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ATTENTION: This is the new thread for Skandinavisk Flygproducent A/S.


Skandinavisk FP (Official name: Skandinavisk Flygproducent A/S) is an Andallan manufacturer of civil and military aircraft. It is the largest civil aircraft manufacturer in Thalassa and the largest military aircraft manufacturer in Andalla. It is also one of Andalla's largest employers, with 48,915 employees by the end of FY 2016. Skandinavisk's corporate headquarters and main office are located along Marius Norgard Boulevard in Enshavn, with major facilities scattered across Andalla. The company is led by CEO Peter Olstad, the grandson of the company's founder, Markus Olstad.

Skandinavisk was founded in 1918 as Olstad Flygmotoren A/S, a producer of aircraft engines based in the town of Skandinavien. 

Skandinavisk owns several subsidiaries across the Western hemisphere. The following is a list of major Skandinavisk subsidiaries:

  • Skandinaverica, 78%-owned subsidiary manufacturing aircraft exclusively sold in @Iverica
  • Skandinavisk Europa, manufacturer and distributor of Skandinavisk aircraft in Europa, headquartered in Nordhaven, @Orioni
  • Skandinavisk Argis, manufacturer and distributor of Skandinavisk aircraft in Argis, headquartered in New Halsham, @Prymont
  • Olstad Aircraft Engines, manufacturer of turbofan and turbojet engines. Descendant of the original company, Olstad Flygmotoren.
  • Flygmotor, 23%-owned subsidiary, manufacturer of turboprop and propeller aircraft engines.
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L-SERIES AIRCRAFT


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The Model 1 is a four-seat, single-engine aircraft, and the very first Skandinavisk aircraft. The first prototype model flew on October 12, 1929, while the aircraft formally began commercial production in December of the same year. It is considered to be the pioneer of the Andallan aerospace industry. Though several aircraft had been in production by other companies in Andalla at that time, it was the Model 1 that proved itself to last. True enough, all of Skandinavisk's early competitors slowly faded into history. Though Skandinavisk was only in its genesis at that time, over 200 models were produced from 1929 to 1940. An estimated 20 are still in existence, while only 8 are in flying condition.

VARIANTS

  • Model 1 (1929 - 1931)
  • Model 2 (1931 - 1938)
  • Model 3 (1937 - 1940)

SPECIFICATIONS (Model 3)

  • Crew: 2 (pilot, co-pilot)
  • Passenger Capacity: 2
  • Length: 7.24 m
  • Wingspan: 12.35 m
  • Height: 2.28 m
  • Cruise Speed: 162 km/h
  • Top Speed: 184 km/h
  • Service Ceiling: 7,000 ft

C140_Aircraft.jpg&key=0792da7b35dca75870

The Model 10 is a two-seat, single-engine general aviation aircraft. It first flew in 1947 and was the first mass-produced Skandinavisk aircraft. Production began in 1948 and an estimated 980 were built across 16 years. It was Skandinavisk's first large financial success and paved the way for the designing of the first Skandinavisk airliner, the SK-1.

VARIANTS

  • Model 10 (1948 - 1953)
  • Model 11 (1954 - 1960)
  • Model 12 (1960 - 1963)
  • L-10 (1962 - 1964)

SPECIFICATIONS (Model 10)

  • Crew: 1 (pilot)
  • Passenger Capacity: 1
  • Length: 6.55 m
  • Wingspan: 10.16 m
  • Height: 1.91 m
  • Cruise Speed: 171 km/h
  • Top Speed: 202 km/h
  • Range: 728 km
  • Service Ceiling: 15,000 ft

SPECIFICATIONS (L-10)

  • Crew: 1 (pilot)
  • Passenger Capacity: 1
  • Length: 6.63 m
  • Wingspan: 10.57 m
  • Height: 1.87 m
  • Cruise Speed: 193 km/h
  • Top Speed: 219 km/h
  • Range: 760 km
  • Service Ceiling: 17,500 ft

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The L-20 Ravn is a four-seat, single-engine, high-wing utility aircraft, and is one of Skandinavisk's most successful aircraft. First flown in 1962, more than 7,000 aircraft have been built since then. The sheer popularity of the aircraft has earned it the nickname "lille fugl", or "little bird". Dozens of variants have been created over the years, ensuring the L-20 to be up-to-date with modern technology and capabilities despite the model itself being over 50 years old. Most L-20 aircraft are owned privately. It has also found a home with military users as border patrol aircraft or trainers, however very few are in service as such.

VARIANTS

  • L-20A (1962 - 1964)
  • L-20B (1963 - 1971)
  • L-20C (1969 - 1987)
  • L-20D (1987 - 1995)
  • L-20E (1992 - 2008)
  • L-20F (2007 - present)

SPECIFICATIONS (L-20F)

  • Crew: 1 (pilot)
  • Passenger Capacity: 3
  • Length: 8.32 m
  • Wingspan: 11.2 m
  • Height: 2.73 m
  • Cruise Speed: 227 km/h
  • Top Speed: 306 km/h
  • Range: 1,293 km
  • Service Ceiling: 18,500 ft

Cessna421B-Landing.jpg&key=2bb2c479cf403

The L-30 Ørn is a six-seat, twin-engine turboprop general aviation aircraft. Skandinavisk's second most widely-produced aircraft after the L-20, it first flew in 1972 and remains in production. 2,600 aircraft have been produced as of August 2017.

VARIANTS

  • L-30A (1974 - 1978)
  • L-30B (1977 - 1989)
  • L-30C (1990 - 2002)
  • L-30D (2002 - present)

SPECIFICATIONS (L-30D)

  • Crew: 1-2 (pilot, co-pilot)
  • Passenger Capacity: 6
  • Length: 11.09 m
  • Wingspan: 12.56 m
  • Height: 3.52 m
  • Cruise Speed: 448 km/h
  • Top Speed: 481 km/h
  • Range: 2,759 km
  • Service Ceiling: 30,300 ft
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T-SERIES AIRCRAFT


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The T-1 Pionjär is a turboprop STOL transport. It was an immediate success, possessing the capability to land nearly anywhere with its low runway requirement of 900 ft.


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The T-5 Buffel is a turboprop STOL utility aircraft. Known for its durability, the F-5 is quickly aging but is still in widespread use. It first flew in 1963 and has been used by both private and military operators. Production ceased in 1992 with 317 aircraft built.The Carabao is extremely popular with small domestic airlines, specially cargo airlines. One extraordinary capability of the Carabao is being able to land and take off with a shorter runway than even the L-20, making it extremely useful in emergency situations. A newer, updated variant, the F-6, was introduced in 1989 and remains in production.

VARIANTS

  • T-5A (1966 - 1979)
  • T-5B (1977 - 1992)
  • T-6 (1989 - present)

SPECIFICATIONS (T-6)

  • Crew: 3 (pilot, co-pilot, crew chief)
  • Capacity: 48 passengers or 18,500 lb payload
  • Length: 24.08 m
  • Wingspan: 29.26 m
  • Height: 8.73 m
  • Cruise Speed: 425 km/h
  • Top Speed: 463 km/h
  • Range: 1,126 km
  • Service Ceiling: 31,400 ft

C-295M.jpg

C-295M.jpgThe T-8 Rensdyr is a short-range, twin-engine turboprop transport introduced in 1996. It can serve as a short-range airliner or a small cargo aircraft, and has continued to sell strongly to small domestic airlines.

VARIANTS

  • T-8 (1996 - present)

SPECIFICATIONS (T-8)

  • Crew: 2 (pilot, co-pilot)
  • Capacity: 28 passengers or 5,800 lb payload
  • Length: 15.67 m
  • Wingspan: 22.06 m
  • Height: 5.05 m
  • Cruise Speed: 381 km/h
  • Top Speed: 408 km/h
  • Range: 1,763 km
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SK-SERIES AIRCRAFT


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The SK-1 is the first Western long-range, all-metal, pressurized commercial airliner. Ever since its first flight in February 1946 and its subsequent introduction 6 months later, it was Andalla's most successful commercial propeller airliner. In 1956, the SK-1 production line was halted in favor of the new jet-powered SK-2. However, in November 1956, 3 months later, the SK-2 production line was also halted due to major design flaws in the aircraft. The SK-1 production line restarted in 1957 to fund the SK-2-200 project, and was ultimately halted in 1961 after the SK-2-200's success.

VARIANTS

  • SK-1 (1946 - 1955, 1957 -1961)

SPECIFICATIONS (SK-1)

  • Crew: 4 (pilot, co-pilot, engineer, radio operator/navigator)
  • Passenger Capacity: 66
  • Length: 32.18 m
  • Wingspan: 35.81 m
  • Height: 8.66 m
  • Cruise Speed: 492 km/h
  • Maximum Speed: 523 km/h
  • Range: 5,927 km
  • Service Ceiling: 25,000 ft

p8comlv1.jpg

The SK-2 is the first Western commercial jet-powered airliner. One of the pioneers of its type, the SK-2 faced many problems after its initial release in 1955. Production was halted in 1956, and extensive tests were carried out to fix the problems in its airframe. The tests threatened to bankrupt the company, and with sales declining due to the SK-2, cancellation was considered. But CEO Olof Olstad, the younger brother of Skandinavisk founder Markkus Olstad, saw a promising future in the aircraft and decided to continue tests. Finally, in 1959, the SK-2-200 debuted, enjoying an extremely successful career. It remained in production for a long 12 years and is widely considered to be one of Thalassa's most iconic and revolutionary aircraft.

VARIANTS

  • SK-2-100 (1955 - 1956)
  • SK-2-200 (1959 - 1965)
  • SK-2-300 (1964 - 1971)

SPECIFICATIONS (SK-2-200)

  • Crew: 4 (pilot, co-pilot, engineer, radio operator/navigator)
  • Passenger Capacity: 78
  • Length: 33.99 m
  • Wingspan: 35.2 m
  • Height: 8.99 m
  • Cruise Speed: 840 km/h
  • Maximum Speed: 893 km/h
  • Range: 5,190 km
  • Service Ceiling: 40,000 ft

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The SK-3 is a long-range narrow-body airliner. One of Thalassa's most iconic aircraft, being the first to fly scheduled Trans-Oriental flights on maximum payload. The SK-3 also broke the record for the fastest crossing of the Oriental Ocean from Arkhavn to O'polis in 10 hours 29 minutes. Its unique design featured two Alminn-Trisk MR.23 turbojets coupled together on both sides at the rear of the aircraft. The SK-3 was extremely popular with airlines that orders soared within the first three years of its announcement. It was produced from 1968 to 1984.

VARIANTS

  • SK-3-100 (1968 - 1975)
  • SK-3-200 (1975 - 1979)
  • SK-3-300 (1978 - 1984)

SPECIFICATIONS (SK-3-300)

  • Crew: 4 (pilot, co-pilot, engineer, radio operator/navigator)
  • Passenger Capacity: 162
  • Length: 48.96 m
  • Wingspan: 45.37 m
  • Height: 12.43 m
  • Cruise Speed: 896 km/h
  • Maximum Speed: 947 km/h
  • Range: 10,156 km
  • Service Ceiling: 45,000 ft

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The SK-4 is a narrow-body tri-jet airliner. Introduced in 1977, it answered the growing demand for a more efficient jet to replace the obsolete SK-2. It could seat up to 125 passengers in a one-class configuration. Several modernized variants were produced until the end of the SK-4 production line in 2009.

VARIANTS

  • SK-4-100 (1977 - 1986)
  • SK-4-100F (1979 - 1993)
  • SK-4-200 (1984 - 1991)
  • SK-4-200ER (1985 - 1994)
  • SK-4-300 (1991 - 2003)
  • SK-4-300F (1992 - 2009)
  • SK-4-300ER (1994 - 2007)

SPECIFICATIONS (SK-4-100)

  • Crew: 3 (pilot, co-pilot, engineer)
  • Passenger Capacity: 125 (1-class), 106 (2-class)
  • Length: 40.59 m
  • Wingspan: 32.92 m
  • Height: 10.44 m
  • Cruise Speed: 917 km/h
  • Maximum Speed: 961 km/h
  • Range: 4,171 km
  • Service Ceiling: 42,000 ft

SPECIFICATIONS (SK-4-200)

  • Crew: 3 (pilot, co-pilot, engineer)
  • Passenger Capacity: 155 (1-class), 134 (2-class)
  • Length: 43.68 m
  • Wingspan: 32.1 m
  • Height: 12.56 m
  • Cruise Speed: 953 km/h
  • Maximum Speed: 986 km/h
  • Range: 3,867 km
  • Service Ceiling: 42,500 ft

SPECIFICATIONS (SK-4-200ER)

  • Crew: 3 (pilot, co-pilot, engineer)
  • Passenger Capacity: 142 (1-class), 124 (2-class)
  • Length: 44.8 m
  • Wingspan: 32.1 m
  • Height: 12.56 m
  • Cruise Speed: 928 km/h
  • Maximum Speed: 972 km/h
  • Range: 4,725 km
  • Service Ceiling: 42,500 ft

SPECIFICATIONS (SK-4-300ER)

  • Crew: 2 (pilot, co-pilot)
  • Passenger Capacity: 160 (1-class), 138 (2-class)
  • Length: 55.4 m
  • Wingspan: 38.15 m
  • Height: 13.2 m
  • Cruise Speed: 973 km/h
  • Maximum Speed: 1,083 km/h
  • Range: 6,323 km
  • Service Ceiling: 42,500 ft

15160985443_0e79557349_b.jpg

The SK-5 is a long-range wide-body tri-jet airliner, and one of Skandinavisk's most successful jet aircraft. It is Skandinavisk's first airliner featuring a glass cockpit. It was extremely successful due to its range, which allowed it to make a Trans-Oriental flight from Arkhavn to O'polis without any layovers. It was introduced in December of 1990 and remained in production until 2004. Most of the SK-5 fleet remains in service, with a number being decommissioned and sold by larger airlines opting for newer, more efficient aircraft. A cargo variant, the SK-5-100F, is a favorite among cargo airlines in Thalassa. Several modernized variants with improved avionics and efficiency are still in production.

VARIANTS

  • SK-5-100 (1989 - 2002)
  • SK-5-100SR (1991 - 2005)
  • SK-5-100F (1991 - present)
  • SK-5-100ER (1997 - 2011)
  • SK-5-200 (2001 - 2016)
  • SK-5-200SR (2002 - present)
  • SK-5-300 (2014 - present)
  • SK-5-300ER (Under development)

SPECIFICATIONS (SK-5-100)

  • Crew: 2 (pilot, co-pilot)
  • Passenger Capacity: 410 (high-density), 380 (1-class), 323 (2-class), 293 (3-class)
  • Cargo Capacity: 32 x LD3 (lower compartment)
  • Length: 61.62 m
  • Wingspan: 51.66 m
  • Height: 17.6 m
  • Top Speed: 945 km/h
  • Cruise Speed: 876 km/h
  • Range: 12,670 km
  • Service Ceiling: 45,000 ft

SPECIFICATIONS (SK-5-100SR)

  • Crew: 2 (pilot, co-pilot)
  • Passenger Capacity: 440 (high-density), 406 (1-class), 344 (2-class), 315 (3-class)
  • Cargo Capacity: 32 x LD3 (lower compartment)
  • Length: 62.73 m
  • Wingspan: 51.66 m
  • Height: 17.6 m
  • Top Speed: 937 km/h
  • Cruise Speed: 865 km/h
  • Range: 8,364 km
  • Service Ceiling: 45,000 ft

SPECIFICATIONS (SK-5-100F)

  • Crew: 3 (pilot, co-pilot, loadmaster)
  • Cargo Capacity: 596m³, 26 pallets (main deck), 32 x LD3 (lower compartment)
  • Length: 61.62 m
  • Wingspan: 51.66 m
  • Height: 17.6 m
  • Top Speed: 945 km/h
  • Cruise Speed: 876 km/h
  • Range: 7,320 km
  • Service Ceiling: 45,000 ft

SPECIFICATIONS (SK-5-200)

  • Crew: 2 (pilot, co-pilot)
  • Passenger Capacity: 422 (high-density), 390 (1-class), 338 (2-class), 298 (3-class)
  • Cargo Capacity: 32 x LD3 (lower compartment)
  • Length: 63.5 m
  • Wingspan: 53.2 m
  • Height: 17.65 m
  • Top Speed: 983 km/h
  • Cruise Speed: 883 km/h
  • Range: 13,104 km
  • Service Ceiling: 46,500 ft

SPECIFICATIONS (SK-5-200SR)

  • Crew: 2 (pilot, co-pilot)
  • Passenger Capacity: 456 (high-density), 422 (1-class), 352 (2-class), 320 (3-class)
  • Cargo Capacity: 32 x LD3 (lower compartment)
  • Length: 63.78 m
  • Wingspan: 53.2 m
  • Height: 17.65 m
  • Top Speed: 982 km/h
  • Cruise Speed: 879 km/h
  • Range: 9,820 km
  • Service Ceiling: 46,500 ft

Cubana_Tupolev_Tu-204-100E.jpg

The SK-6 is a medium-range twinjet airliner and Skandinavisk's primary entry into the short and medium-haul markets. The SK-6 was seen as the "new generation" of the SK-4, boasting improved performance, fuel efficiency, capacity and range. The SK-6 had a significantly lower cruising speed than the SK-4, but a newer variant with increased speed and improved avionics was introduced in 1995.

VARIANTS

  • SK-6-100 (1992 - 2004)
  • SK-6-100SR (1995 - 2009)
  • SK-6-100LR (1998 - 2013)
  • SK-6-200 (2004 - present)
  • SK-6-200SR (2006 - present)
  • SK-6-300 (2012 - present)

SPECIFICATIONS (SK-6-100)

  • Crew: 2 (pilot, co-pilot)
  • Passenger Capacity: 210 (high-density), 190 (1-class), 172 (2-class)
  • Length: 46.14 m
  • Wingspan: 41.8 m
  • Height: 13.9 m
  • Top Speed: 908 km/h
  • Cruise Speed: 852 km/h
  • Range: 6,300 km
  • Service Ceiling: 40,000 ft

SPECIFICATIONS (SK-6-100LR)

  • Crew: 2 (pilot, co-pilot)
  • Passenger Capacity: 202 (high-density), 185 (1-class), 164 (2-class)
  • Length: 46.9 m
  • Wingspan: 41.8 m
  • Height: 13.9 m
  • Top Speed: 896 km/h
  • Cruise Speed: 841 km/h
  • Range: 7,126 km
  • Service Ceiling: 40,000 ft

SPECIFICATIONS (SK-6-200SR)

  • Crew: 2 (pilot, co-pilot)
  • Passenger Capacity: 221 (high-density), 198 (1-class), 178 (2-class)
  • Length: 48.26 m
  • Wingspan: 42.5 m
  • Height: 14.7 m
  • Top Speed: 914 km/h
  • Cruise Speed: 859 km/h
  • Range: 4,620 km
  • Service Ceiling: 45,000 ft

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The SK-7 is a four-engine, wide-body long-haul airliner and Skandinavisk's largest aircraft produced to date. Nicknamed the "Queen of the Skies", the SK-7 is the perfect aircraft for long-range and high-demand routes. First introduced in 1998, a decade before the Aérospatiale Magenta, it continues to rule the high-demand long-haul market and remains in production. Long-range, short-range and freight variants are also available.

VARIANTS

  • SK-7-100 (1997 - 2005)
  • SK-7-100SR (2001 - 2016)
  • SK-7-100F (2001 - present)
  • SK-7-100ER (2004 - present)
  • SK-7-200 (2007 - present)
  • SK-7-200SR (2015 - present)
  • SK-7-200ER (Under development)

SPECIFICATIONS (SK-7-100)

  • Crew: 2 (pilot, co-pilot)
  • Passenger Capacity: 504 (high-density), 436 (1-class), 386 (2-class), 315 (3-class)
  • Cargo Capacity: 18 x LD3 and 114m³ (front cargo hold), 14 x LD3 and 82m³ (rear cargo hold)
  • Length: 64.1 m
  • Wingspan: 60.11 m
  • Height: 15.7 m
  • Top Speed: 915 km/h
  • Cruise Speed: 854 km/h
  • Range: 10,047 km
  • Service Ceiling: 43,000 ft

SPECIFICATIONS (SK-7-100SR)

  • Crew: 2 (pilot, co-pilot)
  • Passenger Capacity: 568 (high-density), 512 (1-class), 468 (2-class), 410 (3-class)
  • Cargo Capacity: 14 x LD3 and 114m³ (front cargo hold), 10 x LD3 and 82m³ (rear cargo hold)
  • Length: 67.8 m
  • Wingspan: 60.11 m
  • Height: 15.7 m
  • Top Speed: 901 km/h
  • Cruise Speed: 824 km/h
  • Range: 7,246 km
  • Service Ceiling: 43,000 ft

SPECIFICATIONS (SK-7-100F)

  • Crew: 3 (pilot, co-pilot, loadmaster)
  • Cargo Capacity: 580m³ (main deck), 18 x LD3 and 114m³ (front cargo hold), 14 x LD3 and 82m³ (rear cargo hold)
  • Length: 63.94 m
  • Wingspan: 60.11 m
  • Height: 15.7 m
  • Top Speed: 915 km/h
  • Cruise Speed: 854 km/h
  • Range: 10,047 km
  • Service Ceiling: 43,000 ft

SPECIFICATIONS (SK-7-100ER)

  • Crew: 2 (pilot, co-pilot)
  • Passenger Capacity: 422 (1-class), 340 (2-class), 307 (3-class)
  • Cargo Capacity: 18 x LD3 and 114m³ (front cargo hold), 14 x LD3 and 82m³ (rear cargo hold)
  • Length: 64.8 m
  • Wingspan: 60.11 m
  • Height: 15.7 m
  • Top Speed: 915 km/h
  • Cruise Speed: 854 km/h
  • Range: 12,802 km
  • Service Ceiling: 43,000 ft

SPECIFICATIONS (SK-7-200SR)

  • Crew: 2 (pilot, co-pilot)
  • Passenger Capacity: 580 (high-density), 527 (1-class), 474 (2-class), 419 (3-class)
  • Cargo Capacity: 14 x LD3 and 114m³ (front cargo hold), 10 x LD3 and 82m³ (rear cargo hold)
  • Length: 66.9 m
  • Wingspan: 62.72 m
  • Height: 16.1 m
  • Top Speed: 910 km/h
  • Cruise Speed: 831 km/h
  • Range: 8,462 km
  • Service Ceiling: 48,000 ft
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D-SERIES


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The D-55 is a long-range business jet. Most aircraft are operated privately, with some in military service as VIP transport. An AEWC variant is also under development, but is expected to be completed by March 2018. It can seat up to 24 passengers in a high-density transport configuration. It is popular with large charter airlines because of its capability to cross the Oriental Ocean, but has also been used by premium regional airlines. The D-55 VIP transport is designated as the L-18 in the Andallan Commonwealth Air Force.

SPECIFICATIONS

  • Crew: 2 (pilot, co-pilot)
  • Capacity: 14-19 passengers, 24 in high-density configuration
  • Length: 29.4 m
  • Wingspan: 28.51 m
  • Height: 7.9 m
  • Cruise Speed: 852 km/h
  • Top Speed: 936 km/h
  • Range: 12,620 km
  • Service Ceiling: 52,000ft
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J-SERIES


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The J-1 Meteorit is a subsonic, single-seat jet fighter. Initially developed by the ACAAC and Saeb Aeronautik under the Joint Andallan Jet Fighter Project (Forenet Andska Stridsplanprojekt) as the Saeb K.9 to become the first Andallan-made jet aircraft, Saeb's share in the project was acquired by Skandinavisk in 1949 following the post-war arms manufacturing crash. At the time, the civil aviation industry was booming and Skandinavisk was only planning to enter the military aviation industry. After 9 years of development, the first fully-operational variant began production in 1951 as the Skandinavisk J-1 Meteorit. Though largely unsuccessful due to numerous factors including low endurance, faulty airframe, unremarkable performance and low demand, the Meteorit proved an important step in the development of Andallan jet aircraft. The Meteorit remained in scarce production until the introduction of the J-2 Komet in 1958.

VARIANTS

  • J-1 Meteorit (1951 - 1958)
  • I-1 Øgle (1952 - 1970)

SPECIFICATIONS (J-1)

  • Crew: 1 (pilot)
  • Length: 13.59 m
  • Wingspan: 11.32 m
  • Height: 3.96 m
  • Top Speed: 957 km/h
  • Range: 915 km
  • Service Ceiling: 43,000 ft

ARMAMENT (J-1)

  • Guns: 4 x 20mm autocannons
  • Rockets: Up to 16 x 76 mm or 8 x 127 mm air-to-ground rockets
  • Bombs: 2 x 1,000 lb bombs

1559702-large.jpg

The J-2 Komet is a transonic delta-wing interceptor fighter, and the first Andallan-made aircraft of its type. A J-2 Komet with serial number 58023, nicknamed the "Mighty Skjellerup" (after the comet 38P/Skjellerup), holds the distinction of being the very first Andallan-made aircraft to break the sound barrier, in a controlled dive on 23 February 1959. The J-2 was known for its maneuverability, owing to its unusual combination of the T-tail and delta wing design. Due to the economic crisis, the J-2 remained in low numbers of production. Two years later, in 1960, the newly-established successor to the Andallan Commonwealth Air Command, the Andallan Commonwealth Air Force, was ready to authorize mass-production of the aircraft. Production continued until 1969.

VARIANTS

  • J-2A (1958 - 1967)
  • J-2B (1964 - 1969)

SPECIFICATIONS (J-2A)

  • Crew: 2 (pilot, navigator)
  • Length: 17.15 m
  • Wingspan: 15.85 m
  • Height: 4.88 m
  • Top Speed: 1,140 km/h
  • Range: 1,530 km
  • Service Ceiling: 52,000 ft

ARMAMENT (J-2A)

  • Guns: 4 x 30mm autocannons

SPECIFICATIONS (J-2B)

  • Crew: 2 (pilot, navigator)
  • Length: 17.15 m
  • Wingspan: 15.85 m
  • Height: 4.88 m
  • Top Speed: 1,140 km/h
  • Range: 1,530 km
  • Service Ceiling: 52,000 ft

ARMAMENT (J-2B)

  • Guns: 4 x 30mm autocannons
  • Bombs: 4 x under-wing pylons for a total of 1,200 lbs of bombs

8fcff8d7f026184de9f5e910deb676ed.jpg

The J-3 Stjernetåge is a supersonic light fighter, and the first Andallan-made purpose-built supersonic aircraft. The J-3 was developed in response to an Andallan Commonwealth Air Force requirement for a "modernized and affordable" fighter design.

Edited by Andalla
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Posted (edited)

B-SERIES


1024px-Avro_Vulcan_Bomber_RAF.JPEG&key=e

The B-1 Glød is a high-altitude, semi-stealth strategic bomber. It was initially scheduled for production in 1971, but several flaws in the design delayed the date to May of 1972. It is the ACAF's only strategic bomber aircraft. It has a built-in ECM suite to fend off against incoming missiles. The Glød's airframe served as the basis for the more advanced @Prymont F-F Cockroach bomber.

SPECIFICATIONS

  • Crew: 5 (pilot, co-pilot, weapon systems officer, navigator, ECM officer)
  • Length: 29.59 m
  • Wingspan: 30.3 m
  • Height: 8.04 m
  • Top Speed: 1,236 km/h
  • Cruise Speed: 953 km/h at 45,000 ft
  • Range: 4,392 km
  • Service Ceiling: 60,000 ft

ARMAMENT

  • 21 x 1,000 lb conventional bombs
  • 42 x 500 lb conventional bombs
Edited by Andalla
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Posted (edited)

I-SERIES


18503777911_a3d05a9813_b.jpg&key=ae98abc

The I-4 Fremstød is a transonic advanced jet trainer. However, it can also serve as a lightly-armed combat aircraft. It was introduced in 1992 and remains in production.

SPECIFICATIONS

  • Crew: 2 (pilot, co-pilot/instructor)
  • Length: 13.08 m
  • Wingspan: 9.94 m
  • Height: 4.6 m
  • Top Speed: 1,036 km/h
  • Range: 1,588 km

ARMAMENT

  • Hardpoints: 2 x air-to-air/air-to-ground missiles or external drop tanks
Edited by Andalla
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Posted (edited)

N-SERIES


1024px-C-123K_ROKAF_Team_Spirit_1989.JPE

The N-1 Leverantör is a turboprop military transport aircraft and the first dedicated military transport aircraft developed by Skandinavisk. It entered production in 1958 and ended 1974. Only few remain in military service while a number of aircraft are privately-operated.

SPECIFICATIONS

  • Crew: 4 (pilot, co-pilot, flight engineer, radio operator/navigator)
  • Capacity: 60 troops or 24,000 lb payload
  • Length: 23.25 m
  • Wingspan: 33.53 m
  • Height: 10.39 m
  • Top Speed: 367 km/h
  • Cruise Speed: 278 km/h
  • Range: 1,654 km

0523749.jpg?v=v40&key=62dac961596e2db318

The N-2 Stjärnlyft is Skandinavisk's only strategic airlifter. It is also the largest Andallan military aircraft ever produced. Production began in 1968 and ended 2001, with a second variant still in production. It has been in service with the ACAF for nearly 5 decades. One aircraft known as the White Dwarf holds the distinct record of being the longest-serving aircraft in the ACAF, beginning service in 1977.

SPECIFICATIONS

  • Crew: 5-7 (pilot, co-pilot, 2 flight engineers, loadmaster, optional: second loadmaster, navigator)
  • Capacity: 154 troops, 123 paratroopers or 50,000 lb payload
  • Length: 51.3 m
  • Wingspan: 48.8 m
  • Height: 12.00 m
  • Top Speed: 912 km/h
  • Cruise Speed: 790 km/h
  • Range: 4,723 km

1024px-50%2B61_German_Air_Force_Transall

The N-3 Reise is a turboprop tactical airlift transport. It is the ACAF's primary tactical airlift transport and has been in service since its introduction in 1973. While the original variant ended production in 1996, newer variants are still being built. The N-3 Reise production line is expected to last until 2030, then it will be replaced by an entirely new aircraft.

SPECIFICATIONS

  • Crew: 4 (pilot, co-pilot, flight engineer, loadmaster)
  • Capacity: 93 troops, 88 paratroopers or 35,275 lb payload
  • Length: 32.40 m
  • Wingspan: 40.03 m
  • Height: 11.65 m
  • Top Speed: 513 km/h
  • Cruise Speed: 495 km/h
  • Range: 1,853 km

Lithuanian_Air_Force_Antonov_AN-26_(04).

The N-4 Løfteren is a twin-engine turboprop transport and electronic warfare aircraft. It began production in 1972 and ended 2001. The N-4 also has an electronic warfare (EW) variant, the E-1 Förundras. Though officially classified as a combat aircraft, it is built along the N-4 production line.

SPECIFICATIONS

  • Crew: 4 (pilot, co-pilot, flight engineer, radio operator/navigator)
  • Capacity: 36 troops, 34 paratroopers or 12,100 lb payload
  • Length: 23.8 m
  • Wingspan: 29.3 m
  • Height: 8.58 m
  • Cruise Speed: 440 km/h
  • Range: 953 km

1024px-CASA_C-295_of_Polish_Air_Force,_R

The N-5 Odysse is a twin-engine turboprop tactical airlift aircraft. It was developed alongside a civilian variant, the NT-9 Iliaden, and was introduced in late 1998. It has twice the capacity of the N-4 while also boasting the new Flygmotor JR-910 turboprops, making it even faster than the N-3 Reise.

SPECIFICATIONS

  • Crew: 2 (pilot, co-pilot)
  • Capacity: 71 troops, 64 paratroopers or 20,600 lb payload
  • Length: 24.5 m
  • Wingspan: 25.8 m
  • Height: 8.61 m
  • Top Speed: 576 km/h
  • Cruise Speed: 480 km/h
  • Range: 1,350 km on full payload
  • Service Ceiling: 30,000 ft
Edited by Andalla
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      @Fulgistan , 20.05.2018 "f*ckingrat.png"
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