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Standard

Pilot Visibility From the Flight Deck

2019-02-28
WIP
ARP4101/2A
This document recommends criteria to assure adequate visibility from the flight deck. The flight deck windshield must provide sufficient external vision to permit the pilot to perform any maneuvers within the operating limits of the aircraft safely and at the same time afford and unobstructed view of the flight instruments and other critical components and displays from the same eye position.
Standard

Pilot Visibility From The Flight Deck

1989-02-01
CURRENT
ARP4101/2
This document recommends criteria to assure adequate visibility from the flight deck. The flight deck windshield must provide sufficient external vision to permit the pilot to perform any maneuvers within the operating limits of the aircraft safely and at the same time afford an unobstructed view of the flight instruments and other critical components and displays from the same eye position.
Standard

On Board Weight and Balance System

1988-07-01
CURRENT
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

Full-Format Printer

2012-07-31
CURRENT
ARP4102/14C
This document recommends criteria for the installation and operation of a printer intended for use by flight crew members on the flight deck. The printer is used to supply the flight crew with hard copies of information that originates from data sources such as FMS, EDMS, ACMS, CMS, and data link. These criteria are in addition to the specifications of the referenced ARINC Characteristic 744A.
Standard

Full-Format Printer

2000-04-01
HISTORICAL
ARP4102/14B
This document recommends criteria for the installation and operation of a printer intended for use by flight crew members on the flight deck. The printer is used to supply the flight crew with hard copies of information that originates from data sources such as FMS, EDMS, ACMS, CMS, and data link. These criteria are in addition to the specifications of the referenced ARINC Characteristic 744A.
Standard

Flight Management Systems Review

1995-08-01
CURRENT
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 Management System (FMS)

2001-12-14
CURRENT
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

1993-06-01
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

Flight Deck Head-Up Displays

1998-11-01
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 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

Electronic Data Management System (EDMS)

2000-07-01
CURRENT
ARP4102/15A
This SAE Aerospace Recommended Practice (ARP) recommends criteria for an Electronic Data Management System (EDMS) for use on the flight deck of transport aircraft. The EDMS may be the primary, and in some cases sole, on board source of documentation and information for flight operations, engineering, aircraft maintenance, cabin services, and training. This document addresses flight operations applications only. It addresses the requirements for the flight deck characteristics of airborne equipment elements for an Electronic Data Management System (EDMS), but not the ground support system requirements. Development of ground support systems for EDMS will be a significant task, which must take account of the end-user information handing requirements specified here. An Electronic Library System (ELS) is a partial implementation of EDMS, which incorporates only the data storage, retrieval and display functions.
Standard

Design Objectives for Handling Qualities of Transport Aircraft

1988-07-01
CURRENT
ARP4104
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

Autopilot, Flight Director, and Autothrust Systems

2001-10-01
CURRENT
ARP5366
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).
Standard

Automatic Braking System (ABS)

1988-07-01
HISTORICAL
ARP4102/2
This document recommends design criteria for an Automatic Braking System. The ABS shall enhance braking performance under most aircraft configurations and all runway conditions.
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

Airborne Windshear Systems

2002-10-21
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

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.
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