N3965K

Substantial
None

Piper PA-28-140 S/N: 28-23848

Accident Details

Date
Friday, February 20, 1998
NTSB Number
MIA98LA082
Location
GRANITEVILLE, SC
Event ID
20001211X09588
Coordinates
33.490974, -81.759483
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

failure of the number three exhaust valve, which resulted in loss of engine power and a forced landing. Related factors were: the obstructions (earthen embankment and fence) in the emergency (forced) landing area.

Aircraft Information

Registration
N3965K
Make
PIPER
Serial Number
28-23848
Engine Type
Reciprocating
Model / ICAO
PA-28-140 P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
KING HENRY H JR
Address
3904 GATEWOOD DR
Status
Deregistered
City
AMARILLO
State / Zip Code
TX 79109
Country
United States

Analysis

On February 20, 1998, about 1115 eastern standard time, a Piper PA-28-140, N3965K, registered to an individual, operating as a 14 CFR Part 91 personal flight, experienced a loss of engine power during initial climb after takeoff from Twin Lakes Airport, Graniteville, South Carolina. Visual meteorological conditions prevailed and no flight plan was filed. The airplane received substantial damage, and the private-rated pilot was not injured. The flight originated about 4 minutes before the accident.

The pilot stated that he was returning the airplane to his home field at Aiken Municipal Airport, South Carolina, having had maintenance performed on the gascolator, primer, and fuel selector by an A&P mechanic. Climbing through 400 feet agl, the engine began to run rough and lose power. The pilot felt his only option was a forced landing to a grass field. His final approach carried him further than his intended touchdown point, and he collided with an earth embankment and fence posts, shearing the landing gear, bending the propeller, both wing spars, and the engine mount.

Subsequent teardown examination of the engine by FAA personnel revealed a broken exhaust valve in the number three cylinder. According to the FAA report, about 30 percent of the valve face was missing. The engine had undergone an annual inspection on June 6, 1997, and time since overhaul on the engine was reported as 1920.1 hours by the pilot.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA98LA082