Robinson R22

Fort Myers, FL — September 6, 2020

Event Information

DateSeptember 6, 2020
Event TypeACC
NTSB NumberERA20LA310
Event ID20200909X14532
LocationFort Myers, FL
CountryUSA
Coordinates26.58667, -81.86333
AirportPAGE FIELD
Highest InjuryNONE

Aircraft

MakeRobinson
ModelR22
CategoryHELI
FAR Part091
Aircraft DamageSUBS

Conditions

Light ConditionDAYL
WeatherVMC

Injuries

Fatal0
Serious0
Minor0
None2
Total Injured0

Event Location

Probable Cause

Foreign object damage of the turning tailrotor by a soft-bodied object, which resulted in the sudden stoppage of the tailrotor and the catastrophic failure of the tailrotor assembly and its mount structure.

Full Narrative

On September 6, 2020, about 0900 eastern daylight time, a Robinson R22 Mariner helicopter, N194HC, was involved in an accident near Fort Myers, Florida. The commercial pilot and his airline transport-rated pilot receiving instruction were not injured. The helicopter was operated as a Title 14 Code of Federal Regulations Part 91 instructional flight.
The instructor and pilot receiving instruction each submitted written statements, and their versions of events were consistent throughout. The preflight and engine-start procedures were completed with no anomalies noted. As the engine accelerated to near its operating rpm, both pilots heard a loud “bang.” The pilot receiving instruction leaned out his door and announced that “the tail was hanging off the back of the aircraft.” The pilots shut down the helicopter and reported the event to the helicopter’s owner and his mechanic.

In a telephone interview, the pilot receiving instruction said that, after the helicopter was shut down, he observed no evidence that an unsecured aircraft cover, clothing item, or bird had struck the tailrotor. He added that the only debris surrounding the helicopter on the ramp was aircraft wreckage.
Examination of photographs revealed damage to the tailrotor driveshaft, tailrotor gearbox, tailrotor blades, and the tailcone’s section forward of the tailrotor gearbox. These areas and components were sectioned and forwarded to the NTSB Materials Laboratory in Washington, DC for examination.
Examination of all the submitted components revealed signatures consistent with overstress fracture on all the fracture surfaces. There was no evidence of fatigue. There was no evidence (mechanical/paint transfer/biological) of foreign object damage (FOD).
The fractures and impact signatures were consistent with the fracture of the tailrotor gearbox mount structure (bulkhead) of the tailcone, followed by impact signatures of the rotating tailrotor assembly against the vertical and horizontal stabilizers.

About This NTSB Record

This aviation event was investigated by the National Transportation Safety Board (NTSB). NTSB investigates all U.S. civil aviation accidents to determine probable cause and issue safety recommendations to prevent future accidents.

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