N2804T

Substantial
Minor

PIPER PA28S/N: 28-7225235

Accident Details

Date
Tuesday, August 15, 2017
NTSB Number
ERA17LA277
Location
Canton, GA
Event ID
20170815X75032
Coordinates
34.312221, -84.422225
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
2
Uninjured
0
Total Aboard
2

Probable Cause and Findings

Maintenance personnel's failure to ensure the proper throttle linkage travel clearance after the installation of an exhaust system.

Aircraft Information

Registration
N2804T
Make
PIPER
Serial Number
28-7225235
Engine Type
Reciprocating
Year Built
1972
Model / ICAO
PA28P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
PARRIS AVIATION LLC
Address
4719 BALL GROUND HWY
Status
Deregistered
City
BALL GROUND
State / Zip Code
GA 30107-4503
Country
United States

Analysis

On August 15, 2017, about 1635 eastern daylight time, a Piper PA-28-140, N2804T, was substantially damaged during a forced landing after takeoff from the Cherokee County Airport (CNI), Canton, Georgia. The flight instructor and student pilot sustained minor injuries. The instructional flight was conducted under the provisions of Title 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed and no flight plan was filed for the local flight.According to the flight instructor, after an uneventful engine run-up, they taxied to the active runway for takeoff. As the takeoff roll commenced, he noted that the airplane felt "sluggish." He asked the student pilot if he had his foot on the brakes, and the student pilot replied "no." The flight instructor checked the throttle and airspeed and noted that the throttle was full forward and the airspeed was increasing slowly. Once the airplane reached 75 knots, the airplane lifted off the runway and began to climb. The climb appeared normal for approximately the first 200 ft. Then, the flight instructor noticed that the airspeed was decreasing but the engine never stopped. He took over the flight controls and elected to perform an emergency landing in a wooded area.

Examination of the wreckage by a Federal Aviation Administration (FAA) inspector revealed that both wings separated from the fuselage and the fuselage of the airplane was buckled. A post-crash fire ensued within the engine cowling and spread to the cockpit. An examination of the engine revealed that the carburetor throttle linkage was striking against the exhaust heat shield. This prevented the carburetor throttle linkage from its full movement at full throttle. A review of the maintenance logbooks revealed that on July 28, 2017, a Power Flow exhaust system was installed on the engine. The airplane accumulated about 6 hours of flight time prior to the accident event.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA17LA277