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In February 1976, work commenced to automate the methods contained in the USAF Stability and Control DATCOM, specifically those contained in sections 4, 5, 6 and 7.The work was performed by the McDonnell Douglas Corporation under contract with the United States Air Force in conjunction with engineers at the Air Force Flight Dynamics Laboratory in Wright-Patterson Air Force Base.
The Spitfire wing may be classified as: "a conventional low-wing cantilever monoplane with unswept elliptical wings of moderate aspect ratio and slight dihedral".. The wing configuration or planform of a fixed-wing aircraft (including both gliders and powered aeroplanes) is its arrangement of lifting and related surfaces.
Aircraft wing configurations are one of the major aspects of an aircraft's design and are a primary feature in aircraft recognition. Subcategories This category has the following 16 subcategories, out of 16 total.
The software to run this is included on a CD-ROM that comes with the plane. This has been upgraded to an EDI card (engine Data Information). This card is a memory card much like in a digital camera, and records all engine data from 0 hours, until the 2000 hour TBO and can be read with a card reader to diagnose problems and observe flight ...
The Maneuvering Characteristics Augmentation System (MCAS) is a flight stabilizing feature developed by Boeing that became notorious for its role in two fatal accidents of the 737 MAX in 2018 and 2019, which killed all 346 passengers and crew among both flights.
Software updates planned for Boeing Inc.’s troubled 737 Max 8 aircraft, grounded worldwide after two deadly crashes, may not be enough to satisfy critics.
Composite aircraft allow the individual components to continue flying independantly - OTOH the top wing of the slip wing would have glided/crashed to the ground after release and lacked any controls (no ailerons, flaps or even a vertical stabilizer) - not the same as the Pemberton Billing "slip wing" which were just another name for a parasite ...
When production of the earlier Martin 2-0-2 was stopped due to problems with wing structural failure the company decided to re-wing an improved version (which had already flown as the Martin 3-0-3). The new aircraft was the Martin 4-0-4 .