N5433

Substantial
None

Curtis-Travel Air 4000S/N: 522

Accident Details

Date
Friday, August 3, 2001
NTSB Number
FTW01LA173
Location
Morrilton, AR
Event ID
20010808X01640
Coordinates
35.150577, -92.739822
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

the pilot's failure to maintain aircraft control during takeoff. Contributing factors were the pilot's lack of experience in the accident airplane, and the rough/uneven runway.

Aircraft Information

Registration
Make
CURTIS-TRAVEL AIR
Serial Number
522
Engine Type
Reciprocating
Year Built
1928
Model / ICAO
4000TVL4
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
3
FAA Model
4000

Registered Owner (Current)

Name
DAVID LEE BRADLEY PRODUCTIONS INC
Address
33133 VISTA DEL MONTE
City
TEMECULA
State / Zip Code
CA 92591-4949
Country
United States

Analysis

On August 3, 2001, at 0830 central daylight time, a Curtis-Travel Air 4000 vintage bi-plane, N5433, was substantially damaged following a loss of engine power during takeoff from a private grass airstrip near Morrilton, Arkansas. The airplane was owned and operated by a private individual. The airline transport pilot and his two passengers, one of whom was the owner, were not injured. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 positioning flight. The cross-country flight was originating at the time of the accident from the Hetrick Ranch Turf Strip, and was destined for McAlester, Oklahoma.

The day prior to the accident, the pilot received flight training and a checkout in the accident airplane at Dennis F Cantrell Field Airport in Conway, Arkansas, from the airplane's previous owner, who was a certificated flight instructor. Due to mechanical problems, the pilot and previous owner flew the airplane back to the previous owner's ranch grass strip to make repairs.

The morning of the accident, the pilot calculated the weight and balance of the airplane to be 40 pounds under maximum gross weight. The airplane's new owner, who did not hold a certificate to act as a pilot-in-command, and his son occupied the two front seats. The pilot occupied the rear seat.

During the takeoff roll, at 50-60 knots, the pilot raised the tail to a takeoff attitude. The right main landing gear hit a bump, the airplane became airborne and banked left. The pilot over corrected back to the right, and the right wingtip hit the ground. The right wingtip drug along the ground, which "caused a directional change to the right," and the airplane went through a barbed wire fence. The pilot "chopped power" to abort the takeoff, and the airplane "pan caked in from about 8 feet," separating the main landing gear. The airplane slid forward, and the left wing struck a "large heavy steer handling implement." The airplane then pivoted to the left impacting a fence post with the right wing before coming to rest upright.

Examination of the airplane by the FAA inspector, who responded to the accident, revealed that the upper and lower wings sustained structural damage.

As of the day of the accident, the pilot had logged a total flight time of 2300 hours of which 500 hours were in tail-wheel equipped airplanes. The pilot had 0.6 hours in the accident airplane.

At 0853, the weather observation facility at the Little Rock International Airport, Little Rock, Arkansas, located 37 nautical miles southeast of the accident site, reported the wind from 210 degrees at 5 knots, visibility 7 statute miles, few clouds at 25,000 feet, temperature 88 degrees Fahrenheit, dew point at 66 degrees Fahrenheit, and an altimeter setting of 30.13 inches of Mercury.

The pilot estimated the wind to be from 190-210 degrees at less than 5 knots at the time of 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# FTW01LA173