NYC83FA102

NTSB accident investigation · Hiller FH-1100 · Gettysburg, PA · April 26, 1983

Accident · FatalField investigationFinal report
Date
April 26, 1983, 12:00 local (16:00 UTC)
Place
Gettysburg, PA
Injuries
2 fatal
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N4034KHiller FH-1100
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19830426016029A
Case key
35040

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

On this page

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.

Abrupt maneuverCruise
Reason for occurrence undeterminedCause
Airframe/component/system failure/malfunctionManeuvering
Rotor drive system,main rotor mast(drive shaft) - overloadCause
Rotor system - separation
Loss of control - in flightManeuvering
In flight collision with terrain/waterDescent - uncontrolled

Analysis

The plt took off on a flt to york, PA to refuel the helicopter & to demonstrate it to a prospective buyer while en route. Witnesses observed the helicopter shortly after departure. Two of 4 witnesses heard a change in the sound of the helicopter, 2 witnesses saw the helicopter swinging from side to side prior to crashing, and 2 or the witnesses saw the main rotor assembly separate from the main rotor drive shaft. One witness, who saw the helicopter flying toward his position, reported that it started to 'swoop' down, then turned upward, and then the main rotor assembly & 2 other pieces separated. The helicopter then turned over & crashed. The 1st person to arrive at the crash site said the plt did not have a seat belt on. An exam of the wreckage revealed that the main rotor mast had separated adjacent to the main rotor sys static stops. All fuselage & flt control separations were examined & found typical of overload failures. The tail cone had been severed by the main rotor.

Aircraft

Registration
N4034K
Reported as
Hiller FH-1100
Category
Helicopter
Serial number
500
Airframe hours
127
Engine
Allison 250-C20B, 420 horsepower, turbo shaft
Damage
Destroyed
Flight
Business · Part 91
Registered owner
East Coast Helicopter, Inc.
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · August 25, 1982 · 21 hours before
Departed
Gettysburg, PA
Destination
York, PA

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
41
Certificates
Airline transport, Flight instructor
Airplane ratings
Multi-engine land, Single-engine land, Single-engine sea
Instrument ratings
Helicopter, Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Toxicology
Performed
Flight hours
8,500 total · 1,200 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
310° at 10 knots
Visibility
15 statute miles
Lowest ceiling
None
Temperature
59 °F, dew point 25 °F
Altimeter
29.00 inHg
Observed at
HAR, 50 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.