What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(.19)On June 5, 2001, about 1630 central daylight time, an Enstrom F28A, N9565, registered to a private individual, rolled over while lifting off a trailer at the Double springs-Winston county airport, Double springs, Alabama. Visual meteorological conditions prevailed at the time and no flight plan was filed for the 14 CFR part 91 personal flight. The helicopter was substantially damaged and the private-rated pilot, the sole occupant, sustained minor injuries. The flight was originating at the time of the occurrence. The pilot stated when interviewed the first time 2 days after the accident that the helicopter was on a trailer that had been in a hangar, but the trailer with helicopter onboard was removed from the hangar onto the ramp. He planned on lifting the helicopter off the trailer onto the ramp first, then intended on landing the helicopter onto a larger trailer. He stated that when he attempted to lift off from the smaller trailer, the rear portion of the left skid caught on the trailer and the helicopter rolled over. (-23) on June 5, 2001, at approx. 1700L, the above identified helicopter was moved on a trailer to a position 40 feet from a hangar to run the engine and check the generator. Mr. Dickerson the owner who holds an airplane single engine land pilots certificate was the the controls. During the engine run, Mr. Dickerson lost control of the helicopter and the left skid fell off the trailer causing the main and tail rotors to strike the ground. There was additional damage to the left skid and the tail section just forward of the tail rotor. To date no further inspections have been perfomed to check for additional damage. (.4) on June 5, 2001, about 1630 central daylight time, an Enstrom F28A, N9565, registered to a private individual, rolled over while lifting off a trailer at the Double springs-Winston county airport, Double springs, Alabama. Visual meteorological conditions prevailed at the time and no flight plan was filed for the 14 CFR part 91 personal flight. The helicopter was substantially damaged and the private-rated pilot, the sole occupant, sustained minor injuries. The flight was originating at the time of the occurrence. The pilot stated when interviewed the first time 2 days after the accident that the helicopter was on a trailer that had been in a hangar, but the trailer with helicopter onboard was removed from the hangar onto the ramp. He planned on lifting the helicopter off the trailer onto the ramp first, then intended on landing the helicopter onto a larger trailer. He stated that when he attempted to lift off from the smaller trailer, the rear portion of the left skid caught on the trailer and the helicopter rolled over. A copy of the record of conversation is an attachment to this report. He submitted a report to the NTSB stating that the purpose of the flight was to perform an engine run only following an annual inspection and there was no intention to fly the helicopter. He stated in the report that during the engine run, the helicopter "vibrated the skids off the trailer, falling on side damaging main and tail rotor blades." A copy of the NTSB report is an attachment to this report.
As the FAA filed it
(.19)ON JUNE 5, 2001, ABOUT 1630 CENTRAL DAYLIGHT TIME, AN ENSTROM F28A, N9565, REGISTERED TO A PRIVATE INDIVIDUAL, ROLLED OVER WHILE LIFTING OFF A TRAILER AT THE DOUBLE SPRINGS-WINSTON COUNTY AIRPORT, DOUBLE SPRINGS, ALABAMA. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AT THE TIME AND NO FLIGHT PLAN WAS FILED FOR THE 14 CFR PART 91 PERSONAL FLIGHT. THE HELICOPTER WAS SUBSTANTIALLY DAMAGED AND THE PRIVATE-RATED PILOT, THE SOLE OCCUPANT, SUSTAINED MINOR INJURIES. THE FLIGHT WAS ORIGINATING AT THE TIME OF THE OCCURRENCE. THE PILOT STATED WHEN INTERVIEWED THE FIRST TIME 2 DAYS AFTER THE ACCIDENT THAT THE HELICOPTER WAS ON A TRAILER THAT HAD BEEN IN A HANGAR, BUT THE TRAILER WITH HELICOPTER ONBOARD WAS REMOVED FROM THE HANGAR ONTO THE RAMP. HE PLANNED ON LIFTING THE HELICOPTER OFF THE TRAILER ONTO THE RAMP FIRST, THEN INTENDED ON LANDING THE HELICOPTER ONTO A LARGER TRAILER. HE STATED THAT WHEN HE ATTEMPTED TO LIFT OFF FROM THE SMALLER TRAILER, THE REAR PORTION OF THE LEFT SKID CAUGHT ON THE TRAILER AND THE HELICOPTER ROLLED OVER. (-23) ON JUNE 5, 2001, AT APPROX. 1700L, THE ABOVE IDENTIFIED HELICOPTER WAS MOVED ON A TRAILER TO A POSITION 40 FEET FROM A HANGAR TO RUN THE ENGINE AND CHECK THE GENERATOR. MR. DICKERSON THE OWNER WHO HOLDS AN AIRPLANE SINGLE ENGINE LAND PILOTS CERTIFICATE WAS THE THE CONTROLS. DURING THE ENGINE RUN, MR. DICKERSON LOST CONTROL OF THE HELICOPTER AND THE LEFT SKID FELL OFF THE TRAILER CAUSING THE MAIN AND TAIL ROTORS TO STRIKE THE GROUND. THERE WAS ADDITIONAL DAMAGE TO THE LEFT SKID AND THE TAIL SECTION JUST FORWARD OF THE TAIL ROTOR. TO DATE NO FURTHER INSPECTIONS HAVE BEEN PERFOMED TO CHECK FOR ADDITIONAL DAMAGE. (.4) ON JUNE 5, 2001, ABOUT 1630 CENTRAL DAYLIGHT TIME, AN ENSTROM F28A, N9565, REGISTERED TO A PRIVATE INDIVIDUAL, ROLLED OVER WHILE LIFTING OFF A TRAILER AT THE DOUBLE SPRINGS-WINSTON COUNTY AIRPORT, DOUBLE SPRINGS, ALABAMA. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AT THE TIME AND NO FLIGHT PLAN WAS FILED FOR THE 14 CFR PART 91 PERSONAL FLIGHT. THE HELICOPTER WAS SUBSTANTIALLY DAMAGED AND THE PRIVATE-RATED PILOT, THE SOLE OCCUPANT, SUSTAINED MINOR INJURIES. THE FLIGHT WAS ORIGINATING AT THE TIME OF THE OCCURRENCE. THE PILOT STATED WHEN INTERVIEWED THE FIRST TIME 2 DAYS AFTER THE ACCIDENT THAT THE HELICOPTER WAS ON A TRAILER THAT HAD BEEN IN A HANGAR, BUT THE TRAILER WITH HELICOPTER ONBOARD WAS REMOVED FROM THE HANGAR ONTO THE RAMP. HE PLANNED ON LIFTING THE HELICOPTER OFF THE TRAILER ONTO THE RAMP FIRST, THEN INTENDED ON LANDING THE HELICOPTER ONTO A LARGER TRAILER. HE STATED THAT WHEN HE ATTEMPTED TO LIFT OFF FROM THE SMALLER TRAILER, THE REAR PORTION OF THE LEFT SKID CAUGHT ON THE TRAILER AND THE HELICOPTER ROLLED OVER. A COPY OF THE RECORD OF CONVERSATION IS AN ATTACHMENT TO THIS REPORT. HE SUBMITTED A REPORT TO THE NTSB STATING THAT THE PURPOSE OF THE FLIGHT WAS TO PERFORM AN ENGINE RUN ONLY FOLLOWING AN ANNUAL INSPECTION AND THERE WAS NO INTENTION TO FLY THE HELICOPTER. HE STATED IN THE REPORT THAT DURING THE ENGINE RUN, THE HELICOPTER "VIBRATED THE SKIDS OFF THE TRAILER, FALLING ON SIDE DAMAGING MAIN AND TAIL ROTOR BLADES." A COPY OF THE NTSB REPORT IS AN ATTACHMENT TO THIS REPORT.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.