MacDonald S-20
The MacDonald S-20 is a single-seat sport aircraft that was designed in the United States in the early 1970s and marketed for home building. The aircraft is a conventional, low-wing cantilever monoplane with fixed tailwheel undercarriage and an open cockpit. Construction is of metal throughout, with a forward fuselage of welded steel tube construction, with the rear fuselage built up of aluminium bulkheads and longerons. The wings and tail are also of aluminium construction, and the entire aircraft is skinned in the same material. Pop rivets are used extensively to simplify construction.
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MacDonald S-20
The MacDonald S-20 is a single-seat sport aircraft that was designed in the United States in the early 1970s and marketed for home building. The aircraft is a conventional, low-wing cantilever monoplane with fixed tailwheel undercarriage and an open cockpit. Construction is of metal throughout, with a forward fuselage of welded steel tube construction, with the rear fuselage built up of aluminium bulkheads and longerons. The wings and tail are also of aluminium construction, and the entire aircraft is skinned in the same material. Pop rivets are used extensively to simplify construction.
has abstract
The MacDonald S-20 is a single ...... he plans were designated S-21.
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manufacturer
number built
origin
Wikipage page ID
19,854,745
Wikipage revision ID
668,340,493
climb rate ftmin
climb rate ms
designer
Robert A. MacDonald
empty weight kg
empty weight lb
eng1 number
eng1 type
converted Volkswagen automotive engine
first flight
1972-03-09
gross weight kg
gross weight lb
height ft
height in
height m
length ft
length in
length m
max speed kmh
max speed mph
metOrEng%3F_
range km
range miles
ref
Jane's All the World's Aircraft 1977–78, 547
span m
type
Sport aircraft
wing area sqft
wing area sqm
hypernym
comment
The MacDonald S-20 is a single ...... vely to simplify construction.
@en
label
MacDonald S-20
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