N1348Z

Substantial
Minor

HILLER UH-12C S/N: 1042

Accident Details

Date
Wednesday, September 6, 1995
NTSB Number
LAX95LA326
Location
PORTERVILLE, CA
Event ID
20001207X04521
Coordinates
35.959510, -118.920219
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
2
Uninjured
0
Total Aboard
2

Probable Cause and Findings

the flight instructor's inadequate supervision of the flight; the dual student's improper use of the flight controls; and improper remedial action.

Aircraft Information

Registration
Make
HILLER
Serial Number
1042
Engine Type
Reciprocating
Year Built
1958
Model / ICAO
UH-12C UH12
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
4
FAA Model
UH-12C

Registered Owner (Current)

Name
POCKRUS PAT B
Address
517 GRANT RD
City
MINERAL WELLS
State / Zip Code
TX 76067-8826
Country
United States

Analysis

On September 6, 1995, at 0906 hours Pacific daylight time, a Hiller UH-12C helicopter, N1348Z, sustained a hard landing at Porterville Municipal Airport, Porterville, California. The pilots were conducting a local visual flight rules instructional flight. The helicopter, operated by Whirlybirds, Inc., Concord, California, sustained substantial damage. The certificated commercial pilot/flight instructor (CFI), and the certificated private pilot/dual student received minor injuries. Visual meteorological conditions prevailed. The flight originated at Porterville Municipal Airport, at 0830 hours.

The CFI reported in a telephone interview conducted on September 7, 1995, that before the accident the dual student was practicing some maneuvers and had landed. During the lift-off, the helicopter began to drift backwards. The dual student immediately applied "full up collective," the helicopter continued to go backwards, and rapidly raised about 15 to 18 feet above the ground.

The CFI immediately assumed the flight controls and applied full throttle. This action did not arrest the decaying main rotor rpm. The CFI simultaneously attempted to regain the main rotor rpm by trying to "milk down the collective," but was unsuccessful.

During this process, the helicopter descended to 10 feet above the ground. Due to the decaying main rotor rpm, the helicopter experienced a loss of tail rotor effectiveness. The CFI then elected to execute a hovering autorotation. He was unable to cushion the landing due to the low main rotor rpm and the helicopter sustained a hard landing.

The CFI reiterated this telephone statement in the Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1/2. He indicated in the form that the helicopter did not experience any preimpact malfunctions or failures.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX95LA326