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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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October 30, 1984 · Hughes 500D/369D · N8069G

Mc Cordsville, IN

Overview

Report Status
Preliminary report
Event Type
Accident
Date
October 30, 1984
Injury Outcomes
No injuries (2 uninjured)
Location
Mc Cordsville, IN
Aircraft
Hughes 500D/369D
Tail Number
N8069G
Injuries
None
Aircraft Damage
Substantial
NTSB Number
CHI85FA034

THE HELICOPTER LANDED HARD DURING AN AUTOROTATIVE DESCENT WHILE ON A TEST FLT & CHOPPED OFF THE TAIL BOOM. THE PLT STATED HE LOST POWER AT 150 FT AGL & ENTERED AUTOROTATION. INVESTIGATION REVEALED THAT THE FUEL QUANTITY FLOAT HAD BECOME INTANGLED WITH THE FUEL PUMP ELECTRICAL LINE. THIS RESULTED IN AN INDICATION OF 150 LBS OF FUEL ON THE FUEL GAUGE WHEN IN FACT THERE WAS NO FUEL IN THE TANKS, LINES OR FILTERS. THERE IS A WARNING IN THE MAINTENANCE MANUAL STATING THE FUEL PUMP ELECTRICAL LINE SHOULD BE TIE WRAPPED TO THE FUEL LINE SO AS NOT TO INTERFERE WITH THE FLOAT.

Full Narrative

THE HELICOPTER LANDED HARD DURING AN AUTOROTATIVE DESCENT WHILE ON A TEST FLT & CHOPPED OFF THE TAIL BOOM. THE PLT STATED HE LOST POWER AT 150 FT AGL & ENTERED AUTOROTATION. INVESTIGATION REVEALED THAT THE FUEL QUANTITY FLOAT HAD BECOME INTANGLED WITH THE FUEL PUMP ELECTRICAL LINE. THIS RESULTED IN AN INDICATION OF 150 LBS OF FUEL ON THE FUEL GAUGE WHEN IN FACT THERE WAS NO FUEL IN THE TANKS, LINES OR FILTERS. THERE IS A WARNING IN THE MAINTENANCE MANUAL STATING THE FUEL PUMP ELECTRICAL LINE SHOULD BE TIE WRAPPED TO THE FUEL LINE SO AS NOT TO INTERFERE WITH THE FLOAT.

Flight

Event TypeAccident
Event Time15:30 EST
Nearest AirportBrookside (1nm SSE)
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHughes 500D/369D
Tail NumberN8069G
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · 250-C20B · Turboshaft · 375
Seats5

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 39 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind210° @ 9 kt
Visibility9 sm
CeilingBroken clouds 8000 ft
Temperature / Dew Point66 F / 57
Altimeter30.00 inHg
Observation Time20:47
Weather SourceWFAC

Appendix: Source Data