Technical Data
Beechcraft King Air 350 · Specifications
Overview
This document provides detailed specifications and performance data for the Beechcraft King Air 350. It is intended for pilots, aviation enthusiasts, and maintenance personnel who require precise technical information about the aircraft. The document includes weight statements, performance characteristics, cabin dimensions, and airport performance metrics, allowing users to understand the operational capabilities and limitations of the King Air 350. Key data points such as maximum weights, fuel capacities, and performance figures are clearly outlined to assist in flight planning and operational decision-making.
- Max Ramp Weight: 15,100 lb (6,849 kg)
- Max Takeoff Weight: 15,000 lb (6,804 kg)
- Max Landing Weight: 15,000 lb (6,804 kg)
- Max Payload: 2,800 lb (1,270 kg)
- Cruise Speed: 312 kt (359 mph) at FL 240
Document
Source
Originally published by www.aviation-broker.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Specifications
- Pages
- 5
- File size
- 36 KB
- Publisher
- www.aviation-broker.com
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- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)Not on file
- Systems & Wiring
- Service BulletinsNot on file
- Type Certificate (TCDS)Not on file
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In this document
Weight Statement
The King Air 350 has a maximum ramp weight of 15,100 lb (6,849 kg) and a maximum takeoff weight of 15,000 lb (6,804 kg). The maximum landing weight is also 15,000 lb (6,804 kg), with a maximum zero fuel weight of 12,500 lb (5,670 kg). The fuel capacity is 3,611 lb (1,638 kg), and the basic empty weight is 9,456 lb (4,289 kg). The useful load is 5,400 lb (2,449 kg).
Specifications and Performance Characteristics
The King Air 350 can accommodate 1 crew member and up to 9 passengers, or a total of 15. It has a wing loading of 48.4 lb/sq. ft. and a power loading of 7.14 lb/SHP. The takeoff noise level is measured at 72.1 dBA. The aircraft's external dimensions include a length of 46 ft 8 in (14.22 m), a height of 14 ft 4 in (4.37 m), and a wingspan of 57 ft 11 in (17.65 m).
Cabin Dimensions and Capacity
The cabin length is 19 ft 6 in (5.94 m), with a height of 4 ft 9 in (1.45 m) and a width of 4 ft 6 in (1.37 m). The total cabin volume is 440 cu. ft. (12.46 cu. m), which includes 355 cu. ft. (10.05 cu. m) for the passenger cabin. Internal baggage capacity is 55.3 cu. ft. (249 kg), while external nacelle lockers provide an additional 16.0 cu. ft. (272 kg).
Airport Performance
At maximum takeoff weight, the King Air 350 requires a takeoff field length of 3,300 ft (1,006 m) at sea level under standard conditions. The landing distance at maximum landing weight is 2,692 ft (821 m). The aircraft can climb to 25,000 ft in approximately 15 minutes with an all-engine climb rate of 2,731 fpm (832 m/min).
Cruise Performance and Range
The King Air 350 achieves a high-speed cruise of 312 kt (359 mph) at FL 240 with a fuel flow of 773 lb/hr (351 kg/hr). For long-range cruise, it operates at 237 kt (273 mph) at FL 330 with a fuel flow of 362 lb/hr (164 kg/hr). The maximum range with NBAA IFR reserves is 899 nm (1,665 km) with a payload of 2,800 lb.
Full document text
Technical Data 1 King Air 350 Weight Statement Design Weights Max. Ramp Weight ........................................................................... 15,100 lb. 6,849 kg. Max. Takeoff Weight ........................................................................ 15,000 lb. 6,804 kg. Max. Landing Weight........................................................................ 15,000 lb. 6,804 kg. Max. Zero Fuel Weight ..................................................................... 12,500 lb. 5,670 kg. Fuel Capacity ...................................................................................... 3,611 lb. 1,638 kg. Weight Breakdown Basic Empty Weight *......................................................................... 9,456 lb. 4,289 kg. 1 pilot .................................................................................................... 200 lb. 91 kg. Basic Operating Weight....................................................................... 9,656 lb. 4,380 kg. Typical Options: Brake De-ice ............................................................................................ 17 lb. 8 kg. Forward Right Side Cabinet ..................................................................... 27 lb. 12 kg. Typically Equipped Basic Operating Weight...................................... 9,700 lb. 4,400 kg. Max. Payload ...................................................................................... 2,800 lb. 1,270 kg. Useful Load ........................................................................................ 5,400 lb. 2,449 kg. * Basic Empty Weight includes 8 lateral tracking chairs, nacelle baggage lockers, EGPWS and Collision Awareness System Technical Data 2 Specifications and Performance Characteristics Seating (Crew + Pax) ....................................................................... 1 + 9 / 15 Wing Loading ............................................................................ 48.4 lb./sq. ft. Power Loading ............................................................................ 7.14 lb./SHP Noise: Takeoff .................................................................................. 72.1 dBA External Dimensions Length ............................................................................................. 46 ft. 8 in. (14.22 m) Height .............................................................................................. 14 ft. 4 in. (4.37 m) Span............................................................................................... 57 ft. 11 in. (17.65 m) Engines Manufacturer ..................................................................................... 2 P&WC Model ................................................................................................ PT6A-60 Output .......................................................................... 1,050 SHP/ISA+10°C Inspection Interval............................................................................. 3,600 hrs. Weights Max Ramp ........................................................................................ 15,100 lb. (6,849 kg.) Max Takeoff ..................................................................................... 15,000 lb. (6,804 kg.) Max Landing..................................................................................... 15,000 lb. (6,804 kg.) Max Zero Fuel .................................................................................. 12,500 lb. (5,670 kg.) Basic Operating .................................................................................. 9,700 lb. (4,400 kg.) Payload / Capacities Max Payload ....................................................................................... 2,800 lb. (1,270 kg.) Useful Load ........................................................................................ 5,400 lb. (2,449 kg.) Max Fuel Capacity .............................................................................. 3,611 lb. (1,638 kg.) (1 US gal = 6.7 lb./US gal.)............................................................ 539 US gal. Fuel w/max payload ............................................................................ 2,600 lb. (1,179 kg.) Technical Data 3 Specifications and Performance (continued) Cabin Dimensions Length ............................................................................................. 19 ft. 6 in. (5.94 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 .............................................................................. 355 cu. ft. (10.05 cu. m) (including lav. & bag) Total Volume ................................................................................... 440 cu. ft. (12.46 cu. m) Baggage Capacity Internal - Heated, Pressurized .............................................. 55.3 cu. ft./550 lb.(1.57 cu. m/249 kg.) External Nacelle Lockers..................................................... 16.0 cu. ft./600 lb.(0.45 cu. m/272 kg.) Pressurization Differential............................................................................................ 6.6 PSI Sea Level Cabin ................................................................................ 15,293 ft. Technical Data 4 Specifications and Performance (continued) Airport Performance Takeoff Field Length Max. TO Wt., SL, ISA........................................................................ 3,300 ft. (1,006 m) Max. TO Wt., 5,000 ft. elevation, 25°C .............................................. 5,376 ft. (1,639 m) Landing Distance
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Max Landing Wt., SL, ISA ................................................................. 2,692 ft. (821 m) Vapproach ............................................................................................. 109 kt Climb Performance (Max Takeoff Weight) Time to Climb / Altitude ......................................................... 15 min / FL 250 All-engine Climb Rate, flaps up ......................................................... 2,731 fpm (832 m/min) All-engine Climb Gradient, flaps up .................................................. 917 ft./nm (151 m/km) Engine-out Rate, T/O flaps ................................................................. 552 fpm (168 m/min) Engine-out Gradient, T/O flaps ......................................................... 304 ft/nm (50 m/km) Ceilings Certified............................................................................................ 35,000 ft. (10,668 m) All Engine Service............................................................................. 35,000 ft. (10,668 m) Engine-out Service............................................................................ 21,500 ft. (6,553 m) Cruise Performance High Speed Cruise Speed ...................................................................................... 312 kt/359 mph (578 km/hr) Fuel Flow......................................................................................... 773 lb./hr. (351 kg./hr) Altitude ................................................................................................ FL 240 Long Range Cruise Speed....................................................................................... 237 kt/273 mph (439 km/hr) Fuel Flow......................................................................................... 362 lb./hr. (164 kg./hr) Altitude ................................................................................................ FL 330 Technical Data 5 Specifications and Performance (continued) Maximum Range Performance (NBAA IFR reserves (w/100 nm alternate) – High Speed Cruise Maximum Payload with Available Fuel (2,800 lb. payload) Range ................................................................................................... 899 nm (1,665 km) Average Speed ...................................................................................... 274 kt. (507 km/hr) Trip Fuel............................................................................................. 1,897 lb. (860 kg.) Maximum Fuel with Available Payload (1,789 lb. payload) Range ................................................................................................ 1,489 nm (2,758 km) Average Speed ...................................................................................... 280 kt. (519 km/hr) Trip Fuel............................................................................................. 2,916 lb. (1,323 kg.) 4 passengers (800 lb. payload) Range ................................................................................................ 1,545 nm (2,861 km) Average Speed ...................................................................................... 286 kt. (530 km/hr) Trip Fuel............................................................................................. 2,959 lb. (1,342 kg.) Ferry (Zero payload) Range ................................................................................................ 1,572 nm (2,911 km) Average Speed ...................................................................................... 290 kt. (537 km/hr) Trip Fuel............................................................................................. 2,966 lb. (1,345 kg.) Mission Performance (4 passengers) 300 nm mission Flight Time..................................................................................... 1 hr. 02 min Trip Fuel................................................................................................ 879 lb. (399 kg.) Flight Level........................................................................................... FL 250 600 nm mission Flight Time..................................................................................... 2 hr. 01 min Trip Fuel............................................................................................. 1,465 lb. (665 kg.) Flight Level........................................................................................... FL 290 1,000 nm mission Flight Time..................................................................................... 3 hr. 26 min Trip Fuel............................................................................................. 2,092 lb. (949 kg.) Flight Level........................................................................................... FL 330