329170
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A total loss of engine power for undetermined reasons.

Aircraft Information

Registration
Make
PFOUTS ALFRED L
Serial Number
7
Engine Type
Reciprocating
Year Built
1969
Model / ICAO
SENIOR AERO SPT D260
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
SENIOR AERO SPT D260

Registered Owner (Current)

Name
ISBELL FRANK
Address
13110 BEACH RD
City
CHESTERFIELD
State / Zip Code
VA 23838-3009
Country
United States

Analysis

On May 4, 2011, about 1345 eastern daylight time, a Pfouts Senior Aero Sport D260, N705AP, experienced a loss of engine power and force landed near Palm Coast, Florida. The airplane was substantially damaged. The experimental, amateur-built airplane was registered to and operated by the commercial pilot under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed and no flight plan was filed. The pilot was not injured. The flight originated from Pierson, Florida (2J8) about 1330.

The pilot reported that he turned off the electric boost pump shortly after takeoff, about 200 feet above the ground. He noted that his fuel pressure was low with only the engine-driven pump operating. He turned the boost pump back on and the fuel pressure returned to an acceptable level. While approaching St. Augustine, the fuel pressure again dropped, and the engine quit. The pilot force landed the airplane and it collided with trees.

Initial examination of the airframe and engine by a Federal Aviation Administration inspector revealed that the wing fuel tanks contained adequate fuel; however the fuel gascolator was dry. The electric pump was a Holley automotive-type fuel pump. The pilot reported that the electric boost pump was installed the day prior to the accident. The FAA inspector reported that the engine-driven pump was overhauled in September, 2010, and the pilot reported that it was installed 40 flight hours prior to the accident.

On May 19, 2011, the FAA inspector examined both fuel pumps at a local FAA part 145 repair station. The electric fuel boost pump, which was a Holley model R90615AA automotive pump, was energized with an external electric source. The pump ran and "provided good suction at the inlet port."

The engine-driven fuel pump was a Lear Sieglar model RD7790. The pump was fitted to a fuel flow test bench and after an initial boost of 1 psi, the pump maintained a pressure of 7 to 9 psi. The FAA inspector did not find any evidence of mechanical failure or malfunction with either pump.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA11LA282