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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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December 9, 1986 · Hughes 369HS · N8390F

Zephyrhills, FL

Overview

Report Status
Preliminary report
Event Type
Accident
Date
December 9, 1986
Injury Outcomes
2 injuries (2 fatalities)
Location
Zephyrhills, FL
Aircraft
Hughes 369HS
Tail Number
N8390F
Operator
F M Mc Gahee
Injuries
Fatal
Aircraft Damage
Destroyed
NTSB Number
MIA87FA046

A WITNESS STATED THAT SHE HEARD THE ENG ON THE HELICOPTER QUIT. SHE LOOKED OUT HER WINDOW AND WATCHED THE HELICOPTER HIT THE GROUND, BOUNCE, HIT AGAIN, FLIP OVER AND THE TAIL BROKE OFF. THE HELICOPTER THEN BURST INTO FLAMES AND EXPLODED.EXAM OF THE ENG REVEALED THAT THE PC AIR FILTER ASSEMBLY WAS BROKEN AT THE FORWARD INLET SIDE OF THE FILTER BODY WHICH RESULTED IN THE LOSS OF PC AIR PRESSURE TO THE FUEL CONTROL.THIS CAUSED THE ENG POWER TO REDUCE TO FLIGHT IDLE. THE PC FILTER HOUSING BROKE DUE TO AN IMPROPER MODIFICATION TO THE FILTER BODY.

Full Narrative

A WITNESS STATED THAT SHE HEARD THE ENG ON THE HELICOPTER QUIT. SHE LOOKED OUT HER WINDOW AND WATCHED THE HELICOPTER HIT THE GROUND, BOUNCE, HIT AGAIN, FLIP OVER AND THE TAIL BROKE OFF. THE HELICOPTER THEN BURST INTO FLAMES AND EXPLODED.EXAM OF THE ENG REVEALED THAT THE PC AIR FILTER ASSEMBLY WAS BROKEN AT THE FORWARD INLET SIDE OF THE FILTER BODY WHICH RESULTED IN THE LOSS OF PC AIR PRESSURE TO THE FUEL CONTROL.THIS CAUSED THE ENG POWER TO REDUCE TO FLIGHT IDLE. THE PC FILTER HOUSING BROKE DUE TO AN IMPROPER MODIFICATION TO THE FILTER BODY.

Flight

Event TypeAccident
Event Time15:30 EST
Nearest Airport0nm N
Runway0
Runway Length0
Runway Width0
Flight Plan FiledNone
Aircraft FireGrd
Aircraft ExplosionGrd

Aircraft

AircraftHughes 369HS
Tail NumberN8390F
Aircraft CategoryHeli
DamageDestroyed
OperatorF M Mc Gahee
Operating RulePart 91
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · 250-C20 · Turboshaft · 278
Seats4

People & Injuries

Injury Summary2 injuries (2 fatalities)
Fatal2
Serious0
Minor0
Uninjured0
Total2
Crew 1Age 68 · First Class

Conditions

ConditionsVMC
LightDaylight
Wind170° @ 8 kt
Visibility7 sm
CeilingNone
Temperature / Dew Point68 F
Altimeter30.00 inHg
Observation Time19:51
Weather SourceWFAC

Appendix: Source Data