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FAA - General
1800-8F, NATIONAL AIRSPACE CONFIGURATION MGMT
1800.8F, NATIONAL AIRSPACE CONFIGURATION MANAGEMENT (May 20, 1991). This order prescribes configuration management (CM) policy, delegates authority, and assigns responsibility for CM of the development, installation, and maintenance of the national Airspace System (NAS).
Ident. Num:
1800.8
Rev. Num:
F
1800.8F, NATIONAL AIRSPACE CONFIGURATION MANAGEMENT (May 20, 1991). This order prescribes configuration management (CM) policy, delegates authority, and assigns responsibility for CM of the development, installation, and maintenance of the national Airspace System (NAS).
DOT/FAA/AR-07/39, REAL-TIME OPERATING SYSTEMS AND COMPONENT INTEGRATION CONSIDERATIONS IN INTEGRATED MODULAR AVIONICS SYSTEMS REPORT (AUG 2007) (FINAL
DOT/FAA/AR-07/39, REAL-TIME OPERATING SYSTEMS AND COMPONENT INTEGRATION CONSIDERATIONS IN INTEGRATED MODULAR AVIONICS SYSTEMS REPORT (AUG 2007) (FINAL REPORT)., The combination of rigorous development assurance and verification assurance has led to safe and reliable operation within civil aviation systems and equipment. Historically, such systems were designed as federated architectures, yet significantly successful efforts in integrated modular avionics (IMA) system integration have occurred, such as the Boeing 777 aircraft. This technical report can be used to formulate a basis for evaluating the integration of real-time operating systems (RTOS) and other associated modules that support partitioning in space, time, input/output, communications, and other shared resources on an IMA system. Several role players (platform supplier, RTOS supplier, application supplier, and the IMA system integrator) in IMA system development are discussed, and their roles of integrating multiple functions at different integration stages are detailed. [Key Words Integrated Modular Avionics, Software, DO-178, DO-297, RTOS, Partitioning]
Ident. Num:
DOT/FAA/AR-07/39
Rev. Num:
-
DOT/FAA/AR-07/39, REAL-TIME OPERATING SYSTEMS AND COMPONENT INTEGRATION CONSIDERATIONS IN INTEGRATED MODULAR AVIONICS SYSTEMS REPORT (AUG 2007) (FINAL REPORT)., The combination of rigorous development assurance and verification assurance has led to safe and reliable operation within civil aviation systems and equipment. Historically, such systems were designed as federated architectures, yet significantly successful efforts in integrated modular avionics (IMA) system integration have occurred, such as the Boeing 777 aircraft. This technical report can be used to formulate a basis for evaluating the integration of real-time operating systems (RTOS) and other associated modules that support partitioning in space, time, input/output, communications, and other shared resources on an IMA system. Several role players (platform supplier, RTOS supplier, application supplier, and the IMA system integrator) in IMA system development are discussed, and their roles of integrating multiple functions at different integration stages are detailed. [Key Words Integrated Modular Avionics, Software, DO-178, DO-297, RTOS, Partitioning]
DOT/FAA/AR-MMPDS-01, Metallic Materials Properties Development and Standardization (MMPDS)
DOT/FAA/AR-MMPDS-01, Metallic Materials Properties Development and Standardization (MMPDS). The Metallic Material Properties Development and Standardization (MMPDS) Handbook is the replacement document for MILHDBK- 5. It is recognized internationally as a reliable source of aircraft materials data for aerospace materials selection and analysis. Consistent and reliable methods are used to collect, analyze, and present statistically based material and fastener allowable properties. The Handbook is the only publicly available source in the U.S. for material allowables that the Federal Avaiation Administration generally accepts for compliance with Federal Aviation Regulations (FAR) for material strength properties and design values for aircraft certification and continued airworthiness. Moreover, it is the only publicly available source worldwide for fastener joint allowables that comply with the FARs. This edition, MMPDS-01, incorporates the additions and changes to aircraft metallic material design properties and analysis guidelines approved at the 1st and 2nd MMPDS government/industry coordination meetings. This year, 2003, marks the first year of publication of the MMPDS Handbook and the final year of publication of MIL-HDBK-5. For this year only, MMPDS-01 and MIL-HDBK-5J will be technically equivalent. In the spring of 2004, when the 1st Change Notice of MMPDS-01 is published, MIL-HDBK-5 will be designated noncurrent and MMPDS will become the only governmentrecognized source in the U.S. of published design allowable properties for metallic commercial and military aircraft structures and mechanically fastened joints. In this way, the 65-year legacy of MIL-HDBK-5, and its predecessor ANC-5, will be maintained.
Ident. Num:
DOT/FAA/AR-MMPDS-01
DOT/FAA/AR-MMPDS-01, Metallic Materials Properties Development and Standardization (MMPDS). The Metallic Material Properties Development and Standardization (MMPDS) Handbook is the replacement document for MILHDBK- 5. It is recognized internationally as a reliable source of aircraft materials data for aerospace materials selection and analysis. Consistent and reliable methods are used to collect, analyze, and present statistically based material and fastener allowable properties. The Handbook is the only publicly available source in the U.S. for material allowables that the Federal Avaiation Administration generally accepts for compliance with Federal Aviation Regulations (FAR) for material strength properties and design values for aircraft certification and continued airworthiness. Moreover, it is the only publicly available source worldwide for fastener joint allowables that comply with the FARs. This edition, MMPDS-01, incorporates the additions and changes to aircraft metallic material design properties and analysis guidelines approved at the 1st and 2nd MMPDS government/industry coordination meetings. This year, 2003, marks the first year of publication of the MMPDS Handbook and the final year of publication of MIL-HDBK-5. For this year only, MMPDS-01 and MIL-HDBK-5J will be technically equivalent. In the spring of 2004, when the 1st Change Notice of MMPDS-01 is published, MIL-HDBK-5 will be designated noncurrent and MMPDS will become the only governmentrecognized source in the U.S. of published design allowable properties for metallic commercial and military aircraft structures and mechanically fastened joints. In this way, the 65-year legacy of MIL-HDBK-5, and its predecessor ANC-5, will be maintained.
FAA-C-2621A, Design and Fabrication of Antenna Support Towers
This specification sets forth requirements for the design and fabrication of self=supporting and guyed antenna support towers and the associated tower concrete foundations.
Ident. Num:
FAA-C-2621
Rev. Num:
A
This specification sets forth requirements for the design and fabrication of self=supporting and guyed antenna support towers and the associated tower concrete foundations.
FAA-C-2760, Design and Fabrication of Antenna Towers for Radio Communications Link
This specification covers design and fabrication of steel antenna towers for a point-to-point radio communications system.
Ident. Num:
FAA-C-2760
This specification covers design and fabrication of steel antenna towers for a point-to-point radio communications system.
FAA-G-2100G, Application Handbook for FAA-G-2100G Electronic Equipment, General Requirements,
he FAA-G-2100g Guide provides assistance to the Integrated Product Teams (IPT) to capture all the necessary/applicable requirements from FAA-G-2100g and to demonstrate how the requirements should be stated in the System Level Specifications (SLS). The requirements set contained in Section 3 of FAA-G-2100stated in the SLS.
Ident. Num:
FAA-G-2100G Application Handbook
Rev. Num:
2
he FAA-G-2100g Guide provides assistance to the Integrated Product Teams (IPT) to capture all the necessary/applicable requirements from FAA-G-2100g and to demonstrate how the requirements should be stated in the System Level Specifications (SLS). The requirements set contained in Section 3 of FAA-G-2100stated in the SLS.
FAA-G-2100H, Electronic Equipment, General Requirements, Specification
This specification is the technical baseline for ground based electronic equipment acquired for applications in the National Airspace System (NAS). This specification defines the conditions under which electronic equipment must operate satisfactorily and reliably: identifies acceptable fabrication materials and processes, selection and application of parts, installation of equipment, and methods to verify electronic equipment meets requirements. Individual electronic equipment specifications must identify applicable requirements of this specification. This specification is intended for use in the procurement of all electronics hardware, prototype systems, developmental equipment or commercial off the shelf integrated systems, delivered in any quantity to satisfy an established air traffic need or proof of concept configuration.
Ident. Num:
FAA-G-2100
Rev. Num:
H
This specification is the technical baseline for ground based electronic equipment acquired for applications in the National Airspace System (NAS). This specification defines the conditions under which electronic equipment must operate satisfactorily and reliably: identifies acceptable fabrication materials and processes, selection and application of parts, installation of equipment, and methods to verify electronic equipment meets requirements. Individual electronic equipment specifications must identify applicable requirements of this specification. This specification is intended for use in the procurement of all electronics hardware, prototype systems, developmental equipment or commercial off the shelf integrated systems, delivered in any quantity to satisfy an established air traffic need or proof of concept configuration.
FAA-H-8083-9, AVIATION INSTRUCTOR’S HANDBOOK (1999) [S/S AC 60-14 (1977), AC 61-101 (1989) and AC 61-115 (1995)]
FAA-H-8083-9, AVIATION INSTRUCTOR’S HANDBOOK (1999) [S/S AC 60-14 (1977), AC 61-101 (1989) and AC 61-115 (1995)].,The Aviation Instructor’s Handbook is designed for ground instructors, flight instructors, and aviation maintenance instructors. It is developed by the Flight Standards Service, Airman Testing Standards Branch in cooperation with aviation educators and industry. This handbook provides the foundation for beginning instructors to understand and apply the fundamentals of instructing. This handbook also provides aviation instructors with up-to-date information on learning and teaching, and how to relate this information to the task of conveying aeronautical knowledge and skills to students. Experienced aviation instructors also may find the new and updated information useful for improving their effectiveness in training activities. Chapters 1 through 5 concentrate on learning theory and the teaching process, emphasizing the characteristics of human behavior and the importance of communication. Chapters 6 and 7 provide valuable tools for critiquing and evaluating student performance and enhancing instructional presen- tations with teaching aids and new training technologies. Chapter 8 defines instructor responsibilities and emphasizes ways that instructors can develop and portray a professional image to their students. Chapter 9 contains useful information that can be applied when teaching in the aircraft, and also provides comprehensive treatment for teaching aeronautical decision making (ADM) and judgment. Chapters 10 and 11 provide valuable information for planning instructional activity and continuing professional development. his handbook supersedes AC 60-14, Aviation Instructor’s Handbook, dated 1977; AC 61-101, Presolo Written Test, dated 1989; and AC 61-115, Positive Exchange of Flight Controls, dated 1995.
Ident. Num:
FAA-H-8083-9
Rev. Num:
-
FAA-H-8083-9, AVIATION INSTRUCTOR’S HANDBOOK (1999) [S/S AC 60-14 (1977), AC 61-101 (1989) and AC 61-115 (1995)].,The Aviation Instructor’s Handbook is designed for ground instructors, flight instructors, and aviation maintenance instructors. It is developed by the Flight Standards Service, Airman Testing Standards Branch in cooperation with aviation educators and industry. This handbook provides the foundation for beginning instructors to understand and apply the fundamentals of instructing. This handbook also provides aviation instructors with up-to-date information on learning and teaching, and how to relate this information to the task of conveying aeronautical knowledge and skills to students. Experienced aviation instructors also may find the new and updated information useful for improving their effectiveness in training activities. Chapters 1 through 5 concentrate on learning theory and the teaching process, emphasizing the characteristics of human behavior and the importance of communication. Chapters 6 and 7 provide valuable tools for critiquing and evaluating student performance and enhancing instructional presen- tations with teaching aids and new training technologies. Chapter 8 defines instructor responsibilities and emphasizes ways that instructors can develop and portray a professional image to their students. Chapter 9 contains useful information that can be applied when teaching in the aircraft, and also provides comprehensive treatment for teaching aeronautical decision making (ADM) and judgment. Chapters 10 and 11 provide valuable information for planning instructional activity and continuing professional development. his handbook supersedes AC 60-14, Aviation Instructor’s Handbook, dated 1977; AC 61-101, Presolo Written Test, dated 1989; and AC 61-115, Positive Exchange of Flight Controls, dated 1995.
FAA-HR-001, HUMAN ENGINEERING PROGRAM PLAN
FAA-HR-001, HUMAN ENGINEERING PROGRAM PLAN. The Human Engineering Program Plan is the single document which describes the contractor’s entire human engineering program, identifies its elements, and explains how the elements will be managed.
Ident. Num:
FAA-HR-001
Rev. Num:
-
FAA-HR-001, HUMAN ENGINEERING PROGRAM PLAN. The Human Engineering Program Plan is the single document which describes the contractor’s entire human engineering program, identifies its elements, and explains how the elements will be managed.
NAS SR-1000A (Functional View), System Requirements Specifications
This document is the compilation of high-level requirements that describe the components and systems that make up the National Airspace System (NAS) today and into the future. In that context, requirements found in this document provide the basis of such activities on-going in the FAA such as the Operational Evolution Partnership (OEP) put in place to support transition to the next generation ATC system or (NEXGEN). OEP, NEXGEN and the Joint Planning and Development Office (JPDO) working together will deliver new systems and capabilities through the year 2025. This document is intended primarily for use as an internal FAA management tool to support the NAS enterprise architecture engineering, and acquisition activities and to manage and control change to the NAS.
Ident. Num:
NAS SR-1000
Rev. Num:
A
This document is the compilation of high-level requirements that describe the components and systems that make up the National Airspace System (NAS) today and into the future. In that context, requirements found in this document provide the basis of such activities on-going in the FAA such as the Operational Evolution Partnership (OEP) put in place to support transition to the next generation ATC system or (NEXGEN). OEP, NEXGEN and the Joint Planning and Development Office (JPDO) working together will deliver new systems and capabilities through the year 2025. This document is intended primarily for use as an internal FAA management tool to support the NAS enterprise architecture engineering, and acquisition activities and to manage and control change to the NAS.
NAS SR-1000A, System Requirements Specification
This document is the compilation of high-level requirements that describe the operational capability requirements to achieve the provisions of the act for the National Airspace System (NAS) as the NAS exists today and is envisioned to exist by the year 2017. In that context, it includes those existing and transitional system capabilities needed for the 2017 system. This document is intended primarily for use as an internal FAA management tool to support the NAS enterprise architecture engineering, and acquisition activities and to manage and control change to the NAS.
Ident. Num:
NAS-SR-1000
Rev. Num:
A
This document is the compilation of high-level requirements that describe the operational capability requirements to achieve the provisions of the act for the National Airspace System (NAS) as the NAS exists today and is envisioned to exist by the year 2017. In that context, it includes those existing and transitional system capabilities needed for the 2017 system. This document is intended primarily for use as an internal FAA management tool to support the NAS enterprise architecture engineering, and acquisition activities and to manage and control change to the NAS.
ORDER 1800-8F, NATIONAL AIRSPACE CONFIGURATION MGMT (MAY 20, 1991)
ORDER 1800-8F, NATIONAL AIRSPACE CONFIGURATION MGMT (MAY 20, 1991). This order prescribes configuration nanagement (CM) policy, delegates authority, and assigns responsibility for CM of the development, installation, and maintenance of the Nationat Airspace System (NAS).
Ident. Num:
1800-8
Rev. Num:
F
ORDER 1800-8F, NATIONAL AIRSPACE CONFIGURATION MGMT (MAY 20, 1991). This order prescribes configuration nanagement (CM) policy, delegates authority, and assigns responsibility for CM of the development, installation, and maintenance of the Nationat Airspace System (NAS).
