NYC86FA127

NTSB accident investigation · Robinson R-22A · East Fishkill, NY · May 10, 1986

Accident · FatalField investigationFinal report
Date
May 10, 1986, 12:24 local (16:24 UTC)
Place
East Fishkill, NY
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N8511ZRobinson R-22A
Weather
Visual (VMC) · Day
Status
Completed · report April 25, 1988
Report
Approved by Office Director
FAA report
19860510016659A
Case key
30186

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

A loss of control in flight for undetermined reasons.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of control - in flightCruise
Reason for occurrence undeterminedCause
Rotor system,main rotor - diverged
Airframe/component/system failure/malfunctionCruise
Rotor drive system,main rotor mast(drive shaft) - separation
Misc rotorcraft,tail boom - separation
Rotorcraft flight control,collective control rod - fatigue
In flight collision with terrain/waterDescent - uncontrolled

Analysis

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.

Aircraft

Registration
N8511Z
Reported as
Robinson R-22A
Category
Helicopter
Serial number
0415
Airframe hours
984
Engine
Lycoming O-320-B2C, 160 horsepower, reciprocating
Damage
Destroyed
Flight
Personal · Part 91
Registered owner
Dad'S Air, Inc.
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · April 18, 1986
Departed
POU · Poughkeepsie, NY
Destination
DXR · Danbury, CT

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
47
Certificate
Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Right
Toxicology
Performed
Flight hours
435 total · 61 in this make and model · 287 as pilot in command · 18 in the last 90 days · 12 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
310° at 6 knots
Visibility
15 statute miles
Lowest ceiling
None
Temperature
66 °F, dew point 34 °F
Altimeter
30.00 inHg
Observed at
POU, 6 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.