BFO92FA022

NTSB accident investigation · Hughes 369D · Edison, NJ · January 15, 1992

Accident · FatalField investigationFinal report
Date
January 15, 1992, 15:55 local (20:55 UTC)
Place
Edison, NJ
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N8674FHughes 369D
Weather
Visual (VMC) · Day
Status
Completed · report September 28, 1993
Report
Approved by Office Director
FAA report
19920115000649A
Case key
11715

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

The blockage of the fuel nozzle which resulted in partial loss of engine power. Contributing was the pilot's failure to maintain rotor RPM.

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(partial) - nonmechanicalCruise
Fuel system,nozzle - blocked(partial)Cause
Fluid,fuel - starvation
Forced landingDescent - emergency
Loss of control - in flightDescent - emergency
Rotor rpm - not maintainedPilot in commandFactor
On ground/water encounter with terrain/waterDescent - emergency
Terrain condition - ground

Analysis

The pilot was returning home, when according to a witness who saw the helicopter about 800 feet above the ground, the engine sounded normal at first. Shortly thereafter, the engine speed increased followed by the helicopter 'dutch rolling' (banking) left and right for two cycles and then rolled over one and half times nose first as it dropped behind the trees. The helicopter collided with power lines before impacting the ground in a nose down attitude and was destroyed by post-crash fire. Examination of aircraft confirmed continuity of the transmission gear box, and internal rotational damage for the engine; however, there was no significant rotational damage to the main rotor, tail rotor, and engine to transmission driveshaft (short shaft). Examination of the shaft revealed it had separaed from the bendix couplings and was crushed almost flat. There was no evidence of rotational damage between the separated halves. Metallurgical examination revealed the fuel nozzle was corroded with ferrous fibers.

Aircraft

Registration
N8674F
Reported as
Hughes 369D (HU-369-D)
Category
Helicopter
Serial number
970185D
Airframe hours
2,100
Engine
Allison 250-C20B, 420 horsepower, turbo shaft
Damage
Destroyed
Fire
On-Ground
Flight
Business · Part 91
Operator
Sun Dun Inc. Of Washington
Registered owner
Sun Dun Inc. Of Washington
Airworthiness certificate
Standard, Normal
Last inspection
Annual · November 5, 1991 · 1,026 hours before
Departed
New York, NY
Destination
Pasadena, MD

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
52
Certificates
Commercial, Private
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Toxicology
Performed
Flight hours
5,000 total

Weather

Conditions
Visual (VMC) · Day
Wind
320° at 14 knots
Visibility
25 statute miles
Lowest ceiling
None
Temperature
28 °F, dew point 3 °F
Altimeter
29.00 inHg
Observed at
EWR, 10 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.

Other investigations on N8674F · 1

Matched to the same aircraft by N-number and date.