19990708008519A

Accident · Substantial damage

FAA accident report · Bell 206B · Deadhorse, AK · July 8, 1999

Date
July 8, 1999 · 12:30 local
Place
Deadhorse, AK
Phase of flight
Starting Engines
Operating rules
Air taxi and commuter (Part 135)
Operator
FXKA
Damage
Substantial damage
Aircraft
N47122
NTSB investigation
NTSBANC99TA090
Reported as
Bell 206B
People aboard
4
Fatal injuries
0
Pilot’s flight hours
6,500 total1,100 in this make and model

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.

Tundra copters air taxi (1973 Bell 206B helicopter) crashed on take-off and sustained substantial damage, no injuries were reported to the pilot and 4 pax, other circumstances are unknown. (.19) on July 8, 1999, about 1230 Alaska daylight time, a Bell 206B helicopter, N47122, sustained substantial damage during engine start-up, about 75 miles southwest of Deadhorse, Alaska. The helicopter was being operated as a visual flight rules (VFR) U.S. Government flight by the u.s department of interior, bureau of land management, fairbanks, Alaska, when the accident occurred. The helicopter, provided by tundra copters inc., fairbanks, Alaska, was utilized on an on-demand 14 CFR part 135 flight. The certificated commercial pilot, and the three passengers, were not injured. Visual meteorological conditions prevailed. VFR company flight following procedures were in effect. During a telephone conversation with the national transportation safety board (NTSB) investigator-in-charge (iic), on July 8, 1999, the director of operations for tundra copters inc. reported the pilot loaded his passengers into the helicopter at a remote biological survey site. The pilot then began an engine start, bu t a main rotor blade tie-down strap was still attached to one of the rotor blades. As the rotor blades began to turn, the strap struck the helicopter's vertical stabilizer. The helicopter received damage to the tail boom, and the stabilizer. (-23) ptrs#AL01199904347 on engine start pilot did not remove blade tie down. Wound around vertical stab. Causing tailboom to twist. No hazmnt on board. (.4) on July 8, 1999, about 1230 Alaska daylight time, a Bell 206B helicopter, N47122, sustained substantial damage during engine start-up, about 75 miles southwest of Deadhorse, Alaska. The helicopter was being operated as a visual flight rules (VFR) U.S. Government flight by the u.s department of interior, bureau of land management, fairbanks, Alaska, when the accident occurred. The helicopter, provided by tundra copters inc., fairbanks, Alaska, was utilized on an on-demand 14 CFR part 135 flight. The certificated commercial pilot, and the three passengers, were not injured. Visual meteorological conditions prevailed. VFR company flight following procedures were in effect. During a telephone conversation with the national transportation safety board (NTSB) investigator-in-charge (iic), on July 8, 1999, the director of operations for tundra copters inc., reported the pilot loaded his passengers into the helicopter at a remote biological survey site. The pilot then began an engine start, but a main rotor blade tie-down strap was still attached to one of the rotor blades. As the rotor blades began to turn, the strap struck the upper end of the vertical stabilizer, crushing the leading edge in an aft direction. The helicopter's tail boom was deformed and wrinkled, just forward of the tail rotor gear box.

As the FAA filed it

TUNDRA COPTERS AIR TAXI (1973 BELL 206B HELICOPTER) CRASHED ON TAKE-OFF AND SUSTAINED SUBSTANTIAL DAMAGE, NO INJURIES WERE REPORTED TO THE PILOT AND 4 PAX, OTHER CIRCUMSTANCES ARE UNKNOWN. (.19) ON JULY 8, 1999, ABOUT 1230 ALASKA DAYLIGHT TIME, A BELL 206B HELICOPTER, N47122, SUSTAINED SUBSTANTIAL DAMAGE DURING ENGINE START-UP, ABOUT 75 MILES SOUTHWEST OF DEADHORSE, ALASKA. THE HELICOPTER WAS BEING OPERATED AS A VISUAL FLIGHT RULES (VFR) U.S. GOVERNMENT FLIGHT BY THE U.S DEPARTMENT OF INTERIOR, BUREAU OF LAND MANAGEMENT, FAIRBANKS, ALASKA, WHEN THE ACCIDENT OCCURRED. THE HELICOPTER, PROVIDED BY TUNDRA COPTERS INC., FAIRBANKS, ALASKA, WAS UTILIZED ON AN ON-DEMAND 14 CFR PART 135 FLIGHT. THE CERTIFICATED COMMERCIAL PILOT, AND THE THREE PASSENGERS, WERE NOT INJURED. VISUAL METEOROLOGICAL CONDITIONS PREVAILED. VFR COMPANY FLIGHT FOLLOWING PROCEDURES WERE IN EFFECT. DURING A TELEPHONE CONVERSATION WITH THE NATIONAL TRANSPORTATION SAFETY BOARD (NTSB) INVESTIGATOR-IN-CHARGE (IIC), ON JULY 8, 1999, THE DIRECTOR OF OPERATIONS FOR TUNDRA COPTERS INC. REPORTED THE PILOT LOADED HIS PASSENGERS INTO THE HELICOPTER AT A REMOTE BIOLOGICAL SURVEY SITE. THE PILOT THEN BEGAN AN ENGINE START, BU T A MAIN ROTOR BLADE TIE-DOWN STRAP WAS STILL ATTACHED TO ONE OF THE ROTOR BLADES. AS THE ROTOR BLADES BEGAN TO TURN, THE STRAP STRUCK THE HELICOPTER'S VERTICAL STABILIZER. THE HELICOPTER RECEIVED DAMAGE TO THE TAIL BOOM, AND THE STABILIZER. (-23) PTRS#AL01199904347 ON ENGINE START PILOT DID NOT REMOVE BLADE TIE DOWN. WOUND AROUND VERTICAL STAB. CAUSING TAILBOOM TO TWIST. NO HAZMNT ON BOARD. (.4) ON JULY 8, 1999, ABOUT 1230 ALASKA DAYLIGHT TIME, A BELL 206B HELICOPTER, N47122, SUSTAINED SUBSTANTIAL DAMAGE DURING ENGINE START-UP, ABOUT 75 MILES SOUTHWEST OF DEADHORSE, ALASKA. THE HELICOPTER WAS BEING OPERATED AS A VISUAL FLIGHT RULES (VFR) U.S. GOVERNMENT FLIGHT BY THE U.S DEPARTMENT OF INTERIOR, BUREAU OF LAND MANAGEMENT, FAIRBANKS, ALASKA, WHEN THE ACCIDENT OCCURRED. THE HELICOPTER, PROVIDED BY TUNDRA COPTERS INC., FAIRBANKS, ALASKA, WAS UTILIZED ON AN ON-DEMAND 14 CFR PART 135 FLIGHT. THE CERTIFICATED COMMERCIAL PILOT, AND THE THREE PASSENGERS, WERE NOT INJURED. VISUAL METEOROLOGICAL CONDITIONS PREVAILED. VFR COMPANY FLIGHT FOLLOWING PROCEDURES WERE IN EFFECT. DURING A TELEPHONE CONVERSATION WITH THE NATIONAL TRANSPORTATION SAFETY BOARD (NTSB) INVESTIGATOR-IN-CHARGE (IIC), ON JULY 8, 1999, THE DIRECTOR OF OPERATIONS FOR TUNDRA COPTERS INC., REPORTED THE PILOT LOADED HIS PASSENGERS INTO THE HELICOPTER AT A REMOTE BIOLOGICAL SURVEY SITE. THE PILOT THEN BEGAN AN ENGINE START, BUT A MAIN ROTOR BLADE TIE-DOWN STRAP WAS STILL ATTACHED TO ONE OF THE ROTOR BLADES. AS THE ROTOR BLADES BEGAN TO TURN, THE STRAP STRUCK THE UPPER END OF THE VERTICAL STABILIZER, CRUSHING THE LEADING EDGE IN AN AFT DIRECTION. THE HELICOPTER'S TAIL BOOM WAS DEFORMED AND WRINKLED, JUST FORWARD OF THE TAIL ROTOR GEAR BOX.

NTSB investigation

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