20010227004159A

Accident · No damage

FAA accident report · Robsin R22 · Seattle, WA · February 27, 2001

Date
February 27, 2001 · 14:31 local
Place
Seattle, WA
Airport
Boeing Field-King County International
Operating rules
General operating rules (Part 91)
Damage
No damage
Aircraft
N8362Q
NTSB investigation
NTSBSEA01LA054
Reported as
Robsin R22

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.

(-23) While performing practice touchdown autorotation to the west taxiway, the aircraft sustained a hard landing/rotor system sudden stoppage. Debris from the aircraft tail boom was spread east in the direction of active runway 31L with the tail roto driveshaft contained inside the tail boom being sent across teh runway, landing in-between runway 31L and the east taxiway. No mechanical abnormalities were reported by the flight crew. Flight control continuity was verified after the accident, with only post crash damage being noted in the tail rotor flight control system. Engine controls were also found to be functional.

As the FAA filed it

(-23) WHILE PERFORMING PRACTICE TOUCHDOWN AUTOROTATION TO THE WEST TAXIWAY, THE AIRCRAFT SUSTAINED A HARD LANDING/ROTOR SYSTEM SUDDEN STOPPAGE. DEBRIS FROM THE AIRCRAFT TAIL BOOM WAS SPREAD EAST IN THE DIRECTION OF ACTIVE RUNWAY 31L WITH THE TAIL ROTO DRIVESHAFT CONTAINED INSIDE THE TAIL BOOM BEING SENT ACROSS TEH RUNWAY, LANDING IN-BETWEEN RUNWAY 31L AND THE EAST TAXIWAY. NO MECHANICAL ABNORMALITIES WERE REPORTED BY THE FLIGHT CREW. FLIGHT CONTROL CONTINUITY WAS VERIFIED AFTER THE ACCIDENT, WITH ONLY POST CRASH DAMAGE BEING NOTED IN THE TAIL ROTOR FLIGHT CONTROL SYSTEM. ENGINE CONTROLS WERE ALSO FOUND TO BE FUNCTIONAL.

NTSB investigation

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

Other reports on N8362Q · 1

Matched to the same aircraft by N-number and date.