Standard

SAE ARP4033

Feb 2008 Withdrawn

Existing or new amendments and versions must be purchased separately.

Language English

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Abstract

A recommended pilot-system integration (i.e., crew interface and system integration) approach for concept development is described in Figure 1 . The approach emphasizes the fundamental need for a top-down design methodology with particular focus on clear operational performance requirements and functional integration. While this document is primarily aimed at aircraft systems design and integration, the methodology is applicable to a wide range of design and integration situations. It is derived from well established human factors engineering design principles.

Products specifications

Standard from SAE International
Published: February 16 2008
Withdrawn: November 3 2020
Document type: IS
Pages
ISBN:

Publisher: SAE International
Distributor: SAE International

Product Relations

Referred by: SAE ARP5898A
Referred by: SAE ARP5430A
Referred by: SAE ARP5364A
Referred by: SAE ARP5119A
Referred by: SAE ARP5365A
Replaced by: SAE ARP4033A
Referred by: SAE ARP5056A
Referred by: SAE ARP5740
Referred by: SAE ARP4032B
Referred by: SAE ARP5898
Referred by: SAE ARP5430
Referred by: SAE ARP5056
Referred by: SAE ARP5119
Refers: SAE ARP4107
Referred by: SAE ARP5365
Referred by: SAE ARP4102/15A
Referred by: SAE ARP5589
Referred by: SAE ARP5364
Refers: SAE ARP4155

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Abstract

Products specifications

Product Relations