DEN08LA071

NTSB accident investigation · Hiller UH-12E · La Porte, TX · April 4, 2008

Accident · Minor injuriesLimited investigationFinal report
Date
April 4, 2008, 15:03 local (20:03 UTC)
Place
La Porte, TX
Injuries
1 minor, 1 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N40289Hiller UH-12E
Defining event
Maneuvering-hover: Loss of control in flight
Weather
Visual (VMC) · Day
Status
Completed · report August 28, 2008
Report
Approved by Office Director
Parties
Houston, Texas
FAA report
20080404832169A
Case key
67780

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

The loss of tail rotor effectiveness. Contributing factors were the sudden windshift to a tailwind, and the pilot initiating a hovering turn in ground effect.

Findings · 4

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Wind: sudden wind shiftEnvironmental issues › Conditions/weather/phenomena · Not specifiedHiller UH-12E: 1 caseAll aircraft: 114 casesProbable cause
Wind: tailwindEnvironmental issues › Conditions/weather/phenomena · Not specifiedHiller UH-12E: 1 caseAll aircraft: 594 casesProbable cause
Action: incorrect action performancePersonnel issues › Action/decision · PilotHiller UH-12E: 3 casesAll aircraft: 1,386 casesProbable cause
Runway/land/takeoff/taxi surface: glassy surfaceEnvironmental issues › Physical environment · Not specifiedHiller UH-12E: 1 caseAll aircraft: 25 cases

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The pilot was test flying the helicopter after maintenance. He did two "quick stop" maneuvers into the wind. After completing the quick stop maneuver, and while in a 5-foot hover, he initiated a slow pedal turn to the left to return to the hangar. As he began the turn, he noticed "a loss of control effectiveness" and he attempted to set the helicopter down. Before he could regain control, the helicopter "slammed" into the ground. The pilot said it had begun to rain, and after he exited the helicopter, he noticed the wind sock had shifted 180 degrees. The tail boom was severed and the main rotor blades were destroyed.

Factual narrative

On April 4, 2008, at 1503 central daylight time, a Hiller UH-12E, N40289, registered to and operated by Ascent Aviation, was substantially damaged when it struck the ground while maneuvering and rolled over at La Porte Municipal Airport (T14), La Porte, Texas. Visual meteorological conditions prevailed at the time of the accident. The test flight was being conducted under the provisions of Title 14 Code of Federal Regulations (CFR) Part 91 without a flight plan. The airline transport certificated pilot received minor injuries, and his pilot certificated passenger was not injured. The local flight originated at T41 approximately 10 minutes before the accident.

According to the pilot's accident report, he was test flying the helicopter after performing some maintenance that had been requested by its new owner. He performed two "quick stop" maneuvers into the wind. After completing the quick stop maneuver and while in a 5-foot hover, he initiated a slow pedal turn to the left to return to the hangar. As he began the turn, he noticed "a loss of control effectiveness" and he attempted to set the helicopter down. Before he could regain control, the helicopter "slammed" into the ground. The pilot said it had begun to rain and after he exited the helicopter, he noticed the wind sock had shifted 180 degrees. The tail boom was severed and the main rotor blades were destroyed.

Aircraft

Registration
N40289
Reported as
Hiller UH-12E
Category
Helicopter
Serial number
5096
Airframe hours
2,216
Engine
Lycoming VO-540-C2A, 305 horsepower, reciprocating
Damage
Substantial damage
Flight
Flight test · Part 91
Operator
Paul Legris
Registered owner
Ascent Aviation
Airworthiness certificate
Standard, Normal
Last inspection
Annual · January 1, 2008
Departed
T41 · La Porte, TX
Destination
T41 · La Porte, TX
Airport
T41 · La Porte Municipal

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
Flight instructor
Age
52
Injuries
Serious
Certificates
Commercial, Flight instructor, Airline transport
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 1, With waivers/limitations
Last flight review
May 1, 2007
Seat
Left
Flight hours
20,000 total · 700 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
330° at 13 knots, gusting 21
Visibility
10 statute miles
Lowest ceiling
800 ft broken
Temperature
64 °F, dew point 61 °F
Altimeter
29.81 inHg

Docket · 3

The files NTSB released with the investigation on July 21, 2008, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.2 MB in all.

FAA reports on this event · 1

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

Other investigations on N40289 · 1

Matched to the same aircraft by N-number and date.