Raytheon 300 Super King Air

Turboprop • twin engine • Low Wing • Retractable gear

Range Visualization

Origin: · click map to move · nm at current load

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
315
KTAS
Cruise Speed
9
Occupants
1480
nm
Max Range
1652
lbs
Wet Payload

Estimated Ownership Costs

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About the Raytheon 300 Super King Air

Overview

The Beechcraft King Air 300 is the second-generation Super King Air, a twin-turboprop introduced by Beech in 1984 as the high-performance evolution of the Model 200. The 300 retained the family’s defining straight-wing planform but added 1,050 SHP Pratt & Whitney Canada PT6A-60A engines (up from 850 SHP in the 200), aerodynamic refinements, and a strengthened airframe. Production ran through 1988, when the type was superseded by the longer-fuselage King Air 350 with the same engines and a redesigned wing.

The marketing nameplate evolved with the manufacturer’s corporate identity. Beech Aircraft Corporation became a Raytheon subsidiary in 1980, four years before the 300 entered service. Early airframes wore the Beechcraft badge; later production was variously marketed as Beech Super King Air 300 or Raytheon 300 Super King Air. The FAA type designator across all variants is BE30.

The 300 occupies a discrete used-market segment between the more numerous Model 200 and the more capable 350. Operationally it offers more performance than a 200 (faster cruise, higher single-engine ceiling, more useful load) and less cabin volume than a 350. The parts and maintenance ecosystem shared across the King Air family carries over.

Key Features for GA Buyers

  • Twin PT6A-60A power. Each engine produces 1,050 SHP, a substantial step up from the 200’s 850-SHP PT6A-42. Hot-and-high climb performance, single-engine ceiling, and altitude capability all benefit from the additional power. The -60A operates within the broad PT6A overhaul ecosystem, with a published factory TBO of 3,600 hours and a Hot Section Inspection at 1,800 hours.
  • Pressurized cabin. Standard cabin pressurization supports cruise from FL270 to FL350. The cabin accommodates up to eight passengers in a typical executive arrangement with a private aft lavatory.
  • Cruise performance. High-speed cruise at FL280 sits in the 310 to 320 KTAS range, with 90 to 110 GPH total fuel burn depending on power setting and altitude. Range at long-range cruise extends past 1,500 NM with reserves, putting most domestic city pairs within nonstop reach.
  • Mature maintenance ecosystem. The King Air series is the most-produced cabin-class turboprop family ever built. Phase inspections, parts, and type-rated shop coverage are widely available. Engine programs (P&WC ESP, JSSI) cover most -60A operators.
  • Upgrade paths. Blackhawk’s PT6A-67 conversions and Raisbeck performance kits are widely fitted to the 300 and extend range, climb, and cruise margins. Avionics retrofits to Garmin G1000NXi, GTN 750/650, and ADS-B Out are routine.

Trade-offs

  • Niche between siblings. The 300 sits between two more-popular King Airs. The 200 has the larger fleet and the lowest operating costs in the family; the 350 has more cabin and the same engines on a longer airframe. Used 300s take longer to move than comparable 200s or 350s of similar vintage.
  • Higher operating cost than the 200. Total fuel burn is roughly 90 to 110 GPH vs. 75 to 90 GPH on a 200 of similar mission. Variable hourly costs run $1,300 to $1,500 at strict variable (fuel, engine reserves, maintenance). Fully-loaded total cost including crew and fixed amortization runs $2,500 to $3,000.
  • Engine reserves dominate. PT6A-60A overhauls run roughly $500K per engine before LLCs, with second overhauls (LLCs replaced) approaching $1M. At 400 hours per year and a 3,600-hour TBO, base engine reserve accrual runs roughly $55K per engine per year. LLC replacement at second overhaul pushes combined reserves to $150K per year or higher.
  • Crew expectations. The 300 is single-pilot certified, but most insurance underwriters require turboprop time and recurrent training (typically Simuflite or FlightSafety initial plus annual recurrent). First-time turboprop owners should budget for initial and annual recurrent training costs.
  • Phase inspection cycle. King Airs use Beech phase inspections rather than a Part 91 annual. Phases 1 through 4 over a 24-month cycle, plus the HUIP inspection, generate uneven scheduled maintenance costs. Expense falls unevenly across the cycle, not spread like a piston annual.

See Also

Technical Specifications

Dimensions

Wingspan
54.5 ft
Length
43.83 ft
Height
14.3 ft
Parking area (ft2)
3149.54 ft2

Weights

Max Takeoff Weight
14,000 lbs
Max Landing Weight
14,000 lbs
Useful Load
5,263 lbs
Fuel Capacity
539 gal

Performance

Cruise Speed
315 KTAS
Never-Exceed (Vne)
318 KIAS
Approach Speed
107 KIAS
Stall, Clean (Vs1)
82 KIAS
Range
1480 NM
Service Ceiling
35,000 ft
Rate of Climb
867 - 2844 fpm
Takeoff over 50 ft obstacle
3,600 ft
Landing ground roll
4,133 ft

Engines

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