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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 5, 1988 · Mbb BO-105 · N2785B

South Marsh 113

Overview

Report Status
Probable Cause
Event Type
Accident
Date
December 5, 1988
Injury Outcomes
1 injury (1 minor injury), 3 uninjured
Location
South Marsh 113
Aircraft
Mbb BO-105
Tail Number
N2785B
Operator
Air Logistics
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
FTW89LA031

AS THE HELICOPTER WAS CLIMBING THRU ABOUT 500 FT, THE PLT HEARD A LOUD NOISE, FELT A SEVERE VIBRATION & SAW DEBRIS FALLING IN FRONT OF THE ACFT. HE BEGAN AN AUTOROTATION & DEPLOYED THE EMERGENCY FLOATS BEFORE LANDING ON WATER IN THE GULF OF MEXICO. THE HELICOPTER REMAINED AFLOAT & THE OCCUPANTS DEPLOYED & ENTERED A RAFT FROM WHICH THEY WERE PICKED UP ABOUT 1 HR LATER. AN INVESTIGATION REVEALED THAT ONE OF THE TAIL ROTOR BLADES HAD SEPARATED & STRUCK A MAIN ROTOR BLADE. THE RESULTING IMBALANCE CAUSED THE GEARBOX TO SEPARATE & FALL IN THE WATER. THE 90 DEG GEARBOX, TAIL ROTOR HUB AND TAIL ROTOR BLADES WERE NOT RECOVERED FROM THE GULF OF MEXICO.

NTSB Probable Cause

FAILURE AND SEPARATION OF ONE OF THE TAIL ROTOR BLADES FOR UNDETERMINED REASONS. THR RESULTING IMBALANCE AND VIBRATION CAUSED THE SEPARATION OF THE 90 DEGREE GEARBOX AND A PORTION OF THE VERTICAL PYLON WHICH NECESSITATED THE EMERGENCY AUTOROTATION TO THE WATER.

Full Narrative

AS THE HELICOPTER WAS CLIMBING THRU ABOUT 500 FT, THE PLT HEARD A LOUD NOISE, FELT A SEVERE VIBRATION & SAW DEBRIS FALLING IN FRONT OF THE ACFT. HE BEGAN AN AUTOROTATION & DEPLOYED THE EMERGENCY FLOATS BEFORE LANDING ON WATER IN THE GULF OF MEXICO. THE HELICOPTER REMAINED AFLOAT & THE OCCUPANTS DEPLOYED & ENTERED A RAFT FROM WHICH THEY WERE PICKED UP ABOUT 1 HR LATER. AN INVESTIGATION REVEALED THAT ONE OF THE TAIL ROTOR BLADES HAD SEPARATED & STRUCK A MAIN ROTOR BLADE. THE RESULTING IMBALANCE CAUSED THE GEARBOX TO SEPARATE & FALL IN THE WATER. THE 90 DEG GEARBOX, TAIL ROTOR HUB AND TAIL ROTOR BLADES WERE NOT RECOVERED FROM THE GULF OF MEXICO.

Flight

Event TypeAccident
Event Time20:06 UTC
Nearest Airport0nm N
Runway0
Flight Plan FiledCvfr
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftMbb BO-105
Tail NumberN2785B
Aircraft CategoryHeli
DamageSubstantial
OperatorAir Logistics
Operating RulePart 135
Engines2
Engine TypeTurboshaft
Engine DetailsAllison · 250-C20B · Turboshaft · 420
Seats5

People & Injuries

Injury Summary1 injury (1 minor injury), 3 uninjured
Fatal0
Serious0
Minor1
Uninjured3
Total4
Crew 1Age 46 · None

Conditions

ConditionsVMC
LightDaylight
Wind20° @ 7 kt
Visibility7 sm
CeilingNone
Temperature / Dew Point64 F / 37 C
Altimeter30.00 inHg
Weather SourcePILO

Appendix: Source Data