N8240U

Substantial
Serious

Beech A36S/N: E-2665

Accident Details

Date
Friday, January 23, 2004
NTSB Number
DEN04LA040
Location
Farmington, NM
Event ID
20040202X00139
Coordinates
36.750530, -108.179115
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

the pilot's improper in-flight planning/decision making and his failure to maintain adequate airspeed which resulted in fuel starvation/exhaustion and a stall spin.

Aircraft Information

Registration
N8240U
Make
BEECH
Serial Number
E-2665
Engine Type
Reciprocating
Year Built
1991
Model / ICAO
A36BE36
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SAN JUAN PILOT TRAINING INC
Address
1296 W NAVAJO ST
Status
Deregistered
City
FARMINGTON
State / Zip Code
NM 87401-5400
Country
United States

Analysis

On January 22, 2004, at approximately 1916 mountain standard time, a Beech A36, N8240U, was substantially damaged when it impacted a building following a loss of engine power and subsequent forced landing during a visual approach to Four Corners Regional Airport (FMN), Farmington, New Mexico. The private pilot sustained serious injuries. Night visual meteorological conditions prevailed at the time of the accident. The local personal flight was being conducted under the provisions of Title 14 CFR Part 91 without a flight plan. The flight originated at approximately 1910.

According to a representative from San Juan Pilot Training, Inc., the pilot departed Farmington at approximately 1500 for a 3-hour cross-country flight to Canyonlands, Utah, Page, Arizona, and then back to Farmington. The pilot returned to the Farmington area at approximately 1800.

Upon his return, the private pilot contacted the tower and requested clearance to do take-offs and landings. He completed nine take-off, and landings on runway 25. Each landing was a full stop, taxi-back, and subsequent take-off (as required by a local training policy). At approximately 1910, the pilot contacted the tower and asked for clearance to take-off and fly the pattern for a tenth time. At approximately 1915, the pilot reported that he had lost engine power.

According to witnesses, the airplane was flying at a low altitude when its wings began to dip side to side. The airplane then pitched nose-up, rolled over, dove, and struck the roof of a police station. The impact crushed the nose section aft, and the leading edge of both wings.

An examination of the airplane at the scene showed that approximately 3 to 5 gallons of fuel had leaked from the airplane's tanks. The fuel selector lever was in the "left tank" position. A subsequent examination showed approximately 4 gallons of fuel in the right wing tank, fuel in the fuel strainer and filter, and no fuel in the lines.

Flight control continuity was confirmed and an examination of the engine and other airplane systems showed no anomalies.

According to the aircraft manufacturer, using a fuel calculation of 15 gallons per hour, and a total flight duration of 4.4 hours, the total calculated fuel used would be 66 gallons. Total useable fuel for the airplane is 74 gallons.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN04LA040