Beechcraft · 1964–2005
Beechcraft King Air C90
Specifications
Performance
Cruise
246KTAS
Range
738nm
Climb
2010fpm
Ceiling
30,000ft
Fuel Burn
88.0gph
Fuel Cap.
384gal
MPG
3.2mpg
Stall (Vs0)
76KIAS
T/O roll
—ft
Ldg roll
1260ft
Size & weight
Seats
7
Useful Load
3,120lbs
Full-fuel payload
547lbs
Max gross
10,100lbs
Wingspan
50.25ft
Length
35.5ft
Engine
Engine
Pratt & Whitney Canada PT6A-21
Power
1100hp
TBO
3,600hrs
Overhaul
$319keach
Hot section
$45keach
Engines
2
Owning it
Hull insurance
$10k/yr
Parts
excellent
Mechanics
common
Gear
Retractable
IFR
Yes
Category
certified
Full specification
V-speeds
Airframe
- Empty weight
- 6,980 lbs
- Max fuel weight
- 2,573 lbs
- Height
- 14.25 ft
- Wing position
- low
Obstacle performance
- Takeoff over 50 ft
- 2,710 ft
- Landing over 50 ft
- 2,290 ft
Paperwork
- Type certificate
- 3A20
- Certification basis
- CAR 3
These figures are typical for the model, not a specification for any individual aircraft. Real-world numbers vary with year, installed equipment, weight, modifications and engine condition — often by more than you would expect. Use them to compare types, and confirm anything you would act on against the Pilot's Operating Handbook for that specific airframe and a prebuy inspection.
Pricing
Typical
$750k
Range
$350k – $1.8M
Annual all-in
~$156k/yr
All-in at ~100 flying hours a year, using the midpoint of each range — the same figures broken out under “Cost to own” below. Your number will differ, and mostly for two reasons. Experience sets your insurance: a 2,000-hour pilot with recent training pays 30–40% less than a 200-hour owner, and student owners pay 20–40% more — on the same aircraft that is often a doubling. Location sets your hangar: a T-hangar runs $200–400 a month in the Midwest against $400–1,500 in a coastal metro, and an outside tie-down is less again. Engine reserves move too — a local shop reusing your serviceable cylinders can come in 30–50% under the national specialty-shop pricing we quote, though you trade the warranty and turnaround that comes with it. Reserves are money set aside toward a future overhaul, not a bill this year, and the annual inspection figure is the shop’s labor to look — whatever they find is separate.
Cost to own — estimate
Set your yearly hours and local fuel price. Fixed costs (insurance, hangar, annual inspection) don't change with hours; fuel, maintenance and the engine reserve do.
- Fuel (88 gph)
- $52,800
- Engine reserve
- $17,722
- Propeller reserve
- $2,500
- Maintenance, parts & wear items ($160/hr)
- $16,000
- Hot section reserve
- $5,000
- Insurance
- $15,000–$33,750
- Hangar
- $10,703–$26,758
- Annual inspection (labor only)
- $12,000
- Databases & subscriptions
- $2,000
- Total per year
- $151,128
- Per flight hour
- $1,511
- Miles flown / year (at cruise)
- 28,309 mi
- Cost per mile
- $5.34/mi
- Time in the air
- 1 hr 13 min
- Fuel burned
- 107 gal
- Out of pocket
- $1,147
Fuel, engine reserve and wear only. Insurance, hangar and the annual are already paid whether you make the trip or not, so they are not charged here.
Estimate, not a quote. Where a line shows a range, the total, per-hour and per-mile figures use its midpoint— insurance moves most with your experience and time in type, hangar with where you base the aircraft, so your own number could sit at either end. Annual inspection is the shop's labor to open and inspect — what they find is the maintenance line, which covers oil changes, plugs, tires, brakes, hoses, lights, a battery and vacuum pump amortised over their life, and the unscheduled squawks that are the largest and least predictable part of it. Reserves are sinking funds toward an overhaul, not a bill you pay this year — and note that a propeller is due on hours or calendar time, typically six years, so flying less does not put it off forever.
Strengths
- Twin turbines with dispatch reliability piston twins cannot match
- Pressurized cabin (5.0 psi) and real-cabin comfort for 5–7 occupants
- Excellent parts and maintenance ecosystem; PT6A is best-supported turbine in aviation
- Proven 60-year track record; forgiving handling and docile characteristics
Weaknesses
- Direct operating cost $700–$900/hr; full all-in ownership ~$200k/yr for active use
- Engine overhauls ~$500k paired; run-out engines severely depress resale value
- Slower than competitors (226 KTAS cruise vs. B200's 265+); no cargo door on most variants
- Older airframes dominated by SID corrosion items (center-section, cabin bilge, insulation); annual variance $15k–$120k
Overview
The King Air 90 series is where the best-selling turboprop family in history began: Beechcraft mated two Pratt & Whitney Canada PT6A free turbines to a pressurized Queen Air-derived airframe in 1964, and kept building straight-tail 90s for 57 years. This page covers the conventional-tail, 550-shp-class line — Model 90 through C90B — which accounts for well over 2,000 airframes and remains the most affordable way into cabin-class turbine twin ownership. The follow-on C90GT/GTi/GTx (2006-2021) is the same airframe with PT6A-135A engines and is a materially different — and much more expensive — airplane, so it has its own page. So do the T-tail F90 and the larger 200/B200.
What the C90 sells is not speed — a Malibu will outrun the early ones — but two turbines, a real cabin with a 5.0 psi pressure vessel, docile handling, a huge support network, and dispatch reliability piston twins cannot match. It is flown by owner-pilots stepping up from piston twins and singles, small charter and medevac operators, and flight departments that value the type's forgiving manners. No type rating is required (under 12,500 lb), which makes insurance, not the FAA, the gatekeeper.
The frontmatter describes a C90B (1992-2005): the last and most refined of the line, with four-blade props, dynamic vibration absorbers, and a 10,100 lb gross weight. On the FAA type certificate the C90B and C90SE are commercial designations of the C90A — a fact that matters when reading the TCDS and ADs.
Variants & History
| Variant | Years | Serials | Engines | shp each (installed) | MTOW | Typical cruise | Notes |
|---|---|---|---|---|---|---|---|
| 90 / A90 / B90 | 1964-1971 | LJ-1 to LJ-501 | PT6A-6 / -20 | 500-550 | 9,300-9,650 lb | ~210-220 KTAS | Round-window originals; 25,000-27,000 ft ceilings; cheapest entry, oldest systems |
| C90 | 1971-1982 | LJ-502 to LJ-1010 | PT6A-20A, then PT6A-21 (LJ-668+) | 550 | 9,650 lb | ~222 KTAS | Longer span than B90; the classic 90 |
| C90-1 | 1982-1983 | LJ-1011 to LJ-1062 | PT6A-21 | 550 | 9,650 lb | ~222 KTAS | Higher cabin pressure differential |
| E90 | 1972-1981 | LW-1 to LW-347 | PT6A-28, flat-rated | 550 | 10,100 lb | 249 KTAS | Own page. 474 gal against this page's 384 — 23% more fuel, so it cannot be scored from these numbers |
| C90A | 1984-1992 | LJ-1063 to LJ-1299 | PT6A-21 | 550 | 9,650 lb early, 10,100 lb from LJ-1138 | ~226 KTAS | Pitot cowlings; gross bump mid-run |
| C90B | 1992-2005 | LJ-1300 and after | PT6A-21 | 550 | 10,100 lb | ~226-246 KTAS | 4-blade props, vibration dampers, quieter cabin; certified as C90A |
| C90SE | 1994-1999 | within LJ-1367 to LJ-1538 | PT6A-21 | 550 | 10,100 lb | ~226 KTAS | Special Edition — decontented C90B, 3-blade props |
The E90's "680 hp" seen in listings is the PT6A-28's thermodynamic rating; installed it is flat-rated to 550 shp, same as the C90 — its advantage is holding that power to altitude, not more of it. (The old catalog page carried 680, which was the trap this rewrite exists to fix.)
Performance
The frontmatter triple is one regime from AOPA's 2003 C90B evaluation: 246 KTAS at maximum power in the 16,000-20,000 ft band, burning 88 gph (592 pph), which yields 738 nm with four passengers and NBAA IFR reserves. That is the airplane flown fast and low. Flown the way most owners actually fly it — FL210-FL290 — plan on 220-230 KTAS at 65-75 gph, and at maximum-range power the same airplane does 196 KTAS at 46 gph for 1,049 nm with reserves. Plane & Pilot's 1,264-mile range figure appears to be a statute-mile or long-range-cruise number and was not stored.
Climb is honest: 2,010 fpm at sea level at gross, 495 fpm single-engine. The certified maximum altitude is 30,000 ft, but the PT6A-21 is breathless up there; the practical band is FL210-FL260. Stall speeds stored are the C90's at 9,650 lb (76 kt landing config / 89 kt clean) — the C90B at 10,100 lb stalls a knot or two faster; Beech did not publish a separate C90B figure in the sources reviewed.
Runway numbers stored are the C90B's: 2,710 ft over 50 ft to take off at gross, 2,290 ft over 50 ft to land (1,260 ft ground roll). A 4,000 ft strip is comfortable; 3,000 ft is possible with discipline and is how the type has served Africa and Alaska for decades.
Vmo is 226 knots and it is calibrated (KCAS) per the type certificate — stored as-is per house convention, not converted.
Payload & Range
C90B, 10,100 lb gross, 6,980 lb equipped empty, 384 gal (2,573 lb) usable:
| Configuration | Fuel | Cabin load | Range |
|---|---|---|---|
| Full fuel | 384 gal | ~547 lb — pilot + 2 light | 738 nm fast / 1,049 nm at LRC, NBAA reserves |
| 4 people + bags (~800 lb) | ~345 gal | 800 lb | ~650 nm fast / ~900 nm LRC |
| Cabin full (~1,400 lb) | ~255 gal | 6 adults | ~450-500 nm |
The full-fuel payload is the honest limitation of the type: 547 lb. The E90 is often said to fix that, and this page used to say it — it does not. The E90 carries 90 more gallons, but they weigh about 600 lb against a 450 lb gross-weight increase, so its full-fuel payload is lower. What the E90 buys is range, not load. A buyer who needs to carry weight should look at a B200. No zero-fuel-weight limit on the C90B simplifies loading. The practical airplane is 4 people, bags, 600 nm, one fuel stop on a coast-to-coast — for half the operating cost of a B200.
Related pages: King Air C90GT/GTi/GTx, King Air F90, King Air 200/B200, King Air 350, Pilatus PC-12, Piper Cheyenne I/II, Cessna 425 Conquest I, valuation-methodology, engine-overhaul-pricing, insurance-underwriting, maintenance-ecosystem, business-travel, cross-country
Mission Suitability
Business travel (8/10). Four to five passengers, 500-700 nm legs, pressurized comfort, into 3,500 ft strips. It gives up 40-60 knots to a B200 and real money per hour to a PC-12, but nothing this side of $1M does the mission with two turbines.
Cross-country (8/10). Boots, radar, known-ice, FL250 weather-topping. Two legs across the continent instead of a B200's one.
Surveying (7/10). Stable, 5+ hour endurance with survey fuel loads, easy camera/sensor installs; decades of survey and air-ambulance service.
Cargo hauling (5/10). ~2,100-3,100 lb useful load depending on variant and equipment; no cargo door on most. Dense freight only.
Backcountry (3/10). It will use good 3,000 ft unimproved strips — bush operators have proven it — but gear, props and boots are expensive down there.
Flight training (2/10). Turbine transition and recurrent platform only.
Local fun (2/10), Aerobatics (1/10). $700+/hr direct; transport-category manners.
Avionics Ecosystem
- Pre-1984 aircraft: Collins/King radios, mechanical gyros. Heavily discounted unless upgraded; budget $150K-$250K for dual GTN Xi + G600 TXi + ADS-B if not done.
- C90A/C90B factory panels: Collins Pro Line II era; EFIS-equipped late C90Bs exist. Serviceable; CRT and gyro support is the pain point.
- The common refresh: dual Garmin GTN 750Xi/650Xi, GTX 345, G600 TXi, keeping the original autopilot overhauled — the panel most 2026 listings advertise.
- Garmin G1000 NXi retrofit (Textron-supported for 90-series): $300K+; transforms resale on late C90Bs.
A strong autopilot and a radar that actually paints matter more than glass. See Avionics Pricing Reference.
STCs & Modifications
- Blackhawk XP135A — replaces PT6A-21s with -135As, effectively building a C90GT out of a C90A/B (~$800K+ installed; see the GT page for what it buys).
- Raisbeck — swept-blade props (certified for the C90 series in 2014), dual aft-body strakes, ram-air recovery, wing lockers. The most common mod package on the fleet.
- BLR winglets, Frakes exhaust stacks, Hartzell 4-blade conversions on 3-blade airplanes.
- Commuter/cargo interiors and air-ambulance conversions are widespread — verify the paperwork and the interior weight.
Maintenance & Support
See Maintenance Ecosystem.
- Parts: excellent. Textron still supports the line; the PT6A side is the best-supported turbine ecosystem in aviation.
- Mechanics: common — every turboprop shop knows King Airs; your field A&P does not.
- Annual/phase: $15,000-$35,000 routine; $60,000-$120,000 in a SID/corrosion year on an old airframe.
- Hot section: ~$45,000/side at 1,800 hr. Overhaul: ~$205,000-$275,000/side flat-rate (stored $250,000) at 3,600 hr — ~$500,000 for the pair.
- Direct operating cost: ~$700-$900/hr with reserves. At 150 hr/yr with hangar, insurance, training and subscriptions, plan $180,000-$230,000/yr all-in — the stored estimate is $200,000.
Valuation Factors
See Aircraft Valuation Methodology. Asking-price bands (2026 market):
| Variant | Typical asking |
|---|---|
| 90/A90/B90 | $300,000-$500,000 |
| C90, E90 | $400,000-$800,000 |
| C90A | $600,000-$950,000 |
| C90B / C90SE | $800,000-$1,800,000 (Raisbeck/late/glass at the top) |
Engine status dominates: a $250K-per-side overhaul against a $600K airframe means run-out C90s trade near salvage-plus-green-time. Program enrollment (P&WC ESP, JSSI) or fresh Vector/StandardAero overhauls carry the value. Avionics generation is the second axis; boots, paint, interior third. Asking is not selling — Vref-style retail for clean mid-time C90Bs runs meaningfully below the top asks.
ADs & Common Problems
- AD 2020-26-16 (wing lower forward fittings): applies across 90/100/200/300 series — repetitive inspection for fatigue cracks after a 2015 in-flight wing separation (a modified airtanker, but the AD reaches the fleet). Confirm compliance method and next due time.
- Wing attachment bolts: inspection/replacement per Beech service instructions (also reflected in the TCDS's later revisions). Ask when they were last changed.
- Beech SIDs / Structural Inspection Program: on a 40-60 year old airframe the corrosion-driven items dominate annual cost variance. Center-section and cabin-bilge corrosion, damp insulation blankets behind the sidewalls.
- PT6A-21 pattern items: compressor turbine blade creep/erosion, fuel nozzle fouling on trend, hot-section condition telegraphed by ITT margin. Buy the trend data, not the log entry.
- Landing gear: older electro-mechanical gear (motor/gearbox/torque shafts) on pre-1984 aircraft wants a shop that knows it; hydraulic on later. Insist on a gear swing.
- Pre-buy red flags: mismatched engine times, gaps around HSI events, freight/medevac interiors removed without weight documentation, boots at end of life ($40K-$60K).
Insurance Profile
See GA Insurance Underwriting and Insurance Costs. Hull runs roughly $6,000-$15,000 on typical C90 values (house turbine band $10K-$30K+ covers the fleet); liability $5,000-$10,000 at $1M smooth. Underwriters require initial school (FlightSafety/SimCom) and annual recurrent, and want roughly 1,500 TT / 500 multi / turbine time or a mentor for 25-50 hours. The C90 is the easiest King Air to place a stepping-up owner in — that is much of why it holds value.
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Beechcraft King Air C90
Listed on BarnstormersAlso worth looking at
What buyers usually weigh against the Beechcraft King Air C90 — aircraft flown for the same kind of mission.