N65PC

Substantial
Minor

SPANGENBERG AR-1KCS/N: 0038

Accident Details

Date
Sunday, February 20, 2022
NTSB Number
ERA22LA134
Location
Sarasota, FL
Event ID
20220224104693
Coordinates
27.395444, -82.554389
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The pilot’s improper control input during an aborted takeoff procedure, which resulted in a main rotor blade contacting the vertical stabilizer, a loss of control, and subsequent runway excursion.

Aircraft Information

Registration
Make
SPANGENBERG
Serial Number
0038
Engine Type
4-cycle
Year Built
2019
Model / ICAO
AR-1KCFEST
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
2
FAA Model
AR-1KC

Registered Owner (Current)

Name
BABY BIRD AVIATION LLC
Address
6301 PORTER RD UNIT 9
City
SARASOTA
State / Zip Code
FL 34240-9612
Country
United States

Analysis

On February 20, 2022, an experimental amateur-built Spangenberg AR-1KC gyrocopter, N65PC, was substantially damaged when it was involved in an accident at Sarasota Bradenton International Airport (SRQ), Sarasota, Florida. The pilot sustained minor injuries. The gyrocopter was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot stated that, during the takeoff roll as the rotors reached 180 rpm, she released the pre-rotator and increased speed for a normal takeoff. Just before becoming airborne, the gyrocopter and the control stick “began to shudder.” The pilot also stated that she immediately aborted the takeoff and pulled back engine power. According to the pilot, she had the control stick “back too far for the conditions at that moment,” which caused a nose-high attitude and a rotor blade to “hit the very top of the tail on two screw heads that held the top of the rudder in place.” The gyrocopter departed the left side of the runway and landed hard, which resulted in substantial damage to the rudder. The pilot reported that she and her flight instructor examined the flight controls after the accident and found no mechanical problems that would have contributed to the accident.

The nose wheel separated from the gyrocopter at the weld point where it attached to the airframe. Metallurgical examination of the fracture surfaces revealed that they failed due to ductile overstress shear fracture from impact. No evidence of fatigue was observed.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA22LA134