SEA94LA030

NTSB accident investigation · Hawkins & Powers UH-1B · North Bend, WA · November 12, 1993

Accident · Minor injuriesLimited investigationFinal report
Date
November 12, 1993, 11:30 local (19:30 UTC)
Place
North Bend, WA
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N91NWHawkins & Powers UH-1B
Weather
Visual (VMC) · Day
Status
Completed · report December 2, 1994
Report
Approved by Office Director
FAA report
19931112042801A
Case key
41853

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

The NTSB’s determination of the probable cause, and any contributing factors.

Total failure of the intermediate gearbox. The lack of suitable terrain for an autorotation was a factor.

Analysis

The pilot heard loud grinding sounds from the rear of the aircraft, followed by banging sounds and a loss of directional control. He jettisoned his logs, then his long line, and executed a powered autorotation into the trees, substantially damaging the aircraft. The 42 degree intermediate gearbox was examined and multiple origin fatigue cracks were found in fragments of the input pinion gear.

Factual narrative

On November 12, 1993, at 1130 Pacific standard time, a Hawkins and Powers UH-1B, N91NW, operated by Northwest Helicopters, impacted terrain 10 miles south of North Bend, Washington, during an emergency forced landing. There was no flight plan filed for the external load flight, conducted under 14 CFR 133 in visual meteorological conditions, that was on takeoff when the accident occurred. The commercial certificated pilot suffered minor injuries in the accident. The aircraft was substantially damaged. There was no fire.

The pilot reported he heard a loud growling/grinding noise from the rear of the aircraft, followed by a slow turn to the right, then a banging sound and a violent rotation to the right. After clearing the choker setters with the load, he jettisoned his external load of logs and attempted to fly the aircraft to a nearby clearcut. Recognizing that he had neither altitude nor airspeed to make it to the clearcut, he reduced power, jettisoned his long line, and executed a powered autorotation into the trees. The aircraft was substantially damaged when it impacted the trees and rough terrain.

The 42 degree intermediate gearbox was examined at the NTSB metallurgy laboratory. Fatigue cracks and overstress fractures were found in the input geat and mating fragments.

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/malfunctionManeuvering
Rotor drive system,intermediate gearbox(42 deg) - failure,totalCause
Forced landingDescent - emergency
In flight collision with terrain/waterLanding - flare/touchdown
Terrain condition - high vegetationFactor
Terrain condition - none suitableCause

Aircraft

Registration
N91NW
Reported as
Hawkins & Powers UH-1B
Category
Helicopter
Serial number
62-1915
Airframe hours
10,106
Engine
Lycoming T53-L11D, 1,100 horsepower, turbo shaft
Damage
Substantial damage
Flight
Other work use · Part 133
Operator
Northwest Helicopters, Inc.
Registered owner
Northwest Helicopters, Inc.
Airworthiness certificate
Special, Restricted (Special)
Last inspection
100 hour · November 8, 1993 · 25 hours before

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
42
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Helicopter
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
11,800 total · 1,500 in this make and model

Weather

Conditions
Visual (VMC) · Day
Visibility
2 statute miles
Lowest ceiling
None
Temperature
61 °F

FAA reports on this event · 1

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