Hubbry Logo
Beechcraft 1900Beechcraft 1900Main
Open search
Beechcraft 1900
Community hub
Beechcraft 1900
logo
8 pages, 0 posts
0 subscribers
Be the first to start a discussion here.
Be the first to start a discussion here.
Beechcraft 1900
Beechcraft 1900
from Wikipedia

The Beechcraft 1900 is a U.S made twin-engine turboprop regional airliner manufactured by Beechcraft. It is also used as a freight aircraft and corporate transport, and by several governmental and military organizations. With customers favoring larger regional jets, then-owner Raytheon ended production in October 2002.[3]

Key Information

Developed from the Beechcraft Super King Air, the aircraft was designed to carry passengers in all weather conditions from airports with relatively short runways. It is capable of flying in excess of 600 miles (970 km), although few operators use its full-fuel range. In terms of the number of aircraft built and its continued use by many passenger airlines and other users, it is one of the most popular 19-passenger airliners in history.[4]

Development

[edit]
A Continental Connection 1900D

The 1900 is Beechcraft's third regional airliner after the Beechcraft Model 18 and Beechcraft Model 99 Airliner.

The Beechcraft 1900's design lineage began in 1949 with the Beechcraft Model 50 Twin Bonanza, a 5-passenger, reciprocating engine utility aircraft designed for the U.S. Army. A larger passenger cabin was added to the Twin Bonanza's airframe, and called the Model 65 Queen Air. This aircraft was, in turn, further modified by adding turboprop engines and cabin pressurization, and named the Model 90 King Air. A stretched version of the King Air was later developed and designated the Model 200 Super King Air. Beechcraft developed the 1900 directly from the Super King Air, in order to provide a pressurized commuterliner to compete with the Swearingen Metro and the British Aerospace Jetstream.[5]

The 1900 first flew on September 3, 1982, with Federal Aviation Administration (FAA) certification awarded on November 22, 1983, under Special Federal Aviation Regulation (SFAR) 41C airworthiness standards.[5] Like the 1900, the 1900C was certified under SFAR 41C, but the later 1900D version was certified to FAR Part 23 "Commuter Category" standards.[6]

The 1900 entered service in February 1984,[5] with the first ExecLiner corporate version delivered in 1985. A total of 695 Beechcraft 1900 aircraft were built, making the airliner the best-selling 19-passenger airliner in history.[4][a] In 1991, the price of a 1900D Airliner was $3.95 million.[7] With market trends favoring larger 50- to 90-seat regional jets, Raytheon ended production of the Beechcraft 1900 in October 2002.[citation needed] Many airlines continue to fly the 1900.

Design

[edit]
Beechcraft 1900C
The 1900 has single passenger seats either side of an aisle

Since the 1900 is derived from the King Air, all 1900s share certain characteristics with that aircraft. Cockpit controls and operations are similar to those of the King Air. The aircraft's noticeable deviations from the King Air comes from its longer fuselage and the presence of "stabilons", which are small horizontal stabilizers at the rear of the fuselage for overcoming T-tail blanking when the aircraft is in higher angles of attack. Additional fins for yaw stability were installed on the tail for 1900Ds, which also feature a taller cabin to allow for a "stand-up cabin" with more walking headspace like conventional airliners. While Federal Aviation Regulations require two pilots for passenger airline operations, the 1900 is designed and certificated for single-pilot operation in corporate or cargo settings, as is the King Air.

The 1900 is powered by two Pratt & Whitney Canada PT6A turboprop engines. The 1900 and 1900C use two PT6A-65B engines, each flat-rated at 1,100 shaft horsepower (820 kW). The 1900D uses two PT6A-67D engines, each rated at 1,279 shaft horsepower (954 kW). The propellers are manufactured by Hartzell, with four blades on each propeller. The blades are made from composite materials.

Performance

[edit]

At FL230, the 1900D cruises at 280 kn (520 km/h) true airspeed while burning 772 lb (350 kg) per hour.[7] Range with 19 passengers for a flight plan with instrument flight rules fuel reserves for a 100 nmi (185 km) alternate airport and 45-minute hold is 680 nmi (1,260 km).[7] It can take off from 3,740 ft (1,140 m) runways at a weight of 16,950 lb (7,690 kg), at sea level and ISA conditions.[7] It can operate on grass and rough runways.

The airplane is certified to fly up to an altitude of 25,000 feet (7,600 m) above mean sea level with its pressurized cabin.[8] It is designed to operate in most weather conditions, including icing conditions, and it is usually equipped with weather radar to help pilots avoid severe weather.[8] The aircraft can be fitted with a lavatory, using space otherwise available for passenger seating and cargo storage.[8]

Variants

[edit]

1900

[edit]

The original design is known simply as the Beechcraft 1900. It features two airstair passenger boarding doors: one near the tail of the aircraft much like the smaller King Airs, and a second at the front just behind the cockpit. It has a small cargo door near the tail for access to the baggage compartment, which is behind the passenger compartment. Only three airframes were built, with "UA" serial numbers of UA-1, UA-2, and UA-3. UA-1 and UA-2 are stored at a Beechcraft facility in Wichita, Kansas. UA-3, registered FAB-043, served in Bolivia until it crashed in November 2011.[9]

1900C

[edit]
Danish Air Transport 1900C

It quickly became clear that having two airstair doors on an aircraft holding only 19 passengers was excessive. In creating the 1900C, Beechcraft kept the front airstair, but eliminated the aft airstair door, installing an enlarged cargo door in its place. Other than the redesigned door layout, the early 1900Cs were substantially similar to the original 1900s. These were assigned serial numbers starting with the letters UB. A total of 74 UB version were built, many of which remain in service.[6] Aircraft in the UA and UB series employ a bladder-type fuel tank system in the wings. Later 1900Cs use a wet wing fuel system: entire sections of the wing are sealed off for use as fuel tanks. This design change allowed more fuel to be stored, substantially increasing the 1900C's range. The wet wing 1900Cs were assigned serial numbers beginning with "UC." These aircraft are also referred to as 1900C-1s. The wet wings proved popular, and the UC is the most common version of the low-ceiling 1900, with 174 UC airframes built.[6]

Raytheon manufactured six 1900C aircraft for use by the U.S. military. These were assigned "UD" serial numbers, UD-1 through UD-6.

1900D

[edit]
The 1900D has a larger cabin to allow passengers to walk upright inside

While the 1900C had become a popular regional airliner, Beechcraft undertook a substantial redesign of the aircraft, and in 1991 introduced a new version called the 1900D.

The 1900 and 1900C, like most 19-passenger airliners and small business jets, have fairly small passenger cabins, with ceilings so low that passengers (of typical male heights) cannot walk through the interior without bending forward. The 1900D was designed to remedy this by providing a "stand-up cabin", which would allow most passengers to walk upright. It is one of only two 19-seat airliners with this feature, the other being the British Aerospace Jetstream 31/32.[6]

Because the taller passenger cabin adds both weight and drag to the airplane, other elements of the 1900D were also changed. More powerful engines and modified propellers were installed, winglets were added to reduce drag and increase the wings' efficiency, and the tail was made larger in response to the more powerful engines. The cockpit was updated with an Electronic Flight Instrument System (EFIS). The 1900D was certified under the then-new FAR Part 23 "Commuter Category" standards, which had replaced the earlier SFAR 41C. Since the UD serial numbers were already in use by the military 1900s, the 1900D airplanes have serial numbers beginning with UE. The 1900D is the most popular version of the airliner, with 439 of the 1900D built.[6]

Super Freighter

[edit]

A supplemental type certificate has been awarded to Alpine Air Express to convert 1900D into cargo aircraft. The STC involved adding a second emergency exit to the cockpit and converting the interior to a cargo configuration. The 1900D can carry 900 cubic feet (25 cubic meters) of cargo, 30% more than a 1900C. Powered by PT6-67D, the super freighter has a max takeoff weight of 17,120 pounds (7,770 kilograms) and is certified under the commuter category. Due to its standup cabin, the 1900D has a large internal volume. The large volume lends the aircraft well to the cargo industry where many packages are bulky and low in density. The 1900D is able to carry nearly as much volume as an EMB-120 and is certified for single pilot cargo operations. The single pilot crew and surplus of airframes allows for reduced operator costs.[10]

Military C-12J

[edit]

The U.S. military designation for the Beechcraft 1900C is C-12J. This is a variant of the C-12 Huron, which is the most common designation for military King Airs. The C-12J includes the six Beechcraft 1900s with 'UD' serial number prefixes built for the U.S. military, as well as other 1900Cs in U.S. military service.

Examples of C-12J aircraft in military service include one used for GPS jamming tests at the 586th Flight Test Squadron, Holloman Air Force Base, New Mexico,[11] and three based at the 459th Airlift Squadron, Yokota Air Base, Japan.[4] The U.S. Army operates both C-12J and 1900D aircraft along with other C-12 (King Air) aircraft.[12]

King Air ExecLiner

[edit]

The King Air ExecLiner was a marketing name for a corporate version of the Beechcraft 1900C.

Operators

[edit]
Two 1900Ds of Maverick Airlines

Civilian operators

[edit]

In July 2018, a total of 114 1900Cs and 192 1900Ds were in airline service: 207 in the Americas, 63 in Africa, 25 in Europe and 11 in the Asia Pacific and Middle East. Airline operators with nine or more aircraft were:[13]

Military operators

[edit]
A 1900D of the Swiss Air Force arrives at the 2016 RIAT, England.

Accidents and incidents

[edit]
  • November 23, 1987: a Ryan Air Services 1900 crashed on approach to the airport at Homer, Alaska. Flight 103 was fully loaded (all 19 seats occupied; 1437 pounds of cargo) when it took off from Kodiak. On departure at Kodiak, the aircraft displayed signs of being overloaded when it lifted off the runway, fell back and accelerated for about another 15 knots before it became airborne. The aircraft was approaching Homer when it was cleared for the localizer/DME approach to runway 3. The crew reported a 2-mile (3.2 km) final five minutes later. On short final the wings were seen to rock back and forth; the aircraft then dropped steeply to the ground in a rather flat attitude, struck the airport perimeter fence and slid to a stop on its belly. Both pilots and sixteen of the nineteen passengers were killed. The investigation into the crash (the first crash of a 1900) stated the probable cause as "the failure of the flight crew to properly supervise the loading of the airplane which resulted in the center of gravity being displaced to such an aft location that the airplane control was lost when the flaps were lowered for landing."[21]
  • May 18, 1990: a 1900C, operating for Aerolift Philippines as Flight 075 to Surigao, took off from runway 13 at Manila's international airport. During takeoff the no. 2 engine failed. The airplane began turning to the right as the crew radioed that they were returning to the airport. With the undercarriage down and the flaps still in takeoff position the airplane impacted a house in the suburban Paranaque neighborhood. All 21 on board the aircraft and a family of four inside the house were killed making the crash the deadliest accident involving the Beechcraft 1900.[22]
  • August 21, 1990: a Republic of China Air Force 1900C crashed in Yunlin County in central Taiwan, killing 18 officers on board.[23]
  • December 28, 1991: a Business Express Airlines 1900C crashed during a training flight when the instructor refused to take back the controls after the students became disoriented due to heavily stressing conditions imposed by the instructor, against the company's flight manual. This conclusion was controversial, as an investigation by the Airline Pilots Association showed that there were many indications of catastrophic airframe failure, not due to pilot error.[24][25][26]
  • January 3, 1992: CommutAir Flight 4821 crashed in Gabriels, New York while on approach to Adirondack Regional Airport, killing the first officer and one passenger.[27]
  • December 7, 1995: an Air St. Martin 1900D drifted off course and crashed into a mountain in Haiti, killing all 20 people on board.
  • November 19, 1996: a United Express 1900C collided on a runway with a Beechcraft King Air at Quincy Regional Airport in Illinois, killing all 14 people on board both aircraft.[28]
  • July 30, 1998: Proteus Airlines Flight 706, a 1900D, collided in midair with a Cessna 177RG over Quiberon Bay in France. None of the 14 passengers and crew survived.[29]
  • January 4, 1999: Régionnair Flight 1707, a 1900C, crashed on approach to Saint-Augustin Airport in Quebec, Canada. All of the 12 passengers and crew survived.[30]
  • August 12, 1999: Régionnair Flight 347, a 1900D, crashed on approach to Sept-Îles Airport in Quebec, Canada. Out of the four occupants on board, the captain was killed, while the first officer and the two passengers survived with injuries.[31]
  • March 17, 2001: A Sociedade de Aviação Ligeira 1900C crashed in Quilemba, Angola, killing 16 of the 17 people on board.[32]
  • December 9, 2002: A Beechcraft 1900D crashed during into the mountains near Mena, Arkansas during a delivery flight. All three people on board were killed, including the president of Hageland Aviation Services, the aircraft's intended customer.[33]
  • January 8, 2003: Air Midwest Flight 5481, a 1900D, crashed into a hangar just after takeoff from Charlotte/Douglas International Airport in North Carolina, killing all 21 people on board.
  • August 26, 2003: Colgan Air Flight 9446, a 1900D operated for US Airways Express, hit the water shortly after taking off from Hyannis, Massachusetts. Both pilots died.[34]
  • January 28, 2004, a Tasili Airlines 1900D crashed on approach to Noumérat – Moufdi Zakaria Airport, killing the first officer.[35]
  • March 16, 2004: A 1900C operating for the United States Air Force crashed [de] on approach to the Tonopah Test Range Airport in Nevada, killing all five people on board.[36]
  • March 15, 2008: A Wings Aviation 1900D crashed in Obanliku, Nigeria, killing all three people on board.[37]
  • May 2, 2008: a South Sudan Air Connection 1900 leased from CemAir crashed, killing 22 people including South Sudan's Minister of Defense Dominic Dim Deng.[38][39]
  • November 9, 2009: a 1900D of Bluebird Aviation crashed during a single-engine landing at Wilson Airport in Nairobi, Kenya, killing the captain and seriously injuring the first officer.[40]
  • November 5, 2010: JS Air Flight 201, a 1900C flying for JS Air (Private) Limited, experienced engine failure and crashed shortly after takeoff from Jinnah International Airport, Karachi, killing all 21 on board including both crew members.[41]
  • September 25, 2011: a Buddha Air 1900D crashed in Nepal during a return scenic flight from the Himalayas killing 19 on board including 3 crew.[42]
  • March 8, 2013: Alaska Central Express Flight 51, a 1900C crashed in mountains during approach of Dillingham Airport, killing 2 on board.
  • April 7, 2013: a 1900C disappeared with one occupant on board, the missionary Jerry Krause.[43]
  • February 11, 2015: A Panamericano 1900C experienced an engine failure after takeoff from Miami Executive Airport and crashed while attempting to make an emergency landing, killing all four people on board.[44]
  • February 9, 2016: a Myanmar Air Force 1900D crashed shortly after taking off from Naypyidaw Airport killing 5 officers on board.[45]
  • June 10, 2021: a Myanmar Air Force 1900D crashed on approach to Anisakan Airport, killing 12 of the 16 people on board.[46]
  • January 29, 2025: A Light Air Services Beechcraft 1900D, that was carrying oil workers, crashed near Unity Oil Field, South Sudan. 20 out of the 21 people onboard were killed.[47]

Specifications (Beechcraft 1900D)

[edit]

Data from Raytheon: Beechcraft 1900D Passenger Specifications and Performance[48]

General characteristics

  • Crew: 1 (2 for airline operations)
  • Capacity: 19 passengers and 6,356 lb (2,882 kg) useful load
  • Length: 57 ft 8 in (17.62 m)
  • Wingspan: 57 ft 9 in (17.64 m)
  • Height: 15 ft 5 in (4.72 m)
  • Empty weight: 10,874 lb (4,932 kg)
  • Gross weight: 17,227 lb (7,814 kg)
  • Max takeoff weight: 17,120 lb (7,764 kg)
  • Fuel capacity: 4,458 lb (2,022 kg)
  • Fuel type: Jet A recommended, others usable
  • Powerplant: 2 × Pratt & Whitney Canada PT6A-67D turboprops, 1,279 shp (955 kW) each

Performance

  • Cruise speed: 280 kn (322 mph, 518 km/h) at 20,000 ft (6,100 m)
  • Range: 382 nmi (439 mi, 707 km) with 19 passenger payload
  • Ferry range: 1,245 nmi (1,432 mi, 2,306 km)
  • Service ceiling: 25,000 ft (7,620 m)
  • Rate of climb: 2,615 ft/min (13.28 m/s)

Avionics

See also

[edit]

Notes

[edit]

References

[edit]

Sources

[edit]
  • Francillon, René J (January 2001). "1900 for 2000: The 'Son of Beech' - Raytheon 1900 Airliner". Air International. pp. 56–58. ISSN 0306-5634.
  • Hoyle, Craig (December 8–14, 2015). "World Air Forces Directory". Flight International. Vol. 188, no. 5517. pp. 26–53. ISSN 0015-3710.
  • Hoyle, Craig (December 4–10, 2018). "World Air Forces Directory". Flight International. Vol. 194, no. 5665. pp. 32–60. ISSN 0015-3710..
  • Hoyle, Craig (2020). "World Air Forces 2021". Flight International. Retrieved December 2, 2020.
  • Jackson, Paul (2003). Jane's All the World's Aircraft 2003–2004. Coulsdon, UK: Jane's Information Group Limited. ISBN 978-0-7106-2537-3.
  • Phillips, Edward H. Beechcraft – Pursuit of Perfection, A History of Beechcraft Airplanes. Flying Books, Eagan, Minnesota 1992.ISBN 0-911139-11-7
[edit]
Revisions and contributorsEdit on WikipediaRead on Wikipedia
from Grokipedia
The Beechcraft 1900 is a pressurized, twin-engine developed by , designed to accommodate up to 19 passengers and one or two pilots in commuter, corporate, or freight configurations. Introduced in the as a versatile short-haul , it features a high-wing design with retractable tricycle , enabling operations from short, unprepared runways while providing reliable performance in diverse environments, from regional routes to remote cargo missions. Development of the Beechcraft 1900 commenced in 1979 as an evolution of Beechcraft's King Air turboprop family, aiming to fill the gap for a dedicated 19-seat airliner amid growing demand for efficient regional transport. The prototype achieved its first flight on September 3, 1982, followed by FAA certification on November 22, 1983, with initial deliveries entering service in February 1984. Production continued until 2002, yielding a total of 695 aircraft across variants, making it one of the most successful 19-passenger airliners in history and a staple for operators worldwide. Key variants include the original 1900, the extended-range 1900C (with 74 units built), the wet-wing 1900C-1 (174 units), and the refined 1900D, which incorporated stronger wings, improved engines, and enhanced avionics for better short-field performance and entered production in 1991. A corporate version, the 1900 ExecLiner, was also offered starting in 1985, while military adaptations like the U.S. Army's C-12J Huron provided utility transport capabilities. The 1900D, the most produced variant with 439 units, is powered by two PT6A-67D engines, each rated at 1,279 shaft horsepower and driving four-bladed Hartzell propellers. It offers a of 17,120 pounds (7,765 kg), a useful load of approximately 6,000 pounds (2,722 kg), and performance including a high-speed cruise of 280 knots (518 km/h) at 20,000 feet, a range of 382 nautical miles (707 km) with full passenger payload, and a service ceiling of 25,000 feet. These attributes made the 1900 ideal for regional airlines, such as Perimeter Aviation and , as well as cargo operators like , with many aircraft remaining in service today for specialized roles including medevac and .

Development

Origins and initial design

In the late 1970s, Beech Aircraft Corporation recognized growing demand among commuter airlines for a larger regional aircraft capable of carrying more passengers than the 10- to 12-seat Super King Air models, prompting the initiation of the Beechcraft 1900 project as a stretched derivative to fill this gap in the short-haul market. Under the leadership of President Frank E. Hedrick, who had guided the company since 1968, Beech aimed to reenter the regional airliner segment by leveraging the proven King Air 200 platform, complementing smaller offerings like the Beechcraft 99 and Model 1300 while addressing airline needs for efficient operations on unpaved runways. Development formally commenced in 1979, building on the Twin Bonanza lineage that traced back to 1949 but focusing on pressurized commuter capabilities for North American routes. The initial design emphasized a 19-passenger capacity within a pressurized cabin to enhance passenger comfort on short-haul flights, featuring a significantly lengthened fuselage—extending to 57 feet 10 inches—to accommodate the increased seating while retaining the King Air's robust structure. Power was provided by two Pratt & Whitney Canada PT6A-65B turboprop engines, each rated at 1,100 shaft horsepower, selected for their reliability and suitability for regional operations, with modifications including a redesigned tail incorporating tailets and stabilons on the lower fuselage for improved stability. Early engineering decisions prioritized simplicity and versatility, avoiding the need for a flight attendant under federal regulations by limiting capacity to 19 seats, which allowed for cost-effective certification as a commuter aircraft. Market analysis at the time targeted North American commuter airlines seeking affordable alternatives to larger jets, positioning the 1900 to compete directly with contemporaries like the Swearingen Metro and in the 15- to 20-seat segment. Conceptual work, including initial sketches and aerodynamic evaluations, began around 1980 to refine the stretched configuration, drawing on Beech's extensive experience with designs to ensure short-field performance and for regional networks.

Testing, certification, and production

The prototype Beechcraft 1900, registered N1900A, performed its on September 3, 1982, marking the beginning of the aircraft's program. This initial testing phase evaluated the airframe's handling qualities, integration, and environmental performance, including behavior and operations in icing conditions, to ensure compliance with regulatory standards. The (FAA) awarded type certification for the Beechcraft 1900 on November 22, 1983, under Special Federal Aviation Regulation (SFAR) 41C, which governed commuter-category airplanes at the time; subsequent variants like the 1900D were certified under the updated (FAR) Part 23 commuter standards. Production of the began in 1984 at Aircraft Corporation's primary manufacturing facility in , where the assembly line supported the rollout of initial units for commercial service. To accommodate growing demand in the late , expanded operations at the Wichita plant, enabling higher output rates that peaked at several units per month during the program's peak years. By the end of production in 2002, a total of 695 had been built across the 1900 series.

Design

Airframe and structure

The Beechcraft 1900's fuselage is constructed as a structure primarily from , providing a yet robust for passengers and systems. This design spans a length of 57 feet 6 inches overall, with the pressurized cabin section enabling operations in high-altitude environments by maintaining a comfortable interior atmosphere. The pressurization system achieves a maximum differential of 6.5 psi, which sustains a cabin altitude of about 8,000 feet during cruise at 25,000 feet. The wings adopt a straight, low-mounted configuration with a span of 54 feet 6 inches on early models like the 1900C, transitioning to 57 feet 9 inches on the 1900D variant due to added winglets for enhanced efficiency. These wings utilize modified NACA 23018 sections at the root, tapering to NACA 23012 at the tips, and incorporate single-slotted flaps for improved low-speed handling. The all-metal wing structure features a continuous main spar and is fully cantilevered, contributing to the aircraft's overall aerodynamic stability. The consists of a conventional assembly, where the horizontal stabilizers mount atop the vertical fin to minimize interference from propeller slipstream while providing effective pitch and yaw control. These stabilizers include dihedral for lateral stability and are reinforced to accommodate the asymmetric loads during twin-engine operations, ensuring reliable performance in various flight regimes. Overall, the incorporates a structural philosophy, with redundant load paths in critical areas such as the frames and spars to enhance and damage tolerance. This design, certified under FAA regulations, supports operations across a range from -54°C to +50°C, reflecting its adaptability to diverse environmental conditions. The base model's basic empty weight is approximately 9,540 pounds, while the reaches 16,600 pounds, balancing capacity with structural integrity.

Powerplant and systems

The Beechcraft 1900 is equipped with twin PT6A turboprop engines mounted on the wings, providing reliable propulsion for regional operations. The initial 1900 and 1900C variants utilize PT6A-65B engines, each flat-rated at 1,100 shaft horsepower (shp) for takeoff, while the 1900D incorporates upgraded PT6A-67D engines rated at 1,279 shp to enhance performance and efficiency. Each engine drives a Hartzell four-bladed, constant-speed, full-feathering designed for and improved climb characteristics, with diameters of 109.5 inches on the 1900C and 110 inches on the 1900D. The fuel system features integral tanks within the wings, offering a usable capacity of approximately 4,458 pounds (665 gallons) of Jet A fuel on later models like the 1900D, with earlier variants having reduced capacity prior to wet-wing modifications. It includes low- and high-pressure boost pumps in each tank, cross-feed valves to balance fuel distribution between engines during unbalanced conditions, and provisions for single-point pressure refueling through a dedicated port on the upper wing surface. Hydraulic power is supplied by a primary electrically driven pump operating at 1,500 psi for actuation of the and flaps, supplemented by an accumulator system for gravity-assisted gear extension in case of primary failure. The electrical system operates on 28 V DC, primarily generated by two 300-ampere starter-generators—one per —with power distributed across essential, non-essential, and battery buses; a 36-ampere-hour nickel-cadmium battery provides backup for essential loads and engine starting. Environmental control systems rely on engine bleed air from the compressor stages for cabin pressurization (maintaining a 6.5 psi differential), heating via heat exchangers, and anti-icing of the propellers, , and air data sensors through pneumatic ducts and electrical elements. Engine maintenance follows guidelines, with time between overhaul (TBO) intervals of 3,600 hours for PT6A-65B models and up to 9,000 hours for PT6A-67D with approved extensions, alongside routine 200-hour inspections to support the aircraft's design for high-utilization, quick-turnaround commuter service.

Avionics and interior

The Beechcraft 1900's cockpit is equipped with the Collins Pro Line II suite as standard, featuring (EFIS) displays such as the EFD-84 for primary flight information, alongside analog backups in earlier configurations. Dual VHF-22A transceivers provide communication capabilities, complemented by dual VIR-32 navigation receivers, ADF-462 automatic direction finders, and DME-42 for precise positioning. Later upgrades often incorporate GPS systems like the Bendix King KLN-90B and TCAS II via the Collins TTR-4000 for enhanced and collision avoidance. The avionics integration supports robust navigation and safety features, including the Collins APS-65 for coupled approaches and the Honeywell MKVI enhanced (EGPWS). , typically from Collins or , is included to detect and , contributing to the aircraft's certification for single-pilot (IFR) operations under FAA A24CE. This setup, powered by the aircraft's electrical systems, enables efficient regional flights while maintaining redundancy for reliability. The passenger cabin accommodates up to 19 occupants in a high-density commuter layout, featuring single seats arranged in a 1-1 configuration across eight rows separated by a narrow aisle, with a rear lavatory and forward baggage compartment. Executive variants reduce capacity to 9-14 passengers, incorporating club seating, fold-out tables, and additional amenities for corporate use, while retaining the same lavatory and baggage provisions. The pressurized and insulated cabin measures approximately 25 feet 2 inches in length, 4 feet 6 inches wide, and 5 feet 11 inches high, promoting comfort on short-haul routes. Cabin noise levels are managed through insulation and optional active structural acoustic control systems, which can achieve reductions of up to 14 dB at propeller blade passage frequencies, resulting in interior sound levels suitable for regional operations. Some variants include quick-change interiors, where high-density commuter seats slide onto existing rails without airframe modifications, facilitating rapid reconfiguration for freight transport by simply removing seats and securing cargo. This adaptability supports mixed passenger-cargo missions while complying with FAA certification standards.

Performance characteristics

The Beechcraft 1900D achieves a high-speed cruise of 276 knots (TAS) at 25,000 feet and a long-range cruise of 224 knots TAS at 25,000 feet, facilitating efficient regional operations with a range of up to 1,040 nautical miles in typical configurations or approximately 382 nautical miles with full 19-passenger , while its ferry range extends to 1,553 nautical miles without . This performance envelope is supported by a service ceiling of 25,000 feet, allowing operations above most systems in typical short-haul scenarios. Initial rate of climb stands at 2,625 feet per minute (fpm) at with both , dropping to 670 fpm on one , which underscores the aircraft's robust climb capability for departure from shorter runways. Takeoff includes a ground run of approximately 2,250 feet at 16,000 pounds under standard conditions, with balanced field length extending to around 3,900 feet over a 50-foot ; at , these figures increase to support operations from runways as short as 5,500 feet for balanced field requirements. ground roll measures about 2,100 feet at 15,300 pounds, with distance over a 50-foot at 4,300 feet, enabling access to remote airfields. Stall speed is 85 knots indicated airspeed (IAS) with full flaps extended at typical landing weights, rising to 99 knots clean, and the aircraft meets Federal Aviation Regulations (FAR) Part 23 handling qualities, including reliable spin recovery characteristics. Fuel efficiency approximates 30-40 nautical miles per 100 pounds of fuel in cruise, derived from typical burn rates of 600-800 pounds per hour at 250-260 knots TAS, making the 1900D particularly suited for routes of 200-500 nautical miles where its powerplants from the PT6A series contribute to balanced climb and endurance performance.

Variants

Early models (1900 and 1900C)

The Beechcraft 1900 series began with the initial 1900 variant, introduced in 1984 as a pressurized commuter aircraft configured for 19 passengers. Powered by two PT6A-65B engines each flat-rated at 1,100 shaft horsepower, the model featured a basic derived from the King Air 200 but with enhancements for regional operations. A total of 3 units were produced, serving primarily as a transitional design to test the stretched configuration for larger capacity. The 1900C, certified in 1985, marked a significant evolution as a production version of the series, accommodating up to 19 passengers in a commuter layout. It was equipped with PT6A-65B engines, each flat-rated at 1,100 shaft horsepower for improved performance at higher altitudes. This variant also increased the to 16,600 pounds (7,531 kg), enabling greater and range capabilities while maintaining the high-wing, twin-engine for short-haul routes. The 1900C included a standard model (74 built) and the extended-range 1900C-1 with wet wings (174 built), totaling 248 units and positioning it as an interim production model prior to the more refined 1900D, with emphasis on achieving Part 23 commuter category certification for scheduled airline service. These early models represented key advancements over the King Air 200 baseline, including the extended cabin length for better passenger accommodation and higher gross weights to support commuter demands, though they retained similar and systems for familiarity in operations. Production of the 1900 and 1900C focused on rapid deployment to meet growing needs in the . By the , most of these had been retired or converted to freighter configurations due to compliance challenges with evolving noise regulations and demands for greater in later variants.

1900D and primary production variant

The 1900D, certified by the FAA on March 19, 1991, marked the primary production variant of the 1900 series, entering service later that year with deliveries commencing in November. Developed to address shortcomings in earlier models like the 1900C, such as limited cabin height, it introduced a taller providing stand-up headroom throughout the passenger compartment. This redesign enhanced passenger comfort and operational versatility while maintaining the core twin-turboprop architecture derived from the Super King Air lineage. Key enhancements included an updated suite featuring a full (EFIS) cockpit for improved situational awareness and pilot workload reduction, along with more powerful PT6A-67D engines rated at 1,279 shp each. The was increased to 17,120 pounds (7,766 kg), enabling greater capacity, and optional winglets were offered to reduce drag and improve , particularly in hot-and-high conditions. These modifications extended the maximum range to approximately 1,498 nautical miles (2,773 km) with reserves (no ), supporting longer regional routes. A total of 439 1900D aircraft were produced between 1991 and 2002, representing over 60% of the entire 1900 fleet and making it the most numerous variant. The model also incorporated refinements like enhanced interior to minimize noise from the engines, contributing to a quieter cabin environment compared to predecessors. Standard configurations seated 19 passengers in a commuter layout, but quick-change options allowed conversion for medevac services with stretchers and medical equipment or all-cargo operations with up to 4,100 lb payload capacity. Production ended in October 2002 as regional operators shifted toward larger , though final deliveries extended into 2009, including to Canadian carriers like Exploits Valley Air Services. This variant's reliability and adaptability solidified its role in short-haul regional worldwide.

Special conversions and military adaptations

The Super Freighter is a dedicated conversion of the 1900D, featuring reinforced floors, a large aft door, and removal of interiors to maximize freight capacity. This modification provides 900 cubic feet of volume and a useful of 7,439 pounds, offering a 40% capacity increase and 23% range extension to 1,356 nautical miles compared to earlier models. Developed by , the conversion received FAA SA00905DE in 2018, with several 1900D airframes modified since then; the program has involved over $5 million in investment as of 2025. The C-12J serves as the primary U.S. military adaptation of the 1900C platform, designated for the and with enhancements for secure communications and utility transport. It incorporates two PT6A-65B engines, each rated at 1,100 shaft horsepower, along with a pressurized cabin capable of carrying up to 19 passengers or 3,500 pounds of . A small production run of four units was completed for the U.S. in the early , with additional examples adapted for use, emphasizing reliability in short-field operations and adverse weather. The 1900 ExecLiner represents an executive transport variant of the 1900C, configured for corporate use with premium leather seating arrangements accommodating 10 to 18 passengers in a spacious, stand-up cabin. Key features include a wet-wing for extended range and customized interiors focused on comfort during longer flights. Limited production occurred starting in 1985, targeting business aviation markets with only a handful of conversions completed. Additional special mission adaptations of the Beechcraft 1900 series incorporate pods and integrations for roles, often via FAA Supplemental Type Certificates issued post-2000 to support non-standard operations without altering the core 1900D . These STCs facilitate modifications such as upgrades and structural reinforcements, enabling diverse applications while maintaining certification compliance.

Operators and operational history

Civilian operators and uses

The Beechcraft 1900 serves primarily in short-haul regional flights covering distances of 100 to 400 nautical miles, remote area transport, and as a feeder service to larger hubs, particularly in challenging environments like rugged terrain or short runways. Major current civilian operators include , which maintains a fleet of 26 Beechcraft 1900 aircraft configured for all-cargo operations, serving over 200 destinations across the with a focus on time-sensitive parcel delivery. Pacific Coastal Airlines in operates nine Beechcraft 1900D models for scheduled passenger and cargo services along the British Columbia coast, leveraging the type's short takeoff and landing () performance for regional connectivity. In , Bering Air utilizes four Beechcraft 1900D aircraft for bush routes, transporting passengers and freight to remote communities with unpaved airstrips. Historically, Era Alaska (later rebranded as ) relied on more than 20 1900s for essential bush operations in until the airline ceased operations in August 2025 amid financial challenges. Similarly, Air Midwest operated a fleet of approximately 20 1900D aircraft as a regional feeder for Express before filing for bankruptcy and shutting down in 2008 due to rising fuel costs and market pressures. As of 2025, around 444 1900 aircraft remain active worldwide in civilian roles, supporting a mix of passenger, cargo, and charter missions. The aircraft's economic viability stems from its relatively low variable operating costs—approximately $2,300 per hour—compared to larger regional jets, enabling efficient service on low-density routes with limited passenger volumes. Its capabilities, with takeoff distances under 2,000 feet on unpaved surfaces, further enhance its utility for remote operations where larger aircraft cannot operate. Recent trends among civilian operators include mandatory upgrades for Automatic Dependent Surveillance-Broadcast (ADS-B) compliance to meet FAA and international airspace requirements, often involving or Collins avionics retrofits. With production ending in 2002, the average fleet age exceeds 30 years, prompting some retirements and transitions to newer turboprops, though many continue in service after maintenance overhauls.

Military operators and missions

The Beechcraft 1900 serves in military roles primarily through its C-12J variant, a militarized version of the 1900C featuring a large aft cargo door for enhanced utility. This adaptation supports diverse operational needs, including secure communications and extended-range configurations for , , and (ISR) tasks. In the United States , five C-12J aircraft are operated for operation support airlift missions, encompassing passenger transport for up to 19 personnel, light hauling of 3,500 pounds, VIP conveyance, embassy support, , and range clearance activities. The maintains three C-12J airframes, assigned to units such as the , for personnel transport across Department of Defense sites and flexible cargo operations enabled by removable bulkheads. These platforms have performed , , and light cargo duties in operational theaters, with additional specialized testing roles like GPS jamming evaluations and troop movements. As of 2025, the C-12J continues active service in U.S. military units, including Reserve operations for global transport missions, though broader C-12 fleet replacements are underway with more advanced turboprops such as the 350.

Incidents and accidents

As of November 2025, the Beechcraft 1900 series has recorded 45 hull-loss accidents, resulting in more than fatalities across its operational . Common causes include (CFIT), often linked to operations in challenging terrain or low visibility, and airframe icing, which has contributed to loss-of-control events during critical phases of flight. These incidents highlight the aircraft's frequent use in regional and short-haul environments, where environmental factors and operational demands can exacerbate risks. On January 29, 2025, a Beechcraft 1900D operated by Eagle Air on behalf of Light Air Services crashed near Bentiu in Unity State, South Sudan, while transporting oil workers. The aircraft struck terrain shortly after takeoff, killing 20 of the 21 people on board. The cause remains under investigation by South Sudanese authorities, but initial reports suggest possible pilot error or mechanical issues in the remote operational environment. This accident marked the deadliest Beechcraft 1900 incident since 2003 and underscored ongoing challenges in bush operations. One notable accident occurred on January 8, 2003, when , a 1900D, stalled shortly after takeoff from in , crashing into a and killing all 21 people on board. The (NTSB) determined the cause was an uncommanded nose-up movement of the due to improper rigging of the elevator control cables during recent maintenance, compounded by the aircraft exceeding its maximum gross weight. Another significant event was the crash of United Express Flight 5925 on January 7, 1994, at Port Columbus International Airport in , where a Beechcraft 1900B encountered severe airframe icing during approach, leading to an aerodynamic and crash that killed 12 of the 19 occupants. The NTSB investigation identified inadequate airframe de-icing equipment performance in known icing conditions as the primary cause, prompting enhanced regulatory focus on winter operations for commuter aircraft. The overall safety record of the Beechcraft 1900 reflects an accident rate comparable to other twin-turboprop regionals, with improvements attributed to post-1990s regulatory changes mandating standardized ground de-icing and anti-icing programs for operations in icing conditions. These measures, implemented by the (FAA) in 1993, required operators to ensure aircraft are free of frost, ice, and snow before takeoff and included pilot training on icing recognition. NTSB investigations have also addressed recurring issues, such as propeller blade failures on Hartzell propellers installed on Beech 1900 aircraft, with reports from 1990 to 1997 documenting six incidents of blade separation; this led to FAA Airworthiness Directive (AD) 94-26-02 requiring inspections and modifications to prevent in-flight failures. Additionally, findings from various accidents emphasized the need for enhanced pilot training on short-field operations, where the aircraft's performance limits have been tested in real-world scenarios. To mitigate structural risks, the FAA issued multiple airworthiness directives, including an emergency AD in 2006 (AD 2006-18-51) mandating one-time visual inspections of rear spar lower caps for cracks on affected models, following discoveries of in high-time . Similar directives for hubs and blades, such as AD 95-04-03 for spar inspections, have been credited with contributing to a decline in incident rates since 2000 by addressing aging fleet vulnerabilities.

Specifications

General characteristics (1900D)

The Beechcraft 1900D features a conventional low-wing design optimized for regional commuter operations, with key physical and capacity specifications as follows.
CharacteristicValue
2 pilots
Capacity19 passengers
Length57 ft 8 in (17.58 m)
57 ft 9 in (17.60 m) with winglets
15 ft 5 in (4.70 m)
Wing area303 sq ft (28.15 m²)
Empty weight10,200 lb (4,627 kg) approximate basic
(MTOW)17,120 lb (7,766 kg)
Fuel capacity4,458 lb (2,022 kg) usable
Engines2 × PT6A-67D turboprops, 1,279 shp (954 kW) each
Propellers4-bladed constant-speed, full-feathering, reversible
Cabin volume (pressurized)760 cu ft (21.5 m³)
These dimensions and capacities reflect the standard configuration for the 1900D variant, which introduced improvements over earlier models such as enhanced winglets for better aerodynamic efficiency.

Performance (1900D)

The Beechcraft 1900D demonstrates strong performance characteristics for a 19-passenger regional turboprop, driven by its twin Pratt & Whitney Canada PT6A-67D engines, each rated at 1,279 shaft horsepower. These engines provide reliable power for short- to medium-haul operations. The design emphasizes efficiency and versatility, allowing the aircraft to serve rugged airstrips while maintaining competitive speeds and ranges compared to contemporary regional airliners. In terms of speed, the 1900D achieves a maximum speed of 280 knots (KTAS), with high-speed cruise at 276 KTAS and normal cruise at 260 KTAS, typically at altitudes around 25,000 feet. Economy cruise reduces to 230 KTAS for extended range missions, optimizing fuel burn at lower power settings. The service ceiling reaches 25,000 feet, and the initial is 2,625 feet per minute (fpm), dropping to 454 fpm with one engine inoperative, which supports safe departure from short fields even under adverse conditions. Range performance extends to a maximum of 1,356 nautical miles (nm) with reserves, though normal operational range is approximately 1,279 nm at typical passenger loads, enabling nonstop service on routes like those in North American regional networks. Takeoff ground roll is 1,740 feet at under standard sea-level conditions, with total distance over a 50-foot obstacle at 3,470 feet; landing rollout requires 3,040 feet, and total distance over a 50-foot obstacle is 4,667 feet. These figures highlight the 1900D's capability for operations from unpaved or short runways, a key advantage for commuter and feeder services.

Key Performance Specifications (1900D)

ParameterValue
Maximum Speed280 KTAS
High-Speed Cruise276 KTAS at 14,000 lb
Normal Cruise260 KTAS
Economy Cruise230 KTAS
Service Ceiling25,000 ft
Rate of Climb2,625 fpm
Single-Engine Climb Rate454 fpm
Maximum Range1,356 nm
Takeoff Distance (over 50 ft)3,470 ft
Landing Distance (over 50 ft)4,667 ft

References

Add your contribution
Related Hubs
User Avatar
No comments yet.