20020304002379A

Accident · Substantial damage

FAA accident report · Bell 206L3 · Tulsa, OK · March 4, 2002

Date
March 4, 2002 · 12:30 local
Place
Tulsa, OK
Airport
Channel 8 Heliport
Phase of flight
Forced Landing
Operating rules
General operating rules (Part 91)
Operator
VXIA
Damage
Substantial damage
Aircraft
N227H
NTSB investigation
NTSBFTW02LA089
Reported as
Bell 206L3
Reported engine
Allison 250C30
People aboard
2
Fatal injuries
0
Pilot’s flight hours
18,000 total4,500 in this make and model30 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.

(.19) On March 4, 2002, at 1235 central standard time, a Bell 206L-3 single-engine helicopter, N227H, was substantially damaged during a forced landing to a road following a total loss of engine power while on approach to a company helipad near Tulsa, Oklahoma. The commercial pilot and his passenger were not injured. The helicopter was owned and operated by Tulsa security patrol inc., d.b.a. action helicopter services of Tulsa, Oklahoma. Visual meteorological conditions prevailed and a flight plan was not filed for the 14 code of federal regulations part 91 business flight. The flight originated from Tulsa's richard lloyd jones jr. airport, approximately 1230, and was en route to the company helipad. The pilot reported that the flight was en route to the helipad for fuel when the engine lost power approximately 300 yards short of the helipad. During an autorotation to a road, the pilot had to execute an evasive maneuver to avoid a vehicle. Subsequently, the main rotor blades struck nearby trees, the helicopter landed hard on the road, and the main rotor blades contacted and severed the tail boom. The pilot stated that he estimated 300 pounds of fuel were on board at the time of theaccident. (-23) enroute from r.l. jones airport the engine shut down. Pilot initiated emergency landing procedures. At apx 10', the main rotor struck trees causing the hard landing. Helicopter skip apx 20' before coming to a stop. Tail boom was severed by main rotor on impact. Skids and possible airframe structure damage also due to hard landing. (.4) on March 4, 2002, at 1235 central standard time, a Bell 206L-3 single-engine helicopter, N227H, was substantially damaged during a forced landing to a road following a total loss of engine power while on approach to a company helipad near Tulsa, Oklahoma. The commercial pilot and his passenger were not injured. The helicopter was owned and operated by Tulsa security patrol inc., d.b.a. action helicopter services of Tulsa. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 code of federal regulations part 91 positioning flight. The flight originated from Tulsa's richard lloyd jones jr. airport, approximately 1230, and was en route to the company helipad. The pilot reported that the flight was en route to the helipad for fuel when the engine lost power approximately 300 yards short of the helipad. During an autorotation to a road, the pilot had to execute an evasive maneuver to avoid a vehicle. Subsequently, at 10 feet AGL, the main rotor blades struck 1.5 inch-diameter tree branches. The main rotor RPM decreased, the helicopter landed hard on the road, and the main rotor blades contacted and severed the tail boom. The pilot estimated 300 pounds of fuel was on board at the time of the accident. On March 14, 2002, at a facility in Tulsa, an FAA inspector, the operator's director of maintenance, and the pilot examined the helicopter. Prior to the FAA inspector's arrival, the main rotor blades and main rotor mast had been removed. During the inspection, the engine was started and test run to idle speed, and no anomalies were noted. The fuel nozzle and fuel filters were inspected, and no anomalies were noted. The reason for the loss of engine power was not determined.

As the FAA filed it

(.19) ON MARCH 4, 2002, AT 1235 CENTRAL STANDARD TIME, A BELL 206L-3 SINGLE-ENGINE HELICOPTER, N227H, WAS SUBSTANTIALLY DAMAGED DURING A FORCED LANDING TO A ROAD FOLLOWING A TOTAL LOSS OF ENGINE POWER WHILE ON APPROACH TO A COMPANY HELIPAD NEAR TULSA, OKLAHOMA. THE COMMERCIAL PILOT AND HIS PASSENGER WERE NOT INJURED. THE HELICOPTER WAS OWNED AND OPERATED BY TULSA SECURITY PATROL INC., D.B.A. ACTION HELICOPTER SERVICES OF TULSA, OKLAHOMA. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AND A FLIGHT PLAN WAS NOT FILED FOR THE 14 CODE OF FEDERAL REGULATIONS PART 91 BUSINESS FLIGHT. THE FLIGHT ORIGINATED FROM TULSA'S RICHARD LLOYD JONES JR. AIRPORT, APPROXIMATELY 1230, AND WAS EN ROUTE TO THE COMPANY HELIPAD. THE PILOT REPORTED THAT THE FLIGHT WAS EN ROUTE TO THE HELIPAD FOR FUEL WHEN THE ENGINE LOST POWER APPROXIMATELY 300 YARDS SHORT OF THE HELIPAD. DURING AN AUTOROTATION TO A ROAD, THE PILOT HAD TO EXECUTE AN EVASIVE MANEUVER TO AVOID A VEHICLE. SUBSEQUENTLY, THE MAIN ROTOR BLADES STRUCK NEARBY TREES, THE HELICOPTER LANDED HARD ON THE ROAD, AND THE MAIN ROTOR BLADES CONTACTED AND SEVERED THE TAIL BOOM. THE PILOT STATED THAT HE ESTIMATED 300 POUNDS OF FUEL WERE ON BOARD AT THE TIME OF THEACCIDENT. (-23) ENROUTE FROM R.L. JONES AIRPORT THE ENGINE SHUT DOWN. PILOT INITIATED EMERGENCY LANDING PROCEDURES. AT APX 10', THE MAIN ROTOR STRUCK TREES CAUSING THE HARD LANDING. HELICOPTER SKIP APX 20' BEFORE COMING TO A STOP. TAIL BOOM WAS SEVERED BY MAIN ROTOR ON IMPACT. SKIDS AND POSSIBLE AIRFRAME STRUCTURE DAMAGE ALSO DUE TO HARD LANDING. (.4) ON MARCH 4, 2002, AT 1235 CENTRAL STANDARD TIME, A BELL 206L-3 SINGLE-ENGINE HELICOPTER, N227H, WAS SUBSTANTIALLY DAMAGED DURING A FORCED LANDING TO A ROAD FOLLOWING A TOTAL LOSS OF ENGINE POWER WHILE ON APPROACH TO A COMPANY HELIPAD NEAR TULSA, OKLAHOMA. THE COMMERCIAL PILOT AND HIS PASSENGER WERE NOT INJURED. THE HELICOPTER WAS OWNED AND OPERATED BY TULSA SECURITY PATROL INC., D.B.A. ACTION HELICOPTER SERVICES OF TULSA. VISUAL METEOROLOGICAL CONDITIONS PREVAILED, AND A FLIGHT PLAN WAS NOT FILED FOR THE 14 CODE OF FEDERAL REGULATIONS PART 91 POSITIONING FLIGHT. THE FLIGHT ORIGINATED FROM TULSA'S RICHARD LLOYD JONES JR. AIRPORT, APPROXIMATELY 1230, AND WAS EN ROUTE TO THE COMPANY HELIPAD. THE PILOT REPORTED THAT THE FLIGHT WAS EN ROUTE TO THE HELIPAD FOR FUEL WHEN THE ENGINE LOST POWER APPROXIMATELY 300 YARDS SHORT OF THE HELIPAD. DURING AN AUTOROTATION TO A ROAD, THE PILOT HAD TO EXECUTE AN EVASIVE MANEUVER TO AVOID A VEHICLE. SUBSEQUENTLY, AT 10 FEET AGL, THE MAIN ROTOR BLADES STRUCK 1.5 INCH-DIAMETER TREE BRANCHES. THE MAIN ROTOR RPM DECREASED, THE HELICOPTER LANDED HARD ON THE ROAD, AND THE MAIN ROTOR BLADES CONTACTED AND SEVERED THE TAIL BOOM. THE PILOT ESTIMATED 300 POUNDS OF FUEL WAS ON BOARD AT THE TIME OF THE ACCIDENT. ON MARCH 14, 2002, AT A FACILITY IN TULSA, AN FAA INSPECTOR, THE OPERATOR'S DIRECTOR OF MAINTENANCE, AND THE PILOT EXAMINED THE HELICOPTER. PRIOR TO THE FAA INSPECTOR'S ARRIVAL, THE MAIN ROTOR BLADES AND MAIN ROTOR MAST HAD BEEN REMOVED. DURING THE INSPECTION, THE ENGINE WAS STARTED AND TEST RUN TO IDLE SPEED, AND NO ANOMALIES WERE NOTED. THE FUEL NOZZLE AND FUEL FILTERS WERE INSPECTED, AND NO ANOMALIES WERE NOTED. THE REASON FOR THE LOSS OF ENGINE POWER WAS NOT DETERMINED.

NTSB investigation

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