DEN83FA224

NTSB accident investigation · Hughes 369D (500) · Provo, UT · September 30, 1983

Accident · No injuriesField investigationFinal report
Date
September 30, 1983, 10:00 local (17:00 UTC)
Place
Provo, UT
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N8693FHughes 369D (500)
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19830930052869A
Case key
16005

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.

Loss of engine power(total) - mech failure/malfManeuvering
Fuel system,line fitting - looseCause
Maintenance,100-hour inspection - inadequateCause
Fuel system,line - leakCause
Fluid,fuel - starvationCause
Forced landingLanding
Autorotation - performedPilot in command
Nose downLanding
Terrain condition - softFactor
Terrain condition - wetFactor

Analysis

The helicopter was on a test flt to track & balance the main rotor system & to complete a 100 hr inspection. Prior to the flt, an occasional flicker of the fuel filter light was noted, but it was thought to be a wiring problem. After taking off, the fuel filter light flickered on a few more times, but never illuminated steadily. After less than a minute of flying time, the plt felt 2 quick 'jerks' (yaws). He start a 180 deg turn to land. After 90 deg of turn, the N2 decreased to 95%, then surged to 105%, then the eng quit running. The plt initiated an autorotation, but during landing on soft, wet terrain, the helicopter rocked forward & the main rotor struck the tail boom. An exam of the helicopter revealed a 'b' nut on 1 of 2 differential pressure lines (connected to the fuel filter differential pressure switch) was loose. During the exam, the 'b' nut separated from its attach point by a 1/2 turn using finger pressure.

Aircraft

Registration
N8693F
Reported as
Hughes 369D (500)
Category
Helicopter
Serial number
180252D
Airframe hours
3,183
Engine
Allison 250-C20B, 420 horsepower, turbo shaft
Damage
Substantial damage
Flight
Part 91
Registered owner
Rocky Mountain Helicopter, Inc
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · September 30, 1983 · 0 hours before

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
40
Certificate
Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Helicopter
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
10,500 total · 500 in this make and model · 200 in the last 90 days · 3 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
45 statute miles
Lowest ceiling
12,000 ft broken
Temperature
57 °F, dew point 48 °F
Altimeter
29.00 inHg
Observed at
PVU, 2 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.