N3689L

Substantial
Minor

BEECH 58PS/N: TJ-302

Accident Details

Date
Thursday, November 20, 2014
NTSB Number
CEN15LA053
Location
San Antonio, TX
Event ID
20141120X10212
Coordinates
29.320755, -98.470726
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The pilot’s improper decision to land long (past the midpoint) on a wet runway and his failure to conduct a go-around when the airplane did not touch down at the approach end of the runway, which resulted in an overrun.

Aircraft Information

Registration
N3689L
Make
BEECH
Serial Number
TJ-302
Engine Type
Reciprocating
Model / ICAO
58PB58T
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2

Registered Owner (Historical)

Name
DODSON INTERNATIONAL PARTS INC
Address
2155 VERMONT RD
Status
Deregistered
City
RANTOUL
State / Zip Code
KS 66079-9014
Country
United States

Analysis

On November 20, 2014, at 1252 central standard time, a Beech 58P, N3689L, landed long and went off the end of the runway at Stinson Municipal Airport (SSF), San Antonio, Texas. The pilot, the sole occupant on board, sustained minor injuries. The airplane was substantially damaged. The airplane was registered to and operated by the pilot under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Instrument meteorological conditions prevailed at the time of the accident, and an instrument flight rules flight plan had been filed. The flight originated from Wiley Post Airport (PWA), Oklahoma City, Oklahoma, at 1059, and was en route to SSF.At 1247, the pilot advised local control that he was 4 miles south of the airport and inbound on approach for landing. The controller instructed the pilot to circle and land on runway 14. He was given the wind conditions and told that there was "rain on the airport." A witness observed the airplane halfway down the runway and still airborne. The airplane touched down, ran off the end of the runway, and went through a barrier fence before coming to a stop on a service road. The left wing leading edge was crushed when it struck a fence post. The nose landing gear had collapsed.

The pilot told a Federal Aviation Administration inspector that his brakes had failed. The brakes were later tested and found to operate normally. Examination of the runway revealed evidence of hydroplaning.

One minute after the accident, the following weather observation was made at SSF: Wind, 270 degrees at 3 knots; visibility, 2 miles, heavy rain; ceiling, 1,600 feet overcast; temperature 18° Celsius (C.); dew point, 15° C.; altimeter, 30.06; Remarks, rain ended 5 minutes past the hour, rain began 49 minutes past the hour.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN15LA053