N14637

Substantial
None

Hiller UH12 S/N: 1577

Accident Details

Date
Monday, July 1, 1996
NTSB Number
FTW96LA285
Location
FRANKLIN, LA
Event ID
20001208X06209
Coordinates
29.800724, -91.510658
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

loss of engine power for undetermined reasons, and the pilot's failure to maintain rotor RPM. A factor was the unsuitable terrain available for the precautionary landing.

Aircraft Information

Registration
Make
HILLER
Serial Number
1577
Engine Type
Reciprocating
Year Built
1993
Model / ICAO
UH12 UH12
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
4
FAA Model
UH-12E

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 July 1, 1996, at 0930 central daylight time, a Hiller UH12E helicopter, N14637, was substantially damaged while executing a precautionary landing following a partial loss of engine power near Franklin, Louisiana. The helicopter, owned and operated by a private owner, was being operated under Title 14 CFR Part 91. Visual meteorological conditions prevailed and a flight plan was not filed. The commercial pilot, sole occupant of the aircraft, was not injured. The local business flight originated from Patterson, Louisiana, at 0815.

During personal interviews, conducted by the FAA inspector, the pilot reported that he heard a "bang" and the helicopter engine started "running rough" while the helicopter was operating at about 100 feet AGL en route between Patterson and Franklin. The pilot further stated that he elected to execute a precautionary landing to "investigate the source of the engine problems."

The pilot further stated that during the precautionary landing the "rotor RPM started to bleed and sufficient RPM could not be maintained for a successful landing." During the low rotor RPM landing touchdown to a muddy grass area, the front cross tube collapsed and the aft skid settled into the mud.

Examination of the airframe revealed that the tailboom, tailrotor gearbox, and a portion of the vertical stabilizer were severed from the helicopter as result of impact with the main rotor blades. The reason for the partial loss of engine power could not be determined.

The pilot did not complete any of the several Pilot/Operator Reports (NTSB Form 6120.1/2) that were mailed to him.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW96LA285