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Atlas / NTSB / GAA17CA258

NTSB CAROL · Event

Event GAA17CA258

2017-05-04 Stevensville, Maryland, United States Airport · W29 Minor 1 aircraft Status: Completed

Registry · N991TC

FAA Aircraft Registry record.

Make / Model

AUTOGYRO GMBH CALIDUS

Year of manufacture

2017 · 0 years old at event

Engine

ROTAX 914UL (115 hp)

Seats / Engines

2 seats · 1 engine

Last airworthiness date

20180202

ADS-B equipped

Yes — Mode-S ADD806

Registrant of record

991TC LLC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot’s improper takeoff procedure, which resulted in a loss of directional control during the takeoff.

Factual narrative

The pilot of the gyrocopter reported that during the takeoff roll, the rotor RPM was not increasing. He continued the takeoff and kept the gyrocopter on the ground to gain airspeed by not moving the stick in the full aft position. He added that this was an "old existing airplane habit". Subsequently, during the takeoff the gyrocopter developed a "rotor flap" and he lost directional control. The gyrocopter came to rest on its side to the left of the runway. The pilot added that not having the stick full aft prevented the rotor RPM from increasing, and the appropriate corrective action would have been to apply full aft stick. The gyrocopter sustained substantial damage to the fuselage and rotors. The pilot reported that there were no pre-accident mechanical failures or malfunctions with the gyrocopter that would have precluded normal operation. The Gyrocopter's Flight Manual states that during the takeoff roll, the pilot must "bring the control stick fully aft". The pilot of the gyrocopter reported that, during the takeoff roll, the rotor rpm was not increasing. He continued the takeoff and kept the gyrocopter on the ground to gain airspeed by not moving the stick to the full-aft position. He added that this was an "old existing airplane habit." Subsequently, during the takeoff, the gyrocopter developed a "rotor flap," and he lost directional control. The gyrocopter came to rest on its side to the left of the runway. The pilot added that not having the stick full aft prevented the rotor rpm from increasing and that the appropriate corrective action would have been to apply full-aft stick. The gyrocopter sustained substantial damage to the fuselage and rotors. The pilot reported that there were no preaccident mechanical failures or malfunctions with the gyrocopter that would have precluded normal operation. The gyrocopter's Flight Manual stated that, during the takeoff roll, the pilot must "bring the control stick fully aft." Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).

  • C Personnel issues-Task performance-Use of equip/info-Use of policy/procedure-Pilot - C
  • C Personnel issues-Action/decision-Action-Incorrect action performance-Pilot - C
  • C Personnel issues-Task performance-Use of equip/info-Use of equip/system-Pilot - C
  • C Aircraft-Aircraft propeller/rotor-Rotorcraft flight control-Main rotor control-Incorrect use/operation - C
  • C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C

Verbatim from NTSB's published report. Source file NTSB_2017_GAA17CA258.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.