N21306

Substantial
Serious

Cessna 182 PS/N: 182-61550

Accident Details

Date
Monday, April 2, 2001
NTSB Number
ATL01LA045
Location
KENNESAW, GA
Event ID
20010405X00699
Coordinates
33.989536, -84.650733
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The loss of engine power for undetermined reasons. Conditions for carburetor icing were present at the time of the accident.

Aircraft Information

Registration
N21306
Make
CESSNA
Serial Number
182-61550
Engine Type
Reciprocating
Year Built
1972
Model / ICAO
182 PC182
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
VX REALTY INC
Address
2774 COBB PKWY NW STE 109-327
Status
Deregistered
City
KENNESAW
State / Zip Code
GA 30152-3469
Country
United States

Analysis

On April 2, 2001, at 1715 eastern daylight time, a Cessna 182P, N21306, collided with the ground 1500 feet from the departure end of runway 27 at McCullum Field in Kennesaw, Georgia. The personal flight was operated by the pilot under the provisions of Title 14 CFR Part 91, with no flight plan filed. Visual weather conditions prevailed at the time of the accident. The pilot received serious injuries at the time of the accident and the airplane was substantially damaged. The flight departed Kennesaw, Georgia, at 1714.

Reportedly, the pilot was conducting touch and go landings, and was executing the climb out phase of the procedure. According to air traffic control, during the initial climb out from runway 27, the pilot reported an unspecified engine problem. The airplane collided with the ground in a nose low attitude and flipped inverted.

Examination of the airframe assembly failed to disclose a mechanical malfunction or component failure. Examination of the engine assembly disclosed that the fuel recovered in the carburetor bowl was brownish in color. The fuel grade and type was not determined. During the subsequent examination, necessary repairs were made to the engine assembly to facilitate a functional check. The engine operated normally up to 2000 rpm during the functional check. The engine ran smooth with no anomalies noted. The entire run was approximately ten minutes in duration. After the engine run-up, the oil sump was removed and inspected, and it was noted that there were pieces of metal found in the sump. The pieces of metal were identified as the oil control ring expander coil. A review of recovered weather data showed that weather conditions at the time of the accident were favorable for carburetor icing conditions.

Reportedly, the airplane had recently undergone a pre-purchase inspection. A review of the inspection findings showed that there were approximately 60 maintenance related write-ups which included water in fuel tanks. A review of the airplane and engine maintenance logs revealed that the engine had a total of 3,277 hours and 1,676.99 hours since the last major overhaul. The last annual inspection was completed on February 1, 2001 at 2463.2 airframe hours.

The pilot was hospitalized after the accident and was placed in intensive care. On May 26, 2001, the pilot passed as a result of the serious injuries sustained in 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# ATL01LA045