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Standard

Airborne Landing Guidance System for Transport Aircraft

2000-06-01
HISTORICAL
ARP4102/12A
This document specifies requirements for an Airborne Landing Guidance System (ALGS) electronic device. This equipment shall derive relative aircraft position and situation information for flight along precision three-dimensional paths within the appropriate coverage area. The precision three-dimensional path may be an ILS straight-in look-alike path or a complex, curved path. The requirements are applicable to electronic devices capable of receiving signals or other information from one or more sources, including but not limited to ILS, MLS, GNSS, or IRU inputs.
Standard

Approach to Landing Guidance System for Transport Aircraft

2020-06-11
CURRENT
ARP4102/12B
This document specifies requirements for an Approach to Landing Guidance System (ALGS) electronic device. This equipment shall display relative aircraft position and situation information for flight along precision three-dimensional paths within the appropriate coverage area. The precision three-dimensional path may be an ILS straight-in look-alike path or a complex, curved path. The requirements are applicable to electronic devices capable of receiving signals or other information from one or more sources, including but not limited to ILS, GNSS, or IRU inputs.
Standard

FLIGHT MANAGEMENT SYSTEM (FMS)

1995-05-01
HISTORICAL
ARP4102/9
This document recommends criteria and requirements for a Flight Management System (FMS) for transport aircraft.
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 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 Management System (FMS)

2001-12-14
CURRENT
ARP4102/9A
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

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

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.
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