Robinson R44

Uvalde, TX — January 8, 2019

Event Information

DateJanuary 8, 2019
Event TypeACC
NTSB NumberCEN19LA065
Event ID20190108X54945
LocationUvalde, TX
CountryUSA
Coordinates29.21028, -99.74306
AirportGarner Field
Highest InjuryMINR

Aircraft

MakeRobinson
ModelR44
CategoryHELI
FAR Part091
Aircraft DamageSUBS

Conditions

Light ConditionDAYL
WeatherVMC

Injuries

Fatal0
Serious0
Minor1
None1
Total Injured1

Event Location

Probable Cause

The slipping of the sprag clutch due to galling of the sprags and corresponding sprag contact surfaces within the clutch assembly, which rendered the helicopter uncontrollable.

Full Narrative

On January 8, 2019, about 1000 central standard time, a Robinson R44 II helicopter, N484AB, experienced a hard landing during an autorotation shortly after takeoff from Garner Field Airport, Uvalde, Texas. The flight instructor sustained minor injuries, the student pilot was not injured, and the helicopter sustained substantial damage. The helicopter was registered to and operated by a private individual as a Title 14 Code of Federal Regulations Part 91 instructional flight. Visual meteorological conditions prevailed at the time of the accident, and a flight plan was not filed. The local flight was originating at the time of the accident.

According to the flight instructor, all pre-takeoff checks were normal with no anomalies noted. Once the helicopter was through effective translational lift and about 40 knots airspeed, the collective was raised to increase the available power to takeoff power setting. Shortly thereafter, a loud pop/bang was heard followed by an uncommanded right yaw and severe vibrations. Due to the low altitude and airspeed, the flight instructor immediately initiated an autorotation. Upon touchdown, the helicopter tilted forward with the main rotor blades about 6 inches from contacting the ground. The flight instructor applied aft cyclic to correct, and the main rotor blades contacted the tailboom.

Postaccident examination of the helicopter revealed the tailboom was partially separated, and the tail rotor driveshaft system was damaged. During the examination, the clutch assembly lubricant was drained and an unusual amount of metallic debris was noted in the strainer. The clutch assembly was removed and sent to Robinson Helicopter Company for further examination.

Examination and disassembly of the clutch assembly revealed galling of the sprags and the corresponding sprag contact surfaces on the shaft and hub.

According to the Robinson R44 maintenance manual, the clutch assemblies are to be inspected for metallic flakes every 500 hours. The most recent inspection on the clutch assembly was completed on April 18, 2018, about 245 hours prior to the accident.

About This NTSB Record

This aviation event was investigated by the National Transportation Safety Board (NTSB). NTSB investigates all U.S. civil aviation accidents to determine probable cause and issue safety recommendations to prevent future accidents.

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