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Standard

Final Approach Spacing System (Fass)

2017-01-27
WIP
ARP5628A
This document recommends criteria and requirements for a Final Approach Spacing System (FASS) for transport aircraft. This is an Aerospace Recommended Practice to support the development of a Final Approach Spacing System (FASS) for Approach Spacing for Instrument Approaches (ASIA) operations.
Standard

Communications and Navigation Equipment

2016-01-18
WIP
ARP4102/6A
This document recommends criteria for the control and display of communications and navigation equipment on the flight deck. The equipment includes: a. Communications: Ultra High Frequency (UHF), Very High Frequency (VHF), and High Frequency (HF) Radios, Cabin/Service Interphones, Public Address (PA), Select Call (SELCAL), Call Select (CALSEL), Satellite Communications (SATCOM), b. Navigation: Very High Frequency Omnidirectional Range (VOR), Tactical Air Navigation (TACAN), Automatic Direction Finder (ADF), Distance Measuring Equipment (DME), Instrument Landing System (ILS), Markers (MKR), Omega, Very Low Frequency (VLF), Inertial Navigation Systems (INS), Inertial Reference Systems (IRS), Satellite Navigation (SATNAV), Low Range Radio Altimeter (LRRA).
Standard

Flight Management System (FMS)

2016-01-18
WIP
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

Design Objectives for Handling Qualities of Transport Aircraft

2011-08-23
WIP
ARP4104A
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

Flight Envelope Awareness/Protection

2011-08-23
WIP
ARP4104/1A
This anex 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 Autoflfight, Autothrottle, or Autothrust performance is compatible.
Standard

Data Link

2016-09-28
WIP
ARP4102/13B
This document recommends criteria for a system designed to manage and communicate information via data link to support flight operations.
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

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.
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.
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