N3221X

Substantial
Serious

MITCHELL AIRCRAFT CORP T-10S/N: 101

Accident Details

Date
Tuesday, July 24, 2001
NTSB Number
ATL01LA091
Location
ASHLAND CITY, TN
Event ID
20010731X01562
Coordinates
36.299999, -87.066665
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
2
Minor Injuries
0
Uninjured
0
Total Aboard
2

Probable Cause and Findings

The restricted movement of the rudder cable, resulting in a loss of control and collision with trees.

Aircraft Information

Registration
N3221X
Make
MITCHELL AIRCRAFT CORP
Serial Number
101
Year Built
1984
Model / ICAO
T-10

Registered Owner (Historical)

Name
SALE REPORTED
Address
XXX
Status
Deregistered
City
OKLAHOMA CITY
State / Zip Code
OK 73125
Country
United States

Analysis

On July 23, 2001, at 1910 central daylight time, a Mitchell Aircraft Corporation T-10, N3221X, collided with trees during an uncommanded roll after takeoff from a private grass strip, near Ashland City, Tennessee. The personal flight was operated by the pilot under the provisions of Title 14 CFR Part 91 with no flight plan filed. Visual weather conditions prevailed at the time of the accident. The commercial rated, aerobatic Certified flight instructor (CFI), and his passenger received serious injuries, and the airplane was destroyed. The flight departed the private airstrip at Ashland City, Tennessee, at 1905.

According to the CFI, after takeoff from the private grass strip, the CFI reported the airplane developed an " extreme vibration". He retarded the throttle and the vibration diminished. When the CFI banked the airplane to return to the private grass strip, the left wing dropped excessively. As engine power was increased to maintain a climb, the airplane made an uncommaded roll and began descending. The airplane collided with trees during the uncontrolled descent and impacted the ground.

The post-impact examination of the airplane showed that the left rudder cable had binded in the in the wing and the left rudder would travel about half the normal distance. According to the CFI, during normal operation, the rudder assemblies are returned to the neutral position by spring action; the rudder assembly is designed to move in only one direction. The examination also showed that the outer half of both wing assemblies was destroyed. The wing design has the rudder assemblies installed vertically on the wing tips. The examination also nation of the airplane revealed the aileron stabilator and rudder were completely destroyed.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL01LA091