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Manufacturing Technical review Vehicle dynamics S-7 Flight Deck Handling Qualities Stds for Trans Aircraft

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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.
Standard

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

Crew Rest Facilities
2006-12-07
HISTORICAL
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

Crew Safety Provisions for Cargo Aircraft
2007-07-10
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

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

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.
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.
Standard

FULL-FORMAT PRINTER
1992-01-30
HISTORICAL
ARP4102/14
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, ACMS, CMS, and Data Link. These criteria are in addition to the specifications of the referenced ARINC Characteristic 744A.
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

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 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

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
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
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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