20210122002339A

Accident · Substantial damage

FAA accident report · Mcdonnell Douglas Helicopter 369E · Queen Creek, AZ · January 22, 2021

Date
January 22, 2021 · 09:30 local
Place
Queen Creek, AZ
Airport
Rittenhouse Army Heliport
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N90TG
NTSB investigation
NTSBWPR21LA093
Reported as
Mcdonnell Douglas Helicopter 369E
Reported engine
Allison 250-C20 series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Airline transport
Pilot’s flight hours
20,456 total1 in this make and model1 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.

On 22 January 2021 at around 1630 zulu 0930 MST N90TG, a 1990 Mcdonnell Douglas Helicopter, model 369E serial number 383E, was on approach to Rittenhouse Army Heliport (A38), which approximately 10 miles south of falcon field (ffz) in mesa, Arizona. The pilot stated he completed a few approaches at the Army heliport practice area and traveled a couple miles south east to set up for a practice approach to an off airport location. Pilot stated all was normal and as he increased in collective and added to come into a hover, he stated the rotorcraft nosed right. Pilot tried to arrest it motion with left pedal input but was unable to recover. Rotorcraft spun right and left skid caught the ground and bent inward as the rotorcraft rolled onto its left side. No injuries reported and 1 person on board. Substantial damage to the rotorcraft. Speaking with an operations safety inspector through an assist, it was determined that the pilot lacked the ability to remember the governor transition of the turbine powered rotorcraft engine to the main drive. It is believed that improper management of the throttle by the pilot resulted in the governor inability to automatically takeover for the power input resulting in a less than normal needed power input physically by the pilot result in a loss of tail rotor effectiveness causing the yaw moment into the rotorcraft rolling over. Pilot had only 0.8 hours in systems training for this make/model and no prior experience in turbine power rotorcraft except for 1 hour of training. The flight was for personal use to build time. The pilot received counseling refer to activity WP07202101570 for counseling details.

As the FAA filed it

ON 22 JANUARY 2021 AT AROUND 1630 ZULU 0930 MST N90TG, A 1990 MCDONNELL DOUGLAS HELICOPTER, MODEL 369E SERIAL NUMBER 383E, WAS ON APPROACH TO RITTENHOUSE ARMY HELIPORT (A38), WHICH APPROXIMATELY 10 MILES SOUTH OF FALCON FIELD (FFZ) IN MESA, ARIZONA. THE PILOT STATED HE COMPLETED A FEW APPROACHES AT THE ARMY HELIPORT PRACTICE AREA AND TRAVELED A COUPLE MILES SOUTH EAST TO SET UP FOR A PRACTICE APPROACH TO AN OFF AIRPORT LOCATION. PILOT STATED ALL WAS NORMAL AND AS HE INCREASED IN COLLECTIVE AND ADDED TO COME INTO A HOVER, HE STATED THE ROTORCRAFT NOSED RIGHT. PILOT TRIED TO ARREST IT MOTION WITH LEFT PEDAL INPUT BUT WAS UNABLE TO RECOVER. ROTORCRAFT SPUN RIGHT AND LEFT SKID CAUGHT THE GROUND AND BENT INWARD AS THE ROTORCRAFT ROLLED ONTO ITS LEFT SIDE. NO INJURIES REPORTED AND 1 PERSON ON BOARD. SUBSTANTIAL DAMAGE TO THE ROTORCRAFT. SPEAKING WITH AN OPERATIONS SAFETY INSPECTOR THROUGH AN ASSIST, IT WAS DETERMINED THAT THE PILOT LACKED THE ABILITY TO REMEMBER THE GOVERNOR TRANSITION OF THE TURBINE POWERED ROTORCRAFT ENGINE TO THE MAIN DRIVE. IT IS BELIEVED THAT IMPROPER MANAGEMENT OF THE THROTTLE BY THE PILOT RESULTED IN THE GOVERNOR INABILITY TO AUTOMATICALLY TAKEOVER FOR THE POWER INPUT RESULTING IN A LESS THAN NORMAL NEEDED POWER INPUT PHYSICALLY BY THE PILOT RESULT IN A LOSS OF TAIL ROTOR EFFECTIVENESS CAUSING THE YAW MOMENT INTO THE ROTORCRAFT ROLLING OVER. PILOT HAD ONLY 0.8 HOURS IN SYSTEMS TRAINING FOR THIS MAKE/MODEL AND NO PRIOR EXPERIENCE IN TURBINE POWER ROTORCRAFT EXCEPT FOR 1 HOUR OF TRAINING. THE FLIGHT WAS FOR PERSONAL USE TO BUILD TIME. THE PILOT RECEIVED COUNSELING REFER TO ACTIVITY WP07202101570 FOR COUNSELING DETAILS.

NTSB investigation

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