N9247R

Substantial
None

Cessna 188B S/N: 18802185T

Accident Details

Date
Saturday, July 11, 1998
NTSB Number
CHI98LA245
Location
ATLANTA, NE
Event ID
20001211X10498
Coordinates
40.359077, -99.469436
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 due to a loose 'B' nut on the fuel line fitting. Contributing to the accident was the inadequate maintain and the soft terrain.

Aircraft Information

Registration
N9247R
Make
CESSNA
Serial Number
18802185T
Engine Type
Reciprocating
Year Built
1975
Model / ICAO
188B C188
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
KRECH DAKOTA AIRSPRAY INC
Address
PO BOX 648
Status
Deregistered
City
HURON
State / Zip Code
SD 57350-0648
Country
United States

Analysis

On July 11, 1998, at 1600 central daylight time, a Cessna 188B, N9247R, piloted by a commercial pilot, sustained substantial damage when it impacted the terrain, following a loss of engine power while maneuvering, near Atlanta, Nebraska. Visual meteorological conditions prevailed at the time of the accident. The 14 CFR Part 91 maintenance flight was not operating on a flight plan. The pilot reported no injuries. The flight departed a private airstrip near Atlanta, Nebraska, for a sprayer calibration test flight, at 1545.

According to the pilot's written statement, the pilot was performing a sprayer calibration test when the engine suffered a substantial loss of power. The pilot was operating at approximately 50 feet above ground level (agl) at the time of the power loss. The pilot stated that he was at too low of an altitude to trouble shoot the power loss and maneuvered the aircraft into an open field. Upon touch down the left main gear dug into the soft mud, collapsed the left main gear, which resulted in the left wing impacting the terrain. The pilot stated that the aircraft rotated about the left wing, approximately 80-degrees, and then came to a stop.

Post accident investigation revealed that the engine would not sustain power at idle or any power setting with the fuel boost pump in the "Off " position. Investigation of the fuel system revealed that the "B" nut on the fuel line from the firewall to the back of the engine was loose. After the nut had been tightened the engine preformed, without hesitation, at all power settings with the fuel pump in the "Off" position. No other aircraft or engine anomalies were found.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI98LA245