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Aviation safety reports, made easier to study

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February 22, 2004 · Hiller UH-12B · N5304V

Bradenton, FL

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
February 22, 2004
Injury Outcomes
No injuries (1 uninjured)
Location
Bradenton, FL
Aircraft
Hiller UH-12B
Tail Number
N5304V
Operator
Danny Bals
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ANC04LA027

The airline transport pilot was on a solo cross-country helicopter flight as part of a helicopter add-on rating. He reported 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. He said that he lowered the helicopter's collective and entered an autorotation, and selected an unoccupied playground as an emergency landing site. As the helicopter descended into the playground area, he had to raise the collective 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. The helicopter sustained 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. An FAA inspector who inspected the helicopter and spoke with the pilot, noted that the helicopter's fuel tank appeared empty, and stated that that the pilot agreed with him.

NTSB Probable Cause

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.

Full Narrative

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.

Flight

Event TypeAccident
Event Time11:25 EST
Nearest Airport0nm
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHiller UH-12B
Tail NumberN5304V
Aircraft CategoryHeli
DamageSubstantial
OperatorDanny Bals
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsFranklin · 6V4 Series · Reciprocating · 210
Seats3

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 52 · First Class · None

Conditions

ConditionsVMC
LightDaylight
Wind1° @ 3 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point61 F
Altimeter30.13 inHg
Observation Time15:53
Weather SourceWFAC

Appendix: Source Data