Talk:Aero AT-3

This is the talk page for discussing improvements to the Aero AT-3 article.
This is not a forum for general discussion of the article's subject.

Put new text under old text. Click here to start a new topic.
New to Wikipedia? Welcome! Learn to edit; get help.

Article policies

Find sources: Google (books · news · scholar · free images · WP refs) · FENS · JSTOR · TWL

Poland Low‑importance

	Poland portal This article is within the scope of WikiProject Poland, a collaborative effort to improve the coverage of Poland on Wikipedia. If you would like to participate, please visit the project page, where you can join the discussion and see a list of open tasks.PolandWikipedia:WikiProject PolandTemplate:WikiProject PolandPoland articles
Low	This article has been rated as Low-importance on the project's importance scale.

Aviation: Aircraft

This article is within the scope of the Aviation WikiProject. If you would like to participate, please visit the project page, where you can join the project and see lists of open tasks and task forces. To use this banner, please see the full instructions.AviationWikipedia:WikiProject AviationTemplate:WikiProject Aviationaviation articles

This article has been checked against the following criteria for B-class status:
Referencing and citation: criterion not met Coverage and accuracy: criterion not met Structure: criterion met Grammar and style: criterion not met Supporting materials: criterion met

This article is supported by the aircraft project.

Incomplete list of AT-3 aircraft:

Polish: SP-TPC, TPD, TPE, TPF, TPG, ICY, CUH, KAC, KOS, KOT, EAR, RAM, PPL
British: G-UKAT, SPAT, SBRK, LGOC, SYWL, SWLL, DPEP, MAVV, SACX, SACY, SRUM, SYEL, TGUN,
French: F-GNMV
Spanish: EC-KHY

AT-3 gross weight & fuel

Some newer AT-3 (like SP-TPE, SP-TPF) have maximum takeoff weight of 630kg. This was an amendment to some early models and factory-set to newer models. Particular planes also vary widely in terms of fuel tank placement. The prototype (still flying, SP-TPC) has a central fuel tank just before the cockpit. Another case (SP-RAM) has a central tank like the prototype, but it is augmented by an add-on tank below the fuselage, thus extending the maximum usable fuel to approx. 120l. Newer models (SP-TPE, SP-TPF) have one tank in each of their wings for a total usable fuel of approx. 100-110l. 2620:10D:C093:500:0:0:6:AA4 (talk) 16:29, 25 June 2024 (UTC)[reply]