N379SH

Substantial
None

ROBINSON HELICOPTER R44S/N: 2240

Accident Details

Date
Sunday, October 1, 2023
NTSB Number
CEN24LA004
Location
Hochatown, OK
Event ID
20231003193182
Coordinates
34.160278, -94.752222
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A total loss of engine power during a practice autorotation due to the improper engine idle setting and rigging of the carburetor heat control which resulted in a hard landing.

Aircraft Information

Registration
N379SH
Make
ROBINSON HELICOPTER
Serial Number
2240
Engine Type
Reciprocating
Year Built
2012
Model / ICAO
R44R44
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
SPITZER HELICOPTER LLC
Address
1209 ORANGE ST
Status
Deregistered
City
WILMINGTON
State / Zip Code
DE 19801
Country
United States

Analysis

On October 1, 2023, about 1230 central daylight time, a Robinson Helicopter Company R44, N379SH, was substantially damaged when it was involved in an accident near Hochatown, Oklahoma. The pilot was not injured. The helicopter was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot, who was also a flight instructor, reported that he was conducting a practice autorotation during a proficiency flight about 400 ft agl. As he reduced the engine speed to idle to simulate a loss of engine power, the engine lost total power. The pilot entered an autorotation and completed a forced landing to a field. The helicopter landed hard and the tailboom was severed by the main rotor blades. The pilot exited the helicopter unassisted.

The helicopter sustained substantial damage to the tailboom and the main rotor blades. A postaccident examination revealed that the carburetor heat control knob was jammed in the full heat position. Further examination revealed that the carburetor heat control cable was rigged so that the cable was pulled beyond the end of the cable conduit sleeve (figure 1). When the carburetor heat knob was actuated, the control cable would bind with the conduit sleeve.

Figure 1: Carburetor heat control cable as found. The cable is free from the conduit sleeve (circled in yellow).

Figure 2 shows a normal engagement of the carburetor heat control cable in the conduit sleeve.

Figure 2. The normal engagement of the carburetor heat cable and conduit. Cable is inserted into the conduit sleeve (circled in yellow).

No other anomalies were found within the rigging or flight controls that would have precluded normal operation.

Single contact marks on the fore and aft faces of the upper sheave and adjacent components are consistent with the engine not running at the time of impact. The V-belts and tail boom were cut and removed to facilitate an engine run. The engine started and ran at various power settings. The idle was set to below 50 percent (the typical idle speed without V-belts is 60-65 percent). Robinson Helicopter Company Safety Notices 27 and 38 advise on how to slowly reduce throttle while practicing autorotations. RHC Safey Notice 27 states that during simulated power failures, “throttle should be rolled off smoothly, never ‘chopped.’”

A review of the helicopter maintenance records revealed that on August 25, 2022, the engine was overhauled and installed, and an annual inspection of the helicopter was completed. The last 100-hour inspection was completed on August 16, 2023. The helicopter had accumulated 44.2 hours since the 100-hour inspection. Investigators were unable to determine the last time the carburetor control cable was rigged or when the engine idle was set.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN24LA004