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Category | Homebuilt aircraft |
---|---|
Manufacturer | Velocity Aircraft |
Seats | 4 |
Length | 23 ft 6 in (7.16 m) |
Wingspan | 30 ft 0 in (9.14 m) |
Height | 7 ft 6 in (2.29 m) |
Empty weight | 1, 700 lb (771 kg) |
Powerplant | 1 × Continental IO-550-N, 310 hp (230 kW) |
Cruise speed | 220 mph (354 km/h, 190 kn) |
Stall speed | 65 mph (105 km/h, 56 kn) |
Rate of climb | 1, 500 ft/min (7.6 m/s) |
Crew | 1 |
Capacity | 3 passengers |
Max takeoff weight | 2, 700 lb |
Gross weight | 2, 700 lb |
Procedures for pre-takeoff checklist, acceleration, and rotation.
Details how to handle crosswind components during takeoff.
Steps to take in case of inflight engine stoppage and restart.
Steps for making an engine-out landing and establishing glide.
Critical dimensions for calculating static CG.
Weighing procedure with oil, but no fuel, after accessories installed.
Records pilot's weight and aircraft scales for ARM calculation.
Records passenger's weight and aircraft scales for ARM calculation.
Procedure to calculate the Fuel ARM for the aircraft.
Formula and example for calculating static CG.
Procedure to calculate ARMs for pilot, passenger, fuel, baggage.
Setting up a weight & balance worksheet for final CG calculation.