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Vehicle dynamics Entry, descent, and landing Engine components S-7 Flight Deck Handling Qualities Stds for Trans Aircraft

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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 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

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

Automatic Braking System (ABS)
2004-06-23
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

Automatic Braking System (ABS)
2012-07-31
CURRENT
ARP4102/2A
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

Autopilot, Flight Director, and Autothrust Systems
2017-01-04
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

Design Objectives for Handling Qualities of Transport Aircraft
2007-07-11
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

Electronic Data Management System (EDMS)
2007-07-11
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

Electronic Displays
2019-03-12
WIP
ARP4102/7A
This document recommends criteria for electronic displays on the flight deck of transport aircraft. Electronic displays include electronic flight instruments, alert displays, aircraft system displays and control/display units for flight management and radio management systems.
Standard

Electronic Displays
2007-07-10
CURRENT
ARP4102/7
This document recommends criteria for electronic displays on the flight deck of transport aircraft. Electronic displays include electronic flight instruments, alert displays, aircraft system displays and control/display units for flight management and radio management systems.
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)
1995-05-01
HISTORICAL
ARP4102/9
This document recommends criteria and requirements for a Flight Management System (FMS) for transport aircraft.
Standard

FULL-FORMAT PRINTER
1992-01-30
HISTORICAL
ARP4102/14
This document recommends criteria for the installation and operation of a printer on the flight deck, to supply the flight crew with hard copies of information that originates from data sources such as FMS, ELS, ACMS, CMS, and Data Link. These criteria are in addition to the specifications of the referenced ARINC Characteristic 744A.
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

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.
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