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Standard

Standard Scenarios and Examples of Operation of Airborne Wake Vortex Safety Systems
2013-11-26
WIP
AIR6288
This document describes operational scenarios and examples of system operation based on the experience of different developers of airborne wake vortex safety systems. This information is intended to supplement the recommendations and guidance given in ARP 6267 “Airborne Wake Vortex Safety Systems” as well as facilitate the application of other wake vortex standards and guidance documents generated by SAE and RTCA.
Standard

Display Latency Evaluation Procedures
2012-12-03
WIP
ARP6238
This Aerospace Recommended Practice will identify the problem with latency in the pilot's instrument control of an aircraft. Recommended evaluation techniques to characterize control problems will be documented.
Standard

AIRBORNE WAKE VORTEX SAFETY SYSTEMS
2013-03-26
WIP
ARP6267
This document recommends criteria for Airborne Wake Vortex Information Systems, including operational objectives, characteristics, and functional requirements. The recommendations in this document apply to transport aircraft, and describe the operational objectives of wake vortex information systems, situational displays, guidance systems, and avoidance/detection systems.
Standard

Human Engineering Considerations with Implementation of Aided Flight Vision forVertical Flight Platforms All Weather Operations
2018-12-14
WIP
ARP8459
Identify the phase of flights that can take benefit of Aided Visual Flight for the various missions of helicopters both VFR and IFR such as: Commercial Air Transport Operations offshore and onshore, EMS (Air ambulance), Law enforcement (Operations with Specific Approvals),Search and Rescue (SAR) operations both in Maritime and Mountainous operations The Aided Flight should be considered with various levels of on-boarded sensor technology and its performance such as, but not limited to: NVG, Addition of Axial IR Sensor (with minimum performance to define), Potential use of orientable search light (night VFR) and other situation awareness means like HTAWS, SVS, and sensor like Radio Altimeter including the display mean head-down or head worn that influence operational aspects.
Standard

Cockpit Information Required for Helicopter Turbine Engine Operation and Maintenance
2022-03-29
WIP
AIR1963B
This SAE Aerospace Information Report (AIR) identifies Propulsion EngineerÕs recommendations for the instrumentation that is required for the safe operation and maintenance of turbine engines as installed in helicopters. It should be used as a guide for cockpit layout, as well as a reference for maintenance considerations throughout the propulsion area. Propulsion instruments should receive attention early in the design phase of the helicopter. Maintenance and diagnostics recorders are not considered within the scope of this document. (See ARP1587, "Aircraft Gas Turbine Engine Monitoring System Guide".)
Standard

Cockpit Information Required for Helicopter Turbine Engine Operation and Maintenance
1997-06-01
CURRENT
AIR1963A
This SAE Aerospace Information Report (AIR) identifies Propulsion Engineer’s recommendations for the instrumentation that is required for the safe operation and maintenance of turbine engines as installed in helicopters. It should be used as a guide for cockpit layout, as well as a reference for maintenance considerations throughout the propulsion area. Propulsion instruments should receive attention early in the design phase of the helicopter. Maintenance and diagnostics recorders are not considered within the scope of this document. (See ARP1587, “Aircraft Gas Turbine Engine Monitoring System Guide”.)
Standard

Flight Deck Head-Up Displays
2007-07-10
CURRENT
ARP4102/8A
This SAE Aerospace Recommended Practice (ARP) recommends criteria for the design and installation of Head-Up Display (HUD) systems. The recommendations are applicable to HUD systems for transport category aircraft, which display flight information (focused at infinity) in the forward field of view. The HUD total system requirement recommendations shall primarily lead to certifiable fail-passive CAT III characteristics and performance. This document forms a part of these recommendations. This document does not address devices for peripheral vision of displays worn by the pilot, nor the presentation of Enhanced Vision System (EVS) information.
Standard

FLIGHT DECK, HEAD-UP DISPLAYS
1994-05-01
HISTORICAL
ARP4102/8
This document recommends criteria for the design and installation of Head-Up Display (HUD) systems. The recommendations are applicable to HUD systems which display flight information focused at infinity in the forward field of view. This annex does not address devices for peripheral vision or displays worn by the pilot (goggles, helmet sights).
Standard

RATE OF CLIMB INDICATOR, PRESSURE ACTUATED (VERTICAL SPEED INDICATOR)
2008-02-16
CURRENT
AS394A
This Aeronautical Standard covers four (4) basic types of direct indicating instruments as follows: TYPE I - Range 0-2000 feet per minute climb and descent TYPE II - Range 0-3000 feet per minute climb and descent TYPE III - Range 0-4000 feet per minute climb and descent TYPE IV - Range 0-6000 feet per minute climb and descent
Standard

On-Board Weight and Balance System
2022-03-17
CURRENT
ARP4102/1A
This document recommends criteria for the flight deck display of an On Board Weight and Balance System. The system may have the capability of a primary operational device or be a secondary advisory source of information of weight and center of gravity position. The recommendations apply to transport aircraft and describe the operational and functional requirements for the display of an On Board Weight and Balance System.
Standard

Flight Management System (FMS)
2021-01-14
CURRENT
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.
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