N6253P

Substantial
None

PIPER PA-24-250 S/N: 24-1360

Accident Details

Date
Monday, February 21, 1994
NTSB Number
ATL94LA052
Location
KINSTON, NC
Event ID
20001206X00700
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

A LOSS OF ENGINE POWER DUE TO A PARTIAL BLOCKAGE OF THE INDUCTION AIR SYSTEM BY A FOREIGN OBJECT (SILICON BAFFLING MATERIAL).

Aircraft Information

Registration
N6253P
Make
PIPER
Serial Number
24-1360
Engine Type
Reciprocating
Model / ICAO
PA-24-250 PA24
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SHNUR MORRIS
Address
RFD#1 PO BOX 59
Status
Deregistered
City
SABATTUS
State / Zip Code
ME 04280
Country
United States

Analysis

On February 21, 1994, at 1337 eastern standard time, a Piper PA-24-250, N6253P, was force landed after a reported engine power loss in Kinston, North Carolina. The aircraft was substantially damaged. The private pilot and two passengers were not injured. The aircraft was owned and operated under 14 CFR Part 91 by the pilot. Visual meteorological conditions prevailed at the time, and an instrument flight rules flight plan was filed for the personal flight to Manchester, New Hampshire. The flight was originating at the time of the accident.

The pilot reported the following: At about 500 feet mean sea level on the initial climb following takeoff, the engine sputtered and lost power. He made a turn toward the airfield, and left the gear up for as long as possible to reduce drag. After the aircraft cleared some trees, the landing gear handle was lowered, however the gear did not have time to extend prior to touchdown. The aircraft landed in a grassy area on the airfield. The aircraft slid across the grass, then across a taxiway before coming to rest in a grassy area.

An inspector from the Federal Aviation Administration examined the aircraft following the accident. He reported that there was a piece of silicon baffling material, approximately 8 inches long and one inch wide, lodged inside the carburetor airbox, with about 2 inches of it extending into the carburetor venturi. The origin of the silicon material could not be determined, and maintenance records did not reveal any recent work which would require such a material to be used. The engine was then prepared for a test run. The engine started normally and sustained rpm and normal cylinder head temperature. This was attempted several times, and each time the engine started normally.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL94LA052