The Seneca V was put into production as a 1997 model year. Again the cowls were redesigned for increased performance, several cockpit switches were relocated from the panel to the headliner, and an improved engine variant, the Continental TSIO-360-RB, fitted with an intercooler, was used.

The Seneca V gross weights remain the same as the Seneca III and IV at 4,750 lb (2,155 kg) for takeoff and 4,513 lb (2,047 kg) for landing, therefore, with all of the added features, the useful load is reduced by about 200 lb (91 kg). The standard useful load for the 2014 model is 1,331 lb (604 kg) but typically is 1,134 lb (514 kg) when the aircraft is equipped with air conditioning, deicing equipment and co-pilot instruments.

Specifications Seneca V:
Engine: Turbocharged six-cylinder Continental TSIO-360-RB 220 hp
Propeller: Three-blade, constant speed, full feathering
Wing Span: 38.9 feet
Length: 28.6 feet
Height: 9.9 feet
Fuel Capacity: 122 US gallons useable
Max T/O Weight: 4,750 pounds
Max Ramp Weight: 4,773 pounds
Standard Empty Weight: 3,442 pounds
Useful Load: 1,331 pounds
Range: 828 NM including 45 minute reserve
Service Ceiling: 25,000 feet
Takeoff Distance: 1,143 feet
Landing Distance: 1,400 feet
Max Cruise Speed: 200 knots
Stall Speed: 61 knots, landing configuration
Passengers: Five, six with extra center seat.

Tips: 💡Nav Lights in Activate #1, 💡 Landing lights in Activate #2. 🛬 Landing with full flaps ( Vtol Down Down) with 🌀10% of Throttle. I hope you're enjoy!! -Psanford-