What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) On June 21, 2003, at about 1600 a Cessna 182-H aircraft departed Cushing municipal aiport (cuh) with six people onboard to conduct a skydiving jump. The aircraft climbed to 3500-4000 feet. According to several witnesses, shortly after the first jumper departed the aircraft, the aircraft went into a stall and a spin. Shortly after the spin started a second jumper departed the aircraft and a few seconds later another jumper departed the aircraft. The aircraft impacted terrain one-half mile south of runway 36 at cuh. The pilot was fatally injured, two parachutist were seriously injured, two parachutist received minor injuries and one parachutist was not injured. The aircraft impacted the ground in a relatively flat attitude. The cabin section of the fuselage was crushed downward and the wings and empennage were twisted consistent with a counter-clockwise rotational force at impact. The vertical stabilizer was bent towards the right. The aircraft came to rest on a heading of 220 degrees. The propeller blades displayed a forward twisting and bending.
As the FAA filed it
(-23) ON JUNE 21, 2003, AT ABOUT 1600 A CESSNA 182-H AIRCRAFT DEPARTED CUSHING MUNICIPAL AIPORT (CUH) WITH SIX PEOPLE ONBOARD TO CONDUCT A SKYDIVING JUMP. THE AIRCRAFT CLIMBED TO 3500-4000 FEET. ACCORDING TO SEVERAL WITNESSES, SHORTLY AFTER THE FIRST JUMPER DEPARTED THE AIRCRAFT, THE AIRCRAFT WENT INTO A STALL AND A SPIN. SHORTLY AFTER THE SPIN STARTED A SECOND JUMPER DEPARTED THE AIRCRAFT AND A FEW SECONDS LATER ANOTHER JUMPER DEPARTED THE AIRCRAFT. THE AIRCRAFT IMPACTED TERRAIN ONE-HALF MILE SOUTH OF RUNWAY 36 AT CUH. THE PILOT WAS FATALLY INJURED, TWO PARACHUTIST WERE SERIOUSLY INJURED, TWO PARACHUTIST RECEIVED MINOR INJURIES AND ONE PARACHUTIST WAS NOT INJURED. THE AIRCRAFT IMPACTED THE GROUND IN A RELATIVELY FLAT ATTITUDE. THE CABIN SECTION OF THE FUSELAGE WAS CRUSHED DOWNWARD AND THE WINGS AND EMPENNAGE WERE TWISTED CONSISTENT WITH A COUNTER-CLOCKWISE ROTATIONAL FORCE AT IMPACT. THE VERTICAL STABILIZER WAS BENT TOWARDS THE RIGHT. THE AIRCRAFT CAME TO REST ON A HEADING OF 220 DEGREES. THE PROPELLER BLADES DISPLAYED A FORWARD TWISTING AND BENDING.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.