On September 20, 2019, about 1230 central daylight time, a Cessna 208B, N895SF, was substantially damaged during a hard landing at Pepperell Airport (26MA), Pepperell, Massachusetts. The commercial pilot and passenger were not injured. Visual meteorological conditions prevailed, and no flight plan was filed for the skydiving flight that departed at 1215. The airplane was privately owned and operated under the provisions of Title 14 Code of Federal Regulations Part 91.
On June 29, 2019, about 0910 eastern daylight time, a Cessna 208B, N80JF, was substantially damaged while landing at Blackwater Creek Ultralight Flightpark (9FD2), Plant City, Florida. The commercial pilot was not injured. The airplane was registered to ISR Aviation LLC and operated as Title 14 Code of Federal Regulations Part 91 skydiving flight. Visual meteorological conditions prevailed at the time of the accident, and no flight plan was filed for the flight. The local flight originated about 0900.
The pilot was conducting parachute jump operations near the airport. After climbing to altitude, he released his jumpers and returned to land. The pilot reported that, during the landing flare, the airplane struck the runway nosewheel first. He added that the airplane bounced, floated down the runway, and then settled to the right of the runway.
The airplane sustained substantial damage to the engine mount and right elevator.
The pilot reported that there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation.
After multiple requests, the pilot did not submit the National Transportation Safety Board Pilot/Operator Aircraft Accident/Incident Report Form 6120.1.
On October 14, 2016, about 1930 eastern daylight time, a Cessna 208, N208KM, was substantially damaged during a skydiving event over Marion County Airport (X35), Dunnellon, Florida. The commercial pilot was not injured and the skydiver was fatally injured. The commercial skydiving flight was conducted under the provisions of 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed and no flight plan was filed for the local flight.
On July 21, 2016, about 1400 central standard time, a Cessna 208B air drop configured airplane, N7581F, registered to Desert Sand Aircraft Leasing Company, Inc., of Carson City, Nevada, sustained substantial damage during a runway excursion after landing on runway 18 at the Baldwin Airport (WI14), Baldwin, Wisconsin. The commercial pilot and 14 passengers were not injured. The air drop flight was being operated by Skydive Twin Cities, of Baldwin, Wisconsin, and conducted under the provisions of Federal Code of Regulations Part 91. No flight plan was filed and local traffic advisory was requested by the pilot. Visual meteorological conditions with light rain showers prevailed throughout the area. The flight originated from WI14 about 1350.
On May 12, 2016, about 1413 Pacific daylight time, a Cessna 208B, N1114A, was substantially damaged during a forced landing near Acampo, California. The airplane was registered to Flanagan Enterprises (Nevada) INC., and operated by the Parachute Center under the provisions of Title 14 Code of Federal Regulations Part 91. The commercial pilot sustained minor injuries and his 17 passengers were not injured. Visual meteorological conditions prevailed and no flight plan was filed for the skydiving flight. The local flight originated about 1 minute prior to the accident.
On March 24, 2015, about 1459 central daylight time, a Cessna 208B, N106BZ, collided with terrain and trees during an off airport forced landing in Verdigris, Oklahoma. The force landing was a result of a loss of engine power during an en route climb. The airline transport rated pilot received minor injuries and the passenger was not injured. The airplane was substantially damaged. The aircraft was owned and operated by the pilot under the provisions of 14 Code of Federal Regulations Part 91 as post maintenance test flight. Visual meteorological conditions prevailed for the flight and it is unknown if a flight plan was filed. The flight originated from the Tulsa International Airport, Tulsa, Oklahoma, at 1441.
According to the pilot, during the landing on a grassy area that was parallel to the paved runway, the airplane touched down and impacted a ditch near an intersecting taxiway. The airplane became airborne, touched down on the other side of the intersecting taxiway, bounced again, and then landed hard on the nose gear, which resulted in substantial damage to the fuselage and subsequent collapse of the nose landing gear.
The pilot said that, while on short final, the airplane experienced a sudden sink rate when the wind changed from a head wind to calm conditions. He was unable to arrest the sink rate even after power was applied because of the lag time for the airplane’s turbine engine to spool up.
Prior to the flight, the pilot fueled the airplane with 16 gallons of jet fuel. He planned to make two local flights carrying skydivers aloft. During the second skydiving flight, he delayed releasing the skydivers due to traffic in the area. As he turned the airplane back toward the drop zone, the airplane’s engine experienced a total loss of power.
The flight was at 13,500 feet overhead the airport, preparing for the skydivers to jump. The pilot turned on the green light to initiate the jump. He then felt the aircraft shudder, but did not lose control of the airplane. After most of the jumpers had left the airplane, one of the skydivers came forward and notified the pilot of damage to the tail.
The pilot reported that the airplane, which was used for sky diving operations, was climbing through 7,000 feet mean sea level (msl) when he heard an explosion followed by a metal grinding noise coming from the engine section of the airplane. He felt the airplane vibrate, and smoke began to fill the cabin. He reported that the engine was not producing any power so he shut the fuel off and performed procedures to rid the cabin of smoke.
The pilot was returning a group of skydivers to their home base after a weekend of skydiving. He flew several jump flights, and then stopped early in the afternoon to prepare the airplane for the flight home. The flight was planned into an area of clouds, turbulence, and icing, which the pilot had researched. He delayed the departure until he decided that he could complete the planned flight under visual flight rules (VFR).
The pilot reported that prior to takeoff he drained the main lower sump, but not the wing sumps, as was company policy. The pilot stated that he was told by the mechanic that “constant use of the wing sumps causes them to leak, and also causes damage to the fuel cells that is hard to repair.” The pilot also reported that the airplane had been fueled a few days prior to the flight from a 55 gallon barrel by an electric pump at the company’s fueling facility.
After a parachute drop flight, the airplane taxied back to the ramp area. The airplane was parked on the ramp, with the engine running, while the next group of parachutists were boarding the airplane. During that time, a parachutist who had just landed, contacted the propeller and sustained a serious injury.
During sport parachute operations the aircraft inadvertently stalled when too many jumpers attached themselves on the outside of the aircraft. The jumpers had been briefed on limiting the number to exit at one time to six; however, they ignored these instructions. As they departed the aircraft the pilot regained control and landed without further incident.
As the plt & 16 jumpers deptd on a skydiving flt, the eng lost pwr at aprx 300′ agl. The acft then banked steeply left, spiraled in a steep nose dwn attitude & crashed. An exam revealed fuel in the tanks was contaminated with wtr & foreign material with the appearance of brown algae. Milky fluid (aprx 65% jet fuel & 34% wtr) was fnd in the eng fuel control, as well as iron contaminants. Dark stringy material was fnd in the fuel filters. The acft had been refueled fm 55 gal drums which contained contaminated fuel. The drums were stored upright & rain water could leak thru the filler caps. N551cc had a history of fuel contamination which on occasions caused the fuel bypass indicator to display. Rprtdly, the stall warning circuit brkr had been disengaged on other occasions, so as not to startle the jumpers; however, due to dmg, its preimpact psn could not be verified. Acft was estd to be 370 lbs ovr its max wt lmt & 1′ fwd of the cg lmt. The9 pax seats had been rmvd to haul up to 18 jumpers. Pax seat belts were not used. Lack of faa surveillance was noted.