SEA89FA111

NTSB accident investigation · Oregon Helicopters UH-1L · Baring, WA · June 14, 1989

Accident · Serious injuriesField investigationFinal report
Date
June 14, 1989, 11:50 local (18:50 UTC)
Place
Baring, WA
Injuries
1 serious, 1 minor
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N157LCOregon Helicopters UH-1L
Weather
Visual (VMC) · Day
Status
Completed · report June 26, 1992
Report
Approved by Office Director
FAA report
19890614015569A
Case key
40922

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

Fatigue failure of the tail rotor 42 degree gear box due to pilot induced overstress. Navy data and FAA type certificate limitations were not adhered to.

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.

Airframe/component/system failure/malfunctionHover
Rotor drive system,intermediate gearbox(42 deg) - overtorqueCause
Design stress limits of aircraft - exceededPilot in commandCause
Instructions,written/verbal - not followedCompany/operator managementCause
Rotor drive system,intermediate gearbox(42 deg) - fatigueCause
Loss of control - in flightHover
Hard landingLanding - flare/touchdown
Autorotation - performedPilot in command
Roll overLanding - flare/touchdown

Analysis

While lifting a log the crew heard unusual noises & felt vibrations. They released the log & flew to a landing site to check the aircraft. While at a high hover the aircraft began spinning and the pilot executed a hovering autorotation. The aircraft landed hard and rolled down a hill. Investigation revealed a failed tail rotor 42 deg gearbox. The board's metallurgical examination showed that the gearbox's input spiral bevel gear had failed in fatigue. The eng N2 torque was red-lined at 55 lbs. Pilot stated that a dash-5 transmission was installed rated for 60 lbs, but observed marked 55 lb limit. Navy operators manual and FAA type certificate both list N2 torque limit as 50 lbs.

Aircraft

Registration
N157LC
Reported as
Oregon Helicopters UH-1L
Category
Helicopter
Serial number
157856
Airframe hours
8,299
Engine
Lycoming T53-L13B, 1,400 horsepower, turbo shaft
Damage
Destroyed
Flight
Other work use · Part 133
Registered owner
Timberline Air Service, Inc.
Airworthiness certificate
Special, Restricted (Special)
Last inspection
100 hour · June 11, 1989 · 16 hours before
Departed
Baring, WA

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
44
Certificates
Commercial, Flight instructor
Airplane ratings
Multi-engine land, Single-engine land, Single-engine sea
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
15,000 total · 1,500 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
340° at 10 knots
Visibility
20 statute miles
Lowest ceiling
5,500 ft broken
Temperature
61 °F, dew point 54 °F
Altimeter
30.00 inHg
Observed at
PAE, 33 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.