Taylorcraft F-21 Explained

The Taylorcraft F-21 is a high-wing American-built certified light aircraft developed from earlier Taylorcraft designs.[1]

Development

The Taylorcraft F-21 is a single-engine, high-wing, conventional-gear aircraft. It was developed from the earlier F-19 model with a larger 118 hp engine and an updated FAA-type certificate.[2]

Production

43 examples of the F-21 basic design were built between 1980 and 1990. These were designated the F-21, F-21A and F-21B, with minor changes in design.

Operational history

Variants

[3]

F-21
  • Conventional gear with 118 h.p. Lycoming O-235-C engine. 1,500 lb TOGW. 22 built 1980-1985.
    F-21A
  • F-21 with fuselage fuel tank deleted and 40 gal fuel capacity in two wing tanks. 6 built 1982-1984.
    F-21B
  • F-21 with 42 gal total fuel capacity and 1,750 TOGW. New wing spars and aluminium under-fuselage skinning. 15 built 1985-1990.

    A further development was the F-22:

    F-22A
  • Tricycle gear
    F-22C STOL 180
  • Tricycle gear 180hp - 1 built

    Bibliography

    . John W. R. Taylor . Jane's All The World's Aircraft 1988–89 . 1988 . Jane's Defence Data . Coulsdon, UK . 0-7106-0867-5 .

    Notes and References

    1. Air Progress. April 1991. 28.
    2. AOPA Pilot. Taylorcraft F21B A Good Bet. 1 May 1997 . Alton K. Marsh.
    3. Simpson, 2005, p. 293