20180707009259A

Accident · Substantial damage

FAA accident report · Autogyro USA CALIDUS · Tacoma, WA · July 7, 2018

Date
July 7, 2018 · 14:00 local
Place
Tacoma, WA
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N623AG
NTSB investigation
NTSBWPR18LA190
Reported as
Autogyro USA Calidus
Reported engine
ROTAX 914UL
People aboard
2
Fatal injuries
0
Other injuries
2
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
682 total32 in this make and model24 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

Based on the pilot?s statement, the Autogyro (gyroplane) was attempting to takeoff from runway 17 but was unable to engage the rotor disc pre-rotator. The control tower requested that he either begin his takeoff or taxi clear of the runway. The pilot taxied off the runway, returned to the ramp and tested the rotor disc pre-rotator and was able to engage it; the pilot then requested taxi and takeoff clearance. After receiving clearance he taxied onto the runway and engaged the pre-rotator and pre-rotated the rotor disc to 200 RPM. He then began his takeoff roll, at about 10 feet above the runway he felt a strong vibration, the aircraft lost altitude, impacted the runway, rolled over on its left side and slid along the runway. Both he and his passenger were able to exit the aircraft with help from a good samaritan and both occupants received minor injuries.

An individual who witnessed the takeoff stated that the Autogyro?s rotor disc was flat during the takeoff roll. The Autogyro?s flight manual requires that the control stick be fully aft during takeoff. A fully aft stick tilts the rotor disc aft. Based on the pilot?s statement and our examination of the Autogyro it appears that there were no mechanical issues with the Autogyro. Based on our investigation it appears that the pilot failed to pull the control stick back to its full aft position which therefore caused the rotor disc to fail to reach the position required for a safe takeoff.

As the FAA filed it

BASED ON THE PILOT?S STATEMENT, THE AUTOGYRO (GYROPLANE) WAS ATTEMPTING TO TAKEOFF FROM RUNWAY 17 BUT WAS UNABLE TO ENGAGE THE ROTOR DISC PRE-ROTATOR. THE CONTROL TOWER REQUESTED THAT HE EITHER BEGIN HIS TAKEOFF OR TAXI CLEAR OF THE RUNWAY. THE PILOT TAXIED OFF THE RUNWAY, RETURNED TO THE RAMP AND TESTED THE ROTOR DISC PRE-ROTATOR AND WAS ABLE TO ENGAGE IT; THE PILOT THEN REQUESTED TAXI AND TAKEOFF CLEARANCE. AFTER RECEIVING CLEARANCE HE TAXIED ONTO THE RUNWAY AND ENGAGED THE PRE-ROTATOR AND PRE-ROTATED THE ROTOR DISC TO 200 RPM. HE THEN BEGAN HIS TAKEOFF ROLL, AT ABOUT 10 FEET ABOVE THE RUNWAY HE FELT A STRONG VIBRATION, THE AIRCRAFT LOST ALTITUDE, IMPACTED THE RUNWAY, ROLLED OVER ON ITS LEFT SIDE AND SLID ALONG THE RUNWAY. BOTH HE AND HIS PASSENGER WERE ABLE TO EXIT THE AIRCRAFT WITH HELP FROM A GOOD SAMARITAN AND BOTH OCCUPANTS RECEIVED MINOR INJURIES.

AN INDIVIDUAL WHO WITNESSED THE TAKEOFF STATED THAT THE AUTOGYRO?S ROTOR DISC WAS FLAT DURING THE TAKEOFF ROLL. THE AUTOGYRO?S FLIGHT MANUAL REQUIRES THAT THE CONTROL STICK BE FULLY AFT DURING TAKEOFF. A FULLY AFT STICK TILTS THE ROTOR DISC AFT. BASED ON THE PILOT?S STATEMENT AND OUR EXAMINATION OF THE AUTOGYRO IT APPEARS THAT THERE WERE NO MECHANICAL ISSUES WITH THE AUTOGYRO. BASED ON OUR INVESTIGATION IT APPEARS THAT THE PILOT FAILED TO PULL THE CONTROL STICK BACK TO ITS FULL AFT POSITION WHICH THEREFORE CAUSED THE ROTOR DISC TO FAIL TO REACH THE POSITION REQUIRED FOR A SAFE TAKEOFF.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.