19990819024739A

(.19) On August 19, 1999, at 0710 hours mountain standard time, a firefly 11 balloon, N7021U, landed hard in open desert terrain in Cave Creek, Arizona. The balloon was not damaged; however, 2 passengers sustained serious injuries while the pilot and the remaining 10 passengers received minor injuries. The balloon was being operated as a sightseeing flight by hot air balloon expeditions under the provisions of 14 CFR part 91 when the accident occurred. The flight originated from open desert terrain in phoenix, Arizona, about 0610 that morning. Visual meteorological conditions were reported at the time and no flight plan was filed. A company pilot in another balloon reported that the balloon encountered a sudden microburst resulting in an inadvertent hard landing. The pilot reported that he was en route to the targeted landing site at 3,000 feet MSL when he was advised that surface winds had increased to 12 knots. Because of the wind conditions the pilot selected an alternate landing site and briefed his passengers on high wind landing procedures. Of the 13 passengers, 10 sat on the floor of the basket and grasped handholds. The approach began at a descent rate of 700 feet pe r minute. During this time he told the two remaining passengers to sit down because they would be experiencing a very rough landing. After descending through 500 feet AGL, the balloon's vertical sink rate suddenly increased and the pilot turned his attention to task of landing the balloon. Prior to touchdown he shut off the fuel to the burner and prepared to open the parachute valve upon contact with the ground. With the increased rate of descent, the balloon landed short of the intended site and skidded before coming to a stop. (-23)aircraft's balloon was partially deflated due to severe wind down draft. Aircraft lost lift and struck ground and was dragged 100 meters prior to coming to a full stop. (.4) while attempting a high wind landing, the balloon hit hard and one passenger sustained serious injuries. The pilot checked weather prior to departure, and said that at 0610, the weather was mostly cloudy with surface winds from the south at 3 to 5 mph. About 0635, the nearby deer valley airport ATCT told the pilot that surface winds were 12 knots from 220 degrees. In addition, another company pilot told him by radio that surface winds in his location were now 25 mph. The pilot's ground crew also confirmed that surface winds had increased substantially. The pilot said that he was 3,000 feet MSL when the change in wind velocity was reported, and he selected an alternate landing site and briefed his passengers on high wind landing procedures. The approach was initiated at a descent rate of 700 fpm. During this time he told the two standing passengers to sit down because they would be experiencing a very rough landing. After descending through 500 feet AGL at 700 fpm, the balloon's vertical sink rate suddenly increased substantially. He said this encounter had caused distortion in the envelope that resulted in the envelope losing hot air (lift), and increasing his rate of descent. His attempt to slow the descent in the time remaining was unsuccessful and the balloon landed short of the intended site, rebounded into the air, and then skidded about 100 yards before coming to a stop with the carriage lying on its side. Another balloon pilot, who saw the landing, said that the balloon appeared to have encountered a sudden microburst that resulted in aninadvertent hard landing. Other witnesses described the final descent as rapid, and noted that the envelope was distorted (flattened) downward as if the balloon was being pushed down. According to the FAA approved performance data sheet, terminal velocity (VT) of the balloon under maximum gross weight conditions is 1,200 fpm with a recovery time to equilibrium 90 seconds, and altitude lost during recovery (from application of burner to equilibrium) to be 1,000 feet. The POH states that should weather conditions deteriorate while in flight, the pilot should land immediately, and "to risk damage if necessary to land while the flight is still under control." The manufacturer reported that the maximum demonstrated wind speed at landing during certification testing was 7 knots.