Aero A.38 : Variants, Specifications (A.38) Wikipedia, the free encyclopedia

Aero A.38

You can help expand this article with text translated from the corresponding article in Czech. (March 2020) Click [show] for important translation instructions.

View a machine-translated version of the Czech article.
Machine translation, like DeepL or Google Translate, is a useful starting point for translations, but translators must revise errors as necessary and confirm that the translation is accurate, rather than simply copy-pasting machine-translated text into the English Wikipedia.
Consider adding a topic to this template: there are already 252 articles in the main category, and specifying|topic= will aid in categorization.
Do not translate text that appears unreliable or low-quality. If possible, verify the text with references provided in the foreign-language article.
You must provide copyright attribution in the edit summary accompanying your translation by providing an interlanguage link to the source of your translation. A model attribution edit summary is Content in this edit is translated from the existing Czech Wikipedia article at [[:cs:Aero A-38]]; see its history for attribution.
You may also add the template {{Translated|cs|Aero A-38}} to the talk page.
For more guidance, see Wikipedia:Translation.

Aero A.38

Role	Airliner Type of aircraft
Manufacturer	Aero Vodochody
Primary users	Československé Státní Aerolinie CIDNA
Developed from	Aero A.35

The Aero A.38 was a Czechoslovakian biplane airliner of the 1920s and 1930s. Following the relatively modern A.35, this aircraft was something of a throwback, marrying a fuselage derived from the A.35 to wings copied from the A.23. A few served with CSA, and others with French airline Compagnie Internationale de Navigation Aérienne. These latter aircraft were powered by a French Gnome-Rhône engine instead.

Variants

A.38-1 : Fitted with a Walter-built Bristol Jupiter radial piston engine. Three built.
A.38-2 : Fitted with a Gnome-Rhône 9A2 Jupiter radial piston engine. Two built.

Specifications (A.38)

General characteristics

Crew: Two (pilot and mechanic)
Capacity: 8 passengers
Length: 12.8 m (42 ft 0 in)
Wingspan: 16.6 m (54 ft 6 in)
Height: 4.5 m (14 ft 9 in)
Wing area: 67 m² (720 sq ft)
Empty weight: 1,740 kg (3,836 lb)
Gross weight: 3,150 kg (6,945 lb)
Powerplant: 1 × Walter-built Bristol Jupiter 9-cyl. air-cooled radial piston engine, 313 kW (420 hp)