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Beechcraft King Air

United States (1964)

Detailing the development and operational history of the Beechcraft King Air Multirole Transport Aircraft.

 Entry last updated on 8/28/2017; Authored by Staff Writer; Content ©www.MilitaryFactory.com



  Beechcraft King Air  
Picture of Beechcraft King Air Multirole Transport Aircraft
Picture of Beechcraft King Air Multirole Transport Aircraft Picture of Beechcraft King Air Multirole Transport AircraftPicture of Beechcraft King Air Multirole Transport AircraftPicture of Beechcraft King Air Multirole Transport AircraftPicture of Beechcraft King Air Multirole Transport AircraftPicture of Beechcraft King Air Multirole Transport Aircraft


The Beechcraft King Air series began operations in 1964 and is still actively marketed today.

The Beechcraft King Air is a utility platform developed from the Beechcraft Queen Air of 1958. It continues to see flying time despite its Cold War-era roots. A prototype saw its first-flight in May of 1963 and the series was introduced on September 9th of 1964. Since then, some 3,100 examples have been produced and many offshoots have appeared for both military and civilian roles. The King Air was born as the company Model 120 in 1961.

The two primary models of the line are the Model 90 and Model 100 with a plethora of subvariants in between. The Model 100 has a lengthened fuselage with additional cabin viewing ports and an increased MTOW. Militarized forms are used United States (as the VC-6A, Pegasus and Ute) and others such as the Israeli Air Force (IAF), the Royal Canadian Air Force and the Japan Maritime Self Defense Force (JMSDF). Beyond this, the type has also been in service at the governmental level and under civilian operators globally. Former operators include Chile, Hong Kong, Ireland and Sweden.
Picture of the Beechcraft King Air Multirole Transport Aircraft
Picture of the Beechcraft King Air Multirole Transport Aircraft


The C90GTi model has a crew of one or two and can carry up to seven passengers. Overall length is 35.5 feet with a wingspan of 50.2 feet and a height of 14.2 feet. Empty weight is 7,000lb against an MTOW of 10,100lb. Power is from 2 x Pratt & Whitney Canada PT6A-135A series turboprop engines outputting 550 horsepower each and driving Hartzell propeller units. Performance includes a maximum speed of 311 miles per hour, a cruising speed of 260 mph, a range out to 1,530 miles and a service ceiling up to 30,000 feet. Rate-of-climb is 2,000 feet-per-minute.

The B100 model switches to 2 x Garrett TPE-331-6-251B or -252 series turboprop engines of 840 horsepower output. Speed is slightly decreased (307mph) as is the service ceiling (24,850 feet).

Variants in the King Air line include the "Super King Air" of 1972, also taken into civilian and military circles with nearly 4,000 units produced.
Cockpit picture from the Beechcraft King Air Multirole Transport Aircraft
Beechcraft King Air Cockpit Picture
Beechcraft King Air C90GTi Specifications
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United States
Year: 1964
Type: Multirole Transport Aircraft
Manufacturer(s): Beechcraft - USA
Production: 3,120
Supported Mission Types
Air-to-Air
Interception
Unmanned
Ground Attack
Close-Air Support
Training
Anti-Submarine
Anti-Ship
Airborne Early Warning
MEDEVAC
Electronic Warfare
Maritime/Navy
Aerial Tanker
Utility/Transport
Passenger Industry
VIP Travel
Business Travel
Search/Rescue
Recon/Scouting
Special Forces
X-Plane/Development
Structural
Crew: 2
Length: 35.50 ft (10.82 m)
Width: 50.26 ft (15.32 m)
Height: 14.24 ft (4.34 m)
Empty Weight: 6,945 lb (3,150 kg)
MTOW: 10,097 lb (4,580 kg)


Installed Power
2 x Pratt & Whitney Canada PT6A-135A turboprop engines developing 550 horsepower.

Standard Day Performance
Maximum Speed: 311 mph (500 kph; 270 kts)
Maximum Range: 1,520 mi (2,446 km; 1,321 nm)
Service Ceiling: 30,000 ft (9,144 m; 5.68 mi)
Rate-of-Climb: 2,000 ft/min (610 m/min)


Armament
None.

Operators List
Argentina; Algeria; Australia; Barbados; Bolivia; Canada; Chile; Colombia; Ecuador; Greece; Guatemala; India; Iraq; Ivory Coast; Mexico; Jamaica; Japan; Morocco; Peru; South Africa; Sri Lanka; Spain; United States; Venezuela; Uruguay

Series Model Variants
• Model 87 - Developmental Test Vehicle; 2 x PT6A-6 turboprop engines.
• Model 65-90 - Initial production model; 2 x PT6A-6 turboprop engines; 112 examples produced.
• Model 65-A90 - Revised cockpit; engine de-icing integrated; increased MTOW.
• Model 65-A90-1 - 2 x PT6A-20 turboprop engines; unpressurized cockpit/cabin.
• Model 65-A90-2 - Electronic Warfare Aircraft (EWA)
• Model 65-A90-3 - Improved EWA version
• Model 65-A90-4 - Reinforced airframe; increased MTOW; 16 examples completed.
• Model B90 - Revised wings; increased MTOW; revised cockpit; 184 examples produced.
• Model C90 - 2 x PT6A-21 turboprop engines; cabin pressurization of Model 100 series; 507 examples produced.
• Model C90-1 - Improved C90 model; 54 examples produced.
• Model C90A - 2 x PT6A-21 turboprop engines; revised undercarriage.
• Model C90B - Updated C90A models; increased MTOW
• Model C90SE - Alternative C90A updated models
• Model C90GT - 2 x PT6A-135A engines of 750 horsepower; 97 examples produced.
• Model C90GTi - Updated C90GT form with digital glass cockpit; 90 examples produced.
• Model C90GTx - Modified C90GT with added winglets; increased MTOW.
• Model D90 - Incomplete prototype initiative
• Model E90 - 2 x PT6A-28 engines of 680 horsepower; 347 examples produced.
• Model F90 - 2 x PT6A-135 engines of 750 horsepower; four-bladed propeller assemblies; T-style tail assembly; 196 produced.
• Model F90-1 - Model F90 with 2 x PT6A-135A engines; 32 examples produced.
• Model G90
• Model H90
• Model 100
• Model A100
• Model B100
• Model A100-1
• YU-21
• U-21A Ute
• EU-21A
• JU-21A
• RU-21A
• RU-21B
• RU-21C
• RU-21D
• RU-21E
• U-21F
• U-21G Ute
• RU-21G
• RU-21H
• U-21H
• U-21H Ute
• JU-21H
• VC-6A
• T-44A Pegasus
• T-44C Pegasus


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