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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

Seats and Restraint Systems for the Flight Deck

2007-07-09
CURRENT
ARP4101/1
This document establishes the minimum requirements for seats and restraint systems for the flight deck. Due to limitations that it would place upon basic aircraft design, it is not considered practical for these requirements to apply fully to the observer seat. However, it is emphasized that every effort should be made to provide the observer seat position with an equivalent level of comfort and safety. This document is also intended to make recommendations for flight crew restraint systems. A properly designed crew restraint system will minimize injury or debilitation during a survivable crash and enable post crash assistance to occupants and escape from the aircraft. Crew member safety is the primary objective, with appropriate provisions for crew comfort taken into consideration. The criteria established herein are designed to standardize restraint systems without hindering the development of new, improved systems.
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

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.
Standard

INTEGRATION PROCEDURES FOR THE INTRODUCTION OF NEW SYSTEMS TO THE COCKPIT

2007-07-11
HISTORICAL
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

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.
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 Deck Layout and Facilities

2003-02-25
CURRENT
ARP4101
This document recommends criteria for the layout and for the design, installation, and operation of flight deck facilities for transport aircraft.
Standard

Flight Deck Environment

2003-02-25
HISTORICAL
ARP4101/4
This document is intended to specify the environmental conditions for transport aircraft necessary to permit the crew to perform their 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 or abnormal crew functions.
Standard

Flight Deck Environment

2012-07-31
CURRENT
ARP4101/4A
This document is intended to specify the environmental conditions for transport aircraft necessary to permit the crew to perform their 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 or abnormal crew functions.
Standard

Flight Deck Alerting System (FAS)

2007-07-10
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

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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