Rockwell Aero Commander (AC-500S)

Rockwell Aircraft

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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