Model
A-Viator AP68TP-600
Manufacturer
Vulcanair SpA
Equipped Price
$ 2,300,000
Pax Exec
7
Description
The Vulcanair A-Viator is an economical non pressurized twin engine high-wing turboprop. Its design is derived from the smaller Vulcanair P68 Series . Like the basic P68 model, the A-Viator is of all-metal unpressurized construction but unlike the earlier design, it has a retractable undercarriage, which helps toward the maximum speed of 220 knots. The extended fuselage can accommodate nine passengers and two pilots, but a large aft door facilitates cargo access and egress. 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.
Relative to Competitors in Class

Performance Stats
| Noise (db) | 71.7 |
| Exterior Length (ft) | 37 |
| Exterior Height (ft) | 11.9 |
| Exterior Wingspan (ft) | 39.4 |
| Cabin Length Net (ft) | 11.9 |
| Cabin Height (ft) | 4.1 |
| Cabin Width Max (ft) | 3.7 |
| Engines | 2 RR 250 B17C |
| Output (lbs) | 328 |
| Inspection Interval (hours) | 3,500t |
| Max Takeoff Weight (lbs) | 6,614 |
| Max Payload (lbs) | 1,718 |
| Useful Load (lbs) | 2,765 |
| Executive Payload (lbs) | 1,400 |
| Available Payload with Max Fuel (lbs) | 1,264 |
| Take Off Distance - Sea Level/ISA (ft) | 2,034 |
| Take Off Distance - 5000ft /25degs (ft) | 2,950 |
| Max Certificated Altitude (ft) | 25,000 |
| High Speed - True Airspeed (kts) | 214 |
| Max Payload Range - (NM) | 324 |
| Max Fuel Range - (NM) | 590 |
| 600nm Trip Flight Time | 3+35 |
| 600nm Trip Fuel Used | 1,100 |
| 1000nm Trip Flight Time | NP |
| 1000nm Trip Fuel Used | 0 |

