LAX00LA257

NTSB accident investigation · Interavia E-3 · Watsonville, CA · July 9, 2000

Accident · Minor injuriesLimited investigationFinal report
Date
July 9, 2000, 15:30 local (22:30 UTC)
Place
Watsonville, CA
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N4426XInteravia E-3
Weather
Visual (VMC) · Day
Status
Completed · report November 25, 2003
Report
Approved by Office Director
Parties
Federal Aviation Administration
FAA report
20000709010559A
Case key
49657

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 total loss of engine power due to the pilot's inaccurate fuel consumption calculations, which resulted in fuel exhaustion.

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) - nonmechanicalManeuvering
Fluid,fuel - exhaustionCause
Fuel consumption calculations - inaccuratePilot in commandCause
Forced landingEmergency descent/landing
In flight collision with terrain/waterEmergency descent/landing
Terrain condition - none suitable

Analysis

The private pilot was flying his experimental single engine airplane after performing maintenance, when the engine lost power after 40 minutes of operation. According to the pilot's written statement, he "checked and measured" the gas in the fuel tanks after performing maintenance on the airplane. He calculated that he had 20 gallons of fuel on board, or 40 minutes of endurance at 100 percent power or 1 hour of endurance at 70 percent power. He started the engine at 1450 and departed at 1500. He reported that he set the power at 70 percent for the flight. The engine quit as the pilot was turning back toward the airport. He checked the fuel gauges and reported that they indicated 5 gallons in each fuel tank. He pumped the fuel pump and the engine started, ran for approximately 30 seconds, and lost power again. The pilot reported that he could not restart the engine. He elected to land in a cow pasture on the side of mountainous terrain. While attempting to land over a fence and trees, the left wing touched down, slewing the plane off course. The left main landing gear separated from the left wing and the wing sustained structural damage. In his statement, the pilot noted that he should have operated the airplane by fuel time, not the gauges.

Factual narrative

On July 9, 2000, at 1530 Pacific daylight time, an experimental Interavia E-3 single engine airplane, N4426X, was substantially damaged during a forced landing after losing engine power while maneuvering near Watsonville, California. The private pilot, who was the sole occupant, received minor injuries. The airplane was registered to and operated by the pilot as a personal flight under 14 Code of Federal Regulations Part 91 when the accident occurred. Visual meteorological conditions prevailed at the time of the accident and no flight plan had been filed. The local flight originated from the Watsonville Municipal Airport approximately 30 minutes prior to the accident.

According to the Pilot/Operator Aircraft Accident Report (NTSB form 6120.1/2) submitted by the pilot, he "checked and measured" the gas in the fuel tanks after performing maintenance on the airplane. He calculated that he had 20 gallons of fuel on board, or 40 minutes of endurance at 100 percent power or 1 hour of endurance at 70 percent power. He started the engine at 1450 and departed at 1500. He reported that he set the power at 70 percent for the flight. While he was "making a long sweeping turn back to the airport at 1530, [the] engine quit." The pilot checked the fuel gauges and reported that they indicated 5 gallons in each fuel tank. He pumped the fuel pump and the engine started, ran for approximately 30 seconds, and lost power again. The pilot reported that he could not restart the engine. He elected to land in a cow pasture on the side of mountainous terrain. While attempting to land over a fence and trees, the "left wing stalled and touched down, slewing the plane off course." The left main landing gear separated from the left wing and the wing sustained structural damage.

In the NTSB form 6120.1/2, under the section titled, "Recommendation (How Could This Accident Have Been Prevented)," the pilot wrote, "operate by fuel time, not gauges."

Aircraft

Registration
N4426X
Reported as
Interavia E-3
Category
Airplane
Serial number
02-06
Airframe hours
56
Engine
unknown M14P, 360 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Charles G. Feemster
Airworthiness certificate
Special, Experimental (Special); Standard, Aerobatic
Last inspection
Annual · March 1, 2000 · 8 hours before
Departed
KWVI · Watsonville, 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
51
Injuries
Minor
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--no waivers/lim.
Last flight review
June 11, 2000
Seat
Rear
Flight hours
1,224 total · 1,129 as pilot in command · 34 in the last 90 days · 8 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
240° at 10 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
63 °F, dew point 54 °F
Altimeter
29.95 inHg
Observed at
WVI

FAA reports on this event · 1

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

Other investigations on N4426X · 1

Matched to the same aircraft by N-number and date.