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The Bleriot-SPAD S.33 was a small French airliner developed soon after World War I. A great success the S.33 dominated its field throughout the 1920s initially on CMA's Paris-London route and later on continental routes serviced by Franco-Roumaine. The aircraft was a biplane of conventional configuration whose design owed much to the Blériot company's then-recent fighter designs such as the S.20.

Made by Blériot Aéronautique.

Empty Weight Lb
2315
More Users
SNETA
Eng 1 Type
Radial engine
Salmson 9 (water cooled engine)
Max Speed Mph
112
Cruise Speed Kmh
160
Ceiling Ft
12470
Cruise Speed Mph
100
Eng 1 Kw
194
Span In
3
Wing Area Sqm
42
Gross Weight Lb
4546
Capacity
5
Number Built
ca. 41
Crew
one pilot
Empty Weight Kg
1050
Gross Weight Kg
2062
Height In
6
Primary user
Manufacturer
Range Miles
670
First Flight
1920-12-12
Max Speed Kmh
180
Height Ft
10
Span Ft
38
Wing Area Sqft
454
Met Or Eng
met
Span M
12
Length Ft
29
Height M
3
Sequence
* ← S.30 - S.31 - S.32 - S.33 - S.34 - S.35 - S.36 → * ← S.41 - S.42 - S.46 - S.48 - S.50 - S.51 - S.54 - S.56 →
Ceiling M
3800
Eng 1 Hp
260
Eng 1 Number
1
Related
Blériot-SPAD S.46
Blériot-SPAD S.56
Range Km
1060
Length In
10
Length M
9
Category

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