Structural Design Sample Clauses
The Structural Design clause defines the responsibilities and standards for creating the structural elements of a project. It typically outlines the requirements for design calculations, compliance with relevant codes and regulations, and the submission of drawings or plans for approval. This clause ensures that the structural aspects of a building or infrastructure are safely and properly engineered, thereby minimizing the risk of design errors and ensuring the integrity and safety of the completed structure.
POPULAR SAMPLE Copied 1 times
Structural Design. 16 The A/E shall perform structural design, calculations 17 and drawings for retaining walls, box culverts, etc. All 18 structural calculations shall conform to the OC Public Works 19 standards and guidelines.
Structural Design. Each floor contains fifty (50) pounds of “live load” per square foot.
Structural Design. The Aircraft is a swept-wing monoplane with a pressurized cabin and is capable of accommodating a pilot, a co-pilot, a third crewmember and up to 19 passengers. The Aircraft structure, in general, is fabricated from aluminum alloy but also includes alloy steels, stainless steel, titanium and composites. Materials used are in accordance with standard U.S. aerospace industry specifications for aircraft quality materials. The Aircraft structure and systems are designed and installed to facilitate inspection, maintenance and permit ready removal of appropriate items. Parts and assemblies subject to ready removal from the Aircraft are interchangeable and/or replaceable from one BD-700-1A10 aircraft to another where Seller considers this practical. The Aircraft and its installed equipment is certified to operate at ground level ambient temperatures from -30ºC (-22ºF) to +45ºC (+113ºF). The Aircraft pressurization system is certificated for operations up to a maximum of pressure altitude of 51,000 ft.
Structural Design. Develop detailed design for new facilities and modifications to existing facilities structures and related equipment lifting and superstructure components, as needed for a complete functional facility.
Structural Design. The Aircraft is a swept-wing monoplane with a pressurized cabin and is capable of accommodating a pilot, a co-pilot, a third crewmember and up to 19 additional occupants. The Aircraft structure, in general, is fabricated from aluminum alloy but also includes alloy steels, stainless steel, titanium and composites. The Aircraft structure and systems are designed and installed to facilitate inspection, maintenance and permit ready removal of appropriate items. Parts and assemblies subject to ready removal from the Aircraft are interchangeable and/or replaceable from one BD-700-1A10 aircraft to another where Seller considers this practical.
Structural Design. Based on the accepted structural system, establish final structural design criteria, foundation design criteria, bay spacing and other dimensions, preliminary sizing of major structural components and critical coordination clearances.
Structural Design. Consultant shall develop a 30% structural design based upon previous reports and their own assessment. Design shall incorporated seismic retrofitting, concrete and reinforcement repair, crack repair, material design, types and strengths, coating requirements, and anchoring. Access, including outlet box, stairways, bridges, ladders, grating, and walkways shall be included as part of the structural design.
Structural Design. All bridge design shall be in conformance with the latest edition of the State’s LRFD Bridge Design Manual, Bridge Project Development Manual, Bridge Detailer’s Manual, and AASHTO LRFD Bridge Design Specifications (HL 93 Loading).
Structural Design. Structural design of the equipment foundation, and supports is covered by this task. Contract drawings and specifications for the structural work shall be prepared;
Structural Design a. No structural assumed for design in this scope of work