New Exodus Aircraft DeltaJet 500 StingRay Microlight Aircraft For Sale

Tandem two-seat flexwing aircraft with weight-shift control. Electrically operated moveable hang-point trim system. Adjustable foot pedal positions. All-terrain wheels & tyres. Hydraulic disc brakes on nose wheel (optional mainwheels only, or all three wheels).

Type:
Airplane (Microlight)
Manufacturer:
Exodus Aircraft
Model:
DeltaJet 500 StingRay
Year:
New
Serial Number:
TBA
Reg. Number:
TBA
Total Time:
Delivery Hours Only
Seats:
2
Price:
Price upon request

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Price:
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Aircraft Model & Manufacturer:
Year:
2023
Total Time:
1
Registration Number:
TBA
Serial Number:
TBA
Seats:
2
Aircraft Location:
Contact Name:
Mike Morris
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Description

DeltaJet 500 StingRay – Rotax 912ULS

Performance
Stall Speed at MAUW – 39 mph
Trim Speed – 49 – 87 mph
Max Straight & level – 112 mph
Never Exceed Speed – 117 mph
Cruise Speed – 80 mph
Rate of Climb at MAUW – 1050 ft/min
Minimum Sink Rate at MAUW – 500 ft/min @ 48 mph
Best Glide Ratio (power off) – 8.02/1 @ 60mph
Take-off distance to clear 15 m obstacle – 242 m on wet grass*
Landing distance to clear 15 m obstacle – 219 m on wet grass*

Wing
Wing Area – 12.85 sq. m
Wingspan – 9.52 m
Nose angle – 128˚
Aspect Ratio – 7.05/1

Trike
Empty Weight – 252 kg
Max Take-off weight – 500 kg
Maximum Payload – 248 kg
Minimum Pilot Weight – 55 kg
Individual Seat Load – 120 kg
Overall Length – 3.30 m
Overall Height – 2.75 m
Wheel track – 1.66 m
Wheelbase – 1.75 m
Wheels – 42 cm dia. overall.

Engine
Rotax 912ULS
Fuel Consumption – 10 – 13 lph (4+ hrs endurance)
Fuel Capacity 55 litres
Warp Drive propeller – 283/1800

Summary
Rogallo wing with keel pocket & winglets.
Pilot suspended below wing in trike unit, using bar to control pitch & roll/yaw by altering relative positions of trike unit & wing.
Wing braced from below by struts; floating cross-tube construction with 86% double-surface Xlam covering;
22 battens on the top surface, 8 battens on the undersurface.
Undercarriage has three wheels in tricycle formation; coil-spring suspension on nosewheel & aerodynamically enclosed one-piece beam suspension on mainwheels.
Push-right go-left nosewheel steering independent from aerodynamic controls.
Aluminium-alloy tube trike unit with GRP body (carbon fibre optional).
Engine mounted below the wing, driving pusher propeller.

*Test Conditions
Airfield altitude 500ft., ground temperature 8˚C., ground pressure n/a., ground windspeed NIL, test payload 472.5 kg