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Standard

NOMENCLATURE AND ABBREVIATIONS FOR USE ON THE FLIGHT DECK

1985-12-15
CURRENT
AS425C
This Standard is intended to establish preferred abbreviations for use on panels, controls, instruments, displays, placards and markings. The recommendations apply to terms used in the flight deck of transport aircraft. The abbreviations, symbols and codes do not supersede those used in airworthiness regulations or aeronautical charts and documents. Where conflict is possible the operational context must be such as to resolve any ambiguity. If doubt exists, an alternative abbreviation or less truncated abbreviation should be used.
Standard

INTEGRATION PROCEDURES FOR THE INTRODUCTION OF NEW SYSTEMS TO THE COCKPIT

1995-03-01
CURRENT
ARP4927
This SAE Aerospace Recommended Practice (ARP) provides guidance to achieve the optimum integration of new aircraft systems which have an impact on the cockpit layout or crew operating procedures. This process may also be used for modification of existing cockpits.
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

1998-10-01
HISTORICAL
ARP4102/14A
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/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 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 Alerting System (FAS)

1988-07-01
CURRENT
ARP4102/4
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.
Standard

FLIGHT DECK, HEAD-UP DISPLAYS

1988-07-01
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

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

1988-07-01
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

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

Crew Safety Provisions for Cargo Aircraft

2013-07-18
CURRENT
ARP4101/9A
This document recommends provisions for crew safety and survival which are intended to apply to cargo or combination aircraft and equipment.
Standard

Crew Safety Provisions for Cargo Aircraft

1988-07-01
HISTORICAL
ARP4101/9
This document recommends provisions for crew safety and survival which are intended to apply to cargo or combination aircraft and equipment.
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

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.
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