N8007N

Destroyed
Serious

Piper PA-28-140S/N: 28-25248

Accident Details

Date
Tuesday, July 3, 2001
NTSB Number
CHI01LA197
Location
Mecosta, MI
Event ID
20010710X01351
Coordinates
43.580585, -85.440338
Aircraft Damage
Destroyed
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

the inadequate preflight planning/preparation by the pilot and fuel starvation. Additional causes were the aircraft control not maintained, and the inadvertent stall by the pilot.

Aircraft Information

Registration
N8007N
Make
PIPER
Serial Number
28-25248
Engine Type
Reciprocating
Year Built
1968
Model / ICAO
PA-28-140P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
MORRIS ROBERT S
Address
7518 REGENCY LN
Status
Deregistered
City
STANWOOD
State / Zip Code
MI 49346-9672
Country
United States

Analysis

On July 3, 2001, at 1655 eastern daylight time, a Piper PA-28-140, N8007N, owned and piloted by a commercial pilot, was destroyed on impacted terrain following a loss of engine power during climbout from the Canadian Lakes Airport, Mecosta, Michigan. Visual meteorological conditions prevailed at the time of the accident. The 14 CFR Part 91 personal flight was not operating on a flight plan. The pilot received serious injuries. The flight was originating at the time of the accident.

Witnesses reported that the airplane departed in a southerly direction. At approximately 200 feet agl, the engine began sputtering. The airplane made a right climbing banked turn and gained 50-100 feet at which time the engine quit. The engine stopped and the left wing dropped.

Examination of the airplane by the Federal Aviation Administration revealed that the fuel selector was selected to the left fuel tank. The left fuel tank did not contain fuel and the right tank contained 15 gallons of fuel. The fuel line from the electric pump to the engine driven pump did not contain fuel. The fuel line leading to the carburetor did not contain fuel. The carburetor fuel bowl contained fuel level which was less than 1/16 inch in depth. The engine was rotated and compression was obtained from all cylinders and engine continuity was established. Electrical continuity of both magnetos was confirmed.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI01LA197