Geometric parameters |
Dimensions of passenger cabin (cargo compartment) and hatches |
Basic specifications |
Options |
Flight deck |
Length, ft | 36,42 |
Wing length, ft | 46 |
Ramp height, ft | 11,15 |
Maximum width of fuselage, ft | 6,56 |
Track of landing gear, ft | 6 |
Wheelbase of landing gear, ft | 11,23 |
Wing area, ft2 | 217,4 |
length, ft | 11,32 |
width, ft | 5,381 |
height, ft | 4,068 |
Cabin capacity, ft3 | 130,7 |
Maximum length of cargo, ft | 14,53 |
Front upper access door, ft | 1,47 õ 1,90 |
Rear upper access door, ft | 5,545 x 4,232 |
Emergency doors (left, right), ft | 2,23 õ 2,23 |
Maximum takeoff weight, lb | 5997 |
Maximum useful comercial load, lb | 1764 |
Maximum fuel capacity (ferrying), gal | 396,3 |
Maximum altitude, ft | 14760 |
Maximum allowable speed, ktas | 189,5 |
Maximum speed of horizontal flight, ktas | 170,9 |
Cruise speed (economy) ktas | 146 |
Range of flight (payload 1764 lb), nm (max) | 648/2160 |
Duration of flight (max t.o.w.), pay load) | 5,6 |
Rate of climb, ft/min. At full load ft/min | 787-1181 |
Runway length land/water level (max t.o.w.), ft | 1148/1476 |
Landing speed (at maximum weight), ktas | 53 |
Maximum overload | +3,8—1,9 |
Basic 0 (standard) avionics set provide the VFR operation. Weight of basic equipment is included in standard empty weight.
The aircraft may be equipped with additional (optional) IFR avionics. This configuration means special architecture of power supply system and air pressure system, in consideration with FAR-23 requirement.
Weight of additional equipment and supply system will be added to standard empty weight.
Configuration of additional avionics will be specified with Customer
2.2.2 Standard avionic and equipment set (Fig.6)
(a) Controls and system’s monitoring, standard
1 – control wheel |
15 – engine diagnostic monitor: |
Basic 1 |
Basic 2 |