N14CL

Substantial
None

PIPER PA-28-151 S/N: 28-7615149

Accident Details

Date
Sunday, January 9, 1994
NTSB Number
ATL94LA037
Location
JASPER, AL
Event ID
20001206X00581
Coordinates
33.819469, -87.290702
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

LOSS OF ENGINE POWER FOR UNDETERMINED REASONS.

Aircraft Information

Registration
N14CL
Make
PIPER
Serial Number
28-7615149
Engine Type
Reciprocating
Model / ICAO
PA-28-151 P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
3015 CEDAR AVE S
Status
Deregistered
City
MINNEAPOLIS
State / Zip Code
MN 55407
Country
United States

Analysis

On January 9, 1994, at about 1330 central standard time, a Piper PA-28-151, N14CL, collided with trees during takeoff from Jasper, Alabama. The aircraft was operated by the pilot under 14 CFR part 91 and visual flight rules. A VFR flight plan had been filed for a cross-country flight to Huntsville, Alabama. The pilot had minor injuries, while the aircraft was substantially damaged. The flight was originating at the time of the accident.

The pilot reported what he believed to be a fouled spark plug which corrected itself during a normal engine run-up. Immediately following a normal takeoff roll and rotation, the aircraft lost power at approximately 200 feet AGL. One witness indicated that a puff of blue smoke emanated from the aircraft's exhaust immediately after power loss. On impact, the aircraft rotated 180 degrees and settled in the trees.

No malfunctions were found during an examination of the aircraft's engine. The engine's magnetos and leads to the spark plugs were tested and found operable. The induction system and air filter were found clear of foreign debris. The spark plugs were clean and of normal coloration in accordance with a spark plug test chart. Fuel in the aircraft was blue in color and free from water contamination. The carburetor was inspected and found to be in good operating condition. Compression tests on the engine revealed that compression ranged from 75-80/80 psi and all valves demonstrated freedom of movement.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL94LA037