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August 25, 2003 · Piper PA-18-150 · N2567L

Avenal, CA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
August 25, 2003
Injury Outcomes
No injuries (2 uninjured)
Location
Avenal, CA
Aircraft
Piper PA-18-150
Tail Number
N2567L
Injuries
None
Aircraft Damage
Substantial
NTSB Number
LAX03LA265

The airplane veered off the runway and nosed over during a precautionary landing at a private airstrip. The landing was precipitated by a partial loss of engine power. The pilot stated that 5 minutes after departure, at an altitude of 500 feet, he heard "a loud noise" from the engine with an ensuing reduction in power. By manipulating the carburetor heat control he regained some power. He landed at the first available landing site, which was a small private airstrip. During the landing roll the airplane veered right, the pilot corrected to the left, and the airplane departed the runway and into soft ground on the left side of the airstrip. The airplane nosed over onto its back. Meteorological data recorded at the nearest reporting station at the approximate time of the accident show that the temperature was 95 degrees Fahrenheit, with a dew point of 60 degrees Fahrenheit. A standard carburetor icing chart indicated that at those temperature and dew point levels, light carburetor icing was possible when in the glide or cruise power configurations. Under the supervision of a FAA inspector, an Airframe & Powerplant mechanic examined the engine and found no anomalies. The mechanic was then able to start the engine and achieved 800-900 rpm before shutting the engine down due to vibrations caused by the bent propeller.

NTSB Probable Cause

the pilot's failure to maintain directional control during a precautionary landing. The reason for the partial loss of engine power was undetermined.

Full Narrative

On August 25, 2003, at 1335 Pacific daylight time, a Piper PA-18-150, N2567L, veered off the runway and nosed over during a precautionary landing at a private airstrip 13 miles southeast of Avenal, California. The forced landing was precipitated by a partial engine power loss. The airplane was operated by the private pilot/owner under the provisions of 14 CFR Part 91. The pilot and one passenger were not injured. The airplane was substantially damaged. Visual meteorological conditions prevailed, and no flight plan had been filed. The personal flight originated at a private airstrip 2 miles north of Lost Hills Airport, California, about 1330. The pilot stated to the National Transportation Safety Board investigator that 5 minutes after departure, and at an altitude of 500 feet, he heard "a loud noise" from the engine with an ensuing reduction in power. By manipulating the carburetor heat control he regained some power. He landed at the first available landing site, which was a small private airstrip. During the landing roll the airplane veered right, and the pilot corrected to the left. The airplane departed the runway and into soft ground on the left side of the airstrip. The airplane nosed over onto its back. The pilot said the airstrip appeared to have been freshly oiled down. Meteorological data recorded at Bakersfield Airport, Bakersfield, California, at the approximate time of the accident show that the temperature was 95 degrees Fahrenheit with a dew point of 60 degrees Fahrenheit. A standard carburetor icing chart indicated that at those temperature and dew point levels, light carburetor icing was likely when in the glide or cruise power configurations. Under the supervision of a Federal Aviation Administration inspector, an Airframe & Powerplant mechanic examined the engine and found no anomalies. The mechanic was then able to start the engine and achieved 800-900 rpm before shutting the engine down due to vibrations caused by the bent propeller.

Flight

Event TypeAccident
Event Time13:35 PDT
Nearest AirportPrivate Airstrip (0nm)
Runway36
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-18-150
Tail NumberN2567L
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-320-A2B · Reciprocating · 150
Seats2

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 45 · Third Class · None

Conditions

ConditionsVMC
LightDaylight
Wind270° @ 10 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point59
Altimeter29.88 inHg
Observation Time21:54
Weather SourceWFAC

Appendix: Source Data