N711EW

Substantial
None

Piper PA-24-250 S/N: 24-2942

Accident Details

Date
Saturday, August 9, 1997
NTSB Number
LAX97LA279
Location
SAN DIEGO, CA
Event ID
20001208X08672
Coordinates
32.799003, -117.130241
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

a loss of engine power for undetermined reasons.

Aircraft Information

Registration
Make
PIPER
Serial Number
24-2942
Engine Type
Reciprocating
Year Built
1961
Model / ICAO
PA-24-250 PA24
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
PA-24-250

Registered Owner (Current)

Name
WARD LUMBER COMPANY INC
Address
11515 FURY LN APT 40
City
EL CAJON
State / Zip Code
CA 92019-4332
Country
United States

Analysis

On August 9, 1997, at 1521 hours Pacific daylight time, a Piper PA24-250, N711EW, was substantially damaged during a forced landing on a city street in Kearny Mesa, a suburb of San Diego, California. The private pilot and one passenger were not injured. The flight departed Montgomery Field on a local flight and encountered loss of engine power during the takeoff initial climb. Visual meteorological conditions prevailed and no flight plan was filed for the personal flight.

The pilot stated in his report that the aircraft had a partial power loss at 1,500 feet msl during climbout, followed by a complete loss of power approximately 2 minutes later. At the time of partial power loss, the pilot applied carburetor heat, turned on the electric fuel pump, switched from the left to the right fuel tank, and checked the position of the magneto switch. Following total loss of power, the pilot stated that he made a forced landing on a city street which resulted in substantial damage to the aircraft and minor damage to three parked cars and a bus stop passenger bench.

During the on-site investigation by Federal Aviation Administration inspectors, both fuel tanks were found to contain 100LL aviation fuel, and fuel continuity was established between the fuel tanks and the engine carburetor. After transport to a local hanger, the engine was placed on a test stand where it started and ran normally with no apparent malfunctions. The magneto internal and external timing was then checked and found within the tolerance specified by the manufacturer and there was a spark across the gap of each sparkplug. According to the sparkplug color chart supplied by the engine manufacturer, plug color indicated that the engine had been running with a slightly rich mixture.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX97LA279