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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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NTSB Report

September 11, 1990 · Hiller OH-23C · N96168

Fort Pierce, FL

Overview

Report Status
Probable Cause
Event Type
Accident
Date
September 11, 1990
Injury Outcomes
No injuries (2 uninjured)
Location
Fort Pierce, FL
Aircraft
Hiller OH-23C
Tail Number
N96168
Operator
Coastal Aviation
Injuries
None
Aircraft Damage
Substantial
NTSB Number
MIA90LA182

THE CFI STATED THAT HE WAS TEACHING LOW ROTOR RPM RECOVERY TECHNIQUES DURING CLIMB OUT AFTER TAKEOFF. THE STUDENT WAS TO TAKE THE CONTROLS & RECOVER THE HELICOPTER TO A 4 FT HOVER. AT 30 FT, WITH THE ROTOR RPM AT 2,900, THE STUDENT TOOK CONTROL & OPENED THE THROTTLE BUT PULLED COLLECTIVE. THE ENG RPM DROPPED BELOW 2,500. THE CFI TOOK THE CONTROLS, VERIFIED THAT THE THROTTLE WAS OPENED & LOWERED COLLECTIVE. DURING THE RUN-ON LANDING AFTER TOUCHDOWN, THE MAIN ROTOR BLADES CONTACTED THE TAIL BOOM. EXAM OF THE ENG BY A MECHANIC WITH INSPECTION AUTHORIZATION REVEALED THAT ONE OF THE PACKING SEALS WHICH SEAL THE DISTRIBUTION ZONE PIPE TO THE INLET MANIFOLD, SEPARATED FOR UNDETERMINED REASONS RESULTING IN THE PARTIAL LOSS OF ENG POWER.

NTSB Probable Cause

LOSS OF ENGINE POWER DUE TO SEPARATION OF THE PACKING SEAL WHICH SEALS THE DISTRIBUTION ZONE PIPE TO THE INLET MANIFOLD, FOR UNDETERMINED REASONS RESULTING IN A HARD LANDING.

Full Narrative

THE CFI STATED THAT HE WAS TEACHING LOW ROTOR RPM RECOVERY TECHNIQUES DURING CLIMB OUT AFTER TAKEOFF. THE STUDENT WAS TO TAKE THE CONTROLS & RECOVER THE HELICOPTER TO A 4 FT HOVER. AT 30 FT, WITH THE ROTOR RPM AT 2,900, THE STUDENT TOOK CONTROL & OPENED THE THROTTLE BUT PULLED COLLECTIVE. THE ENG RPM DROPPED BELOW 2,500. THE CFI TOOK THE CONTROLS, VERIFIED THAT THE THROTTLE WAS OPENED & LOWERED COLLECTIVE. DURING THE RUN-ON LANDING AFTER TOUCHDOWN, THE MAIN ROTOR BLADES CONTACTED THE TAIL BOOM. EXAM OF THE ENG BY A MECHANIC WITH INSPECTION AUTHORIZATION REVEALED THAT ONE OF THE PACKING SEALS WHICH SEAL THE DISTRIBUTION ZONE PIPE TO THE INLET MANIFOLD, SEPARATED FOR UNDETERMINED REASONS RESULTING IN THE PARTIAL LOSS OF ENG POWER.

Flight

Event TypeAccident
Event Time10:39 EDT
Nearest AirportSt. Lucie County Int'L (0nm N)
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHiller OH-23C
Tail NumberN96168
Aircraft CategoryHeli
DamageSubstantial
OperatorCoastal Aviation
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsFranklin · 6V4-335-13 · Reciprocating · 200
Seats3

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 50 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind50° @ 12 kt
Visibility5 sm
CeilingBroken clouds 3000 ft
Temperature / Dew Point0 C
Altimeter30.00 inHg
Observation Time14:39
Weather SourceWFAC

Appendix: Source Data