20210208002329A

Accident · Substantial damage

FAA accident report · MD Helicopters 369E · Mesa, AZ · February 8, 2021

Date
February 8, 2021 · 15:30 local
Place
Mesa, AZ
Airport
Falcon Field
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N7032V
NTSB investigation
NTSBWPR21LA109
Reported as
MD Helicopters 369E
Reported engine
Allison 250-C20 series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
5,641 total620 in this make and model66 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.

MD helicopters instructor pilot was providing training to a foreign military customer pilot when during an autorotation the aircraft landed with the rear end of the skids low and striking the ground first. The student maintained some aft cyclic input lowering the blades rearward so that when the rear struts expanded after compression from striking the ground, the tail boom was pushed upward into the path of the rotor blades. This did significant damage to the tail boom and to the rotor blades. Counseling was given to convey best practices concerning leveling the aircraft before ground contact.

As the FAA filed it

MD HELICOPTERS INSTRUCTOR PILOT WAS PROVIDING TRAINING TO A FOREIGN MILITARY CUSTOMER PILOT WHEN DURING AN AUTOROTATION THE AIRCRAFT LANDED WITH THE REAR END OF THE SKIDS LOW AND STRIKING THE GROUND FIRST. THE STUDENT MAINTAINED SOME AFT CYCLIC INPUT LOWERING THE BLADES REARWARD SO THAT WHEN THE REAR STRUTS EXPANDED AFTER COMPRESSION FROM STRIKING THE GROUND, THE TAIL BOOM WAS PUSHED UPWARD INTO THE PATH OF THE ROTOR BLADES. THIS DID SIGNIFICANT DAMAGE TO THE TAIL BOOM AND TO THE ROTOR BLADES. COUNSELING WAS GIVEN TO CONVEY BEST PRACTICES CONCERNING LEVELING THE AIRCRAFT BEFORE GROUND CONTACT.

NTSB investigation

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