20050626013059A

Accident · Substantial damage

FAA accident report · Hughes 269C · Denver, CO · June 26, 2005

Date
June 26, 2005 · 08:42 local
Place
Denver, CO
Airport
Jeffco Airport
Phase of flight
Pwr On Vertical Ldng/Rtrcrft
Operating rules
General operating rules (Part 91)
Operator
RT6A
Damage
Substantial damage
Aircraft
N308BP
NTSB investigation
NTSBDEN05CA094
Reported as
Hughes 269C
Reported engine
Lycoming HIO360*
People aboard
2
Fatal injuries
0
Pilot’s flight hours
238 total230 in this make and model13 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) On 06/26/2005 the pilot privacy data omitted and one passenger were returning from a photo flight. The pilot privacy data omitted obtained the ATIS and was cleared to the rotors of the rockies facility. When the approach was started to the rotors of the rockies landing pad the wind was a tailwind instead of the headwind that privacy data omitted was expecting. He could not accelerate straight ahead because of a flight rise in the terrain and conflicting traffic on runway 20 which was directly ahead. He pulled back the collective which caused a further drop in RPM and the aircraft contacted the ramp at a high rate of descent damaging the skids and associated structure. The tail rotor contacted the ground and was damaged. The main rotor did not make ground contact and there was no fuel leakage or any other fluid leakage. The pilot privacy data omitted and the passenger did not sustain any injuries.

As the FAA filed it

(-23) ON 06/26/2005 THE PILOT ^PRIVACY DATA^ AND ONE PASSENGER WERE RETURNING FROM A PHOTO FLIGHT. THE PILOT ^PRIVACY DATA^ OBTAINED THE ATIS AND WAS CLEARED TO THE ROTORS OF THE ROCKIES FACILITY. WHEN THE APPROACH WAS STARTED TO THE ROTORS OF THE ROCKIES LANDING PAD THE WIND WAS A TAILWIND INSTEAD OF THE HEADWIND THAT ^PRIVACY DATA^ WAS EXPECTING. HE COULD NOT ACCELERATE STRAIGHT AHEAD BECAUSE OF A FLIGHT RISE IN THE TERRAIN AND CONFLICTING TRAFFIC ON RUNWAY 20 WHICH WAS DIRECTLY AHEAD. HE PULLED BACK THE COLLECTIVE WHICH CAUSED A FURTHER DROP IN RPM AND THE AIRCRAFT CONTACTED THE RAMP AT A HIGH RATE OF DESCENT DAMAGING THE SKIDS AND ASSOCIATED STRUCTURE. THE TAIL ROTOR CONTACTED THE GROUND AND WAS DAMAGED. THE MAIN ROTOR DID NOT MAKE GROUND CONTACT AND THERE WAS NO FUEL LEAKAGE OR ANY OTHER FLUID LEAKAGE. THE PILOT ^PRIVACY DATA^ AND THE PASSENGER DID NOT SUSTAIN ANY INJURIES.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.