LAX89FA314

NTSB accident investigation · Piper PA-31-350 · Ontario, CA · September 15, 1989

Accident · FatalField investigationFinal report
Date
September 15, 1989, 06:52 local (13:52 UTC)
Place
Ontario, CA
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Initial climb
Aircraft
N70PEPiper PA-31-350
Weather
Visual (VMC) · Day
Status
Completed · report September 9, 1992
Report
Approved by Office Director
FAA report
19890915035099A
Case key
26251

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

Failure of the right propeller hub due to metal fatigue which resulted in catastrophic separation of the propeller. Contributing to the accident was damage done to the aircraft airframe in flight by the separating propeller making the aircraft uncontrollable.

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,hub - fatigueCause
Propeller system/accessories,hub - fracturedCause
Propeller system/accessories - separationFactor
Maintenance,overhaul - improperOther maintenance personnel
Altitude deviation,uncontrolledDescent - emergency
Remedial action - attemptedPilot in command
Aircraft control - not possiblePilot in command
In flight collision with terrain/waterDescent - uncontrolled

Analysis

The propeller separated from the right engine during the initial climb. Examination of the wreckage revealed the propeller hub fracture resulted in one of the three propeller blades detaching from the hub. The rest of the propeller hub then separated striking the right front of the fuselage. Oil was spread across the aircraft nose and windsheild. The fuselage right side damage increased aerodynamic drag. Witnesses reported the engine cowling was torn. The aircraft entered a right turn and dive. It impacted the ground in a near inverted attitude. Metallurgical examination of the failed prop hub revealed metal fatigue emanating from the threaded hole for the grease fitting. The threads had been deformed by shot peening, resulting in increased stress concentrations at the threads.

Aircraft

Registration
N70PE
Reported as
Piper PA-31-350
Category
Airplane
Serial number
31-805 2137
Airframe hours
3,118
Engine
Lycoming TIO-540-J2BD, 350 horsepower, reciprocating
Damage
Destroyed
Fire
On-Ground
Flight
Part 135
Operator
Ameriflight
Registered owner
Jack Wall Aircraft Sales Inc.
Airworthiness certificate
Standard, Normal
Last inspection
AAIP · August 22, 1989 · 39 hours before
Departed
ONT · Ontario, CA
Destination
SBA · Santa Barbara, CA
Flight plan
VFR
Airport
ONT · Ontario Int'L, runway 0R

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
24
Certificates
Commercial, Flight instructor
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--w/ waivers/lim
Seat
Left
Toxicology
Performed
Flight hours
1,916 total · 89 in the last 90 days · 49 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
7 statute miles
Lowest ceiling
None
Temperature
70 °F, dew point 45 °F
Altimeter
29.00 inHg
Observed at
ONT, 2 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.