Interstate Cadet

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Interstate Cadet
Interstate L-6 Cadet USAF Museum.jpg
An L-6 of the USAF Museum
Role Utility monoplane
National origin United States
Manufacturer Interstate Aircraft and Engineering Corporation
First flight 1940
Primary user United States Army
Number built 574
Variants Arctic Tern

The Interstate Cadet was an American two-seat tandem, high wing, single-engine monoplane light aircraft. Around 320 of these aircraft were produced between the years 1941 and 1942 by the Interstate Aircraft and Engineering Corporation based in El Segundo, California. The construction techniques employed were a welded steel tube fuselage, wood (spruce) wing structure with metal ribs, and fabric covering, all of which were fairly standard in the 1940s.

Design and development[edit]

The aircraft in its original version (the S1 prototype) was powered by the 50hp Continental A50 engine, but was soon upgraded (the S1-A-65F variant) to the Continental A65 engine. This was the mainstay used in most small two-seat aircraft of the time. This aircraft was also used in WW2, being named the L-6A.

In 1945 the rights to the aircraft were sold to Harlow Aircraft Company which in turn resold the tooling and parts to the Call Aircraft Company of Afton Wyoming in 1946 for $5000. Callair had rebuilt a number of S-1, S-1A and L6 aircraft with and without engine upgrades for local ranchers and bush pilots as well as two examples of their own serial numbered CallAir S-1A-90C before stopping production.[1]

It has been speculated why the S1 did not become successful during the early 40's. One reason was that this aircraft cost almost three times the amount of the comparable Piper J-3 Cub. However, a close look at the two aircraft reveals that the Cadet was far superior. It was faster, stronger, and could be operated in a more rugged environment with its Oleo strut/Compression spring suspension system. Popular upgrades for this airframe included larger engines(75/85/90/100hp), better brakes, and a different tailwheel system.

In the late 1960s the type certificates and tooling were bought by the newly formed Arctic Aircraft Company. Arctic Aircraft transformed the S-1B1 into a bush plane by upgrading structural elements of the fuselage, landing gear and wings. This new aircraft, designated the S-1B2, was reconfigured with a Lycoming O-320 160 HP engine and 82” McCauley propeller for increased performance.

In 1975, the revived and modernised Model S-1B2 was certified as the Arctic Tern.

Type certification was also obtained for some of the original Interstate Cadets to use the 160 hp Lycoming O-320 engine but without the full complement of modifications and upgrades provided in the Arctic Tern.

Variants[edit]

A later S-1B2 Arctic Tern
S-1
Certified in 1940 and powered by a Continental A50-8 engine.[2]
S-1A
Certified in 1941 and powered by a Continental A65-8 engine.[3]
Interstate S-1A-65F Cadet rooftop landing
S-1A-65F
1941 variant powered by a 65hp Franklin 4AC-176-B2 engine.[3]
S-1A-85F
1942 variant powered by a 85hp Franklin 4AC-199-D2 engine.[3]
S-1A-90C
1952 Callair variant powered by a 90hp Continental C90-8 engine.only two built. [3]
S-1A-90F
1942 variant powered by 90hp Franklin 4AC-199-E2 engine.[3]
S-1B1
1942 variant with a Franklin 4ACG-199-H3 engine. Military production as the L-6 Grasshopper.[4]
S-1B2 (Arctic Tern)
1975 improved variant of the S-1B1 powered by a Lycoming O-320-A2B or B2B engine.[4]
XO-63 Grasshopper
United States Army designation for one S-1B for evaluation, later designated the XL-6.[5]
L-6A Grasshopper
United States Army designation for the S-1B1, 250 built.[5]
L-8A Cadet
United States Army designation for eight S-1As ordered on behalf of the Bolivian Air Force.[5]

Specifications (S-1B1)[edit]

General characteristics

  • Crew: two
  • Length: 23 ft 5 in (7.14 m)
  • Wingspan: 35 ft 6 in (10.82 m)
  • Height: 7 ft (2.1 m)
  • Empty weight: 1,103 lb (500 kg)
  • Max takeoff weight: 1,650 lb (748 kg)
  • Powerplant: 1 × Continental A65-8 , 65 hp (48 kW)

Performance

  • Maximum speed: 114 mph (183 km/h; 99 kn)
  • Cruise speed: 105 mph (91 kn; 169 km/h)
  • Range: 540 mi (469 nmi; 869 km)
  • Service ceiling: 16,500 ft (5,029 m)

See also[edit]

Related development
Related lists

References[edit]

Notes
  1. ^ "The Quiet Professor". Air Progress Sport Aircraft. Winter 1969. , {Anelon interviews with former Callair employees}
  2. ^ "Type Certificate Data Sheet #2-558". Federal Aviation Administration. 31 October 2007. Retrieved 2009-12-20. 
  3. ^ a b c d e "Type Certificate Data Sheet #A-737". Federal Aviation Administration. 31 October 2007. Retrieved 2009-12-20. 
  4. ^ a b "Type Certificate Data Sheet #A-754". Federal Aviation Administration. 31 October 2007. Retrieved 2009-12-20. 
  5. ^ a b c Andrade 1979, p. 130
Bibliography
  • Andrade, John (1979). U.S.Military Aircraft Designations and Serials since 1909. Midland Counties Publications. ISBN 0-904597-22-9.