DEN83FA131

NTSB accident investigation · Aero Commander 680FL · Monticello, UT · June 2, 1983

Accident · FatalField investigationFinal report
Date
June 2, 1983, 17:23 local (23:23 UTC)
Place
Monticello, UT
Injuries
2 fatal
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N271VTAero Commander 680FL
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19830602022529A
Case key
15991

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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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 - normal
Fluid,fuel - starvationFactor
Fuel tank selector position - delayedPilot in commandCause
InattentivePilot in commandCause
Fuel boost pump selector position - not selectedPilot in commandCause
Diverted attentionPilot in commandCause
In-flight planning/decision - improperPilot in commandCause
Loss of control - in flightCruise - normal
Airspeed(vmc) - not maintainedPilot in commandCause
Stall - inadvertentPilot in commandCause
In flight collision with terrain/waterDescent - uncontrolled

Analysis

The acft crashed while doing magnetometer surveys at low altitude. The right engine had lost power then regained it for a short period and lost it again. A videotape in the acft recorded the plt saying, 'I changed that # just in time.' The acft yawed and the propeller slowed at the same time. The fuel selector valves were found on the center tanks. The boost pump switches were found in the off position. When changing from outboard to center tanks the boost pumps must be on or fuel starvation will occur. As the acft slowed the tape revealed that the co-plt called out'down to 90'. 90 mph isvmc. The acft stalled, shortly after the asymmetrical thrust rolled the acft to the right and into the ground.

Aircraft

Registration
N271VT
Reported as
Aero Commander 680FL
Category
Airplane
Serial number
1435-74
Engine
Lycoming IGSO-540-B1A, 380 horsepower, reciprocating
Damage
Destroyed
Flight
Business · Part 91
Registered owner
Geodata International,Inc.
Airworthiness certificate
Special, Restricted (Special)
Last inspection
Annual · January 6, 1983
Departed
CEZ · Cortez, CO

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
47
Certificates
Commercial, Flight instructor, Airline transport
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane, Helicopter
Medical
Class 1, Valid Medical--w/ waivers/lim
Seat
Left
Toxicology
Performed
Flight hours
12,200 total

Weather

Conditions
Visual (VMC) · Day
Wind
210° at 12 knots, gusting 20
Visibility
50 statute miles
Lowest ceiling
12,000 ft broken
Temperature
63 °F, dew point 39 °F
Altimeter
29.00 inHg
Observed at
CEZ, 34 nm away

FAA reports on this event · 1

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