N67065

Substantial
None

Hiller UH-12D S/N: 1023

Accident Details

Date
Friday, February 16, 1996
NTSB Number
FTW96LA121
Location
CARRIZO SPRINGS, TX
Event ID
20001208X05250
Coordinates
28.520851, -99.850059
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

a loss of engine power for undetermined reasons, and the pilot's improper touchdown.

Aircraft Information

Registration
Make
HILLER
Serial Number
1023
Engine Type
Reciprocating
Year Built
1957
Model / ICAO
UH-12D UH12
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
3
FAA Model
UH-12D

Registered Owner (Current)

Name
FORT WOLTERS HELICOPTER INC
Address
517 GRANT RD
City
MINERAL WELLS
State / Zip Code
TX 76067-8826
Country
United States

Analysis

On February 16, 1996, at 1015 central standard time, a Hiller UH-12D helicopter, N67065, registered to, and operated by T.M. Davis Construction Inc., as a Title 14 CFR Part 91 aerial observation flight, was substantially damaged following a loss of control while maneuvering near Carrizo Springs, Texas. The private pilot and his passenger were not injured. Visual meteorological conditions prevailed for the personal flight for which a flight plan was not filed. The flight originated at the ranch office at approximately 0830.

The pilot reported that the helicopter departed the Windship Ranch for a local flight to spot deer. "While cruising at about 50 feet and about 40 knots indicated airspeed and after making a 360 degree turn, the engine either lost power or for some other reason would not maintain adequate rotor RPM." The pilot further reported that he lowered the collective in an attempt to increase rotor RPM, "but, the RPM would not reach the minimum required to fly." Subsequently, he landed the helicopter hard, and "the main rotor blade struck the tailboom, severing the boom and 3 feet of blade." The helicopter came to rest on its side.

Examination of the airframe and engine by the FAA inspector did not reveal any pre-mishap discrepancies. The reason for the loss of engine power and rotor RPM could not be determined.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW96LA121