PZL-102 Kos

The PZL-102 Kos is a Polish two-seat touring and training monoplane designed and built by PZL.

Made by PZL.

Empty Weight Lb
992
Wing Area Sqm
11
Eng 1 Type
Continental C90-12F flat-four piston engine
Max Speed Mph
118
Ceiling Ft
15090
Eng 1 Kw
71
Introduced
1959
Max Speed Kmh
190
Span In
10
Gross Weight Lb
1444
Capacity
1
Number Built
10
Crew
1
Empty Weight Kg
418
Gross Weight Kg
655
Height In
2
Range Km
640.0
Manufacturer
PZL
Met Or Eng
met
Range Miles
398
First Flight
23
Production End Year
1962
Height Ft
6
Span Ft
27
Wing Area Sqft
118
Production Start Year
1959
Span M
9
Length Ft
22
Height M
2
Ceiling M
4600
Eng 1 Hp
95
Eng 1 Number
1
Produced
1959
Length In
9
Length M
7
Category
Polish civil utility aircraft 1950-1959

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