Technical Data
King Air B200 Weight Statement
Design Weights
Max. Ramp Weight ........................................................................... 12,590 lb. (5,711 kg.)
Max. Takeoff Weight ........................................................................ 12,500 lb. (5,670 kg.)
Max. Landing Weight........................................................................ 12,500 lb. (5,670 kg.)
Max. Zero Fuel Weight ..................................................................... 11,000 lb. (4,990 kg.)
Fuel Capacity ...................................................................................... 3,645 lb. (1,653 kg.)
Weight Breakdown
Basic Empty Weight *......................................................................... 8,283 lb. (3,757 kg.)
1 pilot .................................................................................................... 200 lb. (91 kg.)
Basic Operating Weight....................................................................... 8,483 lb. (3,848 kg.)
Typical Options:
Brake De-ice ............................................................................................ 17 lb. (8 kg.)
Aft Pyramid Cabinet ................................................................................. 30 lb. (14 kg.)
Typically Equipped Basic Operating Weight ...................................... 8,530 lb. (3,869 kg.)
Max. Payload ...................................................................................... 2,470 lb. (1,120 kg.)
Useful Load ........................................................................................ 4,060 lb. (1,842 kg.)
* Basic Empty Weight includes standard interior, avionics, unusable fuel and oil
1
Technical Data
Specifications and Performance
Characteristics
Seating (Crew + Pax) ....................................................................... 1 + 7 / 15
Wing Loading ............................................................................ 41.3 lb./sq. ft.
Power Loading ............................................................................ 7.35 lb./SHP
Noise: Takeoff .................................................................................. 81.1 dBA
External Dimensions
Length ........................................................................................... 43 ft. 10 in. (13.36 m)
Height ............................................................................................ 14 ft. 10 in. (4.52 m)
Span................................................................................................. 54 ft. 6 in. (16.61 m)
Engines
Manufacturer ..................................................................................... 2 P&WC
Model ................................................................................................ PT6A-42
Output ............................................................................. 850 SHP/ISA+26°C
Inspection Interval............................................................................. 3,600 hrs.
Weights
Max Ramp ........................................................................................ 12,590 lb. (5,711 kg.)
Max Takeoff ..................................................................................... 12,500 lb. (5,670 kg.)
Max Landing..................................................................................... 12,500 lb. (5,670 kg.)
Max Zero Fuel .................................................................................. 11,000 lb. (4,990 kg.)
Typically Equipped Basic Operating ................................................... 8,530 lb. (3,869 kg.)
Payload / Capacities
Max Payload ....................................................................................... 2,470 lb. (1,120 kg.)
Useful Load ........................................................................................ 4,060 lb. (1,842 kg.)
Max Fuel Capacity .............................................................................. 3,645 lb. (1,653 kg.)
(1 US gal = 6.7 lb./US gal.)............................................................ 544 US gal.
Fuel w/max payload ............................................................................ 1,590 lb. (721 kg.)
2
Technical Data
Specifications and Performance (continued)
Cabin Dimensions
Length ............................................................................................. 16 ft. 8 in. (5.08 m)
Height ............................................................................................... 4 ft. 9 in. (1.45 m)
Width................................................................................................. 4 ft. 6 in. (1.37 m)
Cabin Volume
Cockpit .............................................................................................. 85 cu. ft. (2.41 cu. m)
Passenger Cabin .............................................................................. 303 cu. ft. (8.58 cu. m)
(including lav. & bag)
Total Volume ................................................................................... 388 cu. ft. (10.99 cu. m)
Baggage Capacity
Internal - Heated, Pressurized .............................................. 55.3 cu. ft./550 lb.(1.57 cu. m/249 kg.)
Pressurization
Differential............................................................................................ 6.6 PSI
Sea Level Cabin To (ft.) .................................................................... 15,293 ft.
3
Technical Data
Specifications and Performance (continued)
Airport Performance
Takeoff Field Length
Max. TO Wt., SL, ISA........................................................................ 2,600 ft. (792 m)
Max. TO Wt., 5,000 ft. elevation, 25°C .............................................. 3,863 ft. (1,177 m)
Accelerate-Stop Distance
Max. TO Wt, SL, ISA ........................................................................ 3,413 ft. (1,040 m)
Max. TO Wt, 5,000 ft. elevation, 25°C ............................................... 4,576 ft. (1,395 m)
Landing Distance
Max Landing Wt., SL, ISA ................................................................. 2,845 ft. (867 m)
Vapproach ............................................................................................ 103 kt
Climb Performance (Max Takeoff Weight)
Time to Climb / Altitude ......................................................... 16 min / FL 250
Climb Rate ...................................................................................... 2,460 fpm (750 m/min)
Climb Gradient .............................................................................. 1,076 ft/ nm (177 m/km)
Engine-out Rate ................................................................................. 740 fpm (226 m/min)
Engine-out Gradient ......................................................................... 364 ft/nm (60 m/km)
Ceilings
Certified............................................................................................ 35,000 ft. (10,668 m)
All Engine Service............................................................................. 35,000 ft. (10,668 m)
Engine-out Service............................................................................ 21,900 ft. (6,675 m)
Cruise Performance
High Speed Cruise
Speed ...................................................................................... 289 kt/333 mph (535 km/hr)
Fuel Flow......................................................................................... 700 lb./hr. (318 kg./hr)
Altitude ................................................................................................ FL 220
Long Range Cruise
Speed....................................................................................... 228 kt/262 mph (422 km/hr)
Fuel Flow......................................................................................... 378 lb./hr. (171 kg./hr)
Altitude ................................................................................................ FL 290
4
Technical Data
Specifications and Performance (continued)
Maximum Range Performance (NBAA IFR reserves (w/100 nm alternate) – High Speed Cruise
Maximum Payload with Available Fuel (2,470 lb. payload)
Range ................................................................................................... 406 nm (752 km)
Average Speed ...................................................................................... 249 kt. (461 km/hr)
Trip Fuel................................................................................................ 923 lb. (419 kg.)
Maximum Fuel with Available Payload (415 lb. payload)
Range ................................................................................................ 1,644 nm (3,045 km)
Average Speed ...................................................................................... 267 kt. (494 km/hr)
Trip Fuel............................................................................................. 2,999 lb. (1,360 kg.)
4 passengers (800 lb. payload)
Range ................................................................................................ 1,407 nm (2,606 km)
Average Speed ...................................................................................... 265 kt. (491 km/hr)
Trip Fuel............................................................................................. 2,610 lb. (1,184 kg.)
Ferry (Zero payload)
Range ................................................................................................ 1,677 nm (3,106 km)
Average Speed ...................................................................................... 270 kt. (500 km/hr)
Trip Fuel............................................................................................. 3,028 lb. (1,373 kg.)
Mission Performance (4 passengers)
300 nm mission
Flight Time..................................................................................... 1 hr. 07 min
Trip Fuel................................................................................................ 792 lb. (359 kg.)
Flight Level........................................................................................... FL 250
600 nm mission
Flight Time..................................................................................... 2 hr. 13 min
Trip Fuel............................................................................................. 1,324 lb. (601 kg.)
Flight Level........................................................................................... FL 290
1,000 nm mission
Flight Time..................................................................................... 3 hr. 39 min
Trip Fuel............................................................................................. 2,101 lb. (953 kg.)
Flight Level........................................................................................... FL 290
