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Purpose: This document is intended to provide design guidance for the development and installation of an Enhanced Airborne Flight Recorder (EAFR). The EAFR standard addresses combinations of any or all of the following in a single Line Replaceable Unit (LRU), a Digital Flight Data...
This document recommends criteria for the design and installation of Autopilot, Flight Director and Autothrust Systems. These three systems are highly interrelated and will be referred to generically as an Integrated Flight Guidance System (IFGS).
This SAE Aerospace Information Report (AIR) provides a description of the interfaces and their requirements for generic and specific hydraulic actuation systems used in the flight control systems of manned aircraft. Included are the basic control system...
This SAE Aerospace Information Report (AIR) provides a description of the interfaces and their requirements for generic and specific hydraulic actuation systems used in the flight control systems of manned aircraft. Included are the basic control system...
PREFACE Instrument flight procedures based on conventional ground-based navigation aids have always necessitated a high level of quality control. However, with the implementation of area navigation and associated airborne database navigation systems, even small errors in data could...
Purpose: This document is the specification of a generic interface to be used between avionics computing equipment that exchange binary message-oriented data. Several avionics architectures have been considered. For example, the interface could be used between an Flight...
This document recommends criteria and requirements for a Flight Management System (FMS) for transport aircraft.
This document recommends criteria and requirements for a flight management system (FMS) for transport aircraft. The FMS shall provide the functions of lateral navigation, vertical navigation, and performance management and may include time of arrival control. The FMS...
The emerging ultra high bypass ratio ADP engines, with nozzle pressure ratios significantly lower, and bypass ratios significantly higher, than those of the current turbofan engines, may present new in-flight thrust determination challenges that are not specifically covered in AIR1703. This...
Purpose: This document sets forth the characteristics of a Flight Management Computer System specifically designed for installation in new generation commercial transport aircraft. The system is not designed for retrofit in any aircraft other than those utilizing ARINC...
This document recommends criteria and requirements for a Flight Management System (FMS) for transport aircraft. The FMS shall provide the functions of Lateral Navigation, Vertical Navigation, and Performance Management and may include Time of Arrival Control. The FMS...
The purpose of this document is to describe the recommendations of SAE Committee S-7 for a Flight Management Computer System (FMCS) capable of providing the functions and displays listed below to permit completion of a desired flight plan in an energy efficient and/or...
This document establishes the requirements for simulation of the space control system, including the objective, architecture and procedure, etc. This document is applicable to four phases of control system development, including conceptual design, detailed design, prototype and...
This document reflects the joint FAA and industry view of how the air traffic management system will operate in three timefrarnes: near-term, mid-term, and far-term or mature state. For each concept described, the respective roles and responsibilities of the participants in that...
The information contained in this document is based on line experience with current systems. It should be used as a basis for ongoing research and development including the human factors aspects of future flight management systems and their interaction with the ATC...
Purpose and Scope This document sets forth the characteristics of an advanced Flight Management Computer System (FMS) specifically designed for installation in new generation aircraft. The system is also intended for retrofit in aircraft that presently use ARINC 700...
Purpose of this Document This specification defines general architectural philosophy and specific design guidance for the proper installation and interface of various cabin equipment within the seats. Consistency with this specification allows each component installed on the seat to operate in...
SCOPE OF THE DOCUMENT This document includes the definition of the services and the Environmental Conditions relevant to the implementation of the ASPA-FIM System and the operational, safety, performance and interoperability requirements for IM Applications. NOTE: Requirements that provide...
