What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) The pilot in commamd failed to follow the checklist. In doing so, the pilot in command endangered the property and life of another. The bio-hazard area consisted of body fluids (blood) excreted from facial lacerations. On November 28, 2003, at approximately 2214 local time, the pilot in command of N103AE, a Bell 206-L1, attempted to start the aircraft with the main rotor blades secured (tied down) to the tail boom. At approximately 55% N1 during the start sequence, the rotor blade secured to the tail boom severed (broke) approximately 19 to 25 inches outboard of the rotor blade mounting point. With the blade severed, the aircraft entered a violent unbalanced condition, viciously bouncing about the helicopter parking area. The pilot in command successfully placed the throttle to the off position, the engine secured and the rotor system came to rest when the remaining rotor blade made tail boom contact. The aircraft sustained substantial damage, the pilot in command incurred minor injuries and the flight nurse sustained no injuries. The weather was VFR with a slight wind. A company flight plan was filed
As the FAA filed it
(-23) THE PILOT IN COMMAMD FAILED TO FOLLOW THE CHECKLIST. IN DOING SO, THE PILOT IN COMMAND ENDANGERED THE PROPERTY AND LIFE OF ANOTHER. THE BIO-HAZARD AREA CONSISTED OF BODY FLUIDS (BLOOD) EXCRETED FROM FACIAL LACERATIONS. ON NOVEMBER 28, 2003, AT APPROXIMATELY 2214 LOCAL TIME, THE PILOT IN COMMAND OF N103AE, A BELL 206-L1, ATTEMPTED TO START THE AIRCRAFT WITH THE MAIN ROTOR BLADES SECURED (TIED DOWN) TO THE TAIL BOOM. AT APPROXIMATELY 55% N1 DURING THE START SEQUENCE, THE ROTOR BLADE SECURED TO THE TAIL BOOM SEVERED (BROKE) APPROXIMATELY 19 TO 25 INCHES OUTBOARD OF THE ROTOR BLADE MOUNTING POINT. WITH THE BLADE SEVERED, THE AIRCRAFT ENTERED A VIOLENT UNBALANCED CONDITION, VICIOUSLY BOUNCING ABOUT THE HELICOPTER PARKING AREA. THE PILOT IN COMMAND SUCCESSFULLY PLACED THE THROTTLE TO THE OFF POSITION, THE ENGINE SECURED AND THE ROTOR SYSTEM CAME TO REST WHEN THE REMAINING ROTOR BLADE MADE TAIL BOOM CONTACT. THE AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE, THE PILOT IN COMMAND INCURRED MINOR INJURIES AND THE FLIGHT NURSE SUSTAINED NO INJURIES. THE WEATHER WAS VFR WITH A SLIGHT WIND. A COMPANY FLIGHT PLAN WAS FILED
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 N103AE · 1
Matched to the same aircraft by N-number and date.