20050715015809A

Accident · Substantial damage

FAA accident report · Robsin R22 BETA · Phoenix, AZ · July 15, 2005

Date
July 15, 2005 · 09:02 local
Place
Phoenix, AZ
Airport
Williams Gateway Airport
Phase of flight
Hovering
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N7514P
NTSB investigation
NTSBLAX05CA232
Reported as
Robsin R22BETA
People aboard
2
Fatal injuries
0
Pilot’s flight hours
449 total407 in this make and model245 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.

(-23) On July 15, 2005, at approximately 0902 MST, N7514P, a Robinson R-22-beta helicopter, with the pilot privacy data omitted performing as a CFR and pilot-in-command, and privacy data omitted receiving dual instruction, were performing hovering auto practice at Williams Gateway Airport in mesa, Arizona. privacy data omitted Stated he was performing his third hovering autorotation after two previous successful hovering autorotations. The aircraft was positioned at the intersection of taxiway charlie and hotel. While stabilized into the wind on a heading of 300 degrees, with the aircraft at approximately 2 foot skid height, privacy data omitted initiated the maneuver by rolling the throttle up rapidly and adding right anti-torque pedal. This action caused the aircraft to rapidly begin a spin to the right. The instructor attempted to assist on the flight controls and rolled the throttle to idle. Additionally, the instructor attempted to add left anti-torque pedal, but was unable to override the student's appication of right anti-torque pedal due to the student having his right leg locked at the knee. The aircraft began to settle while still in a right spin and the toe of the right skid contacted the ground. The aircraft then encountered dynamic rollover and came to rest on its right side on a heading of approximately 120 degrees. The crew performed an emergency shutdown of the engine and exited the aircraft. Neither crewmemembers sustained injuries. The aircraft sustained damage to the main rotor blades, tail boom assembly, and right side of the fuselage.

As the FAA filed it

(-23) ON JULY 15, 2005, AT APPROXIMATELY 0902 MST, N7514P, A ROBINSON R-22-BETA HELICOPTER, WITH THE PILOT ^PRIVACY DATA OMITTED^ PERFORMING AS A CFR AND PILOT-IN-COMMAND, AND ^PRIVACY DATA OMITTED^ RECEIVING DUAL INSTRUCTION, WERE PERFORMING HOVERING AUTO PRACTICE AT WILLIAMS GATEWAY AIRPORT IN MESA, ARIZONA. ^PRIVACY DATA OMITTED^ STATED HE WAS PERFORMING HIS THIRD HOVERING AUTOROTATION AFTER TWO PREVIOUS SUCCESSFUL HOVERING AUTOROTATIONS. THE AIRCRAFT WAS POSITIONED AT THE INTERSECTION OF TAXIWAY CHARLIE AND HOTEL. WHILE STABILIZED INTO THE WIND ON A HEADING OF 300 DEGREES, WITH THE AIRCRAFT AT APPROXIMATELY 2 FOOT SKID HEIGHT, ^PRIVACY DATA OMITTED^ INITIATED THE MANEUVER BY ROLLING THE THROTTLE UP RAPIDLY AND ADDING RIGHT ANTI-TORQUE PEDAL. THIS ACTION CAUSED THE AIRCRAFT TO RAPIDLY BEGIN A SPIN TO THE RIGHT. THE INSTRUCTOR ATTEMPTED TO ASSIST ON THE FLIGHT CONTROLS AND ROLLED THE THROTTLE TO IDLE. ADDITIONALLY, THE INSTRUCTOR ATTEMPTED TO ADD LEFT ANTI-TORQUE PEDAL, BUT WAS UNABLE TO OVERRIDE THE STUDENT'S APPICATION OF RIGHT ANTI-TORQUE PEDAL DUE TO THE STUDENT HAVING HIS RIGHT LEG LOCKED AT THE KNEE. THE AIRCRAFT BEGAN TO SETTLE WHILE STILL IN A RIGHT SPIN AND THE TOE OF THE RIGHT SKID CONTACTED THE GROUND. THE AIRCRAFT THEN ENCOUNTERED DYNAMIC ROLLOVER AND CAME TO REST ON ITS RIGHT SIDE ON A HEADING OF APPROXIMATELY 120 DEGREES. THE CREW PERFORMED AN EMERGENCY SHUTDOWN OF THE ENGINE AND EXITED THE AIRCRAFT. NEITHER CREWMEMEMBERS SUSTAINED INJURIES. THE AIRCRAFT SUSTAINED DAMAGE TO THE MAIN ROTOR BLADES, TAIL BOOM ASSEMBLY, AND RIGHT SIDE OF THE FUSELAGE.

NTSB investigation

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