N6726G

Substantial
Minor

Cessna 150L S/N: 15072226

Accident Details

Date
Friday, July 23, 1999
NTSB Number
CHI99LA250
Location
UDALL, KS
Event ID
20001212X19209
Coordinates
37.380069, -97.110321
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
1
Total Aboard
2

Probable Cause and Findings

the failure of maintenance personnel to properly safety the aileron control cable during installation, the disconnected aileron control cable, and the unavailability of aileron control to the pilot.

Aircraft Information

Registration
N6726G
Make
CESSNA
Serial Number
15072226
Engine Type
Reciprocating
Year Built
1971
Model / ICAO
150L C150
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
REGISTRATION PENDING
Address
2533 N CARSON ST # A274
Status
Deregistered
City
CARSON CITY
State / Zip Code
NV 89706-0147
Country
United States

Analysis

On July 23, 1999, approximately 1730 central daylight time, a Cessna 150L, N6726G, piloted by a private pilot, sustained substantial damage when it impacted terrain, following a loss of aileron control after takeoff from the Cherokee Strip Airport near Udall, Kansas. The flight was conducted under the provisions of 14 CFR Part 91 and no flight plan had been filed. The pilot received minor injuries and his passenger received no injuries. The flight was originating from the Cherokee Strip Airport and was en route to Cook Airfield, Derby, Kansas.

In a written statement, the pilot said "all [of the aircraft] controls felt normal at the start of the takeoff roll." The pilot stated "after lift off the ailerons would not respond to control input." The pilot stated that he then reduced power to idle and applied left rudder in an attempt to maintain a level attitude. The pilot stated that he was unable to keep the wings level and the aircraft rolled slowly to the right and the right wing contacted the ground. The pilot stated that "the right wing always seemed heavy on this airplane."

A post accident examination of the aircraft was performed. The clevis bolt for the left aileron cable was not in place. No safety pin was located. There was scarring of the painted surface of the tubing forward of the clevis bolt location. No other anomalies were detected.

According to a Federal Aviation Administration inspector, the aileron cable had been replaced 14.5 operational hours prior to the accident flight.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI99LA250