N2342T

Substantial
None

Piper PA-28-180S/N: 28-7105211

Accident Details

Date
Monday, September 29, 2003
NTSB Number
ATL03LA148
Location
Talladega, AL
Event ID
20031128X01961
Coordinates
33.569721, -86.050834
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

The pilot's failure to use carburetor heat when weather conditions were favorable for carburetor icing.

Aircraft Information

Registration
N2342T
Make
PIPER
Serial Number
28-7105211
Engine Type
Reciprocating
Year Built
1971
Model / ICAO
PA-28-180P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
166 FIFTH AVE HANGER 173
Status
Deregistered
City
GREENVILLE
State / Zip Code
MS 38703
Country
United States

Analysis

On September 28, 2003, at 2039 central daylight time, a Piper PA28-180, N2342T, registered to Scott's Auto Country and operated by a private pilot, collided with the ground during take-off climb at Talladega Municipal Airport, Talladega, Alabama. The personal flight was operated under the provisions of Title 14 Part 91 with no flight plan. Visual condition prevailed at the time of the accident. The airplane sustained substantial damage, and the pilot and two passengers were not injured. The flight departed Talladega Municipal Airport, Alabama on September 28, 2003, at 2030.

According to the pilot, the airplane had been taxing for an hour and a half at idle speed. When the airplane was cleared for take-off, the take-off acceleration seemed "sluggish". The airplane reached 65 knots, and the airplane rotated for climb-out. During climb-out the engine miss-fired, and an emergency transmission was made to the control tower. The airplane climbed approximately 200 feet, and the engine quit. The pilot lowered the nose of the airplane and conducted an emergency landing on runway 21. The airplane landed on the runway and rolled off the overrun. The pilot secured the airplane and instructed the passengers to exit.

Examination of the airplane revealed spar damage on the left and right wing assemblies. The fuselage was buckled and the main landing gear was sheared off. All flight control surfaces were examined and found to been operating correctly. A run-up of the engine was conducted, and the engine normally up to 800 rpm. The propeller was bent and a higher rpm was not attainable.

Review of the Piper Cherokee pilot's operating handbook, section: Warm-up and Ground Check, (Carburetor heat should also be checked prior to take-off to be sure that the control is operating properly, and to clear any ice which may have formed during taxiing). A review of weather data, at the time of the accident, disclosed that conditions were favorable for the formation of carburetor ice. The pilot did not report checking carburetor heat following the long period of ground operation.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL03LA148