N7646M

Substantial
Minor

CESSNA 175 S/N: 55946

Accident Details

Date
Thursday, November 4, 1993
NTSB Number
LAX94LA036
Location
PALM SPRINGS, CA
Event ID
20001211X13747
Coordinates
33.850353, -116.560653
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
2
Uninjured
0
Total Aboard
2

Probable Cause and Findings

fuel exhaustion due to the pilot's failure to adequately monitor the fuel consumption during the flight.

Aircraft Information

Registration
N7646M
Make
CESSNA
Serial Number
55946
Engine Type
Reciprocating
Year Built
1959
Model / ICAO
175 C175
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
XXXX
Status
Deregistered
City
OKLAHOMA CITY
State / Zip Code
OK 73135
Country
United States

Analysis

On November 3, 1993, at 1628 Pacific standard time, a Cessna 175, N7646M, nosed over during a forced landing near Palm Springs, California, following a loss of engine power. The aircraft was owned and operated by the pilot. Visual meteorological conditions prevailed at the time and no flight plan was filed for the operation. The aircraft incurred substantial damage. Both the certificated commercial pilot and his one passenger sustained minor injuries. The flight originated at Hollister, California, on the day of the mishap at about 1315 hours as a personal cross- country flight to Palm Springs.

In his statement, the pilot reported that the aircraft was descending toward Palm Springs after an uneventful flight. He stated that both wing fuel tanks were filled to capacity before departure. About eight miles from the airport as the aircraft descended through about 8,000 feet, the engine stopped. The pilot set up a best glide configuration; however, landed short of the airport in soft sand. When the nose gear touched down, the nose gear collapsed and the aircraft nosed over.

The aircraft retrieval firm which recovered the aircraft reported that they observed no fuel spill on the ground under the aircraft, and no fuel stains were noted around the tank caps or vents. Total fuel system continuity was established from the tanks to the engine. One quarter of a gallon of fuel was drained from the left tank while less than five gallons were drained from the right tank. According to the Cessna Aircraft Owners Manual for the aircraft, each wing fuel tank has a 26 gallon capacity, 21 of which is usable.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX94LA036