N81019

Substantial
None

Piper PA-28-161 S/N: 288016098

Accident Details

Date
Friday, April 14, 2000
NTSB Number
LAX00LA154
Location
PALO ALTO, CA
Event ID
20001212X20853
Coordinates
37.449226, -122.099296
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The loss of engine power for undetermined reasons during takeoff climb.

Aircraft Information

Registration
N81019
Make
PIPER
Serial Number
288016098
Engine Type
Reciprocating
Year Built
1979
Model / ICAO
PA-28-161 P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
DOERR RICHARD A
Address
1203 N LEMON AVE
Status
Deregistered
City
MENLO PARK
State / Zip Code
CA 94025
Country
United States

Analysis

On April 14, 2000, at 1547 hours Pacific daylight time, a Piper PA-28-161, N81019, was substantially damaged during an off airport landing following loss of engine power during takeoff initial climb. The commercial certificated pilot was not injured. Visual meteorological conditions prevailed for the local area, post maintenance check flight operated by the Palo Alto Flying Club under 14 CFR Part 91. No flight plan was filed.

According to the operator, the aircraft had just received an engine oil change and it was the operator's practice, following maintenance, to fly the aircraft around the airport traffic pattern a couple of times before releasing it for student use. The pilot/flight instructor told the operator that the start, taxi, and run-up were normal. The engine operated smoothly until, at 300 feet agl on takeoff climb out, the engine quit abruptly, regained power, then quit again. The pilot attempted to return to the departure runway but landed short in a marsh area.

The operator further stated that, at the accident site, the propeller did not appear to have been turning on impact. There was fuel in both wing tanks and there was no contamination at the sumps. The emergency responders had instructed the pilot to turn the fuel selector to the "off" position. The fuel pump functioned audibly. There was clean oil in the engine and the engine rotated freely with good compression.

After recovery, the cowling was removed and the engine was examined by inspectors from the Federal Aviation Administration San Jose Flight Standards District Office. No anomalies were noted. The propeller was replaced and the carburetor heat box was removed due to damage. The engine started promptly, the run-up was normal, and the engine delivered full power. It was noted that, if the fuel tank selector valve was moved out of a tank position detent to the between-tank or off position, the engine operated approximately 1 minute before stopping.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX00LA154