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Standard

Flight Deck Head-Up Displays
2007-07-10
CURRENT
ARP4102/8A
This SAE Aerospace Recommended Practice (ARP) recommends criteria for the design and installation of Head-Up Display (HUD) systems. The recommendations are applicable to HUD systems for transport category aircraft, which display flight information (focused at infinity) in the forward field of view. The HUD total system requirement recommendations shall primarily lead to certifiable fail-passive CAT III characteristics and performance. This document forms a part of these recommendations. This document does not address devices for peripheral vision of displays worn by the pilot, nor the presentation of Enhanced Vision System (EVS) information.
Standard

FLIGHT DECK, HEAD-UP DISPLAYS
1994-05-01
HISTORICAL
ARP4102/8
This document recommends criteria for the design and installation of Head-Up Display (HUD) systems. The recommendations are applicable to HUD systems which display flight information focused at infinity in the forward field of view. This annex does not address devices for peripheral vision or displays worn by the pilot (goggles, helmet sights).
Standard

Flight Management System (FMS)
2021-01-14
CURRENT
ARP4102/9B
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 design shall take human factors considerations into account to produce a fault tolerant system.
Standard

FLIGHT MANAGEMENT SYSTEM (FMS)
1995-05-01
HISTORICAL
ARP4102/9
This document recommends criteria and requirements for a Flight Management System (FMS) for transport aircraft.
Standard

Flight Management System (FMS)
2007-07-10
HISTORICAL
ARP4102/9A
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 design shall take Human Factors considerations into account to produce a fault tolerant system.
Standard

Flight Envelope Awareness/Protection
2007-07-11
CURRENT
ARP4104/1
This annex recommends additional design objectives applicable when control laws or control characteristics are modified for the purpose of Flight Envelope Awareness/Protection. While only manually controlled flight is addressed, it is assumed that Autoflight, Autothrottle, or Autothrust performance is compatible.
Standard

AIRBORNE WINDSHEAR SYSTEMS
1989-11-01
HISTORICAL
ARP4102/11A
This document recommends criteria for Airborne Windshear Systems, including operational objectives, characteristics, and functional requirements. The recommendations of this document apply to transport aircraft, and describe the operational objectives of windshear alerting systems, situational displays, guidance systems, and detection/avoidance systems.
Standard

AIRBORNE WINDSHEAR SYSTEMS
1988-07-01
HISTORICAL
ARP4102/11
This document recommends criteria for Airborne Windshear Systems, including operational objectives, characteristics and functional requirements. The recommendations of this document apply to transport aircraft, and describe the operational objectives of Windshear warning devices, situational displays, guidance systems and detection/avoidance systems.
Standard

Airborne Windshear Systems
2007-07-11
CURRENT
ARP4102/11C
This document recommends criteria for Airborne Windshear Systems, including operational objectives, characteristics, and functional requirements. The recommendations in this document apply to transport aircraft, and describe the operational objectives of windshear alerting systems, situational displays, guidance systems, and avoidance/ detection systems.
Standard

Airborne Windshear Systems
1993-06-29
HISTORICAL
ARP4102/11B
This document recommends criteria for Airborne Windshear Systems, including operational objectives, characteristics, and functional requirements. The recommendations of the document apply to transport aircraft, and describe the operational objectives of windshear alerting systems, situational displays, guidance systems, and avoidance/detection systems.
Standard

Approach to Landing Guidance System for Transport Aircraft
2020-06-11
CURRENT
ARP4102/12B
This document specifies requirements for an Approach to Landing Guidance System (ALGS) electronic device. This equipment shall display relative aircraft position and situation information for flight along precision three-dimensional paths within the appropriate coverage area. The precision three-dimensional path may be an ILS straight-in look-alike path or a complex, curved path. The requirements are applicable to electronic devices capable of receiving signals or other information from one or more sources, including but not limited to ILS, GNSS, or IRU inputs.
Standard

Airborne Landing Guidance System for Transport Aircraft
2008-06-04
HISTORICAL
ARP4102/12A
This document specifies requirements for an Airborne Landing Guidance System (ALGS) electronic device. This equipment shall derive relative aircraft position and situation information for flight along precision three-dimensional paths within the appropriate coverage area. The precision three-dimensional path may be an ILS straight-in look-alike path or a complex, curved path. The requirements are applicable to electronic devices capable of receiving signals or other information from one or more sources, including but not limited to ILS, MLS, GNSS, or IRU inputs.
Standard

Takeoff Performance Monitor (TOPM) System, Airplane, Minimum Performance Standard for
2020-05-15
CURRENT
AS8044A
This Aerospace Standard (AS), establishes minimum performance standards for those sensors, computers, transponders, and airplane flight deck controls/displays which together comprise a Takeoff Performance Monitor (TOPM) System. This standard also defines functional capabilities, design requirements, and test procedures. A TOPM system is intended to monitor the progress of the takeoff and to provide advisory information which the crew may use in conjunction with other available cues to decide to continue or abort the takeoff. See Appendix A for supplementary information relating to NTSB, CAA, and ad hoc committee concerns and background information.
Standard

NOMENCLATURE AND ABBREVIATIONS FOR USE ON THE FLIGHT DECK
1994-05-01
CURRENT
AS425C
This Standard is intended to establish preferred abbreviations for use on panels, controls, instruments, displays, placards and markings. The recommendations apply to terms used in the flight deck of transport aircraft. The abbreviations, symbols and codes do not supersede those used in airworthiness regulations or aeronautical charts and documents. Where conflict is possible the operational context must be such as to resolve any ambiguity. If doubt exists, an alternative abbreviation or less truncated abbreviation should be used.
Standard

Stowage of Flight Crew’s Survival Emergency and Miscellaneous Equipment
2007-07-10
HISTORICAL
ARP4101/6
This document recommends general specifications for the location, accessibility and restraint for those items of survival, emergency, and miscellaneous equipment which are intended to be used by the flight crew, and which are stowed on or near the flight deck.
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