GAA15CA127

NTSB accident investigation · Paquin Michael A A · Concord, NH · June 20, 2015

Accident · No injuriesData collectionFinal report
Date
June 20, 2015, 12:30 local (16:30 UTC)
Place
Concord, NH
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N485MPPaquin Michael A A
Defining event
Takeoff: Loss of control on ground
Weather
Visual (VMC) · Day
Status
Completed · report July 27, 2015
Report
Approved by Office Director
NTSB office
General Aviation Accidents
Parties
Portland FSDO FAA
FAA report
20150620021649A
Case key
91407

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's inability to maintain directional control during takeoff, which resulted in a roll over. Contributing to the loss of control was the pilot's failure to disengage the main rotor brake prior to takeoff.

Findings · 4

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.

Use of equip/info: aircraft controlPersonnel issues › Task performance · PilotPaquin Michael A A: 1 caseAll aircraft: 9,295 casesProbable cause
Performance/control parameters: directional controlAircraft › Aircraft oper/perf/capability · Attain/maintain not possiblePaquin Michael A A: 1 caseAll aircraft: 3,958 casesProbable cause
Action: forgotten action/omissionPersonnel issues › Action/decision · PilotPaquin Michael A A: 1 caseAll aircraft: 440 casesProbable cause
Main rotor drive: main rotor brakeAircraft › Aircraft propeller/rotor · Incorrect use/operationPaquin Michael A A: 1 caseAll aircraft: 1 case

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 pilot of the amateur built gyrocopter reported that during taxi to the runway, he was distracted by his electronic altimeter when it entered a sleep mode. After resetting the altimeter, the pilot immediately entered the active runway and initiated the takeoff roll without disengaging the main rotor brake. Subsequently, at 25 miles per hour during the takeoff roll he reported an unusual vibration and a knocking sound. The pilot attempted to reduce speed, but the gyrocopter tipped forward and to the left, the main rotor impacted the ground, and the gyrocopter rolled over on its right side coming to a stop on the runway. During an interview with the pilot, he explained that the rotor brake must be disengaged before takeoff. He also stated that this accident may have been prevented if the rotor brake was designed in a manner that required manual hand pressure from the pilot. The pilot stated there were no mechanical malfunctions or failures with the gyrocopter that would have precluded normal operation. Substantial damage was found along the main rotor and vertical stabilizer.

Factual narrative

The pilot of the amateur built gyrocopter reported that during taxi to the runway, he was distracted by his electronic altimeter when it entered a sleep mode. After resetting the altimeter, the pilot immediately entered the active runway and initiated the takeoff roll without disengaging the main rotor brake. Subsequently, at 25 miles per hour during the takeoff roll he reported an unusual vibration and a knocking sound. The pilot attempted to reduce speed, but the gyrocopter tipped forward and to the left, the main rotor impacted the ground, and the gyrocopter rolled over on its right side coming to a stop on the runway. During an interview with the pilot, he explained that the rotor brake must be disengaged before takeoff. He also stated that this accident may have been prevented if the rotor brake was designed in a manner that required manual hand pressure from the pilot. The pilot stated there were no mechanical malfunctions or failures with the gyrocopter that would have precluded normal operation. Substantial damage was found along the main rotor and vertical stabilizer.

Aircraft

Registration
N485MP
Reported as
Paquin Michael A A (NO SERIES)
Category
Gyroplane, amateur-built
Serial number
1-2011
Built
2012
Airframe hours
95
Engine
Compact Radial Engines MZ202, 60 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Special, Experimental (Special)
Departed
CON · Concord, NH
Destination
CON · Concord, NH
Airport
CON · Concord Muni, runway 12, 3,200 × 75 ft, asphalt
Equipment
Handheld GPS

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
57
Injuries
None
Certificate
Sport Pilot
Medical
Sport pilot
Last flight review
September 10, 2013
Seat
Front
Restraint
4-point
Flight hours
90 total · 60 in this make and model · 84 as pilot in command · 4 in the last 90 days · 2 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
Variable at 5 knots
Visibility
10 statute miles
Temperature
73 °F, dew point 48 °F
Altimeter
30.11 inHg
Observed at
KCON

Docket · 4

The files NTSB released with the investigation on July 10, 2015, on NTSB’s docket system: statements, records, photos and specialists’ reports. 2.2 MB 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.