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Viewing 121 to 150 of 728
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
2013-04-09
Standard
ARP1307B
Test procedures are described for measuring noise at specific receiver locations (passenger and cargo doors, and servicing positions) and for conducting general noise surveys around aircraft. Procedures are also described for measuring noise level and directivity at noise source locations to facilitate the understanding and interpretation of the data. Requirements are identified with respect to instrumentation; acoustic and atmospheric environment; data acquisition, reduction and presentation, and such other information as is needed for reporting the results. This document makes no provision for predicting APU or component noise from basic engine characteristics or design parameters, nor for measuring noise of more than one aircraft operating at the same time. No attempt is made to suggest acceptable levels of noise or suitable subjective criteria for judging acceptability. ICAO Annex 16 Volume I Attachment C provides guidance on recommended maximum noise levels.
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
2013-04-02
Standard
J2727_201304
The “System Emissions Chart” contained herein is intended to serve as a means of estimating the annual refrigerant emission rate (grams per year) from new production A/C systems equipped with specified component technologies. It provides emission values for various component technologies that are currently available, and can be expanded as new technologies are commercialized. This document provides the information to develop an Excel file template “System Emissions Chart” for system emission analysis. The chart includes automotive compressor technologies for conventional mobile air conditioning systems as well as those using semi-hermetic compressors. This standard can be considered a companion document to SAE J2763 Test Procedure for Determining Refrigerant Emissions from Mobile Air Conditioning Systems. SAE J2727 estimates system emissions, taking into account production assembly variation and accounts for components that are 100% helium leak tested prior to vehicle final assembly.
CURRENT
2013-03-28
Standard
J1088_201303
This SAE Recommended Practice specifies a uniform procedure for the evaluation of gaseous exhaust emissions from small utility engines typically less than 20 kW. Details of engine test setup and exhaust gas analysis techniques are specified with the intent of providing a uniform and reproducible method of measurement. The intent has been to allow as much flexibility as possible in the physical construction of the experimental apparatus. Therefore, only those portions of the apparatus whose operation is critical to the accurate measurement of emissions levels are prescribed in detail. An engine test procedure including a test sequence is outlined such that it would cover the various applications in which small engines are used. The intent is to provide an understanding of the levels of exhaust emissions and does not imply that in given application, an engine would operate in all the modes outlined in the test procedure.
CURRENT
2013-03-28
Standard
ARP4902B
This document provides information and guidance material to assist in assessing the need for and feasibility of developing deicing facilities, the planning (size and location)and design of deicing facilities, and assessing environmental considerations and operational considerations associated with de-icing facilities. The document presents relevant information necessary to define the need for a deicing facility and factors influencing its size, location and operation. The determination of the need for deicing facilities rests with Airports. Although this document intends to provide information to airport operator and deicing facility planner/designer, all stakeholders, including deicing service providers, should be involved in the development process.
CURRENT
2013-03-25
Standard
AS6451A
This specification covers protective shields for engine and tailpipe openings of aircraft and missiles.
CURRENT
2013-03-25
Standard
ARP936B
This Aerospace Recommended Practice (ARP) describes the requirements of a special purpose 10 μF feed through capacitor to be used in series with the power line to an electrical or electronic device during EMI tests.
CURRENT
2013-03-25
Standard
ARP4242A
This SAE Aerospace Recommended Practice (ARP) establishes overall system electromagnetic compatibility (EMC) control requirements. EMC includes the following: Electromagnetic Environmental Effects (E3) Electrostatic Discharge (ESD) Electromagnetic Interference (EMI) Electromagnetic Vulnerability (EMV) Electromagnetic Pulse (EMP) Hazards of Electromagnetic Radiation to Ordnance (HERO) Hazards of Electromagnetic Radiation to Personnel (HERP) Hazards of Electromagnetic Radiation to Fuels (HERF) High Intensity Radiated Fields (HIRF) Lightning Protection Static Electricity TEMPEST This document is intended to be used for the procurement of land, sea, air, or space systems by any procurement activity. Tailoring of specific requirements is necessary and Appendix A has been provided for guidance.
CURRENT
2013-03-25
Standard
ARP935B
This document contains a "sample" Control Plan with explanations as to the intended content of various sections. It also can serve as a sample technical construction file as specified by the European EMC Directive.
CURRENT
2013-03-25
Standard
AS4792A
This SAE Aerospace Standard (AS) covers water conditioning agents used to facilitate aqueous wet-method magnetic particle inspection.
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.
CURRENT
2013-02-24
Standard
ARP5623
This SAE Aerospace Recommended Practice (ARP) covers the requirements for a combined Mobile Digital Infrared Pavement Surface, Ambient Air, and Dew Point Temperature Sensing System (referred to as the system). The system monitors real-time surface, air and dew point temperatures of airfield pavement areas to ensure safe winter ground operations of aircraft and other vehicles. The vehicle mounted electronic system provides the operator with real-time readings of surface, air and dew point temperatures of airfield pavement areas including runways, taxiways, ramps, bridges, vehicular roadways, parking garages and parking lots. The electronic system shall be available with or without the dew point sensing option. This electronic system can be utilized as a stand alone system at small airports, or may be used to augment airport operations that currently have a Stationary Runway Weather Information System (reference ARP5533).
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.
2013-01-22
WIP Standard
AIR1209A
This Aerospace Information Report (AIR) is intended to provide information relating to the construction, calibration, and usage of parallel plate transmission lines in electromagnetic compatibility susceptibility testing.
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
2013-01-14
Standard
J2788_201301
The purpose of this SAE Standard is to establish the specific minimum equipment performance requirements for recovery and recycling of HFC-134a that has been directly removed from, and is intended for reuse in, mobile air-conditioning (A/C) systems. It also is intended to establish requirements for equipment used to recharge HFC-134a to an accuracy level that meets Section 9 of this document and SAE J2099. The requirements apply to the following types of service equipment and their specific applications. Recovery/Recycling Equipment, Recovery/Recycling-Refrigerant Charging, Refrigerant Recharging Equipment Only.
CURRENT
2013-01-11
Standard
ARP5412B
The environment and test waveforms defined in this SAE Aerospace Recommended Practice (ARP) account for the best lightning data and analysis currently available. The quantified environment and levels herein represent the minimum currently required by certifying authorities, consistent with the approach applied in related lightning documents. Lightning, like other weather phenomenon, is probabilistic in nature. Levels and waveforms vary considerably from one flash to the next. Within this document, standardized voltage and current waveforms have been derived to represent the lightning environment external to an aircraft. These standardized waveforms are used to assess the effects of lightning on aircraft. The standardized external current waveforms have in turn been used to derive standardized transient voltage and current test waveforms that can be expected to appear on cable bundles and at equipment interfaces within an aircraft.
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).
HISTORICAL
2013-01-03
Standard
ARP1533B
SAE Aerospace Recommended Practice ARP1533 is a procedure for the analysis and evaluation of the measured composition of the exhaust gas from aircraft engines. Measurements of carbon monoxide, carbon dioxide, total hydrocarbon, and the oxides of nitrogen are used to deduce emission indices, fuel-air ratio, combustion efficiency, and exhaust gas thermodynamic properties. The emission indices (EI) are the parameters of critical interest to the engine developers and the atmospheric emissions regulatory agencies because they relate engine performance to environmental impact. While this procedure is intended to guide the analysis and evaluation of the emissions from aircraft gas turbine engines, the methodology may be applied to the analysis of the exhaust products of any hydrocarbon/air combustor.
CURRENT
2012-11-21
Standard
ARP5062A
The purpose of this SAE Aerospace Recommended Practice (ARP) is to provide recommended test fluids for testing of electrical components used on aircraft exterior or for ground support near aircraft. These fluids were selected based on a consolidation of test fluids used by military and commercial sources and on review of national and international component specifications. These recommendations are general guidelines. Safety factors for any unusual testing applications or operating conditions should be given special consideration by the designer. The test fluids provided are intended to be recommendations and are not intended to limit or supersede those recommended by aircraft or ground support equipment manufacturers.
CURRENT
2012-11-21
Standard
ARP4084B
The purpose of this SAE Aerospace Recommended Practice (ARP) is to standardize locations of aircraft ground service connections to accommodate the trend toward fixed systems, which use the passenger boarding bridge and/or underground “pop-up” or pit systems as a source of utilities. It must be recognized that, in standardizing the locations of the aircraft service connections, they must continue to be served efficiently in those instances where mobile ground support equipment is used. There is an ever increasing number of fixed installations for aircraft servicing. The objectives to be met by standardizing the locations of the aircraft service connections are the following:
HISTORICAL
2012-11-01
Standard
ARP5718A
This document describes: the preparatory steps to test experimental Type II, III, and IV fluids according to AMS1428; the recommendations for the preparation of samples for endurance time testing according to ARP5485; a short description of the recommended field spray test; the protocol to generate draft holdover time guidelines from endurance time data obtained from ARP5485; the protocol for inclusion of Type II, III, and IV fluids on the FAA and Transport Canada lists of fluids and the protocol for updating the lists of fluids; the role of the SAE G-12 Aircraft Deicing Fluids Committee; the role of the SAE G-12 Holdover Time Committee; the process for the publication of Type II, III,and IV holdover time guidelines. This document does not describe laboratory testing procedures. This document does not include the qualification process for AMS1424 Type I fluids.
HISTORICAL
2012-10-16
Standard
AS5681A
This SAE Aerospace Standard (AS)/Minimum Operational Performance Specification (MOPS) specifies the minimum performance requirements of Remote On-Ground Ice Detection Systems (ROGIDS). These systems are ground-based. They provide information that indicates whether frozen contamination is present on aircraft surfaces. Section 1 provides information required to understand the need for the ROGIDS, ROGIDS characteristics, and tests that are defined in subsequent sections. It describes typical ROGIDS applications and operational objectives and is the basis for the performance criteria stated in Section 3 through Section 5. Section 2 provides reference information, including related documents, abbreviations and definitions. Section 3 contains general design requirements for the ROGIDS. Section 4 contains the Minimum Operational Performance Requirements for the ROGIDS, which define performance in icing conditions likely to be encountered during ground operations.
CURRENT
2012-10-15
Standard
AIR5697A
This SAE Aerospace Information Report (AIR) contains regulatory and guidance information related to airplane wheels, tires, and brakes. It contains certain Civil Air Regulations (CAR) and Federal Aviation Regulations (formerly referred to as FARs) from Title 14 Code of Federal Regulations (CFR) in their current version as well as the historical versions. This gives the reader an ability to assemble certain CAR/CFR parts as they existed at any date in the past (referred to as a Regulatory Basis). A certain amount of preamble explanatory material is included, which led to the regulatory rule changes (Amendments to the CFR).
CURRENT
2012-08-30
Standard
ARP997D
The recommendations cover stowage of all portable cabin emergency equipment, including: Oxygen bottles/units Oxygen masks Fire extinguishers Protective breathing equipment (PBE) First aid kits Emergency/expanded medical kits and pouches Megaphones Flashlights Life rafts Survival kits Life preservers Flotation seat cushions Emergency locator transmitters (ELT) Automatic external defibrillators (AED) Resuscitation/life support equipment
2012-08-20
WIP Standard
AS412C
To specify minimum requirements for carbon monoxide detector instruments for use in aircraft, the operation of which may subject the instrument to the environmental conditions specified in Paragraph 3.3. This standard is not intended to cover fire detectors. This Aeronautical Standard covers the basic type of carbon monoxide detector instrument used to determine toxic concentrations of carbon monoxide by the measurement of heat changes through catalytic oxidation.
Viewing 121 to 150 of 728