MIA92LA082

NTSB accident investigation · Burch Rotorway Exec · Lakeland, FL · February 9, 1992

Accident · No injuriesLimited investigationFinal report
Date
February 9, 1992, 15:55 local (20:55 UTC)
Place
Lakeland, FL
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N618VNBurch Rotorway Exec
Weather
Visual (VMC) · Day
Status
Completed · report August 13, 1993
Report
Approved by Office Director
FAA report
19920209002429A
Case key
33063

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 pilot-in-command's improper application of cyclic and collective pitch control during an autorotative landing. This resulted in a hard landing, collision of the main rotor blades with the tailboom, and subsequent roll over of the helicopter. Contributing to the accident was a partial loss of engine power caused by a total failure of the engine assemby exhaust valve.

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/malfApproach - vfr pattern - final approach
Engine assembly,valve,exhaust - failure,totalFactor
Forced landingDescent - emergency
Hard landingLanding - flare/touchdown
Flight controls - improper use ofPilot in commandCause

Analysis

The private pilot was on final approach for landing in VFR conditions when the engine sustained a partial loss of engine power. The pilot entered autorotation. At 30-40 feet AGL a deceleration was initiated and collective pitch was applied at 3-7 feet AGL. The helicopter touched down hard with forward movement and the main rotor blades collided with the tailboom. The helicopter skidded forward and the tip of the left skid became imbedded in a mound of dirt. The helicopter rolled over on its left side sustaining substantial damage. The private pilot was not injured. Examination of the airframe by the FAA and the local police department revealed the left skid separated from the fuselage at the weld joint on the skid support strut. Examination of the engine by a field representative for rotorway international for the registered owner revealed an exhaust valve on the number 2 cylinder had failed.

Aircraft

Registration
N618VN
Reported as
Burch Rotorway Exec (ROTORWAY E)
Category
Helicopter, amateur-built
Serial number
3480
Airframe hours
255
Engine
Rotorway RW152, 150 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Ronald W.Case
Registered owner
Ronald W.Case
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Continuous airworthiness · January 9, 1992 · 3 hours before
Airport
LAL · Lakeland Regional

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
52
Certificate
Private
Airplane ratings
Multi-engine land, Single-engine land, Single-engine sea
Instrument ratings
Airplane
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
1,074 total · 34 in this make and model · 400 as pilot in command · 18 in the last 90 days · 8 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
40° at 5 knots
Visibility
20 statute miles
Lowest ceiling
15,000 ft overcast
Temperature
64 °F, dew point 28 °F
Altimeter
30.00 inHg
Observed at
PIE, 38 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.