N64592

Destroyed
Minor

Evans Aircraft VARIEZE S/N: 01

Accident Details

Date
Sunday, December 10, 2000
NTSB Number
FTW01LA034
Location
INGLESIDE, TX
Event ID
20010114X00298
Coordinates
27.869222, -97.199829
Aircraft Damage
Destroyed
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

the loss of control during takeoff initial climb due to the binding rudder, which restricted the pilot's control of the aircraft.

Aircraft Information

Registration
N64592
Make
EVANS AIRCRAFT
Serial Number
01
Engine Type
Reciprocating
Model / ICAO
VARIEZE VP2
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
13926 WINDJAMMER DR
Status
Deregistered
City
CORPUS CHRISTI
State / Zip Code
TX 78418-6146
Country
United States

Analysis

On December 9, 2000, at 1800 central standard time, an Evans Varieze homebuilt experimental airplane, N64592, was destroyed when it impacted terrain following a loss of control during the initial takeoff climb at the T. P. McCambell Airport, near Ingleside, Texas. The airplane was owned and operated by the pilot under 14 Code of Federal Regulations Part 91. The commercial pilot, sole occupant, received minor injuries. Night visual meteorological conditions prevailed for the personal flight, and a flight plan was not filed. The flight originated from the Corpus Christi International Airport, Corpus Christi, Texas, at an unknown time.

The pilot reported to local authorities and the FAA inspector who responded to the site, that while in the traffic pattern, during the turn from upwind to crosswind, full opposite rudder would not overcome an uncommanded roll to the left, which continued until the left wing struck the ground. The airplane came to rest in brushy terrain, approximately 100 yards east of runway 13.

The FAA inspector examined the aircraft and found extensive structural damage throughout the airplane. He established flight control continuity with all linkages, push/pull rods, and bellcranks. He observed that paint was missing from the rear edge of the rudder control arm, and manual movement of the rudder against the centering spring resulted in the cable eye hooking itself behind the rudder control arm.

The last condition inspection was performed on September 8, 2000, at a total airframe time of 2,173.6 hours. The pilot estimated that the airplane had accumulated 26 hours of flight time since the last condition inspection.

Numerous attempts to obtain a completed Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2) from the pilot were unsuccessful.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW01LA034