N2686

Substantial
None

HILLER UH 12AS/N: 168

Accident Details

Date
Monday, September 11, 2017
NTSB Number
CEN17LA375
Location
Griffith, IN
Event ID
20171023X94913
Coordinates
41.519721, -87.399444
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The loss of tail rotor thrust due to a failed tail rotor driveshaft, which resulted in a loss of tail rotor control and a hard landing.

Aircraft Information

Registration
N2686
Make
HILLER
Serial Number
168
Engine Type
Reciprocating
Model / ICAO
UH 12AUH12
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
DAVIS MONTE L
Address
6119 W 125TH AVE
Status
Deregistered
City
CROWN POINT
State / Zip Code
IN 46307-8721
Country
United States

Analysis

On September 11, 2017, about 1100 central daylight time, a Hiller UH-12A helicopter, N2686, registered to a private individual, sustained substantial damage after a loss of directional control and collision with the ground following a loss of the tail rotor drive in the vicinity of Griffith, Indiana. The certified helicopter flight instructor (CFI) and his student were not injured. Visual meteorological conditions prevailed throughout the area and no flight plane was filed. The local instructional flight was being conducted under the provisions of Federal Code of Regulations Part 91. The fight originated at 1050 from the Griffith-Merriillville Airport (O5C), Griffith, Indiana.

The CFI stated that he was providing dual flight instruction to a student pilot. About 10 minutes into the flight, while in a 3-5 foot hover, the student began to lose control and the helicopter began to spin to the right. As the student could not regain control, the CFI took the controls. Upon taking the controls, the helicopter was not responding to cyclic inputs and left pedal input. At this point, the CFI assumed a loss of thrust from the tail rotor. He rolled the throttle off and the helicopter settled to the ground and landed hard.

After asking if his student was ok, the CFI exited the helicopter while the main rotor was still spinning. He observed the tail rotor and tail rotor drive shaft were not spinning and could hear a grinding noise near the connection of the transmission output shaft and the tail rotor drive shaft. After the main rotor stopped spinning, the CFI found the tail rotor guard had broken off the helicopter and was laying about 20-feet away. The CFI did not recall if or when the tail rotor guard struck the ground.

The helicopter was towed to a hangar and was inspected by a local mechanic and FAA inspector. During the inspection, it was discovered that the tail rotor driveshaft had failed near the output shaft of the tail rotor drive assembly. Substantial damage was incurred to the tail rotor and tail boom. Maintenance records were not available.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN17LA375