LAX00LA301

NTSB accident investigation · Follmer Q200 · Corona, CA · August 15, 2000

Accident · Minor injuriesLimited investigationFinal report
Date
August 15, 2000, 10:03 local (17:03 UTC)
Place
Corona, CA
Injuries
1 minor
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N8427Follmer Q200
Weather
Visual (VMC) · Day
Status
Completed · report June 25, 2003
Report
Approved by Office Director
FAA report
20000815009849A
Case key
50000

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 failure and separation of one wooden propeller blade 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,blade - separationCause
Forced landingEmergency descent/landing
On ground/water collision with objectLanding - roll
Object - utility pole

Analysis

The amateur-built airplane collided with ground obstructions during a forced landing on an interstate highway following the in-flight separation of a portion of one propeller blade. An FAA airworthiness inspector examined the airplane and interviewed the pilot. The pilot reported that the airplane was in cruise flight when it suddenly began to shake violently. The pilot believed he had lost part of the wooden propeller and turned to return to the departure airport. The shaking through the airframe became intense and the pilot was unsure of the continued integrity of the airframe. He decided to land on a major interstate highway beneath the airplane. During the landing rollout, the airplane was quickly catching up to automobiles on the road ahead and the pilot intentionally steered the airplane to the right shoulder to avoid a collision with the vehicles. The right wing contacted a light pole and slued the airplane nose first into another pole. The second collision with the pole shattered the propeller into small splinters. The airplane continued down an embankment and collided with additional brush. The FAA inspector searched the area and was able to identify one propeller blade tip in the propeller fragments scattered over the site. The second tip could not be located. According to the pilot, the aircraft owner built the airplane prior to 1990 and obtained an initial airworthiness and registration certificate, then placed the airplane into storage. The airplane did not fly from 1990 until weeks before the accident. The pilot was in the process of flying the initial 40 operating hours for an unrestricted experimental airworthiness certificate and had flown the airplane about 11 hours.

Factual narrative

On August 15, 2000, at 1003 hours Pacific daylight time, an amateur-built Follmer Q200 airplane, N8427, collided with ground obstructions during a forced landing on an interstate highway in Corona, California. The forced landing was precipitated by an in-flight separation of a portion of one propeller blade. The aircraft was operated by the pilot under the provisions of 14 CFR Part 91 of the Federal Aviation Regulations. The airplane was destroyed in the accident sequence. The commercial pilot, the sole occupant, sustained minor injuries. Visual meteorological conditions prevailed for the local area personal flight that had originated from the Chino, California, airport about 0945.

An Federal Aviation Administration (FAA) airworthiness inspector from the Riverside, California, Flight Standards District Office responded to the accident site and examined the airplane and interviewed the pilot. The pilot reported that the airplane was in cruise flight when it suddenly began to shake violently. The pilot believed he had lost part of the wooden propeller and turned to return to the Chino airport. The shaking through the airframe became intense and the pilot was unsure of the continued integrity of the airframe. He decided to land on a major interstate highway beneath the airplane. During the landing rollout, the airplane was quickly catching up to automobiles on the road ahead and the pilot intentionally steered the airplane to the right shoulder to avoid a collision with the vehicles. The right wing contacted a light pole and slued the airplane nose first into another pole. The second collision with the pole shattered the propeller into small splinters. The airplane continued down an embankment and collided with additional brush.

The FAA inspector searched the area and was able to identify one propeller blade tip in the propeller fragments scattered over the site. The second tip could not be located.

According to the pilot, the aircraft owner built the airplane prior to 1990 and obtained an initial airworthiness and registration certificate, then placed the airplane into storage in a hangar at the Chino airport. The airplane did not fly from 1990 until weeks before the accident. The pilot was in the process of flying the initial 40 operating hours for an unrestricted experimental airworthiness certificate and had flown the airplane about 11 hours.

Aircraft

Registration
N8427
Reported as
Follmer Q200
Category
Airplane, amateur-built
Serial number
2472
Airframe hours
5
Engine
Continental O-200A, 100 horsepower, reciprocating
Damage
Destroyed
Flight
Personal · Part 91
Operator
Birch E. Parker
Registered owner
Frank F. Follmer
Airworthiness certificate
Special, Experimental (Special)
Departed
CNO · Chino, 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
78
Certificate
Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
2,902 total · 2,800 as pilot in command · 4 in the last 90 days · 1 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
280° at 11 knots
Visibility
9 statute miles
Lowest ceiling
None
Temperature
207 °F, dew point 140 °F
Altimeter
29.00 inHg
Observed at
CNO, 10 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.