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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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February 13, 1995 · Sikorsky S-58JT · N1099T

Marblemount, WA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
February 13, 1995
Injury Outcomes
1 injury (1 serious injury)
Location
Marblemount, WA
Aircraft
Sikorsky S-58JT
Tail Number
N1099T
Injuries
Serious
Aircraft Damage
Substantial
NTSB Number
SEA95LA051

THE MAIN ROTOR DRIVESHAFT FAILED DUE TO FATIGUE FAILURE WHILE THE PILOT WAS CONDUCTING HELICOPTER LOGGING OPERATIONS. THE MAIN ROTOR DRIVESHAFT HAD 952 HOURS SINCE NEW, AND HAD BEEN INSTALLED NEW AT THE MOST RECENT GEARBOX OVERHAUL. OVERHAUL PERIOD AND MAIN ROTOR DRIVESHAFT RETIREMENT TIME ARE 2500 HOURS. THE PILOT WAS NOT AT AN ALTITUDE OR AIRSPEED WHERE A SUCCESSFUL AUTOROTATION COULD BE ACCOMPLISHED.

NTSB Probable Cause

FATIGUE FAILURE OF THE MAIN ROTOR DRIVESHAFT.

Full Narrative

On February 13, 1995, approximately 1020 Pacific standard time, a Sikorsky S-58JT, N1099T, sustained substantial damage during a forced landing after a main rotor mast failure while conducting helicopter logging operations. The commercial pilot, who was the sole occupant of the aircraft, was seriously injured. There was no fire, and no flight plan was filed for the flight, which was conducted near Marblemount, Washington, and had departed approximately 1010. The ELT actuated, but did not aid in locating the accident site. A witness stated that the pilot had just hooked a load, then released it and descended rapidly to impact. He described hearing an engine sound increasing in rpm before the crash. The pilot stated that he had a 150 foot long-line attached, and about ten minutes into his cycle, heard a loud bang while picking up a load. He said he tried to move the load downhill, away from the ground crew person, released the load and long-line, and turned the aircraft to head down slope. The aircraft impacted the terrain. Post accident investigation revealed that the main rotor shaft, P/N S1635-20059-2, S/N HR243, which had been installed new on August 16, 1993, during the last main gearbox overhaul, had separated through the shaft-to-flange radius. The part had 952 hours total time since new. The normal transmission overhaul period and main rotor shaft retirement time are both 2500 hours.

Flight

Event TypeAccident
Event Time10:20 PST
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftSikorsky S-58JT
Tail NumberN1099T
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 133
Engines2
Engine TypeTurboshaft
Engine DetailsP&W · PT6-T3 · Turboshaft · 1800
Seats2

People & Injuries

Injury Summary1 injury (1 serious injury)
Fatal0
Serious1
Minor0
Uninjured0
Total1
Crew 1Age 54 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind45° @ 5 kt, gusting 8 kt
Visibility75 sm
CeilingNone
Temperature / Dew Point28 C / 0 C
Altimeter29.00 inHg
Weather SourceWIT

Appendix: Source Data