N1693A

Substantial
None

Piper PA-22-20S/N: 22-449

Accident Details

Date
Monday, July 1, 2002
NTSB Number
MIA02LA122
Location
Jacksonville, FL
Event ID
20020709X01069
Coordinates
30.218610, -81.876663
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The failure of the solo student/owner to maintain directional control of the airplane during takeoff in a crosswind, which resulted in the airplane veering off the runway, a collision with a runway light, and a ground loop.

Aircraft Information

Registration
Make
PIPER
Serial Number
22-449
Engine Type
Reciprocating
Year Built
1952
Model / ICAO
PA-22-20PA22
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
PA-22

Registered Owner (Current)

Name
HARP KENNETH F
Address
PO BOX 263
City
LAKE GENEVA
State / Zip Code
FL 32160-0263
Country
United States

Analysis

On July 1, 2002, about 1120, eastern daylight time, a Piper PA-22-20, N1693A, registered to and operated by a private individual as a Title 14 CFR Part 91 training flight, crashed during takeoff at Cecil Field, Jacksonville, Florida. Visual meteorological conditions prevailed and no flight plan was filed. The airplane incurred substantial damage, and the student-rated pilot and a commercial-rated flight instructor received no injuries. The flight originated from Herlong Airport, Jacksonville, Florida, the same day, about 1114.

The student pilot/owner stated that he possesses a current solo endorsement to operate the accident airplane, and that a flight instructor who had never received a tail wheel endorsement was with him in the airplane when the accident occurred. He further stated that he had performed a touch-and-go landing which had been uneventful, and as he was taking off, the airplane initially tracked along the centerline of the runway, but as it accelerated to about 45 or 50 knots it began to "weather vane" toward the right edge of the runway. He said he retarded the throttle to idle and applied left rudder control input, but rudder effectiveness was reduced and the airplane continued to veer to the right, where it collided with a runway edge light, swung around, and incurred damage to the left wing, left elevator, and horizontal stabilizer.

The flight instructor said that he also tried to apply rudder control input when the airplane started to veer from the centerline of the runway, but that the aircraft turned through an arc of 180 degrees within about 5 to 8 seconds, and his attempts to maintain directional control were unsuccessful.

Both occupants of the accident airplane said that prior to the accident there had been no mechanical failure or malfunction to the airplane or to any of its systems.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA02LA122