A-VIATOR

A-VIATOR

The A-VIATOR is the simple, safe, yet not obvious answer to a large number of operators. Up till now operators did not have any alternative than spending fortunes in very old gas guzzling twin engine antiquated aircraft or having to revert to less safe single engine turboprop aircraft.

The A-VIATOR is an economical non pressurized twin engine turboprop answering to a multiple array of needs from private/charter operations to advanced airborne surveillance and aerial work missions. The A-VIATOR design is derived from the smaller P68 Series and its legendary flight qualities have been maintained.

The fuselage has been stretched to allow more space on board and 2 turbine powerplants replace the piston engines allowing the aircraft to operate in areas where AvGas is not readily available.

The retractable landing gear improves the already excellent speed characteristics, and the stretched fuselage allows a more efficient use of cabin space, resulting in a maximum seating capacity of 9 passengers and 2 pilots.

PERFORMANCE SPECS

2 Engines: Rolls Royce 250B17C (328 HP)  
Max Ramp Weight3025 kg6669 lb
Max Take-Off Weight3000 kg6613 lb
Max Landing Weight2850 kg6283 lb
Operating Empty Weight (std equipped w/avg optionals)1750 kg3858 lb
Max Zero Fuel Weight2550 kg5621 lb
Max Useful Load1275 kg2811 lb
Max Usable Fuel (with aux tanks)

675 kg

840 lt

1488 lb

222 US gal

Cruise Speed @ 100%, ISA, FL 100, MTOW

396 km/h

214 ktas

Long Range Cruise Speed @ 92%, ISA, FL 100, MTOW

313 km/h

169 ktas

Rate of Climb, 2 engines (ISA, S.I, MTOW)8,4 m/s1650 fpm
Single Engine Rate of Climb1.4 m/s270 fpm
Stall Speed (no flaps)139 km/h75 kcas
Stall Speed (full flaps)128 km/h69 kcas
Service Celling7620 m25000 ft
Service Celling (1 engine)2438 m8000 ft
Max Range 6 persons (77 kg): Cruise 95%, FL 100, 30' res1740 km939 nm
Take-Off Distance over 50ft640m2100 ft
Landing Distance over 50ft700 m2296 ft
Take-Off Ground Run400m1312ft
Landing Ground Run

330m

1083ft

INTERNAL

High Density
  • 11 seats
  • baggage compartment
  • volume .5 m3 – 17.66 ft3
Commuter
  • 10 seats
  • baggage compartment
  • volume .75 m3 – 26.5 ft3
Combi
  • 6 seats
  • cargo volume 2.5 m3 – 88 ft3
Special Mission
  • 4 Seats
Cargo
  • cargo volume 6.5 m3 – 230 ft3
Medivac
  • 2 stretchers – 2 assistants
COCKPIT
The A-Viator has dual controls but can be flown without any restrictions with one or two pilots. The pilot doors on the forward right and left hand side of the fuselage offer easy access to the cockpit.

The avionic suite is modern yet conservative to complement the utilitarian aspects of the aircraft with its modern deployment aspirations.

EXTERNAL

The fuselage is non-pressurized and of all metal construction. Seats and cargo are anchored by two sets of double tracks which run the entire length of the floor.
Four doors are available:
  • 2 pilot doors located on the forward right and left hand side
  • a main passenger door located on the left hand side
  • a fourth large double door, located on the aft right hand side, can be used by passengers or for loading cargo.

Wing span

12.00 m

39.37 ft

Wing area

18.60 m2

200.23 ft2

Overall length

11.27 m

36.97 ft

Overall height

3.63 m

11.91 ft

Wheel track

2.17 m

7.12 ft

Wheel base

3.51 m11.52 ft

Prop clearance

0.75 m2.46 ft

Design Features and Information

The A-Viator is powered by two Rolls-Royce 250 B17 C engines flat-rated at 328 SHP at 2030 rpm. The engines drive Hartzell three-blade, constant speed, fully feathering, reversible pitch propellers.

The excellent engine characteristics allow the aircraft to deliver:

  • superior performance relative to piston aircraft
  • excellent weight/power ratio
  • fuel economy
  • low emissions, low noise
  • reverse thrust
  • high TBO

Performance

The excellent performance and economics of the A-Viator can be summarized as follows:

  • low operating costs (low drag and low fuel consumption)
  • operation from short, unprepared airstrips
  • twin engine safety and reliability
  • ease of maintenance
  • excellent payload
  • low noise levels
  • outstanding versatility
  • full IFR capability

Rough Field Performance

A rugged landing gear, coupled with the wide wheel-base and the wing mounted engines that provide substantial ground clearance, allows the A-Viator to operate safely from short and unprepared strips. This capability is essential to operators who must fly into remote and seldom used airfields.

Maintenance

The A-Viator family has been designed and developed for a long service life and to minimize maintenance requirements.

Total maintenance costs are very low thanks to:

  • simple rugged structure
  • high prop tip clearance that considerably reduces foreign object damage
  • easily accessible service points

Dependability and ease of maintenance enable the A-Viator to be operated in remote areas for long periods of time.

Economics

The A-Viator's clean aerodynamics and and excellent weight/power ratio. This economic efficiency gives the A-Viator’s operators a substantial profit margin, unattainable by other turbine aircraft generally utilised for the same missions.

Customer Support

Vulcanair assures comprehensive worldwide product support, both directly and through its dealer network. Maintenance, overhaul and repair operations can be carried out at the Vulcanair Service Centre or at authorized centres worldwide.

For thorough instruction of pilots and ground crew, a modern training program is offered at the Vulcanair Training Centre. Efficient and prompt technical assistance is assured by Vulcanair technical representatives for AOG and other emergencies. The 250 B17 C engines are serviced worldwide by the large network of Rolls-Royce representatives and by their numerous authorized maintenance centres.

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DIscuss your requirements directly with one of our Sales Managers