CEN09CA394

NTSB accident investigation · Sidler Mike Rotorway · Waxahachie, TX · June 27, 2009

Accident · Minor injuriesData collectionFinal report
Date
June 27, 2009, 11:45 local (16:45 UTC)
Place
Waxahachie, TX
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Emergency descent
Aircraft
N1934Sidler Mike Rotorway
Defining event
Autorotation: Loss of tail rotor effectiveness
Weather
Visual (VMC) · Day
Status
Completed · report October 19, 2009
Report
Approved by Office Director
NTSB office
Central Region
Parties
FAA Dallas FSDO
FAA report
20090627011229A
Case key
74158

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

The pilot’s failure to control his rate of descent during autorotation, which required an aggressive recovery maneuver and resulted in a sudden loss of tail rotor effectiveness.

Findings · 5

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Action: delayed actionPersonnel issues › Action/decision · PilotSidler Mike ROTORWAY 162F: 1 caseAll aircraft: 894 casesProbable cause
Tail rotorAircraft › Aircraft propeller/rotor · Capability exceededSidler Mike ROTORWAY 162F: 1 caseAll aircraft: 23 casesProbable cause
Performance/control parameters: descent rateAircraft › Aircraft oper/perf/capability · Not attained/maintainedSidler Mike ROTORWAY 162F: 1 caseAll aircraft: 242 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The private pilot was conducting a practice 180-degree power recovery autorotation in a helicopter with a clockwise rotating main rotor with a right crosswind of three knots. The pilot said he had a higher than expected rate of descent as he was flaring at zero airspeed and attempting a power recovery to terminate at a skid height of approximately 15 feet above ground level. Suddenly, and without warning the pilot lost directional control, the helicopter began to spin nose left, and his application of full right pedal had no effect. The pilot said he tried to keep the helicopter level while it was spinning, but it eventually impacted on the left side of the taxiway. The helicopter was substantially damaged when the left skid gear partially collapsed and the airframe and tail boom buckled. During the impact sequence the main rotor blades struck the tail boom and the main rotor blades and tail rotor blades struck the ground. An on-scene investigation by an FAA maintenance inspector confirmed flight control continuity and confirmed no apparent damage to the tail rotor drive belts. There was no post-crash fire and the pilot received minor injuries.

Factual narrative

The private pilot was conducting a practice 180 degree power recovery autorotation in a helicopter with a clockwise rotating main rotor with a right crosswind of three knots. The pilot said he had a higher than expected rate of descent as he was flaring at zero airspeed and attempting a power recovery to terminate at a skid height of approximately 15 feet above ground level. Suddenly and without warning the pilot lost directional control, the helicopter began to spin nose left, and his application of full right pedal had no effect. The pilot said he tried to keep the helicopter level while it was spinning but it eventually impacted on the left side of the taxiway. The helicopter was substantially damaged when the left skid gear partially collapsed and the airframe and tail boom buckled. During the impact sequence the main rotor blades struck the tail boom and the main rotor blades and tail rotor blades struck the ground. An on-scene investigation by an FAA maintenance inspector confirmed flight control continuity and confirmed no apparent damage to the tail rotor drive belts. There was no post-crash fire and the pilot received minor injuries.

Aircraft

Registration
N1934
Reported as
Sidler Mike Rotorway (162 F)
Category
Helicopter, amateur-built
Serial number
6294
Airframe hours
197
Engine
Rotorway RI 162F, 150 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Sidler Mike
Registered owner
Sidler Mike
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Condition · January 17, 2009 · 20 hours before
Departed
KJWY · Waxahachie, TX
Destination
KJWY · Waxahachie, TX
Airport
KJWY · Mid-Way Regional Airport, runway 18, 4,999 × 40 ft, asphalt

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
50
Injuries
Minor
Certificate
Private
Medical
Class 3, Without waivers/limitations
Last flight review
June 17, 2009
Seat
Left
Flight hours
100 total · 90 in this make and model · 60 as pilot in command · 20 in the last 90 days · 10 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
250° at 3 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
95 °F, dew point 66 °F
Altimeter
29.87 inHg
Observed at
KJWY, 1 nm away

Docket · 2

The files NTSB released with the investigation on August 20, 2009, on NTSB’s docket system: statements, records, photos and specialists’ reports. 305 KB in all.

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.