N6407N

Substantial
Serious

Cessna T210N S/N: 21062983

Accident Details

Date
Saturday, June 12, 1999
NTSB Number
MIA99LA174
Location
SENECA, SC
Event ID
20001212X19064
Coordinates
34.750621, -82.930198
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
3
Uninjured
2
Total Aboard
6

Probable Cause and Findings

The PIC's improper fuel management resulting in loss of engine power during approach to landing due to fuel starvation and the subsequent collision with trees and a residence during an emergency landing. Contributing to the accident was the PIC's failure to follow the airplane's inflight engine failure and before landing checklists.

Aircraft Information

Registration
N6407N
Make
CESSNA
Serial Number
21062983
Engine Type
Reciprocating
Model / ICAO
T210N C210
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
LEBOEUF DAVID
Address
309 EANES SCHOOL RD
Status
Deregistered
City
AUSTIN
State / Zip Code
TX 78746-6417
Country
United States

Analysis

On June 12, 1999, about 1806 eastern daylight time, a Cessna T210N, N6407N, registered to a private individual, operating as a Title 14 CFR Part 91 personal flight, crashed during descent for landing to Clemson-Oconee County Airport, Clemson, South Carolina. Visual meteorological conditions prevailed and the flight had cancelled their IFR flight plan at 1751. The aircraft sustained substantial damage and the commercial-rated pilot suffered minor injuries. One passenger suffered serious injuries, two passengers suffered minor injuries and two passengers suffered no injuries. The flight originated from Olive Branch, Mississippi, about 2 hours 29 minutes before the accident.

The pilot stated that as he raised the nose and applied power to level off his idle power descent, he got no engine response and switched fuel tanks from left tank to right tank. He did not regain engine power, and realizing he could not make his intended landing point, turned toward a private airstrip. He touched down about 20 degrees off runway heading, crossed the runway and adjacent taxiway, collided with trees and a residence.

According to an eyewitness, a pilot/mechanic watching from the window of his Eagle Ridge Airpark residence, he first sighted the airplane in a steep left bank, about 50 feet agl, landing gear and flaps down, windmilling propeller, attempting to line up on runway 23 of the private airpark. The airplane never did get lined up, touched down momentarily about a third of the way down the 2,100-foot asphalt runway, and exited the runway at about 30 degrees off centerline. The airplane left the runway, crossed a parallel taxiway, and collided with trees and the eyewitness' residence. The eyewitness ran to the accident site and began to assist. The left wing was torn off and there was no fuel contained in the ruptured left wing tank. There was no evidence of fuel contained in the left wing tank, precrash. The fuel selector was in the right tank position. Twelve gallons of fuel were removed from the right tank in 5-gallon containers.

According to FAA inspectors, the pilot had just cancelled his IFR flight plan and had called a visual to his landing airport when the engine quit. He switched fuel tanks, but could not get the engine restarted. The inspectors emphasized that the pilot's statement recounted that he did not change tanks until the engine quit. The pilot stated to the FAA inspectors that he uses the "GUMP" acronym for his "before landing checklist" memory jog instead of actual use of the Cessna checklist, i.e. "G" for gas, "U" for undercarriage, "M" for mixture, and "P" for prop. Subsequent examination of the wreckage by FAA inspectors revealed the airplane had sustained three definite and separate tree collisions; (1) left side of fuselage at the firewall area, (2) right wing about 3.5-feet from the tip and, (3) the left wing was separated at the wing root and the fuel tank had been breached and contained no fuel. There was no evidence from the foliage that the left wing tank contained fuel at the time of collision. The aircraft was equipped with an electronic fuel counter that senses fuel flow and reads out fuel remaining. Power was applied to the fuel counter and it indicated 13 gallons of fuel remaining. The engine was started on the airframe using the ship's own battery and fuel. Engine start was instantaneous and operation was smooth. High end rpm was not possible due to the bent propeller.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA99LA174