Standard
Harmonizing weather information sharing for air transport
2016-01-25
WIP
AIR6373
pilots, air traffic controllers, dispatchers, aviation meteorologists
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Standard
Display Latency Evaluation Procedures
2012-12-03
WIP
ARP6238
This Aerospace Recommended Practice will identify the problem with latency in the pilot's instrument control of an aircraft. Recommended evaluation techniques to characterize control problems will be documented.
Standard
Flight Deck Head-Up Displays
2007-07-10
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
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
Instrument Panel Arrangement for Fixed Wing Aircraft Under 12,500 Lb.
2002-12-16
ARP1166
Standard
Flight Deck Environment
2002-12-16
ARP1411
This Aerospace Recommended Practice (ARP) is intended to specify the environmental conditions necessary to permit the operating crew of large civil transport aircraft to perform their required duties and functions in comfort, with minimum fatigue and no distraction. Environmental conditions should cause no short or long-term effects deleterious to health or physical well being, nor significantly impair ability to perform normal flight deck crew functions.
Standard
Flight Management Computer System
2002-12-16
ARP1570
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 cost effective manner while meeting the requirements of Air Traffic Control. The recommendations of this document apply to transport aircraft and describe the operational objectives of the FMCS and related controls and displays.
Standard
On-Board Weight and Balance System
2022-03-17
ARP4102/1A
This document recommends criteria for the flight deck display of an On Board Weight and Balance System. The system may have the capability of a primary operational device or be a secondary advisory source of information of weight and center of gravity position. The recommendations apply to transport aircraft and describe the operational and functional requirements for the display of an On Board Weight and Balance System.
Standard
On Board Weight and Balance System
2004-06-23
ARP4102/1
This document recommends criteria for the flight deck display of an On Board Weight and Balance System. The system may have the capability of a primary operational device or be a secondary advisory source of information of weight and center of gravity position. The recommendations apply to transport aircraft and describe the operational and functional requirements for the display of an On Board Weight and Balance System.
Standard
Flight Management System (FMS)
2021-01-14
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
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
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 Management Systems Review
2017-01-04
AIR4653
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 environment.
Standard
Flight Envelope Awareness/Protection
2011-08-23
WIP
ARP4104/1A
This anex 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 Autoflfight, Autothrottle, or Autothrust performance is compatible.
Standard
Flight Envelope Awareness/Protection
2007-07-11
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
Design Objectives for Handling Qualities of Transport Aircraft
2011-08-23
WIP
ARP4104A
This document specifies the requirements for the design objectives for handling qualities applicable to transport aircraft operating in the subsonic, transonic, and supersonic speed range. These objectives are not necessarily applicable to rotor or VTOL aircraft.
Standard
Data Link
2016-09-28
WIP
ARP4102/13B
This document recommends criteria for a system designed to manage and communicate information via data link to support flight operations.
Standard
DATA LINK
2007-07-11
ARP4102/13A
This document recommends criteria for a system designed to manage and communicate information via data link to support flight operations.
Standard
AIRBORNE WINDSHEAR SYSTEMS
1989-11-01
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
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.
