N53198

Substantial
None

Cessna A188B S/N: 18801677T

Accident Details

Date
Saturday, June 19, 1999
NTSB Number
ATL99LA101
Location
GLEN ALLAN, MS
Event ID
20001212X18926
Coordinates
34.849689, -88.380287
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The improper installation of a nut and bolt assembly by a maintenance personnel that resulted in the in-flight loss of control of the left ailiron.

Aircraft Information

Registration
N53198
Make
CESSNA
Serial Number
18801677T
Engine Type
Reciprocating
Year Built
1974
Model / ICAO
A188B C188
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
NONE
Status
Deregistered
City
XXX
State / Zip Code
OK 73125
Country
United States

Analysis

On June 19, 1999, at 1400 central daylight time, a Cessna A188B, N53198, collided with the ground during a forced landing near Glen Allan, Mississippi, following an in-flight malfunction of the aileron control system. The business flight was operated by the pilot under the provisions of Title 14 CFR Part 91 with no flight plan filed. Visual meteorological conditions prevailed at the time of the accident. The airplane sustained substantial damage and the commercial pilot was not injured. The flight initially departed Glen Allan, Mississippi, at 1355.

The pilot reported that, while surveying a field for future work, the airplane became uncontrollable when the ailerons malfunctioned. The pilot selected an emergency landing area, and made a forced landing in a field. The airplane sustained structural damage during the forced landing when the left wing collided with the ground, and the airplane cartwheeled.

During the examination of the airplane, the pilot reported that the left aileron control bolt had separated from the control surface. When the left aileron was removed from the airframe the missing bolt was recovered from the inter-structure of the wing area. The bolt was reinstalled through the aileron assembly, and appeared to provide enough thread material to secure the aileron assembly. The examination of the bolt assembly also disclosed that the bolt that connects the forward end of the control rod to the bell crank was too short and did not protrude through the nylon lock on the nut. The rod-end bearing was also seized and would not move.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL99LA101