Robinson R44

Sardis, GA — September 17, 2019

Event Information

DateSeptember 17, 2019
Event TypeACC
NTSB NumberERA19LA273
Event ID20190917X85414
LocationSardis, GA
CountryUSA
Coordinates33.02806, -81.78778
Highest InjurySERS

Aircraft

MakeRobinson
ModelR44
CategoryHELI
FAR Part137
Aircraft DamageSUBS

Conditions

Light ConditionDAYL
WeatherVMC

Injuries

Fatal0
Serious1
Minor0
None0
Total Injured1

Event Location

Probable Cause

Fatigue failure of the fasteners on the engine crankshaft, which resulted in a partial loss of engine power and a subsequent forced landing.

Full Narrative

On September 17, 2019, about 1230 eastern daylight time, a Robinson R44, N827JE, was substantially damaged when it was involved in an accident near Sardis, Georgia. The pilot was seriously injured. The helicopter was operated as Title 14 Code of Federal Regulations Part 137 aerial application flight.
The pilot reported that he was flying about 100 ft above ground level, applying spray, when he heard a "pop," followed by alarms and lights activating in the cockpit. The helicopter then lost engine power and the pilot performed an autorotation. During the autorotation, the helicopter impacted trees and terrain.
Examination of the helicopter by a Federal Aviation Administration inspector revealed that it came to rest on its left side. The inspector observed damage to the fuselage and the tail boom had separated.
Subsequent teardown examination of the engine revealed that the left crankshaft idler gear was not engaged in the teeth of the crankshaft gear or the camshaft gear. The idler gear was removed and the idler gear shaft was observed not attached to its left crankcase half mounting location. According to an engine diagram, the idler gear shaft was supposed to secured to the left crankcase half by a bolt and a crankcase stud. Worn fragments of the bolt and crankcase stud, along with the stud nut and fragments of safety wire, were recovered from the oil sump.
Metallurgical examination revealed evidence of wear on crankshaft idler gear, shaft flange, and gear shaft fasteners (bolt and stud). The worn gear shaft fasteners exhibited a rotating bending fatigue failure (for more information, see Materials Laboratory Factual Report in the public docket for this accident).
According to maintenance records and information from the operator, the engine had been operated for about 1,900 hours over a 20-year-period since major overhaul. Review of Lycoming Service Instruction (SI) 1009BD, superseded by SI 1009BE, revealed a recommended time between overhauls as 12 calendar years or 1,500 hours of operation in the case of engines used in crop dusting or other chemical application, whichever occurs first.

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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