- Date
- October 11, 2024, 16:50 local (20:50 UTC)
- Place
- Plymouth, IN
- Injuries
- 2 minor
- Damage
- Substantial damage
- Phase of flight
- Approach
- Aircraft
- N314ACRotorway Exec
- Defining event
- Approach-VFR pattern base: Sys/Comp malf/fail (non-power)
- Weather
- Visual (VMC) · Day
- Status
- Completed
- Report
- Approved by Office Director
- Investigation class
- Class 3
- NTSB office
- Central Region
- Parties
- FAA
- FAA report
- 20241011016869A
- Case key
- 195315
From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.
On this page
Probable cause
A loss of control due to the failed forward tail rotor belt as a result of the owner’s failure to follow the helicopter manufacturer’s tail rotor belt replacement recommendations.
Findings · 5
NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.
Sequence of events
The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.
Analysis
The helicopter owner/pilot reported that while he and his flight instructor were practicing an autorotation, the flight instructor heard a noise. Shortly thereafter, the helicopter started to yaw to the left and the airspeed decreased. The flight instructor took over control of the helicopter and initiated an autorotation to a corn field. The right skid caught the ground, and the helicopter rolled onto its right side. The main rotor and fuselage sustained substantial damage. A postaccident examination revealed that the forward tail rotor belt broke. The belt was found frayed at the separation point. A review of the tail rotor maintenance records revealed that the tail rotor belts had not been replaced since 2006. The manufacturer recommends tail rotor belt replacement at 250 hours, 2 years, or as needed upon conditional inspections, whichever comes first. The operator reported that before the accident the belts appeared to be in satisfactory condition but acknowledged they were beyond the 2-year service life and should have been replaced.
Factual narrative
On October 11, 2024, about 1650 eastern daylight time, a Rotorway Executive 90, N314AC, was substantially damaged when it was involved in an accident near Plymouth, Indiana. The two pilots sustained minor injuries. The helicopter was operated as a Title 14 Code of Federal Regulations Part 91 instructional flight. The owner and his flight instructor were flying the helicopter so the owner could gain proficiency. While preparing to practice an autorotation in the traffic pattern, the flight instructor told the owner that he heard a noise. Shortly thereafter, the nose of the helicopter started to yaw to the left. Airspeed began to slow, and the left yaw accelerated. The flight instructor took control of the helicopter and autorotated into a cornfield. The right skid caught the ground; the helicopter rolled onto its side, and came to rest on its right side. The main rotor and fuselage were substantially damaged. A postaccident examination revealed that the forward tail rotor drive belt was broken. The belt was frayed at the separation point. According to the owner, who is also an airframe and powerplant mechanic, the helicopter was in storage for several years before he purchased it in September 2024. A review of the tail rotor maintenance records revealed that after purchase, the owner inspected the tail rotor pulleys, bearings, bolts, and belt tension. He also greased the tail rotor slider. The annual condition inspection was signed off on the day of the accident. The maintenance manual for the helicopter recommends that the tail rotor belts be replaced every 250 hours, every 2 years, or as needed upon condition inspections, whichever comes first. All three tail rotor belts were replaced in January 2006 and the center tail rotor belt was replaced in September 2006. There is no indication in the tail rotor maintenance records that any of the tail rotor belts were replaced after 2006. The operator reported that before the accident the belts appeared to be in satisfactory condition but acknowledged they were beyond the 2-year service life and should have been replaced.
Aircraft
- Registration
- N314AC
- Reported as
- Rotorway Exec (90)
- Category
- Helicopter, amateur-built
- Serial number
- 1961
- Built
- 2004
- Airframe hours
- 232
- Engine
- Rotorway International RW 162, 150 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Instructional · Part 91
- Operator
- Rutherford Stephen M
- Registered owner
- Rutherford Stephen M
- Airworthiness certificate
- Special, Experimental (Special)
- Last inspection
- Condition · October 11, 2024
- Departed
- C65 · Plymouth, IN
- Airport
- C65 · Plymouth Municipal
- Equipment
- None
Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.
Flight crew · 2
As NTSB recorded them. NTSB leaves out names.
- Role
- Pilot
- Age
- 52
- Injuries
- Minor
- Certificates
- Flight instructor, Commercial
- Airplane ratings
- Single-engine land
- Instrument ratings
- Helicopter, Airplane
- Medical
- Class 3, Without waivers/limitations
- Last flight review
- April 17, 2023
- Seat
- Left
- Restraint
- 4-point
- Flight hours
- 3,457 total · 2 in this make and model · 2,818 as pilot in command · 18 in the last 90 days · 9 in the last 30 days · 2 in the last 24 hours
- Role
- Flight instructor
- Age
- 56
- Injuries
- Minor
- Certificates
- Flight instructor, Commercial
- Airplane ratings
- Single-engine land
- Medical
- Class 2, With waivers/limitations
- Last flight review
- June 23, 2023
- Seat
- Right
- Restraint
- 4-point
- Flight hours
- 3,930 total · 320 in this make and model · 3,865 as pilot in command · 91 in the last 90 days · 37 in the last 30 days · 4 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 230° at 9 knots
- Visibility
- 10 statute miles
- Lowest ceiling
- None
- Temperature
- 81 °F, dew point 45 °F
- Altimeter
- 30.04 inHg
- Observed at
- KC65, 5 nm away
- METAR
- KC65 112055Z AUTO 23009KT 10SM CLR 27/07 A3004
Docket · 5
The files NTSB released with the investigation on April 2, 2025, on NTSB’s docket system: statements, records, photos and specialists’ reports. 4.2 MB in all.
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.