N4592M

Destroyed
Serious

THOMAS E. GEORGES Z-MAX S/N: 459

Accident Details

Date
Sunday, September 25, 1994
NTSB Number
CHI94DEV02
Location
PALMYRA, IL
Event ID
20001206X02189
Coordinates
39.429756, -89.989997
Aircraft Damage
Destroyed
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The pilots's inadvertently stalled the airplane while maneuvering to land. Factors were the loss of engine power due to carburetor ice, carburetor icing conditions, and the unavailability of carburetor heat.

Aircraft Information

Registration
N4592M
Make
THOMAS E. GEORGES
Serial Number
459
Engine Type
Reciprocating
Year Built
1947
Model / ICAO
Z-MAX BPAT
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
ROCKET CITY DUSTING SERVICE INC
Address
MUNICIPAL AIRPORT
Status
Deregistered
City
HUNTSVILLE
State / Zip Code
AL 35800
Country
United States

Analysis

HISTORY OF FLIGHT

On September 25, 1994, at 1337 central daylight time, an experimental Thomas E. Georges Z-Max, N4592M, operated by a private pilot on a pleasure flight, collided with terrain shortly after takeoff near Palmyra, Illinois. The airplane was destroyed and the pilot sustained serious injuries. Visual meteorological conditions prevailed for the 14 CFR Part 91 flight and no flight plan was filed.

The pilot reported that shortly after takeoff, while climbing through an altitude of approximately 150 feet, the engine lost power. He attempted to turn to pick a landing site. The airplane stalled and lost altitude.

METEOROLOGICAL INFORMATION

Visual meteorological conditions existed at the time of the accident. The temperature was 56 degrees and the dew point was 55 degrees. The carburetor icing probability chart contained in DOT/FAA/CT-82/44 specifies the potential for "serious icing at cruise power" under these conditions.

WRECKAGE AND IMPACT INFORMATION

Examination of the wreckage disclosed no evidence of preimpact malfunction. The left wing was shattered. The engine and firewall were torn from the fuselage. The fuselage center section was severely damaged.

The fuel tanks contained fuel. Fuel was found in the fuel lines, filter, and carburetor. The ground wire for the ignition unit was burned resulting in a "hot mag" condition. The ignition unit was examined and functioned normally during an operational test. Carburetor heating was not installed on the airplane. All engine and flight controls were intact.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI94DEV02