Beech Super King Air 350

Turboprop • twin engine • Low Wing • Retractable gear

Range Visualization

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Payload vs. Range

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Default: 190 lbs (FAA standard)

Default: 30 lbs

Passengers
lbs @ lbs / pax
0 lbs
Fuel on board
gal
+ Weight
Range
Available Range / nm
Mission capable — Aircraft can handle the current load with full fuel tanks.
Fuel tradeoff required — You'll need to leave gallons of fuel behind ( gal usable for nm range).
Over max gross weight — Reduce payload by lbs to safely operate this aircraft.

Mission Profile

Endorsements & ratings:
  • High-Performance
  • Complex
  • High-Altitude
  • Pressurization
  • Multi-Engine
  • Instrument
262
KTAS
Cruise Speed
11
Occupants
1806
nm
Max Range
1534
lbs
Wet Payload

Estimated Ownership Costs

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About the Beech Super King Air 350

Overview

The Super King Air 350 is the top-of-line cabin-class twin turboprop in Beechcraft’s King Air family, certified in 1989 and produced through 2015 before being rebranded as the King Air 350i and, eventually, the King Air 360. With two PT6A-60A engines flat-rated to 1,050 shp per side and a 35,000-foot service ceiling, the 350 is the variant that competes meaningfully with light jets on legs under 400 nautical miles, where its short-runway capability and full-payload-with-full-fuel economics outperform jet alternatives.

For the GA buyer, the 350 sits in a different operational tier from the 90/100/200 line. It is one of only two King Airs (alongside the earlier 300) that requires a type rating, certified under FAA Part 23 Commuter category because it exceeds 12,500 pounds gross weight. The mission set is corporate transport, government and ISR work, medevac, and high-utilization charter.

Key Features for GA Buyers

  • Light-jet performance envelope. 312-knot maximum cruise, 35,000-ft service ceiling, and 1,806 nm range cover most domestic business missions without a fuel stop.
  • Full-payload, full-fuel capability. 5,145 lb useful load lets operators top off and still carry eight passengers plus baggage, an economic argument no comparable light jet can match.
  • Short-runway access. Backed by props rather than thrust reversers, the 350 routinely operates from 3,000-foot strips closed to most jets.
  • Mission flexibility. Civilian VIP, medevac, military ISR, and cargo conversions all share the same airframe and parts logistics, supporting strong residual values.

Trade-offs

  • Type rating required. The 350 (and the predecessor 300) cannot be flown on a multi-engine turboprop rating alone; budget for type rating training and recurrent currency.
  • Fuel and acquisition costs. 95 GPH cruise burn and a $4-8M typical pre-owned price place the 350 above most owner-operator budgets; the operator is typically a corporate flight department or charter company.
  • Cabin tighter than light jets. The 4.5-foot cabin width is narrower than a Citation M2 or Phenom 100, a trade-off for the structural and weight advantages of the King Air formula.
  • Newer 360 supersedes the model. Pre-owned 350 buyers are competing with depreciation pressure from the active 360 production line, which adds Pro Line Fusion avionics and other upgrades.

See Also

Technical Specifications

Dimensions

Wingspan
57.917 ft
Length
46.7 ft
Height
14.333 ft
Parking area (ft2)
3511.31 ft2

Weights

Max Takeoff Weight
15,000 lbs
Max Landing Weight
15,000 lbs
Useful Load
5,145 lbs
Fuel Capacity
539 gal

Performance

Cruise Speed
262 KTAS
Never-Exceed (Vne)
312 KIAS
Approach Speed
110 KIAS
Stall, Clean (Vs1)
75 KIAS
Range
1806 NM
Service Ceiling
35,000 ft
Rate of Climb
2700 fpm

Engines

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