N9542J

Substantial
None

Cessna 188 S/N: T18803820T

Accident Details

Date
Wednesday, July 10, 1996
NTSB Number
CHI96LA232
Location
INDEPENDENCE, IA
Event ID
20001208X06171
Coordinates
42.460784, -91.890800
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

the delayed jettison of the dry chemicals by the pilot. The inability of the airplane to climb was a related factor.

Aircraft Information

Registration
N9542J
Make
CESSNA
Serial Number
T18803820T
Engine Type
Reciprocating
Year Built
1981
Model / ICAO
188 C188
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
5110 POPLAR AVE STE 2610
Status
Deregistered
City
MEMPHIS
State / Zip Code
TN 38117-7607
Country
United States

Analysis

On July 10, 1996, at 0700 central daylight time (cdt), a Cessna 188, N9542J, was substantially damaged when the airplane impacted with terrain approximately two miles north of the Independence Airport, Independence, Iowa. The airplane was loaded with dry insecticide, and insecticide was found on the ground just prior to the first impact point. The commercial rated pilot was uninjured in the accident. Visual meteorological conditions prevailed at the time of the 14 CFR part 137 flight, and no flight plan had been filed.

The pilot reported on NTSB form 6120.1/2 that at takeoff, the airplane had 1,200 pounds of dry chemicals, and 240 pounds of fuel on board. The pilot reported that after takeoff, the airplane would not gain airspeed or altitude, and never left ground effect. The pilot reported that on the previous day the temperatures were higher, and with the same load as the accident flight the airplane operated with no difficulties.

After the accident no abnormalities were noted with the airframe or the engine. All engine controls were found attached, and all cylinders had compression when the crankshaft was rotated. The magneto's appeared to operate normally when checked, and when the oil filter was cut open no visible contamination was found. The turbocharger turbine wheel rotated freely after the accident. The air induction system to the engine was compromised. The rudder and elevator controls cables were still attached. The aileron cables were separated from the aileron, and showed signs similar to an overload failure. The airplane's hopper was compromised, and the dry chemicals were not weighed following the accident.

The airplane's left wing, landing gear and engine were separated from the fuselage of the airplane, during the accident.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI96LA232