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September 29, 2006 · Brantly Helicopter B-2B · N888CF

Carrizo Springs, TX

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
September 29, 2006
Injury Outcomes
No injuries (1 uninjured)
Location
Carrizo Springs, TX
Aircraft
Brantly Helicopter B-2B
Tail Number
N888CF
Injuries
None
Aircraft Damage
Substantial
NTSB Number
DFW06CA217

The pilot reported that he had flown the helicopter to a nearby municipal airport to refuel. After topping off the 31-gallon fuel system, the airline transport rated pilot, who reported having accumulated 276 flight hours in helicopters, was westbound to a ranch located about 30 miles away, near the border. About five minutes into the flight, while the helicopter was in cruise flight, the engine "started running rough." The pilot noted that the fuel pressure had dropped to about "half of what is normal" and since the terrain on both sides of the highway were "rough and thick with mesquite trees" he elected to initiate an autorotation to the highway, which at the time was clear of vehicular traffic. During the autorotation, while approximately 50-feet above the ground, the pilot observed unmarked power lines. The pilot attempted to maneuver the helicopter to avoid hitting the power lines with the main rotor. The bottom wire collided with the vertical pylon supporting the tail rotor gear box which resulted in a loss of tail rotor drive. The helicopter impacted the ground while in a right drift which collapsed the right landing gear skid and rolled the helicopter. There was no fire and the pilot was able to egress the helicopter unassisted. The pilot reported that it was later determined that the electric fuel boost pump had malfunctioned. The airframe had accumulated 2,136 hours since new and the 180-horsepower engine had accumulated 704 hours since its last overhaul. At the time of the accident, the pilot reported that the weather was clear with 10 miles visibility and calm winds.

NTSB Probable Cause

The loss of engine power due to a malfunction of the electric fuel pump. A contributing factor was the lack of suitable terrain for the forced landing.

Full Narrative

The pilot reported he had flown the helicopter to a nearby municipal airport in order to refuel the aircraft. After topping off the 31-gallon fuel system, the airline transport rated pilot, who reported having accumulated 276 flight hours in helicopters, was westbound to a ranch located about 30 miles away, near the border. About five minutes into the flight, while the helicopter was in cruise flight, the engine "started running rough." The pilot noted that the fuel pressure had dropped to about "half of what is normal" and since the terrain on both sides of the highway were "rough and thick with mesquite trees" he elected to initiate an autorotation to the highway, which at the time was clear of vehicular traffic. During the autorotation, while approximately 50-feet above the ground, the pilot observed unmarked powerlines. The pylon attempted to maneuver the helicopter to avoid hitting the powerlines with the main rotor. The bottom wire collided with the vertical pylon supporting the tail rotor gear box which resulted in a loss of tail rotor drive. The helicopter impacted the ground while in a right drift which collapsed the right landing gear skid and rolled the helicopter. There was no fire and the pilot was able to egress the helicopter unassisted. The pilot reported that it was later determined that the electric fuel boost pump had malfunctioned. The airframe had accumulated 2,136 hours since new and the 180-horsepower engine had accumulated 704 hours since its last overhaul. At the time of the accident, the pilot reported that the weather was clear with 10 miles visibility and calm winds.

Flight

Event TypeAccident
Event Time18:15 CDT
Nearest Airport0nm
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBrantly Helicopter B-2B
Tail NumberN888CF
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · IVO-360-AIA · Reciprocating · 180
Seats2

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 64 · Second Class · None

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility10 sm
CeilingNone
Temperature / Dew Point0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data