Plane Crash List

Enstrom TH-180 N180TH

12 February 2016 · Menominee, Michigan, United States · No injuries

Summary

On 12 February 2016 at about 17:23 local time, a Enstrom TH-180 registered N180TH was involved in an accident near Menominee, Michigan, United States. One person was on board and nobody was injured. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 17:23
Classification
Accident
Location
Menominee, Michigan, United States
Nearest airport
Menominee-Marinette Twin Count (MNM)
Coordinates
45.1125, -87.6250
Aircraft
Enstrom TH-180
Registration
N180TH
Category
Helicopter
Year built
2015
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Flight Test
Phase of flight
Not recorded
Route
Menominee → Menominee
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
CEN16LA105

People

Nobody was injured.

On board Died Serious Minor Uninjured
1 0 0 0 1

Probable cause

The failure of the torque meter mounting bolts, which resulted in a loss of engine power to the main drive belt and rotors.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The commercial pilot of the helicopter departed to conduct a flight test of an onboard data acquisition system. About 18 minutes later, the pilot decided to return to the airport because of weather moving into the area. On final approach, the pilot felt a "jolt in the airframe," and the helicopter yawed left and began to descend. The pilot added engine power, but the main rotor rpm continued to decay until the low rotor rpm horn sounded. The pilot entered an autorotation to a city street in a residential neighborhood. During the landing, the main rotor struck an electric utility pole and the helicopter slid 300 ft before coming to a stop. A postaccident examination of the helicopter revealed that the eight mounting bolts for the engine torque meter had sheared, separating the engine from the main belt drive system. The torque meter was test equipment installed between the engine prop flange and a modified lower drive pulley for the purpose of gathering engine data during the flight tests. No other preaccident anomalies were found.

Quoted verbatim from the NTSB record.

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