MKC85FA100

NTSB accident investigation · Bell 47G · Calwood, MO · May 9, 1985

Accident · FatalField investigationFinal report
Date
May 9, 1985, 13:30 local (18:30 UTC)
Place
Calwood, MO
Injuries
2 fatal
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N951BBell 47G
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19850509016269A
Case key
33834

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.

Airframe/component/system failure/malfunctionCruise - normal
Rotor system,tail rotor hub - fatigueCause
Tail rotor/anti-torque control - improperManufacturerCause
Inadequate quality controlManufacturerCause
Loss of control - in flightCruise - normal
In flight collision with objectDescent - uncontrolled
Object - tree(s)

Analysis

N951B crashed in a wooded area during a powerline patrol flt which included photography of the powerline. According to witnesses, the helicopter was flying parallel to the powerline in a westerly direction when the accident occurred. Exam of the wreckage revealed the tail rotor gear box and hub, along with on tail rotor blade had separated in flt and was located aprx 50 yards from the main wreckage. The other tail rotor blade was located aprx 160 yards away from the main wreckage. Metallurgical exam of the broken yoke revealed a fatigue fracture which progressed from multiple origins at the root of the internal threads of the spline. The exam also showed that the internal threads were nitride treated. This was not a bell helicopter part. The PMA, under which this part was manufactured, prohibits nitride treatment of the spindle bore & threads.

Aircraft

Registration
N951B
Reported as
Bell 47G
Category
Helicopter
Serial number
695
Airframe hours
9,280
Engine
Franklin 6V-335-A, 200 horsepower, reciprocating
Damage
Destroyed
Fire
On-Ground
Flight
Aerial observation · Part 91
Registered owner
Dick Hill Helicopters, Inc.
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · April 15, 1985 · 48 hours before
Departed
COU · Columbia, MO

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
24
Certificates
Commercial, Flight instructor
Airplane ratings
Single-engine land
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
210 total · 210 in this make and model · 155 as pilot in command · 130 in the last 90 days · 4 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
230° at 13 knots
Visibility
20 statute miles
Lowest ceiling
None
Temperature
75 °F, dew point 50 °F
Altimeter
30.00 inHg
Observed at
COU, 21 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.