LAX05LA270

NTSB accident investigation · Prescott Aeronautical Pusher · Redding, CA · August 14, 2005

Accident · Serious injuriesLimited investigationFinal report
Date
August 14, 2005, 12:17 local (19:17 UTC)
Place
Redding, CA
Injuries
1 serious
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N43PPPrescott Aeronautical Pusher
Weather
Visual (VMC) · Day
Status
Completed · report May 30, 2006
Report
Approved by Office Director
Parties
Federal Aviation Administration
FAA report
20050814020029A
Case key
62246

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 in-flight separation of the propeller for undetermined reasons.

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 - separationCause
Forced landingDescent - emergency
On ground/water collision with objectEmergency landing
Object - tree(s)

Analysis

The pusher configuration propeller departed the airplane during flight and the airplane impacted trees during a forced landing in a field. The pilot was established in cruise flight at 7,500 feet mean sea level when he felt a vibration. The vibration then became "severe" and he heard a series of clinking noises. He immediately began preparations for an emergency landing because he knew that his propeller had separated from the airplane. The pilot force-landed the airplane in a vacant field. The pilot stated that about 2 weeks prior to the accident he had removed the wooden American Propeller and installed a different propeller. The new propeller was too long for ground clearance so the pilot reinstalled the original wooden American Propeller. The original hardware was used to install the propeller and the bolts were torqued to the recommended amount. The bolts were also safety wired. After its installation, the propeller was operationally tested. Prior to its removal, the propeller had been installed on the airplane for about 1 year with no operational or mechanical problems noted. The pilot did not have any other reported vibrations on flights leading up to the accident. Post accident examination by the responding airport personnel showed that the propeller and the attachment bolts were not on the propeller flange. Three of the bolt holes showed evidence of rubbing and partial elongation of the holes. The propeller and its attachment hardware were not recovered.

Factual narrative

On August 14, 2005, at 1217 Pacific daylight time, an experimental Prescott Aeronautical Pusher, N43PP, lost its propeller during flight and the pilot made a forced landing in a field 1/2-mile south of Redding Municipal Airport (KRDD), Redding, California. During the forced landing, the airplane impacted trees and sustained substantial damage. The pilot was operating the privately registered airplane under the provisions of 14 CFR Part 91. The pilot sustained serious injuries. Visual meteorological conditions prevailed for the cross-country flight. The flight departed from Pearson Field Airport (KVUO), Vancouver, Washington, at 0920, and was destined for Willows-Glenn County Airport (KWLW), Willows, California. No flight plan had been filed.

According to the pilot, he was going to stop at Willows for fuel, and then continue to Whiteman Airport, Los Angeles, California. He was established in cruise flight at 7,500 feet mean sea level when he felt a vibration. The vibration then became "severe" and he heard a series of clinking noises. He radioed the Redding Air Traffic Control Tower and advised that he needed to land immediately because he knew that his propeller had separated from the pusher airplane. The pilot force-landed the airplane in a vacant field. The pilot stated that about 2 weeks prior to the accident he and a friend had removed the wooden American Propeller and installed a different propeller. The new propeller was too long for ground clearance so the pilot and his friend reinstalled the original wooden American Propeller. The original hardware was used to install the propeller and the bolts were torqued to the recommended amount. The bolts were also safety wired. After its installation, the propeller was operationally tested. Prior to its removal, the propeller had been installed on the airplane for about 1 year with no operational or mechanical problems noted. The pilot did not have any reported vibrations on flights leading up to the accident flight.

The responding airport personnel sent photos of the accident site to the National Transportation Safety Board investigator-in-charge. The photos showed that the propeller and the attachment bolts were not on the propeller flange. Three of the bolt holes showed evidence of rubbing and partial elongation of the holes. The propeller and its attachment hardware were not recovered.

Aircraft

Registration
N43PP
Reported as
Prescott Aeronautical Pusher
Category
Airplane, amateur-built
Serial number
050
Airframe hours
154
Engine
Hibbler IO-360-C1C, 200 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Norris Hibbler
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Continuous airworthiness · February 1, 2005 · 35 hours before
Departed
VUO · Vancouver, WA
Destination
WLW · Willows Glen, CA

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
70
Injuries
Serious
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 2, With waivers/limitations
Last flight review
July 1, 2005
Seat
Left
Flight hours
1,652 total · 51 in this make and model · 1,632 as pilot in command · 15 in the last 90 days · 8 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
Variable at 5 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
90 °F, dew point 54 °F
Altimeter
29.96 inHg
Observed at
RDD, 1 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.