N3206V

Substantial
Minor

Cessna 150M S/N: 15076421

Accident Details

Date
Sunday, August 1, 1999
NTSB Number
MIA99LA209
Location
GREENVILLE, SC
Event ID
20001212X19582
Coordinates
34.849998, -82.399879
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
1
Total Aboard
2

Probable Cause and Findings

A total loss of engine power while in descent for landing due to fuel exhaustion as a result of the pilot's failure to properly plan and load the fuel required, and the subsequent collision with the terrain during a forced landing.

Aircraft Information

Registration
N3206V
Make
CESSNA
Serial Number
15076421
Engine Type
Reciprocating
Model / ICAO
150M C150
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
ADDYMAN JEFFREY D
Address
424 RASPBERRY LN
Status
Deregistered
City
FOUNTAIN INN
State / Zip Code
SC 29644-3512
Country
United States

Analysis

On August 1, 1999, about 1354 eastern daylight time, a Cessna 150M, N3206V, registered to a private individual, operating as a Title 14 CFR Part 91 personal flight, crashed on approach to Donaldson Center Airport, Greenville, South Carolina. Visual meteorological conditions prevailed and no flight plan was filed. The airplane sustained substantial damage, the private-rated pilot was not injured, and a passenger received minor injuries. The flight originated from Myrtle Beach, South Carolina, at 1116.

According to the pilot, the fuel onboard when he made his takeoff from Myrtle Beach International Airport was 16 gallons. Most of the cruise portion of the flight was flown at 8,500 feet msl, 2,550 rpm, and mixture leaned. He was in his descent at 2,600 feet msl, and about 3 miles from his landing airport when the airframe and engine began to vibrate and the engine quit. He set up a glide for the nearest possible airport landing site, a closed runway at Donaldson Center Airport, but instead, impacted an embankment short of the runway.

According to the FAA inspector, the total amount of fuel remaining in the airplane's fuel system, postcrash, was about 3 quarts. About 1 quart was spilled moving the wreckage, and another 2 quarts were removed, using a 32-ounce container. The wing tanks had not been compromised in the crash and there was no evidence of fuel leakage, precrash. The pilot had mentioned that one of his pre-purchase discrepancies was a leaking gascolator. According to the maintenance records, the fuel selector valve was replaced, and no repeat of the fuel leak was noted. The airplane had undergone an annual inspection about 63 tachometer recorded hours before the accident.

From the "Operational Data" chapter of the Cessna 150M operating handbook, the fuel consumption rate at standard atmospheric conditions, with proper leaning, for a cruise altitude of 8,500 feet at 2,550 rpm is about 4.3 gallons/hour and takeoff and climb is another 2.8 gallons. Accordingly, a 2- hour 38-minute flight would use about 14.1 gallons. The accident flight's total usable fuel load , using the pilot's figures, was about 12.5 gallons, (the Cessna 150M operating handbook states the fuel system contains unusable fuel of 3.5 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# MIA99LA209