ERA16CA203

NTSB accident investigation · Beech F33A · Fairfield, NJ · June 5, 2016

Accident · No injuriesData collectionFinal report
Date
June 5, 2016, 12:05 local (16:05 UTC)
Place
Fairfield, NJ
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N444VTBeech F33A
Defining event
Approach-IFR missed approach: Loss of engine power (total)
Weather
Instrument (IMC) · Day
Status
Completed · report July 14, 2016
Report
Approved by Office Director
NTSB office
Eastern Region Aviation
Parties
FAA/FSDO
FAA report
20160605024269A
Case key
93302

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

On this page

Probable cause

The pilot's failure to adequately manage the available fuel supply, resulting in fuel starvation and a total loss of engine power.

Findings · 2

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Fluids: fuelAircraft › Fluids/misc hardware · Fluid managementBeech F33A: 4 casesAll aircraft: 1,695 casesProbable cause
Planning/preparation: fuel planningPersonnel issues › Task performance · PilotBeech F33A: 2 casesAll aircraft: 719 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The pilot of the single-engine airplane stated that he departed on a cross country flight but did not visually check the amount of fuel in the main tanks before departure and relied on his fuel gauges, which indicated 2/3-full (left tank) and 1/2-full (right tank). Both wingtip fuel tanks were empty. The pilot departed with the fuel selector on the left main tank. He then switched over to the right main tank while en route, but noticed the needle on the fuel gauge was not moving as the flight progressed. The flight was uneventful and the pilot made an instrument approach into his destination airport; however, he had to execute a missed approach due to low clouds. During the missed approach procedure he entered visual conditions and asked air traffic control (ATC) if he could maintain visual conditions and circle to land. The pilot said that as he was turning crosswind the engine began to run rough and stopped producing power. He tried to re-start the engine twice as he prepared for a forced landing to a closer runway. The pilot did not have time to switch the fuel selector to the left tank and ended up striking trees and landing short of the runway threshold. A postaccident examination revealed substantial damage to the firewall and fuselage. The landing gear was also damaged. Neither the left nor right wing fuel tanks were breached. About 20 oz of fuel was drained from the right main tank and about 21 gallons of fuel were drained from the left main tank. Though the pilot said the right fuel gauge was not reading properly, he acknowledged that he should have monitored fuel burn rate over a given period of time versus relying on just the fuel gauge.

Factual narrative

The pilot of the single-engine airplane stated that he departed on a cross country flight but did not visually check the amount of fuel in the main tanks before departure and relied on his fuel gauges, which indicated 2/3-full (left tank) and 1/2-full (right tank). Both wingtip fuel tanks were empty. The pilot departed with the fuel selector on the left main tank. He then switched over to the right main tank while en route, but noticed the needle on the fuel gauge was not moving as the flight progressed. The flight was uneventful and the pilot made an instrument approach into his destination airport; however, he had to execute a missed approach due to low clouds. During the missed approach procedure he entered visual conditions and asked air traffic control (ATC) if he could maintain visual conditions and circle to land. The pilot said that as he was turning crosswind the engine began to run rough and stopped producing power. He tried to re-start the engine twice as he prepared for a forced landing to a closer runway. The pilot did not have time to switch the fuel selector to the left tank and ended up striking trees and landing short of the runway threshold. A postaccident examination revealed substantial damage to the firewall and fuselage. The landing gear was also damaged. Neither the left nor right wing fuel tanks were breached. About 20 oz of fuel was drained from the right main tank and about 21 gallons of fuel were drained from the left main tank. Though the pilot said the right fuel gauge was not reading properly, he acknowledged that he should have monitored fuel burn rate over a given period of time versus relying on just the fuel gauge.

Aircraft

Registration
N444VT
Reported as
Beech F33A (A)
Category
Airplane
Serial number
CE-1073
Built
1985
Airframe hours
3,784
Engine
Continental Motors IO-550-B5F, 300 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Standard, Normal
Last inspection
Annual · December 21, 2015 · 41 hours before
Departed
BED · Bedford, MA
Destination
CDW · Caldwell, NJ
Flight plan
IFR
Airport
CDW · Essex County, runway 10, 3,719 × 75 ft, asphalt
Equipment
Auto-pilot

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
46
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 3, Without waivers/limitations
Last flight review
January 2, 2016
Seat
Left
Restraint
3-point
Flight hours
2,100 total · 50 in this make and model · 2,000 as pilot in command · 57 in the last 90 days · 29 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Instrument (IMC) · Day
Wind
140° at 6 knots
Visibility
10 statute miles
Lowest ceiling
1,000 ft overcast
Temperature
66 °F, dew point 63 °F
Altimeter
29.81 inHg
Observed at
CDW

Docket · 5

The files NTSB released with the investigation on June 27, 2016, on NTSB’s docket system: statements, records, photos and specialists’ reports. 2.4 MB in all.

FAA reports on this event · 1

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