DEN84FA207

NTSB accident investigation · Bell 206B · Englewood, CO · July 2, 1984

Accident · FatalField investigationFinal report
Date
July 2, 1984, 17:14 local (23:14 UTC)
Place
Englewood, CO
Injuries
2 fatal
Damage
Destroyed
Phase of flight
Approach
Aircraft
N3173LBell 206B
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19840702032049A
Case key
16226

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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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/malfunctionApproach - vfr pattern - final approach
Rotorcraft flight control,cyclic control - disconnectedCause
Maintenance,installation - improperCompany maintenance personnelCause
Checklist - inadequateManufacturerFactor
Aircraft preflight - inadequatePilot in commandFactor
Loss of control - in flightApproach - vfr pattern - final approach
Directional control - not possiblePilot in command
In flight collision with terrain/waterDescent - uncontrolled

Analysis

Witnesses stated the helicopter entered a 'hard left turn' into a near inverted position before 'it went down hard and fast.' Inspection disclosed the metal connection for the left cyclic stick was broken in half. (Plt was flying from left seat.) Exam of the cyclic stick quick disconnect locking nut revealed it was held in place on the connector by 1 thread. Properly installed, the locking nut tightens down over 6 threads on the connector. When backed out to 1 thread, movement of the cyclic will not not produce a corresponding change in the lateral control hydraulic servos. The cyclic was last removed aprx 80 hrs prior to the accident during maintenance. On 7/17/84, bell issued operations safety notice which in part read, 'flight crews are cautioned to assure quick removal flight controls are properly installed prior to operating the helicopter.' Prior to this notice, no requirements existed to do so.

Aircraft

Registration
N3173L
Reported as
Bell 206B
Category
Helicopter
Serial number
3677
Airframe hours
2,770
Engine
Allison 250-C20J, 317 horsepower, turbo shaft
Damage
Destroyed
Flight
Personal · Part 91
Registered owner
Ferris F. Hamilton
Airworthiness certificate
Standard, Normal
Last inspection
Annual · September 20, 1983 · 805 hours before
Departed
Englewood, CO
Airport
APA · Arapahoe County

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
39
Certificate
Airline transport
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Toxicology
Performed
Flight hours
5,000 total · 101 in the last 90 days

Weather

Conditions
Visual (VMC) · Day
Wind
90° at 12 knots
Visibility
40 statute miles
Lowest ceiling
None
Temperature
84 °F, dew point 46 °F
Altimeter
30.00 inHg
Observed at
APA, 1 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.