NYC90LA125

NTSB accident investigation · Hughes 369HS · Brookville, PA · June 5, 1990

Accident · Serious injuriesLimited investigationFinal report
Date
June 5, 1990, 09:15 local (13:15 UTC)
Place
Brookville, PA
Injuries
1 serious, 2 minor
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N8315FHughes 369HS
Weather
Visual (VMC) · Day
Status
Completed · report March 17, 1992
Report
Approved by Office Director
FAA report
19900605018529A
Case key
36658

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

Worn tail rotor pitch control assembly, due to improper maintenance/installation, and subsequent fatigue failure of the tail rotor swashplate.

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
Rotorcraft flight control,tail rotor control - wornCause
Maintenance,installation - improperOther maintenance personnelCause
Rotorcraft flight control,tail rotor control - fatigueCause
Loss of control - in flightManeuvering
Directional control - not possible
Forced landingDescent - emergency
Autorotation - attemptedPilot in command
In flight collision with objectDescent - uncontrolled
Object - wire,transmission
In flight collision with terrain/waterDescent - uncontrolled

Analysis

During a power line patrol flt over wooded terrian, at about 60 to 85 ft AGL, tailrotor control of the helicopter was lost. The helicopter began to spin to the right and the plt attempted a hovering autorotation. The helicopter began spinning faster. Subsequently, it settled onto the power line, then crashed to the ground. An exam revealed that the tail rotor swashplate had failed from fatigue. The swashplate outer diameter was worn with evidence of spalling, the bearing inner diameter was lightly scored, the swashplate threads were severely worn with evidence of spalling due to relative motion with the mating threads of the locknut, and the lockwasher tang had worn a significant pattern in the swashplate keyway.

Aircraft

Registration
N8315F
Reported as
Hughes 369HS
Category
Helicopter
Serial number
801S
Engine
Allison 250-C20, 278 horsepower, turbo shaft
Damage
Destroyed
Flight
Aerial observation · Part 91
Operator
Helicopter Minit Men, Inc.
Departed
Dubois, PA
Flight plan
Company VFR

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
60
Certificates
Flight instructor, Commercial
Airplane ratings
Single-engine land
Instrument ratings
Helicopter
Medical
Class 2, Valid Medical--no waivers/lim.
Flight hours
11,500 total · 1,000 in this make and model · 11,000 as pilot in command · 60 in the last 90 days · 60 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
225° at 5 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
-0 °F, dew point -0 °F

FAA reports on this event · 1

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