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This template has provisions for four sections: General characteristics, performance, armament, and avionics. What follows is list of the parameters that appear in each section, and specialised instructions for their use where necessary.
Template:Aircraft specs displays aircraft specifications, automatically formatted and converted for either metric or imperial units. Usage A "note" parameter is available for every parameters for qualifying the entry.
This template is used on approximately 12,000 pages and changes may be widely noticed. Test changes in the template's /sandbox or /testcases subpages, or in your own user subpage . Consider discussing changes on the talk page before implementing them.
[[Category:Aircraft specs templates]] to the <includeonly> section at the bottom of that page. Otherwise, add <noinclude>[[Category:Aircraft specs templates]]</noinclude> to the end of the template code, making sure it starts on the same line as the code's last character.
Data from source name General characteristics Crew: one pilot Capacity: lots of passengers Length: 20 m (65 ft 7 in) nose probe to tail light Wingspan: 30 m (98 ft 5 in) with extra tips Height: 5 m (16 ft 5 in) to top of rudder Airfoil: NACA something Empty weight: 5,000 kg (11,023 lb) absolutely dry Gross weight: 7,500 kg (16,535 lb) all up Max takeoff weight: 7,800 kg (17,196 lb) if you must ...
There are 200 articles in Category:Aircraft specs templates using afterburner without dry parameter but most (possibly all) have dry thrust values By experimenting the template is looking for completed hp (horsepower), shp (shaft horsepower) and kW (metric power) parameters, none of these apply to jet engines. I believe that if those three ...
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