LAX85FA136

NTSB accident investigation · Hughes 369D · Hilo, HI · February 6, 1985

Accident · FatalField investigationFinal report
Date
February 5, 1985, 15:50 local (Feb 6, 1985, 01:50 UTC)
Place
Hilo, HI
Injuries
1 fatal
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N369LAHughes 369D
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19850205063719A
Case key
24469

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/malfunctionCruise - normal
Maintenance,modification - improperOther maintenance personnelCause
Maintenance,inspection - inadequateFactor
Fuselage,fairing - distortedCause
Aircraft preflight - inadequatePilot in commandCause
Rotor drive system,engine to transmission drive - wornCause
Rotor drive system,engine to transmission drive - failure,totalCause
Engine assembly,mount - failure,totalCause
Forced landingDescent - emergency
Autorotation - performedPilot in command
In flight collision with objectLanding - flare/touchdown
Terrain condition - none suitableFactor
Object - tree(s)Factor
Roll overLanding - flare/touchdown
Terrain condition - high vegetationFactor
Terrain condition - mountainous/hillyFactor

Analysis

A search was initiated when the helicopter did not arrive. It was fnd 2 days later where it crashed drg an autorotation in a rain forest. Drg the flare/touchdown, vegetation had caught on a tundra pad on the l skid & the acft rolled over. An exam revealed the lwr bendix coupling on the eng-to-transmission drive shaft, pn 369A4410, & the upper r eng mount, pn 369H8017, had failed. Unapproved mod/repairs had been made to both the drive shaft & overlying cover panel. A steel reinforcing rod had been installed inside the cover panel. Due to pressure of cargo (large wtr bucket), the steel rod had been forced onto the drive shaft. There was evidence of angular misalignment & later failure of the drive shaft. A metallurgical exam of the eng mount revealed low cyclic fatigue in the threaded rod area of the adjusting screw. The fracture area of the drive shaft was too badly damaged to determine the mode of failure. Acft prev operd in Canada, reg c-gvtj. Annual inspn & U.S. Airworthiness certificate issued despite unapproved mod. Date of mod unknown.

Aircraft

Registration
N369LA
Reported as
Hughes 369D
Category
Helicopter
Serial number
1260036D
Airframe hours
2,165
Engine
Allison 250-C20B, 375 horsepower, turbo shaft
Damage
Substantial damage
Flight
Positioning · Part 91
Registered owner
Kenai Helicopters
Airworthiness certificate
Standard, Normal
Last inspection
Annual · October 9, 1984 · 101 hours before
Departed
OGG · Kahului, HI
Destination
Volcano Natl Pk, HI

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
41
Certificates
Private, Commercial
Airplane ratings
Multi-engine land, Single-engine land
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Toxicology
Performed
Flight hours
7,500 total · 500 in this make and model · 7,300 as pilot in command · 75 in the last 90 days · 30 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
120° at 9 knots
Visibility
15 statute miles
Lowest ceiling
24,000 ft broken
Temperature
79 °F, dew point 63 °F
Altimeter
29.00 inHg
Observed at
ITO, 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.