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WIP Standard
2014-06-23
This ARP covers the system design, human interface considerations, and hardware performance recommendations and requirements for touch interactive electronic display systems installed in the cockpit/flight deck for use by pilots. System design and human interface considerations include: identification of functions that could use and benefit from touch interactions, the pilot and cockpit/flight deck environment characteristics that impact usability, and specific pilot interface characteristics such as touch mode, single and multi touch applications, feedback, latency, potential human error, and basic usability. Also addressed are workload, fatigue, and transition from hard to soft control considerations. Hardware issues cover performance aspects of touch screens installed on cockpit/flight deck displays. This ARP is intended to cover Part 23 and 25 category airplanes as well as Part 27 and 29 rotorcraft.
Standard
2014-02-01
This Engineering Bulletin and its annexes provide guidance on the application of Human Engineering principles and practices to the analysis, design, development, testing, fielding, support, accident investigation, and training for military and commercial products throughout their intended life cycles.
WIP Standard
2013-11-26
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
2013-07-18
This document recommends general specifications for the location, accessibility and restraint for those items of survival, emergency, and miscellaneous equipment which are intended to be used by the flight crew, and which are stowed on or near the flight deck.
Standard
2013-07-18
The purpose of this document is to recommend criteria for the provision of crew escape facilities from the flight deck area.
Standard
2013-07-18
This document recommends provisions for crew safety and survival which are intended to apply to cargo or combination aircraft and equipment.
WIP Standard
2013-05-30
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.
WIP Standard
2013-05-22
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, ELS/EDMS, ACMS, CMS, and data link.
WIP Standard
2013-05-22
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.
WIP Standard
2013-05-22
This document is intended to specify the environmental conditions for transport aircraft necessary to permit the crew to perform their duties and functions in comfort, with minimum fatigue and no distraction. Environment conditions should cause no short or long-term effects deleterious to health or physical well-being, nor significantly impair ability to perform normal or abnormal crew functions.
WIP Standard
2013-03-26
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.
WIP Standard
2012-12-03
Loss-of-control is the major type of mishap to transport airplanes. This report will review loss-of-control events to revenue air carrier flights occurring from 1981 through 2010. During this period, 202 mishaps resulted in 8469 fatalities. Aerodynamic stalls (48 events; 1505 fatalities) was the most frequent cause. Spatial disorientation produced the second greatest number of fatalities (25 events; 1228 fatalities). Nineteen events involved faulty recovery techniques and resulted in 1329 fatalities. Areas for improvements in pilot training will be listed: Addressing loss of instrument skills; stall recovery training; and specific SDO training. Envelope protection appears to be the most significant airframe-related safety factor. Several high level recommendations will be listed.
WIP Standard
2012-12-03
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
2012-11-19
This document is intended to establish preferred abbreviations and acronyms for terms used on panels, controls, displays, instruments, placards, and markings. The recommendations apply to equipment used by crew members in the flight deck of transport aircraft.
WIP Standard
2012-08-15
The scope of this document is to provide a definition of the minimum set of flight information and symbology required for safe operation of aircraft when displayed on an electronic flight information system (EFIS), including but not limited to Primary Flight Display (PFD) as a Minimum Information Display List (MIDL).
Standard
2012-07-31
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, ELS/EDMS, ACMS, CMS, and data link.
Standard
2012-07-31
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
2012-07-31
This document is intended to specify the environmental conditions for transport aircraft necessary to permit the crew to perform their duties and functions in comfort, with minimum fatigue and no distraction. Environment conditions should cause no short or long-term effects deleterious to health or physical well-being, nor significantly impair ability to perform normal or abnormal crew functions.
Standard
2012-06-11
The scope of this document is limited to descriptions of the display characteristics of the Flight Dynamics, Inc. (FDI) Model 1000WS Head up Guidance System (HGS) as installed on the Boeing 727 airplane and certified by the Federal Aviation Administration for use in Category III landing operations. The symbology depicted in this document is refeenced to the particular pilot task(s) for which it was designed. Also included are descriptions of operational features of the particular symbol along with any associated criteria regarding symbology constraints, source data, or position error.
Standard
2012-06-11
This specification covers hand-held prismatic stereoscopic binoculars for aeronautical use in search, rescue, and patrol operations.
Standard
2010-06-10
This document recommends criteria for the location, arrangement and other requirements of aircraft circuit breakers and fuses on the flight deck.
Standard
2005-12-01
This Engineering Bulletin and its annexes provide guidance on the application of Human Engineering principles and practices to the analysis, design, development, testing, fielding, support, accident investigation, and training for military and commercial products throughout their intended life cycles.
Standard
2005-11-28
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
2002-12-16
The purpose of this document is to describe the recommendations of SAE Committee S-7 for a Flight Management Computer System (FMCS) capable of providing the functions and displays listed below to permit completion of a desired flight plan in an energy efficient and/or cost effective manner while meeting the requirements of Air Traffic Control. The recommendations of this document apply to transport aircraft and describe the operational objectives of the FMCS and related controls and displays.
Standard
2002-12-16
This Aerospace Recommended Practice (ARP) is intended to specify the environmental conditions necessary to permit the operating crew of large civil transport aircraft to perform their required duties and functions in comfort, with minimum fatigue and no distraction. Environmental conditions should cause no short or long-term effects deleterious to health or physical well being, nor significantly impair ability to perform normal flight deck crew functions.
Standard
2002-10-21
This document recommends criteria for Airborne Windshear Systems, including operational objectives, characteristics and functional requirements. The recommendations of the document apply to transport aircraft, and describe the operational objectives of windshear alerting systems, situational displays, guidance systems and avoidance/detection systems.
Standard
2001-10-01
This document recommends criteria for the design and installation of Autopilot, Flight Director and Autothrust Systems. These three systems are highly inerrelated and will be referred to generically as an Integrated Flight Guidance System (IFGS).
Standard
2000-06-01
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
2000-04-01
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, ELS/EDMS, ACMS, CMS, and data link. These criteria are in addition to the specifications of the referenced ARINC Characteristic 744A.
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