- Date
- February 13, 1995, 10:20 local (18:20 UTC)
- Place
- Marblemount, WA
- Injuries
- 1 serious
- Damage
- Substantial damage
- Phase of flight
- Maneuvering
- Aircraft
- N1099TSikorsky S-58JT
- Weather
- Visual (VMC) · Day
- Status
- Completed · report July 24, 1995
- Report
- Approved by Office Director
- FAA report
- 19950213001699A
- Case key
- 42110
From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.
On this page
Probable cause
Fatigue failure of the main rotor driveshaft.
Sequence of events
NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.
Analysis
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.
Factual 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.
Aircraft
- Registration
- N1099T
- Reported as
- Sikorsky S-58JT
- Category
- Helicopter
- Serial number
- 58-1646
- Airframe hours
- 9,776
- Engine
- P&W PT6-T3, 1,800 horsepower, turbo shaft
- Damage
- Substantial damage
- Flight
- Other work use · Part 133
- Registered owner
- Glacier Helicopters
- Airworthiness certificate
- Standard, Transport
- Last inspection
- Continuous airworthiness · February 9, 1995 · 14 hours before
Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.
Flight crew
As NTSB recorded them. NTSB leaves out names.
- Role
- Pilot
- Age
- 54
- Certificate
- Commercial
- Airplane ratings
- Single-engine land
- Instrument ratings
- Airplane
- Medical
- Class 2, Valid Medical--w/ waivers/lim
- Seat
- Left
- Flight hours
- 11,389 total · 3,139 in this make and model · 11,389 as pilot in command · 95 in the last 90 days · 53 in the last 30 days · 2 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 45° at 5 knots, gusting 8
- Visibility
- 75 statute miles
- Lowest ceiling
- None
- Temperature
- 28 °F
- Altimeter
- 29.00 inHg
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.