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Standard

Flight Deck Interior Doors for Transport Aircraft

2016-01-18
WIP
ARP4101/8A
This document recommends criteria for standardization of flight deck interior doors and their operation which will provide optimum use under normal and emergency conditions.
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

Takeoff Performance Monitor (TOPM) System, Airplane, Minimum Performance Standard For

2007-09-02
WIP
AS8044A
This Aerospace Standard (AS), establishes minimum performance standards for those sensors, computers, transponders, and airplane flight deck controls/displays which together comprise a Takeoff Performance Monitor (TOPM) System. This standard also defines functional capabilities, design requirements, and test procedures. A TOPM system is intended to monitor the progress of the takeoff and to provide advisory information which the crew may use in conjunction with other available cues to decide to continue or abort the takeoff. See Appendix A for supplementary information relating to NTSB, CAA, and ad hoc committee concerns and background information.
Standard

TAKEOFF PERFORMANCE MONITOR (TOPM) SYSTEM, AIRPLANE, MINIMUM PERFORMANCE STANDARD FOR

1987-08-01
CURRENT
AS8044
This Aerospace Standard (AS), establishes minimum performance standards for those sensors, computers, transponders, and airplane flight deck controls/displays which together comprise a Takeoff Performance Monitor (TOPM) System. This standard also defines functional capabilities, design requirements, and test procedures. A TOPM system is intended to monitor the progress of the takeoff and to provide advisory information which the crew may use in conjunction with other available cues to decide to continue or abort the takeoff. See Appendix A for supplementary information relating to NTSB, CAA, and ad hoc committee concerns and background information.
Standard

Cockpit Visibility for Commercial Transport Aircraft

1964-03-01
CURRENT
AIR32B
INTRODUCTION This report is intended to encourage more effort to be directed toWard improving the pilot's visibility from the cockpit of transport type aircraft wih the ultimate objective of improving safety. In the preparation of this Aeronautical Information Report, consideration Was given to pilot surveys made by the Civil Aeronautics Administration, studies made by manufacturers, and a review of the cockpit visibility provided in present day transport aircraf`t. It is recognized that a rigid specification is undesirable and may restrict development and utilization of initiative. For this reason the report is in general terms and offered as a guide.
Standard

Cockpit Visibility For Commercial Transport Aircraft

1960-06-01
HISTORICAL
AIR32A
INTRODUCTION This report is intended to encourage more effort to be directed toWard improving the pilot's visibility from the cockpit of transport type aircraft wih the ultimate objective of improving safety. In the preparation of this Aeronautical Information Report, consideration Was given to pilot surveys made by the Civil Aeronautics Administration, studies made by manufacturers, and a review of the cockpit visibility provided in present day transport aircraf`t. It is recognized that a rigid specification is undesirable and may restrict development and utilization of initiative. For this reason the report is in general terms and offered as a guide.
Standard

Cockpit Visibility For Commercial Transport Aircraft

1952-08-15
HISTORICAL
AIR32
INTRODUCTION This report is intended to encourage more effort to be directed toWard improving the pilot's visibility from the cockpit of transport type aircraft wih the ultimate objective of improving safety. In the preparation of this Aeronautical Information Report, consideration Was given to pilot surveys made by the Civil Aeronautics Administration, studies made by manufacturers, and a review of the cockpit visibility provided in present day transport aircraf`t. It is recognized that a rigid specification is undesirable and may restrict development and utilization of initiative. For this reason the report is in general terms and offered as a guide.
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

Crew Safety Provision for Cargo Aircraft

1994-02-15
CURRENT
ARP1139
This document recommends provisions for crew safety and survival which are intended to apply to cargo aircraft and equipment. This ARP applies specifically to cargo aircraft regardless of means of propulsion or design speed regimes, including V/STOL types.
Standard

Flight Management Computer System

2002-12-16
CURRENT
ARP1570
The purpose of this document is to describe the recommendations of SAE Committee S-7 for a Flight Management Computer System (FMCS) capable of providing the functions and displays listed below to permit completion of a desired flight plan in an energy efficient and/or cost effective manner while meeting the requirements of Air Traffic Control. The recommendations of this document apply to transport aircraft and describe the operational objectives of the FMCS and related controls and displays.
Standard

Crew Rest Facilities

2013-05-30
WIP
ARP4101/3A
This document recommends criteria for the design and installation of flight crew rest facilities on commercial transport aircraft capable of ultra long-range operations with augmented/enlarged crew complement.
Standard

Crew Rest Facilities

1992-02-28
CURRENT
ARP4101/3
This document recommends criteria for the design and installation of flight crew rest facilities on commercial transport aircraft capable of ultra long-range operations with augmented/enlarged crew complement.
Standard

Flight Deck Environment

1988-07-01
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

Seats and Restraint Systems for the Flight Deck

2013-05-22
WIP
ARP4101/1A
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 mminimize 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.
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