N2420R

Substantial
None

Cessna 182GS/N: 18255520

Accident Details

Date
Saturday, September 8, 2007
NTSB Number
SEA07LA255
Location
Fairfield, ID
Event ID
20070911X01380
Coordinates
43.350353, -114.979866
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The loss of engine power as a result of fuel exhaustion due to the pilot's inadequate preflight inspection. Contributing to the accident was the lack of suitable terrain for the forced landing.

Aircraft Information

Registration
N2420R
Make
CESSNA
Serial Number
18255520
Engine Type
Reciprocating
Year Built
1964
Model / ICAO
182GC182
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
PACIFIC AEROMOTIVE CORPORATION
Address
PO BOX 450
Status
Deregistered
City
ERIE
State / Zip Code
CO 80516-0450
Country
United States

Analysis

On September 8, 2007, about 0900 mountain daylight time, a Cessna 182G, N2420R, sustained substantial damage during a forced landing following a loss of engine power approximately 20 miles north of Fairfield, Idaho. The private pilot and the passenger were not injured. The pilot was operating the airplane as a 14 CFR Part 91 personal flight. Visual meteorological conditions prevailed and no flight plan was filed for the local flight that departed from Twin Falls, Idaho, about 0700.

According to the pilot, the purpose of the flight was to spot elk. During his pre-flight inspection, he did not visually check the quantity of fuel in the airplane's tanks. He stated that he had filled the airplane with fuel two days prior to the day of the accident. He further stated that at the time of takeoff, both tanks registered full on the fuel gauges. Approximately 2 hours into the flight, the engine lost power, and the pilot executed a forced landing to a clearing filled with sand, gravel and brush. During the landing roll, the nose wheel sank into the sand, and the nose landing gear separated. The airplane sustained damage to the firewall and to the bottom fuselage structure.

An FAA inspector examined the airplane at the accident site and found no fuel in either the left or right fuel tank or in the header tank just forward of the firewall. Additionally, no fuel was present at the fuel injector spider on top of the engine. The inspector noted no evidence of fuel leakage onto the ground at the accident site or on the outer skins of the airplane. When power was applied, the fuel gauges indicated empty.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA07LA255