Airframes Unlimited T-103
It is proposed that this article be deleted because of the following concern:
If you can address this concern by improving, copyediting, sourcing, renaming, redirecting, or merging the page, please edit this page and do so. You may remove this message if you improve the article or otherwise object to deletion for any reason. Although not required, you are encouraged to explain why you object to the deletion, either in your edit summary or on the talk page. If this template is removed, do not replace it. The article may be deleted if this message remains in place for seven days, i.e., after 19:54, 4 October 2026 (UTC). Find sources: "Airframes Unlimited T-103" – news · newspapers · books · scholar · JSTOR Nominator: Please consider notifying the author/project: {{subst:proposed deletion notify|Airframes Unlimited T-103|concern=[[WP:DEL8]]: No sources of [[WP:N|notability]] in article or available on the web. This article is a collection of facts from directories and the product's manufacturer as its only sources. These uncontroversial deletions are [[User talk:Ahunt#Proposed deletion of Airborne Redback|not opposed by the original author]] after notification. Relevant: [[WP:NOTDIRECTORY]] and [[Wikipedia:Articles for deletion/Ozone Peak|this AfD nomination]].}} ~~~~ |
| T103 | |
|---|---|
| General information | |
| Type | Powered parachute |
National origin | United States |
| Manufacturer | Airframes Unlimited |
| Status | In production |
The Airframes Unlimited T-103 is an American powered parachute designed and produced by Airframes Unlimited of Athens, Texas.[1][2]
The aircraft was originally offered as plans only by Powered Parachute Plans, also of Athens, Texas. When parts for complete aircraft were made available these were supplied by Airframes Unlimited and gradually the two enterprises were unified under the latter name.[1][2]
Design and development
[edit]The aircraft was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 254 lb (115 kg). The manufacturer says "The T-103 can be built to be part 103 compliant without any trouble." It features a parachute-style high-wing, two-seats-in-tandem, tricycle landing gear and accepts a wide variety of two stroke and four stroke engines mounted in pusher configuration.[1][3]
The aircraft is built from welded 4130 steel tubing, with a 6061-T6 aluminum engine mount plate. In flight steering is accomplished via levers that actuate the canopy brakes, creating roll and yaw. On the ground the aircraft has lever-controlled nosewheel steering. The main landing gear incorporates spring rod suspension. The design uses an overhead adjustable canopy hang point, called a "cg spreader bar" to establish the correct canopy attachment point and hence the aircraft's flight attitude and torque offset.[1]
The aircraft was originally supplied only in the form of illustrated plans provided on a CD-ROM in Microsoft Word .doc format. Later parts and sub-assemblies were made available and then complete carriages, less canopy, propeller and engine.[1][3]
Specifications (T103)
[edit]| This aircraft article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them. |
References
[edit]- 1 2 3 4 5 Cliche, Andre: Ultralight Aircraft Shopper's Guide 8th Edition, page D-19. Cybair Limited Publishing, 2001. ISBN 0-9680628-1-4
- 1 2 Chalmers, Buzz (n.d.). "Powered Parachute Ultralights for the Budget-Minded". Light Sport and Ultralight Flying Magazine. Archived from the original on December 11, 2013. Retrieved March 25, 2012.
- 1 2 Airframes Unlimited (March 1, 2012). "Plans". Retrieved March 25, 2012.