What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(.19)On April 27, 2001, at 1740 CDT, a Hughes 269B helicopter, N9508F, was substantially damaged when it impatched wires and terrain while repositioning at the a.l. managham jr. regional airport near Nacogdoches, Texas. The airplane was registered to and operated by the pilot. The airline transport pilot, who was the sole occupant, received minor injuries. Visual meteorological conditions prevailed and a flight plan was not filed for the 14 CFR part 91 repositioning flight. The flight was originating at the time of the accident. According to the FAA inspector, who responded to the accident site, the helicopter was parked on a trailer between two t-hangers and under a power line. The pilot stated that he cleared the area around the helicopter;however, he did not clear the aera directly over the helicopter. The pilot lifted off the trailer and impacted the power line approximately 30 feet above the ground. The FAA inspector stated that the power line wrapped around the main rotor mast and partially separated one of the main rotor blades. The helicopter then descended and impacted the ground. The FAA inspector stated that the mast, main rotor blades and cabin area sustained structural damage. (-23)owner/operator lifted off the trailer/landing pad for reposioning of the helicopter. At approximately 25 to 30 feet above the trailer/landing pad the helicopter struck power lines. These power lines run between the t-hangers and supply power to the airport. The power lines cables were cut and rapped around the rotor mask. The helicopter lost power and landed facing the opposite direction. Minor injuries to the pilot. (.4) on April 27, 2001, at 1740 central daylight time, a Hughes 269B helicopter, N9508F, was substantially damaged when it impacted wires and terrain during takeoff at the a.l. Mangham jr. regional airport near Nacogdoches, Texas. The airplane was registered to and operated by the pilot. The airline transport pilot, who was the sole occupant, received minor injuries. Visual meteorological conditions prevailed and a flight plan was not filed for the 14 code of federal regulations part 91 repositioning flight. The flight was originating at the time of the accident. According to the pilot, the helicopter was parked on a trailer between two t-hangars and under a power li NE. The pilot stated that he cleared the area around the helicopter; however, he did not clear the area directly over the helicopter. The pilot lifted off the trailer and impacted the power line approximately 30 feet above the ground. The pilot mentioned that at the time of the accident, "the sun was at an angle and intensity so that the wires were not visible." He also stated that the wires were not marked with red balls. The FAA inspector stated that the power line wrapped around the main rotor mast and partially separated one of the main rotor blades. The helicopter then descended and impacted the ground. The FAA inspector stated that the mast, main rotor blades and cabin area sustained structural damage.
As the FAA filed it
(.19)ON APRIL 27, 2001, AT 1740 CDT, A HUGHES 269B HELICOPTER, N9508F, WAS SUBSTANTIALLY DAMAGED WHEN IT IMPATCHED WIRES AND TERRAIN WHILE REPOSITIONING AT THE A.L. MANAGHAM JR. REGIONAL AIRPORT NEAR NACOGDOCHES, TEXAS. THE AIRPLANE WAS REGISTERED TO AND OPERATED BY THE PILOT. THE AIRLINE TRANSPORT PILOT, WHO WAS THE SOLE OCCUPANT, RECEIVED MINOR INJURIES. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AND A FLIGHT PLAN WAS NOT FILED FOR THE 14 CFR PART 91 REPOSITIONING FLIGHT. THE FLIGHT WAS ORIGINATING AT THE TIME OF THE ACCIDENT. ACCORDING TO THE FAA INSPECTOR, WHO RESPONDED TO THE ACCIDENT SITE, THE HELICOPTER WAS PARKED ON A TRAILER BETWEEN TWO T-HANGERS AND UNDER A POWER LINE. THE PILOT STATED THAT HE CLEARED THE AREA AROUND THE HELICOPTER;HOWEVER, HE DID NOT CLEAR THE AERA DIRECTLY OVER THE HELICOPTER. THE PILOT LIFTED OFF THE TRAILER AND IMPACTED THE POWER LINE APPROXIMATELY 30 FEET ABOVE THE GROUND. THE FAA INSPECTOR STATED THAT THE POWER LINE WRAPPED AROUND THE MAIN ROTOR MAST AND PARTIALLY SEPARATED ONE OF THE MAIN ROTOR BLADES. THE HELICOPTER THEN DESCENDED AND IMPACTED THE GROUND. THE FAA INSPECTOR STATED THAT THE MAST, MAIN ROTOR BLADES AND CABIN AREA SUSTAINED STRUCTURAL DAMAGE. (-23)OWNER/OPERATOR LIFTED OFF THE TRAILER/LANDING PAD FOR REPOSIONING OF THE HELICOPTER. AT APPROXIMATELY 25 TO 30 FEET ABOVE THE TRAILER/LANDING PAD THE HELICOPTER STRUCK POWER LINES. THESE POWER LINES RUN BETWEEN THE T-HANGERS AND SUPPLY POWER TO THE AIRPORT. THE POWER LINES CABLES WERE CUT AND RAPPED AROUND THE ROTOR MASK. THE HELICOPTER LOST POWER AND LANDED FACING THE OPPOSITE DIRECTION. MINOR INJURIES TO THE PILOT. (.4) ON APRIL 27, 2001, AT 1740 CENTRAL DAYLIGHT TIME, A HUGHES 269B HELICOPTER, N9508F, WAS SUBSTANTIALLY DAMAGED WHEN IT IMPACTED WIRES AND TERRAIN DURING TAKEOFF AT THE A.L. MANGHAM JR. REGIONAL AIRPORT NEAR NACOGDOCHES, TEXAS. THE AIRPLANE WAS REGISTERED TO AND OPERATED BY THE PILOT. THE AIRLINE TRANSPORT PILOT, WHO WAS THE SOLE OCCUPANT, RECEIVED MINOR INJURIES. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AND A FLIGHT PLAN WAS NOT FILED FOR THE 14 CODE OF FEDERAL REGULATIONS PART 91 REPOSITIONING FLIGHT. THE FLIGHT WAS ORIGINATING AT THE TIME OF THE ACCIDENT. ACCORDING TO THE PILOT, THE HELICOPTER WAS PARKED ON A TRAILER BETWEEN TWO T-HANGARS AND UNDER A POWER LI NE. THE PILOT STATED THAT HE CLEARED THE AREA AROUND THE HELICOPTER; HOWEVER, HE DID NOT CLEAR THE AREA DIRECTLY OVER THE HELICOPTER. THE PILOT LIFTED OFF THE TRAILER AND IMPACTED THE POWER LINE APPROXIMATELY 30 FEET ABOVE THE GROUND. THE PILOT MENTIONED THAT AT THE TIME OF THE ACCIDENT, "THE SUN WAS AT AN ANGLE AND INTENSITY SO THAT THE WIRES WERE NOT VISIBLE." HE ALSO STATED THAT THE WIRES WERE NOT MARKED WITH RED BALLS. THE FAA INSPECTOR STATED THAT THE POWER LINE WRAPPED AROUND THE MAIN ROTOR MAST AND PARTIALLY SEPARATED ONE OF THE MAIN ROTOR BLADES. THE HELICOPTER THEN DESCENDED AND IMPACTED THE GROUND. THE FAA INSPECTOR STATED THAT THE MAST, MAIN ROTOR BLADES AND CABIN AREA SUSTAINED STRUCTURAL DAMAGE.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.
Other reports on N9508F · 1
Matched to the same aircraft by N-number and date.