N9285

Substantial
None

ENSTROM 280S/N: 1003

Accident Details

Date
Saturday, August 21, 2021
NTSB Number
ERA21LA339
Location
Port Orange, FL
Event ID
20210826103759
Coordinates
29.079762, -81.047110
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The failure of the tail rotor drive shaft at the coupling due to torsionally applied shear stress.

Aircraft Information

Registration
Make
ENSTROM
Serial Number
1003
Engine Type
Reciprocating
Year Built
1978
Model / ICAO
280EN28
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
3
FAA Model
280C

Registered Owner (Current)

Name
MOTT WILLIAM R
Address
115 WELCOME LAKE ESTATES LN
City
BEACH LAKE
State / Zip Code
PA 18405-7722
Country
United States

Analysis

On August 21, 2021, about 1330 eastern daylight time, an Enstrom 280C, N9285, was substantially damaged when it was involved in an accident in Daytona Beach, Florida. The pilot was not injured. The helicopter was operated as a Title 14 Code of Federal Regulations Part 91personal flight.

According to the pilot, he conducted a local flight around Spruce Creek Airport (7FL6), Daytona Beach, Florida, and was approaching to land. Just prior to touchdown, the helicopter made an uncommanded climb and started to spin to the right. The pilot applied full left pedal, but the helicopter continued to spin to the right. He lowered the collective and the helicopter landed hard on the skids. The left skid was damaged during, fuselage frame, and the tail rotor blades were damaged during the landing.

Postaccident examination of the helicopter revealed that the tail rotor driveshaft was free to spin inside the coupling and not connected by a through bolt. The coupling and a section of the drive shaft were forwarded to the National Transportation Safety Board’s Material Laboratory for further examination. The examination revealed that the bolt holes in the drive shaft tube were mechanically distorted consistent with the presence of an axially applied torsional shear-stress in the drive shaft tube in the clockwise direction. Macroscopically, the fracture surface in the drive shaft tube was consistent with overstress due to torsionally applied shear stress (for more information, see Materials Laboratory Factual Report in the public docket for this investigation).

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA21LA339