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2013-04-24
WIP Standard
AIR6247
This document is intended to serve two purposes: (1) provide a list of topics for potential customers to ask of the facility to aid their selection decision-making, and (2) provide a list of icing wind tunnel and engine test stand facilities that simulate flight through icing or ice crystal clouds.
CURRENT
2013-04-20
Standard
AIR4496A
This SAE Aerospace Information Report (AIR) provides guidance criteria for the storage of personal wheelchairs in the passenger compartment of transport category aircraft, which have not been provided by the air carrier and are designated for the sole use of the passenger requiring such assistance.
CURRENT
2013-04-18
Standard
J881_201304
This SAE Standard covers minimum dimensional relationship for sheaves, drums, and wire rope for mobile, construction type lift cranes.
CURRENT
2013-04-09
Standard
J2939_201304
CURRENT
2013-04-04
Standard
AIR1815A
This AIR defines the major groups of impairments and disabilities among passengers who use aircraft as a transportation mode, and the types of safety problems which might be associated with each impairment. These impairments, and their safety-related problems, should be considered when referring to ARP's related to the design of cabin furnishings and equipment.
CURRENT
2013-04-04
Standard
AIR5648A
Specific federal aviation regulations (Titled 14 of the United States Code of Federal Regulations, or 14 CFR) define oxygen system requirements for an in-flight decompression incident. This AIR addresses the operational oxygen system requirements for a decompression incident that may occur at any point during a long-range flight, with an emphasis for a decompression at the equal time point (ETP). This AIR identifies fuel and oxygen management contingencies, and presents possible solutions for the efficient, safe, and optimum fuel/oxygen flight continuation. Oxygen management is a concern to all aircraft, such as single engine types that fly above 10 000 feet and use supplemental oxygen. This document provides a method which can help guide users in developing an oxygen solution for their aircraft.
CURRENT
2013-03-28
Standard
J1289_201303
To establish conditions to be taken into consideration in determining rated loads for mobile cranes when overturning stability is the controlling factor. This recommended practice applies to mobile, construction-type lifting cranes with either lattice booms or cantilevered, telescopic booms.
2013-03-26
WIP Standard
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.
CURRENT
2013-03-26
Standard
J1388_201303
This SAE Standard is intended to provide personnel protection guidelines for skid steer loaders. This document is intended as a guide towards standard practice, but may be subject to frequent change to keep pace with experience and technical advances. This should be kept in mind when considering its use. This document provides performance criteria for newly manufactured loaders and it is not intended for in-service machines.
CURRENT
2013-03-25
Standard
ARP4032B
This document is intended for the application of color to cathode-ray-tube (CRT) displays, liquid crystal displays (LCD) and other types of display technologies such as projection displays. Emerging color display technologies other than those noted above, may not be adequately covered by these recommendations. Color recommendations will not address Night Vision Devices (NVD), Head-Up Displays (HUD) or Head or Helmet Mounted Displays (HMD). This document is applicable to aircraft as understood in 14 CFR Parts 23, Part 25, Part 27 and Part 29, and EASA CS-23, CS-25. CS-27 and CS-29 certification standards.
2013-03-19
WIP Standard
J1078
This analysis applies to crane types as covered by Power crane and shovel Association Standard Number Two, Mobile Hydraulic Crane standards and ANSI B30.15; refer to 5.1. This calculation method has been established to illustrate an analysis to determine the competence of hydraulic telescopic cantilevered crane booms.
CURRENT
2013-03-15
Standard
AIR4015D
This Icing Technology Bibliography is a compendium of references from the open literature that were published prior to the original 1987 issuance of the AIR, including both national and foreign sources. Due to the generality of the subject, and the difficulty of fully investigating every available source, the Bibliography in this document is not intended to be complete.
2013-03-07
WIP Standard
ARP6244
This document describes technical approaches that can be applied to show that proposed oxygen equipment and systems achieve suitable oxygenation in users. These approaches can be used to demonstrate that items under test meet performance criteria sufficient to justify certification for use in aircraft applications.
2013-03-07
WIP Standard
AIR825/7
This AIR provides an overview of several emerging technologies for on board oxygen generation. It complements AIR 825/6, which covers pressure swing adsorption using zeolite molecular sieve beds to concentrate and separate oxygen from atmospheric gases. Topics covered here include use of dense ion conductive ceramics, electrolysis of water, high pressure chemical generation, membrane separations, and use of carbon based molecular seive beds.
CURRENT
2013-03-01
Standard
AS1426/2B
This appendix covers requirements for system and end item documentation and procedures used for the standard galley system.
2013-02-25
WIP Standard
AS5727
This Aerospace Standard (AS5727) will provide the basis for a certification approach and contain the methods or criteria for verification of performance required of Oxygen Dispensing Units for use by cabin occupants in the range of 40,000 to 45,000 ft. cabin altittude. 1.1 Purpose - This AS is intended to identify the performance required of Personal Oxygen Dispensing Units in the range of 40,000 to 45,000 ft.
CURRENT
2013-02-21
Standard
J1460_201302
While this report does not include a discussion of all of the available data defining human response or address all body areas, for those areas addressed it does utilize references generally judged by those in the field to be practical and meaningful guidelines for the development of human surrogates. This report is intended to be a “living” document that will be updated periodically. A number of problems need to be addressed in defining human impact response characteristics. There is the problem of human response variability from subject to subject in volunteer tests. There is the problem of extrapolating such volunteer data which are obtained at low impact severities to higher impact severities using human cadaver response data obtained at injurious levels of impacts. Live animal experiments have been conducted over the years in an attempt to define human impact response and tolerance.
CURRENT
2013-02-14
Standard
AS8040B
This SAE Aerospace Standard (AS) covers combustion heaters used in the following applications: Cabin heating (all occupied regions and windshield heating) Wing and empennage anti-icing Engine and accessory heating (when heater is installed as part of the aircraft) Aircraft de-icing
2013-02-11
WIP Standard
J1100
This SAE Recommended Practice defines a set of measurements and standard procedures for motor vehicle dimensions. The dimensions are primarily intended to measure the design intent of a vehicle within a design environment (i.e., CAD). All dimensions in this practice can be measured this way. In addition, some dimensions can be taken in an actual vehicle. If measurements are taken on physical properties, some differences in values should be expected. Also, care should be taken to not confuse design intent measurements with those taken on a physical property. It is intended that the dimensions and procedures described in this practice be generic in their application to both the HPM, described in SAE J826, and the HPM-II, described in SAE J4002. In some circumstances, the figures may only reflect one or the other.
2013-01-31
WIP Standard
AIR6242
to provide a description of the Multi-Crew Pilot License (MPL) and its related training program. This is intended to provide information and guidance for scheduled passenger and cargo air carriers, as well as for training providers.
CURRENT
2013-01-21
Standard
ARP4120C
This document provides design guidelines for an on-board wheelchair (OBW) used in commercial aircraft operations. All Federal Regulations must be complied with.
CURRENT
2013-01-07
Standard
AS6271
This AS establishes minimum requirements for halocarbon clean agent hand-held fire extinguishers carried on board civil aircraft. The requirements include: design (cylinder, valve, gauge, mounting equipment), performance (firefighting effectiveness - hidden fire test, discharge test, type, etc.), environmental (ozone depleting/global warming potential, atmospheric life span), and occupant safety concerns (toxicology - seat fire test).
CURRENT
2012-12-18
Standard
ARP5677
The scope of this document is limited to Enhanced Synthetic Vision Systems ESVS human factors considerations and requirements in comprehension, interpretation and application of imagery and integrated symbology in Enhanced (sensor) and Synthetic (database) Vision Systems in aircraft. Any overlap into logic problems or hardware/software design should be considered to be incidental to the human factors issues. Where the performance characteristics of specific technologies are relevant they will be identified, and where performance criteria are relevant to specific intended functions/use they will be identified. From a regulatory view, intended function (Guidance or Information/Situation Awareness support) has a tremendous effect upon the design of an ESV System.
HISTORICAL
2012-12-06
Standard
AS4156B
This document defines the method for voltage identification by use of color coded insulators at the base of the lamp. Table 1 shows the design volts and corresponding insulator colors. The part numbers shown are for example purposes only. Insulator colors are to be easily distinguishable as green, yellow, red, and white. Additional colors may be added by a revision process as required.
2012-12-03
WIP Standard
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.
CURRENT
2012-12-03
Standard
AIR825D
This report provides information on the design and use of aircraft oxygen systems. It explains the physiological oxygen requirements of the human body in both a normal environment and in an hypoxic environment. It includes an overview of the continuous flow, demand and pressure demand, and liquid oxygen systems. A basic understanding of how each system operates is then specifically addressed in its own titled section. The charts, tables, and schematics provide a specific example of a theoretical oxygen system design and the calculations showing how that system would meet the regulations established by the FAR’s. A comprehensive overview of the theoretical oxygen requirements of the human body at altitude is also provided. A detailed list of specifications and standards applicable to aircraft oxygen systems is included.
CURRENT
2012-11-19
Standard
ARP4105C
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.
CURRENT
2012-11-09
Standard
J115_201211
SAE J115 specifies the relevant ISO standards for application to safety signs for use on off-road work machines as defined in SAE J1116.
2012-10-17
WIP Standard
J3023
The purpose of this document is to establish guidelines for determining the critical refrigerant charge for off-road, self-propelled work machines, general purpose industrial, agricultural, forestry, and specialized mining machinery. It will develop a minimum to maximum refrigerant charge range in which the HVAC system can maintain proper operation. Operating conditions and characteristics of the equipment will influence the optimum charge. Since these conditions and characteristics vary greatly from one application to another, careful consideration should be taken to determine the optimum refrigerant charge for the HVAC system.
Viewing 241 to 270 of 1266