N4721K

Substantial
None

Cessna 182P S/N: 18263720

Accident Details

Date
Friday, March 2, 2001
NTSB Number
FTW01LA074
Location
Tuttle, OK
Event ID
20010307X00559
Coordinates
35.289554, -97.750396
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

fuel exhaustion due to a loose fuel cap as a result of the pilot's inadequate preflight. A contributory factor was the lack of suitable terrain for the forced landing.

Aircraft Information

Registration
N4721K
Make
CESSNA
Serial Number
18263720
Engine Type
Reciprocating
Year Built
1975
Model / ICAO
182P C182
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
KREMMLING FLG INC
Address
P O BOX 97
Status
Deregistered
City
DILLON
State / Zip Code
CO 80435
Country
United States

Analysis

On March 2, 2001, at 1545 central standard time, a Cessna 182P single-engine airplane, N4721K, was substantially damaged during a forced landing following a loss of engine power near Tuttle, Oklahoma. The private pilot, sole occupant of the airplane, was not injured. The airplane was registered to and operated by Kremmling Flying, Inc., of Kremmling, Colorado. Visual meteorological conditions prevailed and a visual flight rules flight plan was filed for the 14 Code of Federal Regulations Part 91 personal flight. The airplane departed Kremmling, Colorado, at 1045 mountain standard time, and was destined for the University of Oklahoma Westheimer Airport near Norman, Oklahoma.

The pilot stated that prior to takeoff, both fuel tanks were topped off. Approximately 15 miles from the intended destination, at 3,500 feet msl, the engine RPM began to decrease. The pilot pulled the carburetor heat ON, and the "RPMs picked back up." Approximately 10 seconds later, the engine RPM started to decrease again. The pilot adjusted the mixture control, applied full propeller RPM, and repositioned the fuel selector, in an attempt to regain engine power; however, no change in engine power was noted. The pilot contacted the Westheimer control tower and declared an emergency. With the propeller windmilling, the pilot executed a forced landing to a field. During the touchdown, the nose landing gear contacted a "drainage terrace," and the airplane nosed over and came to rest inverted.

According to an FAA inspector, who responded to the accident site, after the airplane was turned upright, the right fuel tank was found empty, and the left fuel tank contained residual fuel. The right fuel cap was found unlocked and hanging out of the fuel cell by its retaining chain.

The pilot reported that the airplane was equipped with long-range 88-gallon capacity fuel tanks and had an endurance of approximately 6 hours and 45 minutes of flight time. The pilot stated that some of the fuel may have been syphoned out of the fuel tank due to a loose fuel cap.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW01LA074