SEA07LA156

NTSB accident investigation · Cessna 340A · Ludlow, CA · June 12, 2007

Accident · Minor injuriesLimited investigationFinal report
Date
June 12, 2007, 15:30 local (22:30 UTC)
Place
Ludlow, CA
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N340WSCessna 340A
Weather
Visual (VMC) · Day
Status
Completed · report September 27, 2007
Report
Approved by Office Director
Parties
FAA FSDO
FAA report
20070612009929A
Case key
65975

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

The loss of engine power from both engines due to fuel starvation resulting from the pilot's improper fuel tank selector position. Contributing factors were the pilot's inadequate preflight inspection and the lack of suitable terrain for the forced landing.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine power(total) - nonmechanicalCruise
2 engines
Aircraft preflight - inadequatePilot in commandFactor
Fluid,fuel - starvationCause
Fuel tank selector position - improperPilot in commandCause
Forced landingDescent - emergency
On ground/water encounter with terrain/waterEmergency landing
Terrain condition - rock(s)/boulder(s)
Terrain condition - none suitableFactor

Analysis

The pilot stated that he did not visually inspect the fuel level in the tanks of the twin-engine airplane before departure. About 15 minutes into the flight, he noticed that the fuel gages were "erratic." About 5 minutes later, the left engine lost power and then regained power with no action by the pilot. Shortly thereafter, the right engine lost power, and the pilot "went to aux pumps" and attempted a restart with no success. The left engine then lost power for the second time, and the pilot "went to aux pumps" and attempted a restart with no success. The pilot made a forced landing in the desert, and during the landing roll, the airplane struck rocks. Examination of the airplane revealed that the right main tank was intact and contained no fuel, and the left main tank was punctured and contained a trace of fuel. The right and left auxiliary tanks contained 27 and 21 gallons of fuel, respectively. Both the left and right fuel selectors were positioned to the right main tank, and both auxiliary fuel pump switches were in the low position. Review of the Pilot's Operating Handbook for the Cessna 340A indicated that in order to utilize the fuel in the auxiliary tanks, the left and right fuel selectors must be positioned to the left and right auxiliary tanks, respectively, and the auxiliary fuel pump switches should be placed in the low position. When questioned about the amount of fuel on board the airplane at departure, the pilot stated that he believed fuel must have been stolen from the airplane while it was parked on the ramp for three days prior to the accident. A written statement was obtained from the line service technician who refueled the airplane, which confirmed that he topped off the airplane with 74.6 gallons of 100LL three days before the accident.

Factual narrative

On June 12, 2007, about 1530 Pacific daylight time, a Cessna 340A, N340WS, experienced a dual loss of engine power and sustained substantial damage during the ensuing forced landing in the desert near Ludlow, California. The private pilot, the sole occupant, received minor injuries. The airplane was registered to and operated by the pilot under 14 CFR Part 91. Visual meteorological conditions prevailed and no flight plan was filed for the personal cross country flight from Bullhead City, Arizona, to Ontario, California. The flight departed Laughlin/Bullhead City International Airport about 30 minutes prior to the accident.

During a telephone interview conducted by the NTSB investigator-in-charge and in a written statement, the pilot reported he landed at Bullhead City on June 9 and had the airplane refueled with 74.6 gallons of 100LL, which filled the main and auxiliary fuel tanks. The pilot stated that he did not visually inspect the fuel level in the tanks before departure. About 15 minutes into the flight, he noticed that the fuel gages were "erratic." About 5 minutes later, the left engine lost power and then regained power with no action by the pilot. Shortly thereafter, the right engine lost power, and the pilot "went to aux pumps" and attempted a restart with no success. The left engine then lost power for the second time, and the pilot "went to aux pumps" and attempted a restart with no success. The pilot made a forced landing in the desert alongside Interstate 40. During the landing roll, the airplane struck rocks. Damage to the airplane included a bent and buckled left wing, puncture of the left wing tip (main) tank, collapsed landing gear, and deformation of the fuselage bottom.

Examination of the airplane at the accident site by an FAA inspector revealed that the right main tank was intact and contained no fuel, and the left main tank was punctured and contained a trace of fuel. Both auxiliary tanks contained fuel. When drained by recovery personnel, the right auxiliary tank yielded 27 gallons of fuel and the left auxiliary tank yielded 21 gallons of fuel. The FAA inspector reported that both the left and right fuel selectors were positioned to the right main tank, and the auxiliary fuel pump switches were both in the low position. Review of the Pilot's Operating Handbook for the Cessna 340A indicated that in order to utilize the fuel in the auxiliary tanks, the left and right fuel selectors must be positioned to the left and right auxiliary tanks, respectively, and the auxiliary fuel pump switches should be placed in the low position.

When questioned about the amount of fuel on board the airplane at departure from Bullhead City, the pilot stated that he believed fuel must have been stolen from the airplane while it was parked on the ramp between June 9 and June 12. A written statement was obtained from the line service technician who refueled the airplane, which confirmed that he topped off the airplane with 74.6 gallons of 100LL about 1930 on June 9.

Aircraft

Registration
N340WS
Reported as
Cessna 340A
Category
Airplane
Serial number
340A1813
Airframe hours
1,498
Engines
Teledyne Continental TSIO-520NB, 310 horsepower, reciprocatingTeledyne Continental TSIO-520, 310 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Standard, Normal
Last inspection
Annual · February 1, 2007
Departed
IFP · Bullhead City, AZ
Destination
ONT · Ontario, CA

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
74
Injuries
Minor
Certificate
Private
Airplane ratings
Single-engine sea, Single-engine land, Multi-engine land
Medical
Class 3, With waivers/limitations
Last flight review
December 1, 2004
Seat
Left
Flight hours
2,128 total · 1,664 in this make and model · 4 in the last 90 days · 4 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
10 statute miles
Temperature
108 °F

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.