N7799H

Substantial
None

Piper PA-12 S/N: PA-12-696

Accident Details

Date
Saturday, July 5, 1997
NTSB Number
ATL97LA098
Location
SWANSBORO, NC
Event ID
20001208X08293
Coordinates
34.690830, -77.119049
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot's failure to maintain directional control. A factor was the gusting winds.

Aircraft Information

Registration
N7799H
Make
PIPER
Serial Number
PA-12-696
Engine Type
Reciprocating
Year Built
1946
Model / ICAO
PA-12 PA12
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
PEACOCK ENTERPRISES INC
Address
302 SILVER CREEK LANDING
Status
Deregistered
City
SWANSBORO
State / Zip Code
NC 28584
Country
United States

Analysis

On July 5, 1997, at 1500 eastern daylight time, a Piper PA-12, N7799H, veered off the right side of runway 23 during an attempted takeoff, and collided with an embankment at a private airstrip in Swansboro, North Carolina. The banner tow flight operated under the provisions of Title 14 CFR Part 91 with no flight plan filed. Visual weather conditions prevailed at the time of the accident. The airplane sustained substantial damage. The rated pilot was not injured. The local flight departed Swansboro, North Carolina, at approximately 0900.

The pilot reported that they had a busy morning and afternoon of banner activity. On this leg of the operation, he dropped the banner as normal, and returned to the airstrip for a normal landing. The airplane touched down at the mid-field point of the 2400 foot long sod strip. After rolling several hundred feet, the airplane started drifting right of the centerline. As the airplane neared the edge of the runway, the pilot advanced the throttle and attempted a takeoff. The airplane continued off the right side of runway 23 and collided with an embankment. According to the pilot, he experienced gusting winds during the attempted landing.

During the examination of the airframe, corrosion was found on the right landing gear strut. A review of the aircraft records also showed previous corrosion on the left landing gear strut. The landing assembly remained intact throughout the landing roll on the runway. The left main landing gear was torn from the airframe after the airplane departed the runway surface. The examination of the brake system failed to disclose a mechanical malfunction or component failure. The pilot did not report a mechanical problem with the airplane.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL97LA098