N9583G

Destroyed
Serious

CESSNA A188B S/N: 18801545T

Accident Details

Date
Friday, July 8, 1994
NTSB Number
ATL94LA132
Location
TIFTON, GA
Event ID
20001206X01661
Coordinates
31.459693, -83.510101
Aircraft Damage
Destroyed
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

THE PILOT'S FAILURE TO FOLLOW THE AIRCRAFT CHECKLIST, RESULTING IN AN ATTEMPTED TAKEOFF WITH THE ELEVATOR TRIM IMPROPERLY SET. A FACTOR WAS THE TREES AT THE PERIMETER OF THE AIRSTRIP.

Aircraft Information

Registration
N9583G
Make
CESSNA
Serial Number
18801545T
Engine Type
Reciprocating
Model / ICAO
A188B C188
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
ROGERS GEORGE SAMUEL
Address
ROUTE #5 BOX 524
Status
Deregistered
City
TIFTON
State / Zip Code
GA 31794
Country
United States

Analysis

On July 8, 1994, at 1140 eastern daylight time, a Cessna A188B, N9583G, collided with trees and terrain during takeoff from a private, dirt airstrip near Tifton, Georgia. The aircraft was destroyed by impact forces and fire. The commercial pilot had serious injuries. The aircraft was operated under 14 CFR Part 137 by the pilot. Visual meteorological conditions existed at the time, and no flight plan was filed for the local, aerial application flight. The flight was originating at the time of the accident.

The pilot reported the following: He had loaded the hopper with water so that he could practice aerial application maneuvers. During the takeoff, the aircraft became airborne about 2/3 down the dirt runway. There was a gully located on the runway prior to the point of takeoff. The aircraft became airborne, then settled back down. He attempted to dump the load of water, however he did not gain sufficient altitude to clear perimeter trees. The aircraft contacted the trees, then crashed in an open field. The pilot did not report any loss of engine power.

Two inspectors with the Federal Aviation Administration visited the accident site and inspected the wreckage. There was evidence that four trees had been damaged about 40 feet above ground level. The wreckage was found in a cleared area, on a heading of about 090 degrees magnetic. The aircraft was almost consumed by fire after ground impact, with the empennage and engine sections remaining essentially intact. The throttle, mixture, and propeller controls were in the full forward position. Both propeller blades exhibited a wavy, or "s" curved appearance. An examination of the flight controls revealed that the elevator trim was in the full nose down position.

The limits for elevator trim tab travel are as follows:

Full tab up: 12 degrees above neutral (+/- 1 deg.)

Full tab down: 27 degrees below neutral (+/- 1 deg.)

Takeoff trim setting: Neutral.

In the "Normal Procedures" section of the aircraft checklist (Before Takeoff Checklist), the following step is included:

"9. Elevator Trim -- SET for takeoff."

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL94LA132