N8293G

Substantial
None

Cessna A188B S/N: 18801290T

Accident Details

Date
Thursday, June 5, 1997
NTSB Number
CHI97LA157
Location
LA MOURE, ND
Event ID
20001208X08074
Coordinates
46.370166, -98.280220
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

a loss of engine power for undetermined reasons and the pilot's failure to jettison the load. Factors involved were the exceeded weight and balance limits, and the pilot's inadequate preflight planning and preparation.

Aircraft Information

Registration
N8293G
Make
CESSNA
Serial Number
18801290T
Engine Type
Reciprocating
Year Built
1973
Model / ICAO
A188B C188
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
LUX DAVID J
Address
7517 97TH AVE SE
Status
Deregistered
City
LAMOURE
State / Zip Code
ND 58458-9000
Country
United States

Analysis

On June 4, 1997, at 1940 central daylight time (cdt), a Cessna A188B, N8293G, sustained substantial damage resulting from an inflight collision with the terrain, after takeoff from La Moure Rott Airport, La Moure, North Dakota. The pilot reported no injures. The 14 Part 137 agricultural flight was operating in visual meteorological conditions. No flight plan was on file. The flight departed La Moure, North Dakota at 1935 cdt, for a local aerial application flight.

In a written statement, the pilot stated that during the initial climb out, he noticed a developing power loss and was unable to maintain both airspeed and altitude. The pilot said he, "...lowered the nose of the airplane to regain airspeed, but keep losing airspeed so took a turn to the right to perform a forced landing into a corn field." During the landing roll the right main gear fractured, and the right wing tip made contact with the terrain. The airplane then nose over, coming to rest inverted.

Subsequently, after the accident, the pilot contacted the owner of the spraying company to retrieve him from the accident site. In a telephone conversation with the owner of the spraying company, he said "I think he [pilot] was operating behind the power curve, that's what it looks like to me." The owner also mentioned that the pilot didn't give him a clear statement on why he didn't jettison the load, but he confirmed that the release button and hopper seal were installed, calibrated, and fully operational before the accident.

An Airframe & Powerplant Mechanic (A&P) did an examination of the aircraft's engine, which showed that there was engine continuity, compression in all cylinders, positive fuel flow, and that all leads showed spark. There was evidence of a leak in the engine driven fuel pump. Further bench testing showed the leak did not hinder positive fuel pressure to the cylinders.

A Federal Aviation Administration (FAA) Inspector stated that the pilot was operating the airplane approximately 30 pounds over the specified max gross weight as determined in the Pilot's Operating Handbook.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI97LA157