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Autopilot, Flight Director, and Autothrust Systems

2001-10-01
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).
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COLLISION AVOIDANCE SYSTEM

1993-09-03
CURRENT
ARP4102/10A
This document presents criteria for flight deck controls and displays for Airborne Collision Avoidance Systems providing vertical-only guidance, and provides design guidance for operational, functional, and installation characteristics and requirements for airborne collision avoidance systems in existing and future aircraft.
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COMMUNICATIONS AND NAVIGATION EQUIPMENT

1988-07-01
CURRENT
ARP4102/6
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). c Weather Radar d Data Link: Company, Air Traffic Control (ATC) Transponders (Mode-S) and others.
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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.
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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.
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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.
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Collision Avoidance System

2016-01-18
WIP
ARP4102/10B
This document presents criteria for flight deck controls and displays for airborne collision avoidance systems providing vertical-only guidance, and provides design guidance for operational, functional, and installation characteristics and requirements for airborne collision avoidance systems in existing and future aircraft.
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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).
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Crew Rest Facilities

1992-02-28
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.
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Crew Rest Facilities

2019-04-01
CURRENT
ARP4101/3A
This document recommends criteria for the design and installation of flight crew rest facilities (FCRF) on transport category aircraft when operations with an augmented flight crew are performed. NOTE: Within this ARP, the term “must” will indicate items required for compliance with outside known government regulations, especially 14 CFR Part 117. “Shall” describes sections which are required if this ARP is used as a means of compliance. The term “should” will indicate optional requirements, preferences, and recommendations of the approving SAE committee. Wherever noted and bracketed as [FAA] or [EASA], this document includes agency regulations for reference that are not otherwise evaluated herein.
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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.
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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.
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Crew Safety Provisions for Cargo Aircraft

1988-07-01
HISTORICAL
ARP4101/9
This document recommends provisions for crew safety and survival which are intended to apply to cargo or combination aircraft and equipment.
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DATA LINK

1993-06-18
CURRENT
ARP4102/13A
This document recommends criteria for a system designed to manage and communicate information via data link to support flight operations.
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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.
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Design Objectives For Handling Qualities Of Transport Aircraft

1994-02-01
CURRENT
ARP842C
This recommended practice sets forth 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.
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Design Objectives For Handling Qualities Of Transport Aircraft

1964-08-01
HISTORICAL
ARP842
This recommended practice sets forth 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.
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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.
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