N731PS

Substantial
Serious

CESSNA 188 S/N: 18803053

Accident Details

Date
Saturday, October 1, 1994
NTSB Number
ATL95LA002
Location
COVINGTON, TN
Event ID
20001206X02378
Coordinates
35.560199, -89.640792
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The pilot's failure to maintain directional control during landing.

Aircraft Information

Registration
N731PS
Make
CESSNA
Serial Number
18803053
Engine Type
Reciprocating
Model / ICAO
188 C188
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
MID-CONTINENT AIRCRAFT CORPORATION
Address
PO BOX 540
Status
Deregistered
City
HAYTI
State / Zip Code
MO 63851-0540
Country
United States

Analysis

On October 1, 1994, about 1700 central daylight time, a Cessna 188, N731PS, groundlooped during the landing roll at Covington, Tennessee. The airplane was operated by Baker Flying Service under the provisions of 14 CFR Part 137, and visual flight rules. Visual meteorological conditions prevailed. A flight plan was not filed for the aerial application flight. There were serious injuries to the commercial pilot, and the airplane was substantially damaged. Origination of the flight was Covington, Tennessee, about 1615.

The pilot reported that the airplane veered left during the landing and that the right rudder pedal and brake did not operate to oppose the divergent ground path. An inspector from the Tennessee Flight Standards District Office, Memphis, Tennessee, spoke with the pilot, and examined the accident site and the airplane, after the accident. He reported that the pilot said he was attempting to land on the runway, and overshot it. The airplane landed in the grass beside the runway. Tire tracks showed a normal landing roll, until about the last 700 feet where the tracks showed the airplane veered left, then entered a skid, breaking off the right main landing gear at the attachment point. The right wing then, struck the ground. According to the inspector, the rudder pedal, rudder cable, and rudder functioned. The brake pad did not exhibit excessive wear and the hydraulic line did not exhibit any pre-impact failure.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL95LA002