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Horizontal lifeline systems require careful engineering due to the specific nature of the structures they are designed for, ensuring safety in high-risk areas. [ 3 ] Lifeline wire has traditionally been available in 1/8" ( 3.175 mm) and 3/16" ( 4.763 mm) wire diameters, with a soft but durable vinyl coating increasing the effective diameters to ...
Some of Honeywell's systems were minicomputers, such as their Series 60 Model 6 and Model 62 [28] [29] and their Honeywell 200. The latter was an attempt to penetrate the IBM 1401 market. In 1987, HIS merged with Groupe Bull , a global joint venture with Compagnie des Machines Bull of France and NEC Corporation of Japan to become Honeywell Bull.
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At the time of its IPO in 1983, Lifeline Systems reported programs at 528 hospitals and other healthcare providers, and had shipped 21,931 subscriber units. [8] To service growth, Lifeline developed high-capacity PERS call center technology and offered central monitoring to its customers. [7] Arthur Phipps became CEO 1989–1992.
Bull SAS (also known as Groupe Bull, Bull Information Systems, or simply Bull) is a French computer company headquartered in Les Clayes-sous-Bois, in the western suburbs of Paris. The company has also been known at various times as Bull General Electric , Honeywell Bull , CII Honeywell Bull , and Bull HN .
During the 1990s, a series of issues affecting the rudder of Boeing 737 passenger aircraft resulted in multiple incidents. In two separate accidents (United Airlines Flight 585 and USAir Flight 427), pilots lost control of their aircraft due to a sudden and unexpected rudder movement, and the resulting crashes killed everyone on board, 157 people in total. [1]
It is produced by Honeywell Aerospace, a division of Honeywell based in Phoenix, Arizona, and was originally designed by the Turbine Engine Division of Lycoming Engines in Stratford, Connecticut, as a scaled-up version of the smaller Lycoming T53. The T55 serves as the engine on several major applications including the CH-47-Chinook, the Bell ...
"EVS Enhanced Vision System" is an industry-accepted term which the FAA decided not to use because "the FAA believes [it] could be confused with the system definition and operational concept found in 91.175(l) and (m)" [21] In one EVS installation, the camera is actually installed at the top of the vertical stabilizer rather than "as close as ...
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