N6905M

Substantial
None

Stinson 108-3 S/N: 108-4905

Accident Details

Date
Saturday, May 6, 2000
NTSB Number
FTW00LA139
Location
SOCORRO, NM
Event ID
20001212X20991
Coordinates
34.049167, -106.899337
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 during the aborted takeoff, which resulted in an inadvertent groundloop.

Aircraft Information

Registration
Make
STINSON
Serial Number
108-4905
Engine Type
Reciprocating
Model / ICAO
108-3 S108
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
108-3

Registered Owner (Current)

Name
MARQUARDT JOHN WAYNE
Address
120 LANE 102 CROOKED LK
City
ANGOLA
State / Zip Code
IN 46703-9150
Country
United States

Analysis

On May 6, 2000, at 1300 mountain daylight time, a Stinson 108-3, tailwheel equipped airplane, N6905M, groundlooped during an aborted takeoff at the Socorro Municipal Airport, near Socorro, New Mexico. The airplane was owned and operated by the pilot under 14 Code of Federal Regulations Part 91. The commercial pilot, sole occupant, was not injured, and the airplane sustained substantial damage. Visual meteorological conditions prevailed for the planned cross-country flight, and a flight plan was not filed. The flight was originating at the time of the accident.

The pilot reported that he was flying the airplane from the state of California to the state of Michigan. The previous leg of the flight was from Cottonwood, Arizona, to Socorro. After refueling at Socorro, the pilot aborted the first takeoff on runway 24 because he felt that the engine was not developing power. Subsequently, he "taxied the airplane to runway 15, leaned the engine for the density altitude conditions, and initiated the takeoff roll on the 5,800-foot runway." On the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2), the pilot stated that he "determined [he] wasn't going to develop adequate speed for takeoff." He aborted the second takeoff; however, he "couldn't control the aircraft to a straight stop." The airplane veered off the right side of runway 15 and groundlooped. The left wing spars and the left wing strut attachment point sustained structural damage. The propeller, engine cowling, and tailwheel spring were damaged.

The pilot reported the wind from 210 degrees at 7 knots and a temperature of 91 degrees Fahrenheit. At 1256, the surface weather observation facility at Albuquerque, New Mexico, (60 nautical miles south of Socorro) reported the wind from 280 degrees at 16 knots gusting to 21 knots, temperature at 29 degrees centigrade (84.2 degrees Fahrenheit), and an altimeter setting of 30.04 inches Mercury. The density altitude was calculated as 8,000 feet.

The FAA inspector examined the airplane at the accident site. No mechanical discrepancies were found that would have contributed to the accident.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW00LA139