DEN04CA101

NTSB accident investigation · Whitlock Rotorway Exec 162F · Meeker, CO · July 10, 2004

Accident · No injuriesData collectionFinal report
Date
July 10, 2004, 10:30 local (16:30 UTC)
Place
Meeker, CO
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N518WWhitlock Rotorway Exec 162F
Weather
Visual (VMC) · Day
Status
Completed · report September 29, 2004
Report
Approved by Office Director
Parties
FAA Flight Standards District Office
FAA report
20040710012599A
Case key
59608

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

aircraft control not maintained by the pilot. A contributing factor was the failure of the supercharger.

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.

Loss of engine power(partial) - mech failure/malfCruise - normal
Exhaust system,external supercharger - failureFactor
Forced landingDescent - emergency
Autorotation - attemptedPilot in command
Roll overEmergency descent/landing
Aircraft control - not maintainedPilot in commandCause

Analysis

The pilot stated that approximately 3 minutes after departing the airport, he heard a "loud squealing noise" from the engine and rotor rpm began to decrease. The pilot initiated an autorotation at 1,200 feet agl and positioned the helicopter to land in a nearby field. The pilot stated that several feet off the ground he heard a "growling noise" and the helicopter "yawed to the right," approximately 70 degrees. The helicopter landed on the left skid and subsequently rolled onto its side causing substantial damage. According to the pilot, post accident examination revealed that the supercharger on the engine had failed.

Factual narrative

On July 10, 2004, at approximately 1030 mountain daylight time, a Whitlock Rotorway Exec 162F, N518W, piloted by a private pilot, sustained substantial damage when it impacted terrain during an autorotation 3 miles north of Meeker Airport (EEO), Meeker, Colorado. Visual meteorological conditions prevailed at the time of the accident. The personal flight was being conducted under the provisions of Title 14 CFR Part 91 without a flight plan. The private pilot and his passenger were not injured. The flight originated at Meeker, Colorado, at 1027 and was en route to Craig, Colorado.

According to the report submitted by the pilot, approximately 3 minutes after departing Meeker, he heard a "loud squealing noise" from the engine and rotor rpm began to decrease. The pilot initiated an autorotation at 1,200 feet agl and positioned the helicopter to land in a nearby field. The pilot stated that several feet off the ground he heard a "growling noise" and the helicopter "yawed to the right," approximately 70 degrees. The helicopter landed on the left skid and subsequently rolled onto its side. The main rotor, landing skids and tail boom bent during the impact. According to the pilot, post accident examination revealed that the supercharger on the engine had failed.

Aircraft

Registration
N518W
Reported as
Whitlock Rotorway Exec 162F
Category
Airplane, amateur-built
Serial number
6618
Engine
Rotorway R1 162F, 150 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Guy E. Whitlock
Airworthiness certificate
Special, Experimental (Special)
Departed
EEO · Meeker, CO
Destination
Craig, CO
Airport
EEO · Meeker

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
48
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--no waivers/lim.
Last flight review
March 5, 2004
Seat
Left
Flight hours
372 total · 112 in this make and model · 298 as pilot in command · 29 in the last 90 days · 10 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
160° at 4 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
79 °F, dew point 43 °F
Altimeter
30.23 inHg
Observed at
EEO, 3 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.