ATL89DKG06

NTSB accident investigation · Bell UH-1B · Plains, GA · September 29, 1989

Accident · FatalFinal report
Date
September 29, 1989, 16:40 local (20:40 UTC)
Place
Plains, GA
Injuries
2 fatal
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N840MCBell UH-1B
Weather
Visual (VMC) · Day
Status
Completed · report June 30, 1992
Report
Approved by Office Director
FAA report
19890929037199A
Case key
7830

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

Improper modification of the helicopter by the company/operator, and failure of the spray boom, which resulted in mast bumping, and subsequent failure of the main rotor assembly.

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
Aerial application equipment - improperCause
Maintenance,modification - improperCompany/operator managementCause
Aerial application equipment - failure,totalCause
Rotor drive system,main rotor mast(drive shaft) - failure,totalCause
In flight collision with terrain/waterDescent - uncontrolled

Analysis

During a positioning flt, an in-flight breakup of the helicopter occurred in the vicinity of where it was crossing a line of trees between 2 cleared areas. Wreckage was found scattered over an area of aprx 300 yds in length, along a heading of 340 deg. At the se end, pieces were found from the left spray boom & main rotor aerodynamic fairing. Further to the nw, various parts were found from the left side of the helicopter, left spray boom & tail rotor. The main rotor & main rotor hub were found about 120 yds to the right of the wreckage path. The fuselage, eng & trans- mission were found about 240 yds nw of the 1st part of the wreckage. An exam of the wreckage revealed the main rotor system had separated due to mast bumping. There was evidence the left spray boom had contacted the main rotor blades during flt. All of the fractures of the spray boom, steel truss & assoc lugs indcd overload failure in aft & upward drctn. The spray assembly & boom had not been installed in accordance with FAR part 23.

Aircraft

Registration
N840MC
Reported as
Bell UH-1B
Category
Helicopter
Serial number
60-3619
Airframe hours
4,921
Engine
Lycoming T53-11D, 1,100 horsepower, turbo shaft
Damage
Destroyed
Flight
Positioning · Part 137
Registered owner
Agrotors, Inc.
Airworthiness certificate
Special, Restricted (Special)
Last inspection
100 hour · September 20, 1989 · 4 hours before
Departed
Plains, GA
Destination
82A · Buena Vista, GA

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
28
Certificates
Commercial, Flight instructor
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Right
Toxicology
Performed
Flight hours
4,165 total · 1,351 in this make and model · 4,024 as pilot in command · 122 in the last 90 days · 58 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
7 statute miles
Lowest ceiling
1,300 ft overcast
Temperature
79 °F, dew point 72 °F

FAA reports on this event · 1

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