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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

May 10, 1986 · Robinson R-22A · N8511Z

East Fishkill, NY

Overview

Report Status
Probable Cause
Event Type
Accident
Date
May 10, 1986
Injury Outcomes
1 injury (1 fatality)
Location
East Fishkill, NY
Aircraft
Robinson R-22A
Tail Number
N8511Z
Injuries
Fatal
Aircraft Damage
Destroyed
NTSB Number
NYC86FA127

After departure, another pilot advised N8511Z that a cowl door was open. The pilot acknowledged, but continued the flight. During the VFR flight, witnesses heard a loud pop and observed the R22 helicopter break apart in flight. One witness observed a light airplane traveling in the opposite direction at the same time. The tail boom was the first piece of the helicopter found along the 584' long wreckage path. The main rotor separated from its drive shaft and there were multiple strikes to the tail boom. Metallurgical examination of the main rotor head components and examination of the engine revealed no evidence of malfunction or failure that could have contributed to the main rotor blade diverging and striking the tail boom, resulting in the in-flight separation of the tail boom. Examination of the right collective control tube revealed a fatigue fracture in the inboard wall of the tube where it is normally lightly loaded. The evidence did not support a conclusion that this was related to loss of main rotor control.

NTSB Probable Cause

A LOSS OF CONTROL IN FLIGHT FOR UNDETERMINED REASONS.

Full Narrative

AFTER DEPARTURE, ANOTHER PILOT ADVISED N8511Z THAT A COWL DOOR WAS OPEN. THE PILOT ACKNOWLEDGED, BUT CONTINUED THE FLIGHT. DURING THE VFR FLIGHT, WITNESSES HEARD A LOUD POP & OBSERVED THE R22 HELICOPTER BREAK APART IN FLIGHT. ONE WITNESS OBSERVED A LIGHT AIRPLANE TRAVELING IN THE OPPOSITE DIRECTION AT THE SAME TIME. THE TAIL BOOM WAS THE FIRST PIECE OF THE HELICOPTER FOUND ALONG THE 584' LONG WRECKAGE PATH. THE MAIN ROTOR SEPARATED FROM ITS DRIVE SHAFT & THERE WERE MULTIPLE STRIKES TO THE TAIL BOOM. METALLURGICAL EXAMINATION OF THE MAIN ROTOR HEAD COMPONENTS & EXAMINATION OF THE ENGINE REVEALED NO EVIDENCE OF MALFUNCTION OR FAILURE THAT COULD HAVE CONTRIBUTED TO THE MAIN ROTOR BLADE DIVERGING & STRIKING THE TAIL BOOM, RESULTING IN THE IN-FLIGHT SEPARATION OF THE TAIL BOOM. EXAMINATION OF THE RIGHT COLLECTIVE CONTROL TUBE REVEALED A FATIGUE FRACTURE IN THE INBOARD WALL OF THE TUBE WHERE IT IS NORMALLY LIGHTLY LOADED. THE EVIDENCE DID NOT SUPPORT A CONCLUSION THAT THIS WAS RELATED TO LOSS OF MAIN ROTOR CONTROL.

Flight

Event TypeAccident
Event Time12:24 EDT
Nearest Airport0nm N
Runway0
Runway Length0
Runway Width0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftRobinson R-22A
Tail NumberN8511Z
Aircraft CategoryHeli
DamageDestroyed
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-320-B2C · Reciprocating · 160
Seats2

People & Injuries

Injury Summary1 injury (1 fatality)
Fatal1
Serious0
Minor0
Uninjured0
Total1
Crew 1Age 47 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind310° @ 6 kt
Visibility15 sm
CeilingNone
Temperature / Dew Point66 F / 34 C
Altimeter30.00 inHg
Observation Time16:43
Weather SourceWFAC

Appendix: Source Data