LAX90FA008

NTSB accident investigation · Beech F33A · Goodyear, AZ · October 11, 1989

Accident · FatalField investigationFinal report
Date
October 11, 1989, 09:33 local (16:33 UTC)
Place
Goodyear, AZ
Injuries
3 fatal
Damage
Destroyed
Phase of flight
Initial climb
Aircraft
N67536Beech F33A
Weather
Visual (VMC) · Day
Status
Completed · report September 9, 1992
Report
Approved by Office Director
FAA report
19891011039919A
Case key
26595

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 inflight separation of one propeller blade due to a fatigue fracture of undetermined origin, and failure of the pilot to maintain control of the aircraft during an attempt to return to the runway. A factor in the accident was the oil covered windsheild, which hindered the pilot in maintaining outside visual references during a low altitude maneuver.

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/malfunctionTakeoff - initial climb
Propeller system/accessories,blade - fatigueCause
Propeller system/accessories,blade - separationCause
Loss of control - in flightManeuvering - turn to landing area (emergency)
Visual lookout - not possiblePilot in commandFactor
Aircraft control - not maintainedPilot in commandCause
Stall/spin - inadvertentPilot in command
In flight collision with terrain/waterDescent - uncontrolled

Analysis

During the takeoff initial climb, one propeller blade separated and the resulting imbalance caused the remaining propeller blade and hub to separate. Witnesses saw the aircraft pitch up, then enter a right turn, in an apparent maneuver to return to the runway. Witnesses saw the aircraft bank angle continue to steepen until the aircraft rolled over and entered a spin. Metallurgical examination of the failed blade revealed that it separated due to a fatigue fracture in the first full thread of the threaded shank portion, which fitted inside a ferruled fitting. Extensive metallurgical examination of the fracture failed to identify the initiating defect in the fatigue fracture. On site examination revealed that the windshield was heavily coated with engine oil.

Aircraft

Registration
N67536
Reported as
Beech F33A
Category
Airplane
Serial number
CE-1025
Airframe hours
5,344
Engine
Continental IO-520-BB, 285 horsepower, reciprocating
Damage
Destroyed
Flight
Instructional · Part 91
Operator
Airline Training Center
Last inspection
AAIP · September 27, 1989 · 45 hours before
Departed
GYR
Flight plan
Company VFR
Airport
GYR · Litchfield, runway 21, 8,500 × 150 ft, asphalt

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
28
Certificate
Student
Medical
Class 3, Valid Medical--no waivers/lim.
Toxicology
Performed
Flight hours
68 total · 68 in this make and model · 39 as pilot in command · 68 in the last 90 days · 24 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
40 statute miles
Lowest ceiling
None
Temperature
81 °F, dew point 46 °F
Altimeter
30.00 inHg
Observed at
GYR

FAA reports on this event · 1

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