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Drivmatic Retrofit Northrop Grumman Corporation

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Latimer, Michael, author.
Conference Name:
Aerofast Conference & Exposition (1994-10-24 : Montreal, Canada)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1994
Summary:
Fuselage panels for the Boeing 747 aircraft have been assembled at the Northrop Commercial Aircraft Division Alameda (D2) facility since the mid 1960's. The assembly work has been accomplished using Gemcor CNC Drivmatic systems. These systems have performed reliably since their initial installation in the late 1960's, but have recently begun to show their age.In 1992, the decision was made to establish a project that would direct the retrofit of these systems to state-of-the-practice condition.This paper will discuss the planning, scheduling and specification development for that project
Notes:
Vendor supplied data
Publisher Number:
941838
Access Restriction:
Restricted for use by site license

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