SEA86FA137

NTSB accident investigation · Bell UH-1L · Wenatchee, WA · May 31, 1986

Accident · FatalField investigationFinal report
Date
May 31, 1986, 07:10 local (14:10 UTC)
Place
Wenatchee, WA
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N4964NBell UH-1L
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19860531019929A
Case key
40284

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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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) - fatigueCause
In flight collision with terrain/waterDescent - uncontrolled
Terrain condition - none suitableCause
Autorotation - not possiblePilot in command

Analysis

N4964N, a bell UH-1L, was being operated in logging ops by an experienced, military trained plt who possessed 6000 hrs of flt experience in model. While lifting a sling load gnd crew rptd smoke from the tail rotor area. Plt released sling load & acknowledged the warning radioing his intentions to land nearby. The subsequent loss of tail rotor/directnl cntrl placed rotorcraft in a condition whereby an autorotation was not possbl & a run on lndg was necessary. Unsuitable terrain left the plt with only two forced lndg options, one on curving, hilly hwy with potential for a collision with auto traffic, or the other into heavily treed terrain. The plt appears to have chosen the latter. It is not apparent why he chose this option rather than diverting to a nearby airstrip or some other level forced lndg area. The 42 degree gearbox, which had been overhauled and installed 195 hrs previously in acft, was found to have failed when the input pinion gear fractured in fatigue originating from corrosion.

Aircraft

Registration
N4964N
Reported as
Bell UH-1L
Category
Helicopter
Serial number
157854
Airframe hours
7,899
Engine
Lycoming T53-L13B, 1,250 horsepower, turbo shaft
Damage
Destroyed
Fire
On-Ground
Flight
Part 133
Registered owner
A.M. Mcdowell & Associates
Airworthiness certificate
Special, Restricted (Special)
Last inspection
100 hour · May 18, 1986 · 41 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
39
Certificate
Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane, Helicopter
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Toxicology
Performed
Flight hours
11,250 total · 6,000 in this make and model · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
260° at 8 knots
Visibility
30 statute miles
Lowest ceiling
None
Temperature
66 °F, dew point 52 °F
Altimeter
29.00 inHg
Observed at
EAT, 15 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.