FTW96LA285

NTSB accident investigation · Hiller UH12 · Franklin, LA · July 1, 1996

Accident · No injuriesLimited investigationFinal report
Date
July 1, 1996, 09:30 local (14:30 UTC)
Place
Franklin, LA
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N14637Hiller UH12
Weather
Visual (VMC) · Day
Status
Completed · report February 18, 1997
Report
Approved by Office Director
FAA report
19960701015659A
Case key
19891

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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Probable cause

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.

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 engine powerCruise
Reason for occurrence undeterminedCause
Hard landingLanding - flare/touchdown
Terrain condition - none suitableFactor
Rotor rpm - not maintainedPilot in commandCause

Analysis

The pilot reported that he heard a 'bang' and the engine started 'running rough' while the helicopter was operating at about 100 feet AGL. The pilot elected to execute a precautionary landing to 'investigate the source of the engine problems.' The pilot 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.

Factual narrative

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.

Aircraft

Registration
N14637
Reported as
Hiller UH12
Category
Helicopter
Serial number
1577
Engine
Lycoming VO-540, 225 horsepower, reciprocating
Damage
Substantial damage
Flight
Business · Part 91
Registered owner
Dewayne C. Davis
Airworthiness certificate
Standard, Normal
Departed
PTN · Patterson, LA

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
Certificate
Commercial
Airplane ratings
Single-engine land
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Right
Flight hours
3,500 total

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
10 statute miles
Lowest ceiling
None

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.