N5304V

Substantial
None

Hiller UH-12BS/N: 575

Accident Details

Date
Sunday, February 22, 2004
NTSB Number
ANC04LA027
Location
Bradenton, FL
Event ID
20040315X00322
Coordinates
27.395277, -82.554168
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot's inadequate in-flight planning/decision which resulted in fuel exhaustion. Also causal was the pilot's failure to maintain adequate rotor speed, resulting in a hard landing.

Aircraft Information

Registration
N5304V
Make
HILLER
Serial Number
575
Engine Type
Reciprocating
Model / ICAO
UH-12BUH12
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
BIALS SEBASTIEN
Address
2005 NEW STONECASTLE TER
Status
Deregistered
City
WINTER PARK
State / Zip Code
FL 32792-1777
Country
United States

Analysis

On February 22, 2004, about 1125 Eastern standard time, a skid equipped Hiller UH-12B helicopter, N5304V, sustained substantial damage during an emergency landing following a loss of engine power in Bradenton, Florida. The helicopter was being operated as a visual flight rules (VFR) cross-country instructional flight under Title 14, CFR Part 91, when the accident occurred. The solo certificated airline transport pilot was not injured. Visual meteorological conditions prevailed, and no flight plan was filed. The flight originated at the Orlando Executive Airport, Orlando, Florida, about 1000, and was en route to the Dove Heliport, Sarasota, Florida.

During a telephone conversation with the National Transportation Safety Board investigator-in-charge on February 22, the pilot reported that the purpose of the flight was a solo cross-country flight as part of a helicopter add-on rating. He said that he thought that there was enough fuel for about 1.7 hours of flight time, but after only 1.5 hours of flight time, as the flight neared the destination heliport, the engine began to run rough and lose power. The pilot said that he lowered the helicopter's collective and entered an autorotation, and selected an unoccupied playground as an emergency landing site. He said that as the helicopter descended into the playground area, he had to raise the collective slightly in order to avoid a stand of trees, and the main rotor speed decayed. The helicopter's skids subsequently struck the ground hard, and the helicopter rolled onto its right side, sustaining structural damage to the fuselage, tail boom, and main rotor drive system. The pilot noted that there were no preaccident mechanical anomalies with the helicopter.

On February 22, a Federal Aviation Administration (FAA) Airworthiness Inspector from the Tampa Flight Standards District Office (FSDO), traveled to the accident site and inspected the helicopter wreckage prior to recovery. The FAA inspector reported that the helicopter's fuel tank appeared to be empty, and that the accident pilot agreed with 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# ANC04LA027