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Pazmany
PL-4A
The Pazmany PL-4A is a senior
among the homebuilt designs. This single place low wing aircraft
features a fully enclosed cockpit, all aluminium construction with
folding wings. A very rugged time-tested design. Won "Outstanding
New Design" at EAA Oshkosh 1972.
specifications
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
useful load
gross weight
fuel capacity
range |
VW1600cc
HP Range 50-90
x
16
ft 5ins
5
ft 7ins
26
ft 7ins
89 sq.ft
1
578
lbs
x
850
lbs
12
gal
280 s.m |
performance
takeoff distance,
ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
service ceiling |
560
ft
650
fpm
120mph
97mph
440
ft
13000
ft |
limiting and recommended speeds
design manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed |
x
x
46mph
x |
All specifications are based on manufacturer's
calculations
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