LAX92LA216

NTSB accident investigation · Questair Venture · Ely, NV · May 23, 1992

Accident · Minor injuriesLimited investigationFinal report
Date
May 23, 1992, 14:15 local (21:15 UTC)
Place
Ely, NV
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N3VDQuestair Venture
Weather
Visual (VMC) · Day
Status
Completed · report June 30, 1993
Report
Approved by Office Director
FAA report
19920523016049A
Case key
27624

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 inadequate installation of the engine oil temperature/pressure transducer by the pilot/owner that resulted in a fatigue failure of the transducer mounting fitting in the engine oil system. The soft landing surface and the mountainous terrain in which the airplane landed were factors in the accident.

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) - mech failure/malfCruise - normal
Single engine aircraftCause
Maintenance,installation - inadequateOther maintenance personnelCause
Lubricating system,oil line - fatigueCause
Engine assembly - seizedCause
Forced landingDescent - emergency
Gear collapsedLanding - roll
Terrain condition - softFactor
Landing gear - overloadFactor
Nose overLanding - roll

Analysis

After assembling the home built aircraft the co-owner/pilot installed an aluminum fitting between the engine case and a heavy transducer. The fitting that attached the transducer to the engine failed after 31 hours of operations while the aircraft was in cruise flight over mountainous terrain. The failure resulted in the loss of engine oil and the engine seized. The pilot attempted to land the aircraft on a soft surface in mountainous terrain. The landing gear sank into the soft earth during the landing roll and the aircraft nosed over on its back. A metallurgical examination of the fitting disclosed that the failure resulted from fatigue. The heavy transducer should have been mounted to the engine or airframe with flexible oil lines that would endured the vibrations that are inherently associated with the reciprocating engine.

Aircraft

Registration
N3VD
Reported as
Questair Venture
Category
Airplane, amateur-built
Serial number
446
Airframe hours
31
Engine
Continental IO-550G1B, 280 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
D. G. Lewis
Registered owner
D. G. Lewis
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Unknown · January 2, 2000
Departed
H10 · Portland, OR
Destination
SGU · St George, UT

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
34
Certificate
Private
Airplane ratings
Multi-engine land, Single-engine land
Medical
Class 3, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
3,700 total · 41 in this make and model · 3,700 as pilot in command · 72 in the last 90 days · 41 in the last 30 days · 3 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
100° at 7 knots
Visibility
55 statute miles
Lowest ceiling
7,000 ft broken
Temperature
72 °F, dew point 30 °F
Observed at
ELY, 45 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.