DEN90LA098

NTSB accident investigation · Cessna 310B · Elizabeth, CO · April 21, 1990

Accident · No injuriesLimited investigationFinal report
Date
April 21, 1990, 17:00 local (23:00 UTC)
Place
Elizabeth, CO
Injuries
3 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N6641BCessna 310B
Weather
Visual (VMC) · Day
Status
Completed · report September 28, 1992
Report
Approved by Office Director
Case key
17923

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 pilot's attempt to takeoff with a known deficiency and the partial failure of the propeller feathering system.

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.

Airframe/component/system failure/malfunctionCruise
Propeller system/accessories,feathering system - failure,partial
Precautionary landing - performedPilot in command(cfi)
Airframe/component/system failure/malfunctionTakeoff - initial climb
Propeller system/accessories,feathering system - failure,partialCause
Operation with known deficiencies in equipment - attemptedPilot in commandCause
Propeller system/accessories,dome - cracked
Loss of control - in flightTakeoff - initial climb
In flight collision with terrain/waterDescent - uncontrolled
Terrain condition - open field
Terrain condition - rough/uneven

Analysis

The commercial, (CFI), pilot was performing a training flight. During single engine training, the left propeller began an uncommanded return to flat pitch. The CFI took the controls, made a precautionary landing, and inspected the propeller. After an extensive runup, the CFI elected to attempt a tkaeoff from a nearby dirt road. During initial climb, at 20 feet AGL, the left propeller went into flat pitch, caused the plane to yaw to the left, the left wing dropped and the plane landed hard, with the gear retracted. The landing gear, both wings, and the guselage were bent and twisted. The left propeller dome showed evidence of oil leakage over a period of time. The left engine contained 3 quarts of oil, which was below the minimum level. One propeller blade on the left engine had a broken pitch change link. The dome was extensively cracked and had begun to disintegrate.

Aircraft

Registration
N6641B
Reported as
Cessna 310B
Category
Airplane
Serial number
35741
Airframe hours
4,625
Engine
Continental O-470-M, 240 horsepower, reciprocating
Damage
Substantial damage
Fire
Unknown
Flight
Instructional · Part 91
Operator
Preferred Avitation, Ltd.
Last inspection
100 hour · October 25, 1989 · 77 hours before
Departed
APA · Denver, CO
Destination
APA
Airport
NONE

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
49
Certificates
Commercial, Flight instructor
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
2,600 total · 96 in this make and model · 2,582 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
50 statute miles
Lowest ceiling
5,000 ft broken
Temperature
-0 °F, dew point -0 °F

Other investigations on N6641B · 1

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