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Accidents · NTSB WPR18LA190 · Final report

Autogyro CALIDUS accident near Tacoma, Washington, July 7, 2018

On July 7, 2018 at about 8:00 pm local time, a 2017 Autogyro CALIDUS (gyroplane), registered N623AG, was substantially damaged in an accident during takeoff near Tacoma, Washington (Tacoma Narrows airport). It was a personal flight under general aviation rules (Part 91). 2 people had minor injuries. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilot's failure to properly configure the gyrocopter for takeoff, which resulted in it developing high speed and led to a subsequent loss of control.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
July 7, 2018 · about 8:00 pm local time
Place
Tacoma, Washington · Tacoma Narrows · map
Type
Accident
Injuries
2 people had minor injuries.
Weather
visual conditions (good weather)
Aircraft
Autogyro CALIDUS No Series, built 2017
Registration
N623AG · no longer on the register · serial US-C00491
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

While preparing for takeoff in the gyrocopter, the commercial pilot had difficulty getting the prerotator to engage with the rotor ring gear, so he aborted the takeoff attempt. He then taxied off the runway to a run-up area and successfully engaged the prerotator to the rotor ring gear. The pilot then taxied onto the runway, and the rotor reached 200 rpm, after which he began the second takeoff attempt. The pilot stated that he recalled pulling the control stick aft while the gyrocopter was accelerating down the runway. Subsequently, the gyrocopter suddenly began climbing and shaking violently. The pilot then lost control of the gyrocopter, and it descended, struck the runway, skidded about 100 ft, exited the left side of the runway, and then came to rest on its left side. A witness reported that the gyrocopter began the takeoff roll with the rotor level with the runway. During an interview with the flight instructor who trained the pilot in the gyrocopter, she stated that, when engaging the prerotator for takeoff, it is essential to keep the control stick fully forward to protect the airframe from the slow-spinning rotor. A fully forward control stick would place the rotor level with the ground, as described by the witness. The rotor then needs to achieve 200 rpm, followed by the control stick being moved fully aft for the takeoff roll, tilting the rotor. Further, the Airplane Owner's Manual contained a warning stating that "Prior to releasing the wheel brake, make sure that the control stick is fully aft…A takeoff run with a flat rotor system may have fatal consequences." Given the pilot and witness statements and that the gyrocopter skidded 100 ft after impacting the runway, it is likely that the pilot did not pull the control stick fully aft after prerotating the rotor to 200 rpm and conducted the second takeoff attempt with the control stick not fully aft and with the rotor level with the ground. The pilot’s failure to properly configure the gyrocopter for takeoff resulted in it developing high speed during the takeoff roll and the subsequent loss of control.

The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.

The factual record from the NTSB's investigation tables, in plain English

What happened, in order

  1. Miscellaneous/other during takeoff
  2. Loss of control in flight during takeoff defining event
  3. Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent

The NTSB's findings

  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Configuration › Incorrect use/operation
  • cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot

Pilot

  • Certificate: commercial pilot, private, sport pilot
  • Ratings: single-engine land; single-engine sea; instrument: airplane; rotorcraft: gyroplane; rotorcraft: helicopter
  • Flight time: 682 hours in all; 32 in this make and model; 24 in the last 90 days; 16 in the last 30 days; 569 as pilot in command
  • Last flight review: September 28, 2016
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: frt
  • Injury: minor injuries

Passenger

  • Seat: rear
  • Injury: minor injuries

The aircraft

  • Airframe total time: 56 hours
  • Last inspection: 100-hour inspection, June 1, 2018; 31 hours since
  • Maximum gross weight: 992 lb
  • Seats: 2
  • Landing gear: fixed
  • Engine: Rotax 914 UL2-01 (piston); 56 hours total

The flight

  • Departed from: KTIW Tacoma WA at 8:00 pm
  • Destination: KTIW Tacoma WA
  • Flight plan: none
  • Runway 17, 5,002 ft by 100 ft

Weather at the time

  • Light: daylight
  • Wind: from 270° at 6 knots
  • Visibility: 10 statute miles
  • Sky: broken clouds at 6,000 ft; scat at 1,200 ft
  • Temperature: 66°F (19°C), dew point 54°F (12°C)
  • Altimeter: 30.21 inHg
  • Observation at 7:53 pm from KTIW

Injuries

FatalSeriousMinorNone
Flight crew1
Passengers1

Documents from the investigation the NTSB's docket: the evidence folder behind the report

5 documents, released by the NTSB on February 8, 2019. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.

The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.

Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.