DeLand - DeLand
Flight / Schedule
DeLand - DeLand
Aircraft
Pilatus PC-6 (Porter & Turbo Porter)Registration
N7895J
MSN
767
Year of Manufacture
1976
Operator
Skydive DeLandDate
October 3, 2005 at 03:05 PM
Type
CRASHFlight Type
Skydiving / Paratroopers
Flight Phase
Takeoff (climb)
Crash Site
Airport (less than 10 km from airport)
Crash Location
DeLand Florida
Region
North America • United States of America
Coordinates
29.0281°, -81.3034°
Crash Cause
Human factor
Narrative Report
On October 3, 2005 at 03:05 PM, DeLand - DeLand experienced a crash involving Pilatus PC-6 (Porter & Turbo Porter), operated by Skydive DeLand, with the event recorded near DeLand Florida.
The flight was categorized as skydiving / paratroopers and the reported phase was takeoff (climb) at a airport (less than 10 km from airport) crash site.
10 people were known to be on board, 0 fatalities were recorded, 10 survivors were identified or estimated. This corresponds to an estimated fatality rate of 0.0%.
Crew on board: 1, crew fatalities: 0, passengers on board: 9, passenger fatalities: 0, other fatalities: 0.
The listed crash cause is human factor. The airline transport certificated pilot with 10 skydiving passengers began a takeoff in a tailwheel-equipped and turboprop powered airplane on a CFR Part 91 skydiving flight. As the airplane started its climb, the pitch angle of the nose of the airplane increased until the airplane appeared to stall about 50 to 100 feet agl. It descended and impacted the runway in a left wing, nose low attitude. Several FAA inspectors responded to the accident site and documented the accident scene and the airplane systems. The inspectors reported that flight control continuity was established, and they noted that the stabilizer appeared to be in a nose up trim position. Measurement of the stabilizer trim position equated to a 56.5 percent nose up trim condition. The airplane's horizontal stabilizer trim system is electrical. An electric trim indicator, and a trim warning light were installed in the upper left portion of the instrument panel. The light will illuminate if "full-up" trim is set, and the engine is producing over 80 percent power. A placard stating, "Set Correct Trim for Takeoff," was installed on the lower instrument panel in front of the pilot position. The airplane's flight manual contains a "Before Takeoff" warning, which states, in part: "Warning - An extreme out-of-trim stabilizer can, in combination with loading, flaps position and power influence, result in an uncontrollable aircraft after the aircraft leaves the ground." In addition, a caution states, in part: "Caution - Failure to set correct trim settings will result in large control forces and/or unrequested pitching/yawing." Pilot actions listed in the "Before Takeoff" checklist include stabilizer trim settings. The airplane contained seat belts for all passengers, but the pilot's shoulder harness was not used, as it was folded and tie-wrapped near its upper attach point.
Aircraft reference details include registration N7895J, MSN 767, year of manufacture 1976.
Geospatial coordinates for this crash are approximately 29.0281°, -81.3034°.
Fatalities
Total
0
Crew
0
Passengers
0
Other
0
Crash Summary
The airline transport certificated pilot with 10 skydiving passengers began a takeoff in a tailwheel-equipped and turboprop powered airplane on a CFR Part 91 skydiving flight. As the airplane started its climb, the pitch angle of the nose of the airplane increased until the airplane appeared to stall about 50 to 100 feet agl. It descended and impacted the runway in a left wing, nose low attitude. Several FAA inspectors responded to the accident site and documented the accident scene and the airplane systems. The inspectors reported that flight control continuity was established, and they noted that the stabilizer appeared to be in a nose up trim position. Measurement of the stabilizer trim position equated to a 56.5 percent nose up trim condition. The airplane's horizontal stabilizer trim system is electrical. An electric trim indicator, and a trim warning light were installed in the upper left portion of the instrument panel. The light will illuminate if "full-up" trim is set, and the engine is producing over 80 percent power. A placard stating, "Set Correct Trim for Takeoff," was installed on the lower instrument panel in front of the pilot position. The airplane's flight manual contains a "Before Takeoff" warning, which states, in part: "Warning - An extreme out-of-trim stabilizer can, in combination with loading, flaps position and power influence, result in an uncontrollable aircraft after the aircraft leaves the ground." In addition, a caution states, in part: "Caution - Failure to set correct trim settings will result in large control forces and/or unrequested pitching/yawing." Pilot actions listed in the "Before Takeoff" checklist include stabilizer trim settings. The airplane contained seat belts for all passengers, but the pilot's shoulder harness was not used, as it was folded and tie-wrapped near its upper attach point.
Cause: Human factor
Occupants & Outcome
Crew On Board
1
Passengers On Board
9
Estimated Survivors
10
Fatality Rate
0.0%
Known people on board: 10
Operational Details
Schedule / Flight
DeLand - DeLand
Operator
Skydive DeLandFlight Type
Skydiving / Paratroopers
Flight Phase
Takeoff (climb)
Crash Site
Airport (less than 10 km from airport)
Region / Country
North America • United States of America
