ATL84LA205

NTSB accident investigation · Sikorsky CH-19E · Iva, SC · June 20, 1984

Accident · No injuriesLimited investigationFinal report
Date
June 20, 1984, 07:00 local (11:00 UTC)
Place
Iva, SC
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N4721Sikorsky CH-19E
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19840620026009A
Case key
6482

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.

Loss of control - on ground/waterTakeoff
Landing gear,main gear strut - pressure too lowFactor
Maintenance,service of aircraft/equipment - improperFactor
Terrain condition - rough/unevenFactor
Operation with known deficiencies in equipment - continuedPilot in commandCause
Fuselage - vibrationCause
Airframe/component/system failure/malfunctionTakeoff
Misc rotorcraft,tail boom - overload

Analysis

The helicopter was being operated from sloping terrain. After returning from a spray mission, the plt remained inside the helicopter with the eng & rotor at ground idle while the ground crew refilled the spray tank. After completing the loading operation, the plt began applying power to increase the rotor RPM for takeoff. A severe ground-resonance type of vibration developed. The plt disengaged the eng & applied the rotor brake. When the rotor had stopped & the eng was secured, the plt egressed & observed that the aft end of the tail boom was laying on the ground. No pre-accident cracks or failures were found in the tail boom. Some components of the rotor sys had cracks, but none had failed or separated. The main rotor lead-lag dampers were removed & checked for time & all were within specifications. Personnel who recovered the helicopter noted that the left front landing gear strut was flat & the left rear main landing gear strut was low. They estimated the terrain was sloping 10 degs.

Aircraft

Registration
N4721
Reported as
Sikorsky CH-19E
Category
Helicopter
Serial number
129028
Airframe hours
4,319
Engine
Wright R-1300-3, 800 horsepower, reciprocating
Damage
Substantial damage
Flight
Aerial application · Part 137
Registered owner
Ag-Rotor, Inc.
Airworthiness certificate
Standard, Normal
Last inspection
Annual · April 18, 1984 · 79 hours before

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
41
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
4,793 total · 79 in this make and model · 2,988 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
360° at 4 knots
Visibility
5 statute miles
Lowest ceiling
None
Temperature
73 °F, dew point 72 °F
Altimeter
30.00 inHg
Observed at
AND, 17 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.