N6725P

Substantial
Serious

PIPER PA-24-250 S/N: 24-1852

Accident Details

Date
Monday, September 25, 1995
NTSB Number
CHI95LA332
Location
LUDINGTON, MI
Event ID
20001207X04468
Coordinates
43.949478, -86.440002
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

fuel exhaustion resulting from the pilot's inaccurate fuel calculations and the failure to refuel the airplane prior to takeoff. An additional cause was the stall/mush during the forced landing.

Aircraft Information

Registration
N6725P
Make
PIPER
Serial Number
24-1852
Engine Type
Reciprocating
Year Built
1960
Model / ICAO
PA-24-250 PA24
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
KIEFER DAVID R
Address
261 HARBOR DR
Status
Deregistered
City
LUDINGTON
State / Zip Code
MI 49431
Country
United States

Analysis

On September 24, 1995, at 2019 eastern daylight time (edt), a Piper PA-24-250, N6725P, piloted by a private pilot, sustained substantial damage during a forced landing to a plowed field. Visual meteorological conditions prevailed at the time of the accident. The flight was operated under 14 CFR Part 91. A flight plan was not on file. The pilot sustained serious injuries. The flight departed Rochester, New York, at 1745 edt, and was en route to Ludington, Michigan.

The pilot reported that he was approximately six miles from his destination airport at 2200 feet mean sea level when he "ran out of fuel." He turned on the fuel pump and switched tanks with no success. The pilot stated that he then "turned the airplane into the wind and looked for a place to put the airplane down." He selected a plowed field to do a forced landing in, but had to clear trees in front of him to reach it. The pilot stated that he was knocked unconscious at impact. In a subsequent telephone conversation with the pilot, he said that he had taken off knowing that he was "probably stretching his fuel to reach his planned destination," but felt that he could "get fuel somewhere en route."

The Federal Aviation Administration (FAA) inspector who examined the wreckage stated that the airplane "impacted in soft dirt and slid approximately 50 feet before coming to rest." The right main gear strut was found driven up through the right wing skin. The left main gear was bent outward and the nose gear was found separated from the rest of the airplane wreckage. The cowling and forward fuselage were bent underneath. Examination of the propeller showed one blade undamaged and the other blade bent aft. There were severe wrinkles observed throughout the skin of the airplane. The cabin was found intact, but the seats, control panel and luggage had been jarred loose. Examination of the flight controls showed no evidence of preimpact damage. There was no evidence of fuel at the accident site. Examination of the fuel system indicated no sign of fuel in the system prior to impact.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI95LA332