20050103000409A

Accident · Destroyed

FAA accident report · Urocop EC135T1 · Casa Grande, AZ · January 3, 2005

Date
January 3, 2005 · 13:45 local
Place
Casa Grande, AZ
Airport
Casa Grande Municipal Airport
Phase of flight
Forced Landing
Operating rules
General operating rules (Part 91)
Operator
RMXA
Damage
Destroyed
Aircraft
N135NW
NTSB investigation
NTSBLAX05LA060
Reported as
Urocop EC135T1
Reported engine
TMECA ARRIUS2B1
Fatal injuries
0
Pilot’s flight hours
14,000 total100 in this make and model90 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 January 3, 2005, at approximately 1345 local, N135NW, an EC-135 helicopter operated by omniflight helicopters was destroyed during a forced landing near the Casa Grande airport. The aircraft departed from williams gateway airport to conduct a part 135 flight evaluation and was conducting closed traffic pattern work at Casa Grande airport. After approximately 40 minutes of closed pattern work, while on right downwind for runway 5, the crew felt that the aircraft had flown through some turbulence. After turning base, as a descent was initiated, the aircraft began an uncommanded 60-90 degree bank to the right, followed by another 60-90 degree bank to the left. The PIC assumed the controls and initiated a powered descent while attempting to maintain a level attitude. At approximately 40-60 feet, with both crewmembers on the controls, aft cyclic was entered to flare the aircraft. The aircraft was witnesses to level momentarily, and then descend vertically to the ground. The crew does not recall if collective was applied to cushion the landing. The aircraft impacted the ground in a tail low attitude causing the tailboom to separate. The aircraft then contacted the ground on bothskids with significant force. Both skids spread, the right skid separated and flew up into the main rotor and was flung to the left side of the aircraft approximately 50 feet away. The aircraft then rolled to the left causing main rotor blade contact with the ground. All four blades were destroyed. The aircraft came to rest upright with the tailboom partially separated and displaced at a 45 degree angle to the right. The crew performed an emergency shutdown of the engines with the engine control switches (both engines were still operating). The crew was able to egress the aircraft unassisted and received only minor injuries.

As the FAA filed it

(-23) ON JANUARY 3, 2005, AT APPROXIMATELY 1345 LOCAL, N135NW, AN EC-135 HELICOPTER OPERATED BY OMNIFLIGHT HELICOPTERS WAS DESTROYED DURING A FORCED LANDING NEAR THE CASA GRANDE AIRPORT. THE AIRCRAFT DEPARTED FROM WILLIAMS GATEWAY AIRPORT TO CONDUCT A PART 135 FLIGHT EVALUATION AND WAS CONDUCTING CLOSED TRAFFIC PATTERN WORK AT CASA GRANDE AIRPORT. AFTER APPROXIMATELY 40 MINUTES OF CLOSED PATTERN WORK, WHILE ON RIGHT DOWNWIND FOR RUNWAY 5, THE CREW FELT THAT THE AIRCRAFT HAD FLOWN THROUGH SOME TURBULENCE. AFTER TURNING BASE, AS A DESCENT WAS INITIATED, THE AIRCRAFT BEGAN AN UNCOMMANDED 60-90 DEGREE BANK TO THE RIGHT, FOLLOWED BY ANOTHER 60-90 DEGREE BANK TO THE LEFT. THE PIC ASSUMED THE CONTROLS AND INITIATED A POWERED DESCENT WHILE ATTEMPTING TO MAINTAIN A LEVEL ATTITUDE. AT APPROXIMATELY 40-60 FEET, WITH BOTH CREWMEMBERS ON THE CONTROLS, AFT CYCLIC WAS ENTERED TO FLARE THE AIRCRAFT. THE AIRCRAFT WAS WITNESSES TO LEVEL MOMENTARILY, AND THEN DESCEND VERTICALLY TO THE GROUND. THE CREW DOES NOT RECALL IF COLLECTIVE WAS APPLIED TO CUSHION THE LANDING. THE AIRCRAFT IMPACTED THE GROUND IN A TAIL LOW ATTITUDE CAUSING THE TAILBOOM TO SEPARATE. THE AIRCRAFT THEN CONTACTED THE GROUND ON BOTHSKIDS WITH SIGNIFICANT FORCE. BOTH SKIDS SPREAD, THE RIGHT SKID SEPARATED AND FLEW UP INTO THE MAIN ROTOR AND WAS FLUNG TO THE LEFT SIDE OF THE AIRCRAFT APPROXIMATELY 50 FEET AWAY. THE AIRCRAFT THEN ROLLED TO THE LEFT CAUSING MAIN ROTOR BLADE CONTACT WITH THE GROUND. ALL FOUR BLADES WERE DESTROYED. THE AIRCRAFT CAME TO REST UPRIGHT WITH THE TAILBOOM PARTIALLY SEPARATED AND DISPLACED AT A 45 DEGREE ANGLE TO THE RIGHT. THE CREW PERFORMED AN EMERGENCY SHUTDOWN OF THE ENGINES WITH THE ENGINE CONTROL SWITCHES (BOTH ENGINES WERE STILL OPERATING). THE CREW WAS ABLE TO EGRESS THE AIRCRAFT UNASSISTED AND RECEIVED ONLY MINOR 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.