Air Tractor AT-802 vs Beechcraft Super King Air

Air Tractor AT-802 — licensed reference photograph

ASupport aircraft

Air Tractor AT-802

Agricultural / Fire-fighting aircraft

Credit

Daniel VA · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified

Beechcraft Super King Air — licensed reference photograph

BSupport aircraft

Beechcraft Super King Air

Civil utility aircraft

Credit

Gordon Elias · OGL v1.0 · Resized · OGL v1.0 · Source ↗ · Modified

First system

Second system

At a glance

Side by side

Length comparisonOne shared metre scale

Air Tractor AT-802AT-802 · Length

10.95 m

Length source ↗

Beechcraft Super King AirLength

13.36 m

Length source ↗

Lengths retain their source configuration and measurement scope.

Measured figures

Head to head

15 of 32 rows sourced on both sides

10.95mAT-802 · Length

13.36m

Length

All recorded figures & sources

10.95 m

AT-802 · Length

Single source

35 ft 11 in (10.95 m)^[source]

13.36 m

Length

Single source

43 ft 10 in / 13.36 m^[source]

18.06mAT-802 · Wingspan

17.65m

Wingspan

All recorded figures & sources

18.06 m

AT-802 · Wingspan

Single source

59 ft 3 in (18.06 m)^[source]

17.65 m

Wingspan

Single source

57 ft 11 in / 17.65 m^[source]

3.89mAT-802 · Height

4.52m

Height

All recorded figures & sources

3.89 m

AT-802 · Height

Single source

12 ft 9 in (3.89 m)^[source]

4.52 m

Height

Single source

14 ft 10 in / 4.52 m^[source]

7.3t

5.7tMaximum take-off; Maximum takeoff weight

MassScopes differ

All recorded figures & sources

2,951 kg

Empty; AT-802 · Empty weight

Single source

7,257 kg

Maximum take-off; AT-802 · Max takeoff weight

Single source

6,505 lb (2,951 kg)^[source]

16,000 lb (7,257 kg)^[source]

5,670 kg

Maximum take-off; Maximum takeoff weight

Single source

12,500 lb / 5,670 kg^[source]

One or Two (AT-802A – single-seat)

1–2people

Crew

All recorded figures & sources

One or Two (AT-802A – single-seat)^[source]

1–2 people

Crew

Single source

1–2^[source]

356km/hCruise; AT-802 · at 8,000 ft (2,440 m)

574km/hCruise; Cruise speed

SpeedScopes differ

All recorded figures & sources

356 km/h

Cruise; AT-802 · at 8,000 ft (2,440 m)

Single source

221 mph (356 km/h, 192 kn) at 8,000 ft (2,440 m)^[source]

574 km/h

Cruise; Cruise speed

Single source

310 kn / 574 km/h^[source]

1,300kmAT-802 · Range

3,185kmFerry; Ferry range

RangeScopes differ

All recorded figures & sources

1,300 km

AT-802 · Range

Single source

800 mi (1,300 km, 700 nmi)^[source]

3,185 km

Ferry; Ferry range

Single source

1,720 nmi / 3,185 km^[source]

1,010kW

—

Power

All recorded figures & sources

1,010 kW

AT-802 · 1 × Pratt & Whitney PT6A -67AG turboprop , 1,350 shp (

Single source

1 × Pratt & Whitney PT6A -67AG turboprop , 1,350 shp (1,010 kW)^[source]

37.3m²AT-802 · Wing area

—

Wing area

All recorded figures & sources

37.25 m²

AT-802 · Wing area

Single source

401.0 sq ft (37.25 m 2 )^[source]

4,000mAT-802 · Service ceiling

10,668mCeiling

Service ceilingScopes differ

All recorded figures & sources

4,000 m

AT-802 · Service ceiling

Single source

13,000 ft (4,000 m)^[source]

10,668 m

Ceiling

Single source

35,000 ft / 10,668 m^[source]

4.3m/sAT-802 · 850 ft/min (

—

Rate of climb

All recorded figures & sources

4.3 m/s

AT-802 · 850 ft/min (

Single source

850 ft/min (4.3 m/s)^[source]

Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.

Configuration

Details

Air Tractor AT-802 and Beechcraft Super King Air configuration
Specification	Air Tractor AT-802	Beechcraft Super King Air
Type	Agricultural / Fire-fighting aircraft^[source]	Civil utility aircraft^[source]
National origin	United States^[source]	—
Manufacturer	Air Tractor^[source]	Beechcraft^[source]
Status	Active^[source]	Active service^[source]
Manufactured	1990–present^[source]	1972–present^[source]
First flight	1990^[source]	October 27, 1972^[source]
Variant	L3Harris OA-1K Skyraider II^[source]	Beechcraft C-12 Huron^[source]
Capacity	820 US gal (683 imp gal; 3,104 L)^[source]	10^[source]
Aspect ratio	8.8:1^[source]	—
Airfoil	NACA 4415^[source]	—
Stall speed	91 mph (146 km/h, 79 kn) (power off, flaps down)^[source]	—
Primary users	—	United States Air Force United States Army Royal Flying Doctor Service Royal Australian Air Force^[source]
Number built	—	4,442 (at end of 2025)^[source]
Introduction date	—	1972 (military) February 1974 (civil)^[source]
Developed from	—	Beechcraft King Air^[source]
Developed into	—	Beechcraft 1900^[source]
OEW	—	8,830 lb / 4,005 kg^[source]
Useful load	—	3,760 lb / 1,706 kg^[source]
Powerplant	—	PWC PT6A -52^[source]
Source measurement	—	The Model 200 was originally conceived as the Model 101 in 1969, and was a development of the Model 100 King Air.^[source]Beechcraft Super King Air · Development / Super King Air 200; only the objects and conditions stated in this passage Apart from the T-tail, other changes included Pratt & Whitney Canada PT6 A-41 engines rated at 850 shp (630 kW) instead of the 680 shp (510 kW) engines of the Model A100 then in production, and an increased wing span with extra fuel capacity.^[source]Beechcraft Super King Air · Development / Super King Air 200; only the objects and conditions stated in this passage Overall, the 200 was 3 ft 10 in (117 cm) longer than the A100, with a wingspan 4 ft 3 in (130 cm) greater, containing 60 US gallons (230 L) more fuel.^[source]Beechcraft Super King Air · Development / Super King Air 200; only the objects and conditions stated in this passage Maximum Take-Off Weight (MTOW) was increased by 1,000 lb (450 kg).^[source]Beechcraft Super King Air · Development / Super King Air 200; only the objects and conditions stated in this passage After protracted development, including extensive wind tunnel testing of the design (especially of the T-tail which was wind tunnel-tested for 375 hours), the first prototype flew for the first time on October 27, 1972; a second prototype took to the air on December 15 the same year.^[source]Beechcraft Super King Air · Development / Super King Air 200; only the objects and conditions stated in this passage The next model was the Model 200C in 1979, equipped with a large cargo door on the left-hand side of the rear fuselage with an airstair door similar to the Model 200's door built into it. The door opening was 4 ft 4 in (1.33 m) high and 4 ft 4 in (1.33 m) wide, allowing a larger range of items to be loaded into the cabin, and the new model was popularly outfitted as an air ambulance . The 200C fuselage was a new design and not a modification of the Model 200 fuselage. The Model A200C military version was developed concurrently. In 1981, a Model 200C (c/no. BL-24) was modified as the Model 200CT, fitted with the same wingtip fuel tanks as installed on Model 200Ts; there was only one 200CT, but it led to other aircraft after an updated version of the Model 200 entered production.^[source]Beechcraft Super King Air · Development / Super King Air 200; only the objects and conditions stated in this passage Fitted with PT6A-42 engines, rated at 850 shp (630 kW), but with improvements that resulted in greater aircraft performance.^[source]Beechcraft Super King Air · Development / Super King Air 200; only the objects and conditions stated in this passage A total of 14 B200s were produced in 1989 and 1990 in a 13-seat high density configuration with a belly cargo pod; these were marketed by Beechcraft as a commuter airliner under the designation Model 1300. Customers for this version included Mesa Airlines . The propeller installation changed again in 1992, when Beechcraft offered the option of having 4-bladed Hartzell or McCauley propellers, or 3-bladed Hartzell propellers; the 3-bladed McCauley propellers were no longer available. From October 1995 Beechcraft offered an updated B200 with Electronic Flight Instrument System (EFIS) avionics , marketed as the "B200SE Super King Air" (for Special Edition). The following year the "Super" name was dropped from all marketing and advertising. In October 2003, Beechcraft announced another avionics upgrade for the B200, the Rockwell Collins Pro Line 21 suite.^[source]Beechcraft Super King Air · Development / Super King Air 200; only the objects and conditions stated in this passage The B200GT is fitted with a new model of PT6 engine developed specifically for it by Pratt & Whitney Canada ; while still rated at 850 shp (630 kW) the new PT6A-52 develops maximum power to an even higher altitude than the −42 it replaces, thus further improving aircraft performance.^[source]Beechcraft Super King Air · Development / Super King Air 200; only the objects and conditions stated in this passage In 2014 Beechcraft announced the availability of an option (available at manufacture and for existing aircraft) to increase the MTOW of the B200GT from 12,500 pounds (5,700 kg) to 13,420 pounds (6,090 kg), marketed as the King Air 250EP (for E xtra P ayload). The upgrade puts the 250EP into the same weight class as the King Air 350, necessitating various system changes to meet certification requirements and a special rating for pilots. In 2019, the 250 unit cost was US$6.61M (~$7.98 million in 2024).^[source]Beechcraft Super King Air · Development / Super King Air 200; only the objects and conditions stated in this passage On December 2, 2020, Textron updated the King Air 200 series with the 260, with deliveries expected in early 2021. The model has an improved autothrottle , a Multi-Scan weather radar , a range of 1,720 nmi (3,190 km) and a top cruise speed of 310 kn (360 mph; 570 km/h) with up to nine passengers. The type was FAA certified in March 2021, and European Aviation Safety Agency type certified in September 2021.^[source]Beechcraft Super King Air · Development / Super King Air 200 / King Air 260; only the objects and conditions stated in this passage In 2023, its equipped price was $7.78M.^[source]Beechcraft Super King Air · Development / Super King Air 200 / King Air 260; only the objects and conditions stated in this passage The Canadian Forces Air Command took delivery of two second-hand early-production Model 200 Super King Airs leased from Awood Air in 1990. These were given the designation CT-145 under the CF's identification system and were used as multi-engine trainers, replacing Douglas C-47s . One was subsequently returned to the lessor and a third Model 200 placed into service in order that the two aircraft used would have the same cockpit layout. The two aircraft were replaced by eight civilian-operated 90 Model King Airs in 1995. In 2025 the Royal Canadian Air Force announced the acquisition of 7 King Air 260 aircraft. Designated the CT-145E Expeditor II, the aircraft will be used as multi-engine trainers based at 3 Canadian Forces Flying Training School in Southport, Manitoba .^[source]Beechcraft Super King Air · Development / Super King Air 200 / Model 200 military variants; only the objects and conditions stated in this passage The B200's airframe was "cleaned up" and more powerful engines (PT6A-60A, rated at 1,050 shp (780 kW)) were installed in redesigned cowlings (known as "pitot cowlings" due to the reshaped engine air intakes), with MTOW increased to 14,000 lb (6,400 kg).^[source]Beechcraft Super King Air · Development / Super King Air 300/350; only the objects and conditions stated in this passage Because not all nations would then allow an aircraft of this type to be certified at an MTOW greater than 12,500 lb (5,700 kg), the Model 300LW was also developed at the same time, limited to the lower MTOW.^[source]Beechcraft Super King Air · Development / Super King Air 300/350; only the objects and conditions stated in this passage The King Air 350 is based on the King Air 300 with a 3.4 ft (1.0 m) span increase and winglets , a 2.9 ft (0.88 m) fuselage stretch for an over 17 ft (5.2 m) main cabin, long enough for double club seating. By 1988, Beechcraft had begun work on the replacement for the 300, it was introduced in 1990 and initially marketed as the Super King Air 350. It has two extra cabin windows on each side and MTOW was increased again to 15,000 lb (6,800 kg); as the same regulatory situation that led to the development of the 300LW still existed, that model continued to be produced until 1994. Like the 200 and B200 before it, a version with a large cargo door was developed, the Model B300C marketed as the "Super King Air 350C". The first deliveries of this model also took place in 1990. In 1998, the UltraQuiet active noise canceling system, made by Elliott Aviation, was added as standard equipment on all B300s. In October 2003, Beechcraft announced that it would deliver future B300 and B300C King Airs with the Rockwell Collins Pro Line 21 avionics suite.^[source]Beechcraft Super King Air · Development / Super King Air 300/350; only the objects and conditions stated in this passage On June 13, 2005, Beechcraft announced at the Paris Air Show that it was developing the King Air 350ER version of the B300, an equivalent to the earlier Model 200T and B200Ts of the 200 series. Changes include an increase of MTOW to 16,500 lb (7,430 kg), provision for surveillance equipment in a belly pod, the landing gear of the Beechcraft 1900 to handle the increased weight and provide ground clearance for the belly pod, and extra fuel capacity in the engine nacelles to increase range (because of the B300s winglets, it was unfeasible to fit wingtip fuel tanks as found on the 200T and B200T). On November 11, 2007, Hawker Beechcraft announced that the 350ER had been certified by the FAA.^[source]Beechcraft Super King Air · Development / Super King Air 300/350; only the objects and conditions stated in this passage The cabin sound level is reduced by 4 dB to 78-dB due to better insulation. More than 440 350i have been delivered in less than ten years. On a one hour trip, it is 10-15 min slower than a jet while burning 700–900 lb (320–410 kg) less fuel. It cruises at 292 kn (336 mph; 541 km/h) TAS at FL350 while burning 503 lb (228 kg) per h, and can reach 312 kn (359 mph; 578 km/h) TAS at FL240. The $1.8 million Blackhawk PT6A-67A upgrade offers a 68 kn (78 mph; 126 km/h) TAS faster cruise and up to 60% shorter time to climb.^[source]Beechcraft Super King Air · Development / Super King Air 300/350 / King Air 350i; only the objects and conditions stated in this passage Direct operating costs are around $1,300-1,500 per hour, including a 900 lb (410 kg) average fuel flow per h. At 3,600 h, the first pair of engine overhauls cost $500,000-550,000, but second overhauls can cost $800,000-1.2 million. By September 2019, second-hand aircraft were priced between $3 million for early models to more than $4 million for late models. In 2019, the King Air 350i price was US$7.755M, and US$8.8M for the King Air 350iER.^[source]Beechcraft Super King Air · Development / Super King Air 300/350 / King Air 350i; only the objects and conditions stated in this passage The Model 350 ER is an extended-range, special-mission version for surveillance and reconnaissance operations; it was introduced at the Paris Air Show in June 2005. Features of this model include engine nacelle fuel tanks, heavy duty landing gear, and an increased maximum take-off weight of 7,484 kg (16,500 lb). The typical mission profile involves a 100 nautical mile (185 km; 115 mile) flight to on-station; a low-altitude surveillance sortie for 7 hours 20 minutes; and return to base with 45 minutes' fuel reserve.^[source]Beechcraft Super King Air · Development / Super King Air 300/350 / Model 350ER (Extended Range); only the objects and conditions stated in this passage The King Air 360 and 360ER have a cockpit including an avionics upgrade, digital pressurisation control, autothrottle , and a modernized cabin featuring a 10% lower altitude pressure. The 360 has a maximum range of 1,806 nmi (3,345 km,) while the 360ER has a maximum range of 2,539 nmi (4,702 km). Both models were FAA type certified in October 2020 and European Aviation Safety Agency certified in September 2021.^[source]Beechcraft Super King Air · Development / Super King Air 300/350 / King Air 360 and 360ER; only the objects and conditions stated in this passage In 2023, the equipped price was $9.255M for the 360 and $9.76M for the 360ER.^[source]Beechcraft Super King Air · Development / Super King Air 300/350 / King Air 360 and 360ER; only the objects and conditions stated in this passage More than 1,800 King Air 200 series have been delivered during more than 40 years of production. In early 2017 a used 2011 model King Air 250 was worth US$ 3 million and a late 2015 to early 2016 model was worth US$5 million, with an annual utilization estimated at 240 hours and 216 cycles, while a King Air 350i is US$800,000 to US$1 million more.^[source]Beechcraft Super King Air · Operational history; only the objects and conditions stated in this passage By April 2017 sales of the King Air series were in decline with just 12 examples delivered in the first quarter of the year, compared to 26 in the same period of 2016, due to a weak international market for the design. The company expected the annual sales to be about the same as 2016, though, which totaled 106 in that year.^[source]Beechcraft Super King Air · Operational history; only the objects and conditions stated in this passage Two versions, the standard Model 300 with increased MTOW of 14,000 lb (6,300 kg) and the Model 300LW with MTOW limited to 12,500 lb (5,700 kg) to meet the aviation regulatory requirements of various countries; 247 built including 35 Model 300LW and including two Model 300s modified and another 17 built specifically for the FAA for use in navaid calibration. The 300LW has a lower certified Take-Off Gross Weight of 12,500 lb for the European market related to tax.^[source]Beechcraft Super King Air · Variants; only the objects and conditions stated in this passage B200 configured as a regional airliner, with room for two crew and 13 passengers, fitted with two overwing emergency exits instead of the standard model's single overwing exit and an optional 455 lb (206 kg) belly cargo pod; a nose baggage compartment provided by relocating avionics from the nose to elsewhere in the aircraft. A total of 14 were built.^[source]Beechcraft Super King Air · Variants; only the objects and conditions stated in this passage Re-engined with PT6A-67As and five-blade composite propellers instead of the PT6A-60A engines with unit power increasing from 1,050 to 1,200 hp (780 to 890 kW), boosting the maximum cruise speed by 50 kn (58 mph; 93 km/h) to 340 kn (390 mph; 630 km/h) and capable of climbing to 35,000ft in 19min; Blackhawk targets 30% of the 850 King Air 300 globally.^[source]Beechcraft Super King Air · Variants; only the objects and conditions stated in this passage February 21, 1980: A Model 200 operating as Advance Airlines Flight 4210 crashed adjacent to the runway at Sydney Airport, killing 13 people in the worst civil aviation accident in Australia since 1968.^[source]Beechcraft Super King Air · Accidents and incidents; only the objects and conditions stated in this passage September 4, 2000: After departing Perth, Western Australia, the pilot of a Model 200 Super King Air failed to respond to ATC after the aircraft climbed above its assigned altitude. It continued to fly across Australia for five hours before crashing near Burketown in northwestern Queensland, killing all eight on board. Dubbed the " Ghost Flight " by the media, an investigation concluded that the occupants likely became incapacitated due to hypoxia .^[source]Beechcraft Super King Air · Accidents and incidents; only the objects and conditions stated in this passage October 30, 2014: A B200 King Air crashed at Wichita, Kansas . The pilot and three people on the ground were killed; six people were injured.^[source]Beechcraft Super King Air · Accidents and incidents; only the objects and conditions stated in this passage December 22, 2015: A B200 King Air crashed at Indira Gandhi International Airport in Delhi, India. All ten occupants were killed; one person on the ground was injured.^[source]Beechcraft Super King Air · Accidents and incidents; only the objects and conditions stated in this passage September 1, 2019: A B300 King Air crashed into a resort in Calamba, Philippines. All nine occupants aboard were killed; two people on the ground were injured.^[source]Beechcraft Super King Air · Accidents and incidents; only the objects and conditions stated in this passage
Country of origin	—	United States^[source]Country/countries explicitly given in the equipment row Origin column; not the country operating the row. Super King Air United States^[source]Inventory Origin column; table 1, row 35, cell 2; revision 1377921935; retrieved 2026-10-02

FORCETALLY

Loading the evidence…

Preparing your view.

Air Tractor AT-802

Beechcraft Super King Air

Type

Agricultural / Fire-fighting aircraft^[source]

Civil utility aircraft^[source]

National origin

United States^[source]

—

Manufacturer

Air Tractor^[source]

Beechcraft^[source]

Status

Active^[source]

Active service^[source]

Manufactured

1990–present^[source]

1972–present^[source]

First flight

1990^[source]

October 27, 1972^[source]

Variant

L3Harris OA-1K Skyraider II^[source]

Beechcraft C-12 Huron^[source]

Capacity

820 US gal (683 imp gal; 3,104 L)^[source]

10^[source]

Aspect ratio

8.8:1^[source]

—

Airfoil

NACA 4415^[source]

—

Stall speed

91 mph (146 km/h, 79 kn) (power off, flaps down)^[source]

—

Primary users

—

United States Air Force United States Army Royal Flying Doctor Service Royal Australian Air Force^[source]

Number built

—

4,442 (at end of 2025)^[source]

Introduction date

—

1972 (military) February 1974 (civil)^[source]

Developed from

—

Beechcraft King Air^[source]

Developed into

—

Beechcraft 1900^[source]

OEW

—

8,830 lb / 4,005 kg^[source]

Useful load

—

3,760 lb / 1,706 kg^[source]

Powerplant

—

PWC PT6A -52^[source]

Source measurement

—

The Model 200 was originally conceived as the Model 101 in 1969, and was a development of the Model 100 King Air.^[source]Beechcraft Super King Air · Development / Super King Air 200; only the objects and conditions stated in this passage

Apart from the T-tail, other changes included Pratt & Whitney Canada PT6 A-41 engines rated at 850 shp (630 kW) instead of the 680 shp (510 kW) engines of the Model A100 then in production, and an increased wing span with extra fuel capacity.^[source]Beechcraft Super King Air · Development / Super King Air 200; only the objects and conditions stated in this passage

Overall, the 200 was 3 ft 10 in (117 cm) longer than the A100, with a wingspan 4 ft 3 in (130 cm) greater, containing 60 US gallons (230 L) more fuel.^[source]Beechcraft Super King Air · Development / Super King Air 200; only the objects and conditions stated in this passage

Maximum Take-Off Weight (MTOW) was increased by 1,000 lb (450 kg).^[source]Beechcraft Super King Air · Development / Super King Air 200; only the objects and conditions stated in this passage

After protracted development, including extensive wind tunnel testing of the design (especially of the T-tail which was wind tunnel-tested for 375 hours), the first prototype flew for the first time on October 27, 1972; a second prototype took to the air on December 15 the same year.^[source]Beechcraft Super King Air · Development / Super King Air 200; only the objects and conditions stated in this passage

The next model was the Model 200C in 1979, equipped with a large cargo door on the left-hand side of the rear fuselage with an airstair door similar to the Model 200's door built into it. The door opening was 4 ft 4 in (1.33 m) high and 4 ft 4 in (1.33 m) wide, allowing a larger range of items to be loaded into the cabin, and the new model was popularly outfitted as an air ambulance . The 200C fuselage was a new design and not a modification of the Model 200 fuselage. The Model A200C military version was developed concurrently. In 1981, a Model 200C (c/no. BL-24) was modified as the Model 200CT, fitted with the same wingtip fuel tanks as installed on Model 200Ts; there was only one 200CT, but it led to other aircraft after an updated version of the Model 200 entered production.^[source]Beechcraft Super King Air · Development / Super King Air 200; only the objects and conditions stated in this passage

Fitted with PT6A-42 engines, rated at 850 shp (630 kW), but with improvements that resulted in greater aircraft performance.^[source]Beechcraft Super King Air · Development / Super King Air 200; only the objects and conditions stated in this passage

A total of 14 B200s were produced in 1989 and 1990 in a 13-seat high density configuration with a belly cargo pod; these were marketed by Beechcraft as a commuter airliner under the designation Model 1300. Customers for this version included Mesa Airlines . The propeller installation changed again in 1992, when Beechcraft offered the option of having 4-bladed Hartzell or McCauley propellers, or 3-bladed Hartzell propellers; the 3-bladed McCauley propellers were no longer available. From October 1995 Beechcraft offered an updated B200 with Electronic Flight Instrument System (EFIS) avionics , marketed as the "B200SE Super King Air" (for Special Edition). The following year the "Super" name was dropped from all marketing and advertising. In October 2003, Beechcraft announced another avionics upgrade for the B200, the Rockwell Collins Pro Line 21 suite.^[source]Beechcraft Super King Air · Development / Super King Air 200; only the objects and conditions stated in this passage

The B200GT is fitted with a new model of PT6 engine developed specifically for it by Pratt & Whitney Canada ; while still rated at 850 shp (630 kW) the new PT6A-52 develops maximum power to an even higher altitude than the −42 it replaces, thus further improving aircraft performance.^[source]Beechcraft Super King Air · Development / Super King Air 200; only the objects and conditions stated in this passage

In 2014 Beechcraft announced the availability of an option (available at manufacture and for existing aircraft) to increase the MTOW of the B200GT from 12,500 pounds (5,700 kg) to 13,420 pounds (6,090 kg), marketed as the King Air 250EP (for E xtra P ayload). The upgrade puts the 250EP into the same weight class as the King Air 350, necessitating various system changes to meet certification requirements and a special rating for pilots. In 2019, the 250 unit cost was US$6.61M (~$7.98 million in 2024).^[source]Beechcraft Super King Air · Development / Super King Air 200; only the objects and conditions stated in this passage

On December 2, 2020, Textron updated the King Air 200 series with the 260, with deliveries expected in early 2021. The model has an improved autothrottle , a Multi-Scan weather radar , a range of 1,720 nmi (3,190 km) and a top cruise speed of 310 kn (360 mph; 570 km/h) with up to nine passengers. The type was FAA certified in March 2021, and European Aviation Safety Agency type certified in September 2021.^[source]Beechcraft Super King Air · Development / Super King Air 200 / King Air 260; only the objects and conditions stated in this passage

In 2023, its equipped price was $7.78M.^[source]Beechcraft Super King Air · Development / Super King Air 200 / King Air 260; only the objects and conditions stated in this passage

The Canadian Forces Air Command took delivery of two second-hand early-production Model 200 Super King Airs leased from Awood Air in 1990. These were given the designation CT-145 under the CF's identification system and were used as multi-engine trainers, replacing Douglas C-47s . One was subsequently returned to the lessor and a third Model 200 placed into service in order that the two aircraft used would have the same cockpit layout. The two aircraft were replaced by eight civilian-operated 90 Model King Airs in 1995. In 2025 the Royal Canadian Air Force announced the acquisition of 7 King Air 260 aircraft. Designated the CT-145E Expeditor II, the aircraft will be used as multi-engine trainers based at 3 Canadian Forces Flying Training School in Southport, Manitoba .^[source]Beechcraft Super King Air · Development / Super King Air 200 / Model 200 military variants; only the objects and conditions stated in this passage

The B200's airframe was "cleaned up" and more powerful engines (PT6A-60A, rated at 1,050 shp (780 kW)) were installed in redesigned cowlings (known as "pitot cowlings" due to the reshaped engine air intakes), with MTOW increased to 14,000 lb (6,400 kg).^[source]Beechcraft Super King Air · Development / Super King Air 300/350; only the objects and conditions stated in this passage

Because not all nations would then allow an aircraft of this type to be certified at an MTOW greater than 12,500 lb (5,700 kg), the Model 300LW was also developed at the same time, limited to the lower MTOW.^[source]Beechcraft Super King Air · Development / Super King Air 300/350; only the objects and conditions stated in this passage

The King Air 350 is based on the King Air 300 with a 3.4 ft (1.0 m) span increase and winglets , a 2.9 ft (0.88 m) fuselage stretch for an over 17 ft (5.2 m) main cabin, long enough for double club seating. By 1988, Beechcraft had begun work on the replacement for the 300, it was introduced in 1990 and initially marketed as the Super King Air 350. It has two extra cabin windows on each side and MTOW was increased again to 15,000 lb (6,800 kg); as the same regulatory situation that led to the development of the 300LW still existed, that model continued to be produced until 1994. Like the 200 and B200 before it, a version with a large cargo door was developed, the Model B300C marketed as the "Super King Air 350C". The first deliveries of this model also took place in 1990. In 1998, the UltraQuiet active noise canceling system, made by Elliott Aviation, was added as standard equipment on all B300s. In October 2003, Beechcraft announced that it would deliver future B300 and B300C King Airs with the Rockwell Collins Pro Line 21 avionics suite.^[source]Beechcraft Super King Air · Development / Super King Air 300/350; only the objects and conditions stated in this passage

On June 13, 2005, Beechcraft announced at the Paris Air Show that it was developing the King Air 350ER version of the B300, an equivalent to the earlier Model 200T and B200Ts of the 200 series. Changes include an increase of MTOW to 16,500 lb (7,430 kg), provision for surveillance equipment in a belly pod, the landing gear of the Beechcraft 1900 to handle the increased weight and provide ground clearance for the belly pod, and extra fuel capacity in the engine nacelles to increase range (because of the B300s winglets, it was unfeasible to fit wingtip fuel tanks as found on the 200T and B200T). On November 11, 2007, Hawker Beechcraft announced that the 350ER had been certified by the FAA.^[source]Beechcraft Super King Air · Development / Super King Air 300/350; only the objects and conditions stated in this passage

The cabin sound level is reduced by 4 dB to 78-dB due to better insulation. More than 440 350i have been delivered in less than ten years. On a one hour trip, it is 10-15 min slower than a jet while burning 700–900 lb (320–410 kg) less fuel. It cruises at 292 kn (336 mph; 541 km/h) TAS at FL350 while burning 503 lb (228 kg) per h, and can reach 312 kn (359 mph; 578 km/h) TAS at FL240. The $1.8 million Blackhawk PT6A-67A upgrade offers a 68 kn (78 mph; 126 km/h) TAS faster cruise and up to 60% shorter time to climb.^[source]Beechcraft Super King Air · Development / Super King Air 300/350 / King Air 350i; only the objects and conditions stated in this passage

Direct operating costs are around $1,300-1,500 per hour, including a 900 lb (410 kg) average fuel flow per h. At 3,600 h, the first pair of engine overhauls cost $500,000-550,000, but second overhauls can cost $800,000-1.2 million. By September 2019, second-hand aircraft were priced between $3 million for early models to more than $4 million for late models. In 2019, the King Air 350i price was US$7.755M, and US$8.8M for the King Air 350iER.^[source]Beechcraft Super King Air · Development / Super King Air 300/350 / King Air 350i; only the objects and conditions stated in this passage

The Model 350 ER is an extended-range, special-mission version for surveillance and reconnaissance operations; it was introduced at the Paris Air Show in June 2005. Features of this model include engine nacelle fuel tanks, heavy duty landing gear, and an increased maximum take-off weight of 7,484 kg (16,500 lb). The typical mission profile involves a 100 nautical mile (185 km; 115 mile) flight to on-station; a low-altitude surveillance sortie for 7 hours 20 minutes; and return to base with 45 minutes' fuel reserve.^[source]Beechcraft Super King Air · Development / Super King Air 300/350 / Model 350ER (Extended Range); only the objects and conditions stated in this passage

The King Air 360 and 360ER have a cockpit including an avionics upgrade, digital pressurisation control, autothrottle , and a modernized cabin featuring a 10% lower altitude pressure. The 360 has a maximum range of 1,806 nmi (3,345 km,) while the 360ER has a maximum range of 2,539 nmi (4,702 km). Both models were FAA type certified in October 2020 and European Aviation Safety Agency certified in September 2021.^[source]Beechcraft Super King Air · Development / Super King Air 300/350 / King Air 360 and 360ER; only the objects and conditions stated in this passage

In 2023, the equipped price was $9.255M for the 360 and $9.76M for the 360ER.^[source]Beechcraft Super King Air · Development / Super King Air 300/350 / King Air 360 and 360ER; only the objects and conditions stated in this passage

More than 1,800 King Air 200 series have been delivered during more than 40 years of production. In early 2017 a used 2011 model King Air 250 was worth US$ 3 million and a late 2015 to early 2016 model was worth US$5 million, with an annual utilization estimated at 240 hours and 216 cycles, while a King Air 350i is US$800,000 to US$1 million more.^[source]Beechcraft Super King Air · Operational history; only the objects and conditions stated in this passage

By April 2017 sales of the King Air series were in decline with just 12 examples delivered in the first quarter of the year, compared to 26 in the same period of 2016, due to a weak international market for the design. The company expected the annual sales to be about the same as 2016, though, which totaled 106 in that year.^[source]Beechcraft Super King Air · Operational history; only the objects and conditions stated in this passage

Two versions, the standard Model 300 with increased MTOW of 14,000 lb (6,300 kg) and the Model 300LW with MTOW limited to 12,500 lb (5,700 kg) to meet the aviation regulatory requirements of various countries; 247 built including 35 Model 300LW and including two Model 300s modified and another 17 built specifically for the FAA for use in navaid calibration. The 300LW has a lower certified Take-Off Gross Weight of 12,500 lb for the European market related to tax.^[source]Beechcraft Super King Air · Variants; only the objects and conditions stated in this passage

B200 configured as a regional airliner, with room for two crew and 13 passengers, fitted with two overwing emergency exits instead of the standard model's single overwing exit and an optional 455 lb (206 kg) belly cargo pod; a nose baggage compartment provided by relocating avionics from the nose to elsewhere in the aircraft. A total of 14 were built.^[source]Beechcraft Super King Air · Variants; only the objects and conditions stated in this passage

Re-engined with PT6A-67As and five-blade composite propellers instead of the PT6A-60A engines with unit power increasing from 1,050 to 1,200 hp (780 to 890 kW), boosting the maximum cruise speed by 50 kn (58 mph; 93 km/h) to 340 kn (390 mph; 630 km/h) and capable of climbing to 35,000ft in 19min; Blackhawk targets 30% of the 850 King Air 300 globally.^[source]Beechcraft Super King Air · Variants; only the objects and conditions stated in this passage

February 21, 1980: A Model 200 operating as Advance Airlines Flight 4210 crashed adjacent to the runway at Sydney Airport, killing 13 people in the worst civil aviation accident in Australia since 1968.^[source]Beechcraft Super King Air · Accidents and incidents; only the objects and conditions stated in this passage

September 4, 2000: After departing Perth, Western Australia, the pilot of a Model 200 Super King Air failed to respond to ATC after the aircraft climbed above its assigned altitude. It continued to fly across Australia for five hours before crashing near Burketown in northwestern Queensland, killing all eight on board. Dubbed the " Ghost Flight " by the media, an investigation concluded that the occupants likely became incapacitated due to hypoxia .^[source]Beechcraft Super King Air · Accidents and incidents; only the objects and conditions stated in this passage

October 30, 2014: A B200 King Air crashed at Wichita, Kansas . The pilot and three people on the ground were killed; six people were injured.^[source]Beechcraft Super King Air · Accidents and incidents; only the objects and conditions stated in this passage

December 22, 2015: A B200 King Air crashed at Indira Gandhi International Airport in Delhi, India. All ten occupants were killed; one person on the ground was injured.^[source]Beechcraft Super King Air · Accidents and incidents; only the objects and conditions stated in this passage

September 1, 2019: A B300 King Air crashed into a resort in Calamba, Philippines. All nine occupants aboard were killed; two people on the ground were injured.^[source]Beechcraft Super King Air · Accidents and incidents; only the objects and conditions stated in this passage

Country of origin

—

United States^[source]Country/countries explicitly given in the equipment row Origin column; not the country operating the row. Super King Air

United States^[source]Inventory Origin column; table 1, row 35, cell 2; revision 1377921935; retrieved 2026-10-02