N32411

Substantial
None

PIPER PA-28-151 S/N: 287515151

Accident Details

Date
Monday, January 16, 1995
NTSB Number
ATL95LA040
Location
ORANGE BEACH, AL
Event ID
20001207X02823
Coordinates
30.280870, -87.590934
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

A LOSS OF ENGINE POWER FOR UNDETERMINED REASONS.

Aircraft Information

Registration
N32411
Make
PIPER
Serial Number
287515151
Engine Type
Reciprocating
Year Built
1974
Model / ICAO
PA-28-151 P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
DOGGETT J EDWARD
Address
RT 2 BOX 131
Status
Deregistered
City
ARDMORE
State / Zip Code
AL 35739
Country
United States

Analysis

On January 15, 1995, at 1938 central standard time, a Piper PA-28-151, N32411, force landed in a swamp following an in flight loss of engine power near Orange Beach, Alabama. The commercial pilot and one passenger were not injured. The aircraft was substantially damaged. The aircraft was operated under the provisions of 14 CFR Part 91 by the pilot. Visual meteorological conditions existed at the time, and no flight plan was filed for the personal flight. The flight originated in Ft. Myers, Florida, at an undetermined time.

The pilot reported that he was switching fuel tanks prior to the visual approach to the Jack Edwards Airport in Gulf Shores, Alabama. After switching to the left fuel tank, which indicated 8 to 10 gallons of fuel, the engine "roughened up, and consequently quit." His altitude at the time was insufficient to make the runway, so he set up for a tree top landing. The aircraft impacted in a swampy area, coming to rest on its nose.

The aircraft was transported to a storage and salvage facility, where an engine inspection could be performed. There was evidence of fuel in both fuel tanks. The fuselage was secured, and the engine was test run on the airframe. The engine started on the first attempt. The electric boost pump operated satisfactorily. The engine was run for about 20 minutes, and the test run was terminated. Compression was observed on all cylinders, and both magnetos were operative.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL95LA040