N80750

Substantial
None

Robinson R22 BETA S/N: 1316

Accident Details

Date
Friday, September 6, 1996
NTSB Number
FTW96LA378
Location
LOREAUVILLE, LA
Event ID
20001208X06725
Coordinates
30.070772, -91.670700
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot's inadequate preflight planning/preparation for the flight, resulting in exceeding the maximum gross weight and performance of the helicopter. A factor was the high density altitude.

Aircraft Information

Registration
N80750
Make
ROBINSON
Serial Number
1316
Engine Type
Reciprocating
Model / ICAO
R22 BETA R22
Aircraft Type
Rotorcraft
No. of Engines
1

Analysis

On September 6, 1996, at 1545 central daylight time, a Robinson R22 Beta helicopter, N80750, registered to a private owner and operated by Acadiana Helicopters under Title 14 CFR Part 137, impacted terrain during takeoff near Loreauville, Louisiana. The commercial pilot was not injured, and the helicopter received substantial damage. Visual meteorological conditions prevailed for the local aerial application flight and a flight plan was not filed. The flight was originating at the time of the accident.

The pilot reported in the NTSB Form 6120.1/2 Pilot/Operator Aircraft Accident Report that the weather was "hot and humid, with little to no breeze," and during the attempted takeoff from the transport trailer, the helicopter descended, "hit the ground, the main rotor blades flexed down and cut the tail off." The pilot also reported that the helicopter "couldn't get any lift."

The pilot reported to the FAA inspector that he did not calculate the weight and balance, nor do any performance planning. He also reported he did not know the height above the ground or what the rotor RPM and manifold pressure indicated prior to takeoff.

Weight and balance and performance calculations were performed using figures provided by the manufacturer. The weight of the helicopter at the time of the accident was estimated at 1,384.8 pounds. The maximum gross weight of the helicopter was 1,370 pounds. According to aircraft performance charts, with the density altitude of 2,400 feet, at the gross weight of 1,384.8 pounds, the helicopter was not capable of hovering out of ground effect.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW96LA378