N53109

Substantial
None

Cessna A188B S/N: 18801628T

Accident Details

Date
Tuesday, September 3, 1996
NTSB Number
MIA96LA225
Location
WINONA, MS
Event ID
20001208X06786
Coordinates
33.479225, -89.719779
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

improper maintenance of the airplane by the unqualified pilot/owner, by providing inadequate clearance between a flexible oil hose and a heat shield, which resulted in chafing of the hose, an oil leak, and subsequent oil starvation. A factor relating to the accident was: rough terrain in the emergency landing area.

Aircraft Information

Registration
N53109
Make
CESSNA
Serial Number
18801628T
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
UNKNOWN
Status
Deregistered
City
XXX
State / Zip Code
OK 73169
Country
United States

Analysis

On September 3, 1996, about 1230 central daylight time, a Cessna A188B, privately registered, experienced a loss of engine power and was substantially damaged during a forced landing near Winona, Mississippi. Visual meteorological conditions prevailed at the time and no flight plan was filed for the 14 CFR Part 137 aerial application flight. The commercial-rated pilot was not injured. The time of departure has not been determined.

The pilot/airplane owner stated to an FAA inspector that he had completed his spray operations and was returning to his base of operation when smoke entered the cockpit. He then reduced power and the smoke dissipated, but when he reapplied power the engine did not respond. He landed in a cotton field and after touchdown with obstructions ahead, he attempted to maneuver to avoid the obstructions. The left main landing gear traveled into a depression separating the landing gear wheel, and the airplane then nosed up and came to rest upright.

Examination of the airplane revealed oil externally on the fuselage and in the engine compartment area. Examination of the engine compartment revealed a hole chaffed in a flexible hose from the outlet of the oil cooler. Only 2 quarts of oil registered on the oil dipstick. The oil capacity of the engine is 12 quarts.

The airplane owner/pilot stated that he is not an airframe or powerplant mechanic and he had about 2 or 3 weeks before the accident, repaired engine baffling located on the right forward side of the engine. This required loosening of "B" nuts at the engine crankcase for the inlet and outlet hoses to and from the oil cooler. After tightening of the "B" nuts for the hoses following repair to the baffle, the outlet hose was too close to a heat shield between the engine exhaust for cylinder Nos. 1, 3, and 5. The owner/pilot also stated that he performed the repair after the annual inspection which was performed on March 14, 1996. The airplane had been operated for about 50 hours since the repair to the baffle.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA96LA225