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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

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 Deck Environment

2002-12-16
CURRENT
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

On-Board Weight and Balance System

2022-03-17
CURRENT
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

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 Systems Review

2017-01-04
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 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
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

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
CURRENT
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

2016-09-28
WIP
ARP4102/11D
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 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

Final Approach Spacing System (Fass)

2017-01-27
WIP
ARP5628A
This document recommends criteria and requirements for a Final Approach Spacing System (FASS) for transport aircraft. This is an Aerospace Recommended Practice to support the development of a Final Approach Spacing System (FASS) for Approach Spacing for Instrument Approaches (ASIA) operations.
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.
Standard

Stowage of Flight Crew's Survival Emergency and Miscellaneous Equipment

2013-07-18
CURRENT
ARP4101/6A
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.
Standard

Flight Deck Alerting System (FAS)

2017-01-27
WIP
ARP4102/4A
This document recommends design criteria for the Flight Deck Alerting System. The FAS shall enhance safety of flight by providing early crew recognition of aircraft system or component status or malfunction as well as of crew operational error. The FAS, therefore, relates to aircraft configuration and flight phase as well as the aircraft systems. To fulfill this objective, the FAS must attract the attention of the crew, must state with clarity the nature and location of the problem, and must be highly reliable and thoroughly responsive to the operational requirements and environment. Wherever possible, it should provide guidance as to the corrective action.
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