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NTSB Report
June 7, 1984 · Hughes 500D · N5106Y
Bedford, PA
Overview
Report Status
Preliminary report
Event Type
Accident
Date
June 7, 1984
Injury Outcomes
No injuries (1 uninjured)
Location
Bedford, PA
Aircraft
Hughes 500D
Tail Number
N5106Y
Injuries
None
Aircraft Damage
Substantial
NTSB Number
NYC84LA204
ACCORDING TO THE PLT, THE HELICOPTER TOOK OFF WITH UNDER 200 LBS OF FUEL INDICATING ON THE FUEL GAGE. FIFTEEN MINUTES AFTER TAKEOFF AT 125 FT AGL THE ENGINE OUT WARNING SYSTEM INDICATED AN ENGINE FAILURE. THE ACFT BEGAN TO ROTATE ABOUT ITS VETICAL AXIS AND DESCENDED. AT THIS POINT THE PLT OBSERVED THE FUEL GAGE TO BE 'ONE NEEDLE WIDTH BELOW THE 100 LB MARK.' THE PLT LOWERED THE COLLECTIVE ALMOST TO THE BOTTOM THEN PULLED IT ALL THE WAY UP JUST PRIOR TO IMPACT WHICH OCCURRED IN A DESCENT RATE OF 800 TO 1000 FPM. THE IMPACT BROKE THE RIGHT SKID AND THE HELICOPTER ROLLED OVER ON ITS RIGHT SIDE. AN INSPECTION OF THE ACFT FUEL SYSTEM FOLLOWING THE ACCIDENT REVEALED NO FUEL IN THE ANKS AND NOTHING WRONG WITH THE FUEL INDICATING SYSTEM.
Full Narrative
ACCORDING TO THE PLT, THE HELICOPTER TOOK OFF WITH UNDER 200 LBS OF FUEL INDICATING ON THE FUEL GAGE. FIFTEEN MINUTES AFTER TAKEOFF AT 125 FT AGL THE ENGINE OUT WARNING SYSTEM INDICATED AN ENGINE FAILURE. THE ACFT BEGAN TO ROTATE ABOUT ITS VETICAL AXIS AND DESCENDED. AT THIS POINT THE PLT OBSERVED THE FUEL GAGE TO BE 'ONE NEEDLE WIDTH BELOW THE 100 LB MARK.' THE PLT LOWERED THE COLLECTIVE ALMOST TO THE BOTTOM THEN PULLED IT ALL THE WAY UP JUST PRIOR TO IMPACT WHICH OCCURRED IN A DESCENT RATE OF 800 TO 1000 FPM. THE IMPACT BROKE THE RIGHT SKID AND THE HELICOPTER ROLLED OVER ON ITS RIGHT SIDE. AN INSPECTION OF THE ACFT FUEL SYSTEM FOLLOWING THE ACCIDENT REVEALED NO FUEL IN THE ANKS AND NOTHING WRONG WITH THE FUEL INDICATING SYSTEM.
Flight
Event TypeAccident
Event Time08:30 EDT
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo
Aircraft
AircraftHughes 500D
Tail NumberN5106Y
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 133
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · L-250B · Turboshaft · 375
Seats4
People & Injuries
Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 35 · Second Class
Conditions
ConditionsVMC
LightDaylight
Wind270° @ 5 kt, gusting 10 kt
Visibility15 sm
CeilingNone
Temperature / Dew Point0 C / 0 C
Altimeter30.00 inHg
Weather SourcePILO