Search Results

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.

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Pilot Visibility From The Flight Deck

2003-02-25

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.

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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

On Board Weight and Balance System

2004-06-23

HISTORICAL

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.

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Loss-of-Control Mishaps in Revenue Airline Service

2016-07-12

CURRENT

AIR6237

The scope of this document is to provide review of recent history of loss-of-control accidents during airline revenue operations.

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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.

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Full-Format Printer

2007-07-11

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.

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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.

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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)

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.

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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.

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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.

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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.

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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.

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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.

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DESIGN OBJECTIVES FOR FLYING QUALITIES OF CIVIL TRANSPORT AIRCRAFT

1966-08-15

HISTORICAL

ARP842A

Standard

DESIGN OBJECTIVES FOR FLYING QUALITIES OF CIVIL TRANSPORT AIRCRAFT

1964-08-01

HISTORICAL

ARP842

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DESIGN OBJECTIVES FOR FLYING QUALITIES OF CIVIL TRANSPORT AIRCRAFT

1970-11-30

HISTORICAL

ARP842B

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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

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.