Rockwell Aero Commander (AC-500S)
Rockwell Aircraft
![](/content/rus/mnu/986/rockwell_500.jpg)
фотография с сайта www.airliners.net
STANDARD AIRCRAFT SPECIFICATIONS
Type: Rockwell AC-500S Aero Commander Engines: Lycoming IO-540-E1B5 (piston) Crew: 2 Pilots + 3 Scientists Ceiling: 12,500 feet (without supplemental cabin oxygen) 18,000 feet (with supplemental cabin oxygen) Rate of Climb: 1750 feet/minute Operational Airspeeds: 90-150 knots Electrical: Two 28 VDC 100 ampere alternators Max. Gross Weight: 6,750 lbs. Empty Weight: 5,341 lbs. (5,621 lbs. including RC-8 Aerial Camera) (5,756 lbs. including Snow System) Useful Load: 1,409 lbs. (fuel, personnel, cargo) (1,129 lbs. with camera installed) (994 lbs. with Snow System installed) Fuel Load: 958 lbs. (159 gal) Type Fuel: 100 LL Standard Fuel Burn: Normal Cruise Speed - 164 lbs./hr (27.3 gal/hr) Fuel Burn for specific mission configuration will be calculated during mission planning and will vary with environmental conditions. Maximum Range and Duration: @Normal Cruise - 670 nm @Max. Endurance - 860 nm @Normal Cruise - 4 hr 30 min @Max. Endurance - 6 hr 10 min Dimensions (external): Wing Span - 49 ft 0.6 in Total Length - 36 ft 9.7 in Fuselage Height - 14 ft 3.5 in Tail Height - 14 ft 8.2 in Forward Cabin Doors - 3 ft 10 in x 1 ft 11in Aft Cabin Doors - 3 ft 9 in x 2 ft 4 in Baggage Doors - 1 ft 11 in x 1 ft 7 in Dimensions (internal): Cabin Length - 10 ft 7.5 in Cabin Height - 4 ft 5 in Cabin Width - 4 ft 4 in Useable Volumes: Cabin - 177 cu ft Baggage compartment - 32 cu ft Additional Standard Equipment Cockpit: Weather radar, radar altimeter, GPS navigation system Cabin: Camera ports on bottom of fuselage (approx. 1' x 1') RC-8 aerial camera GPS data port |