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Viewing 1 to 30 of 3743
2017-12-08
WIP Standard
AS85421B
Revision clarifies qualification/manufacturing details regarding initial form of fitting (standard near-net forgings, oversize forgings or bar stock). Additionally, replacing the lot-to-lot destructive testing with standardized periodic test procedures.
CURRENT
2017-12-07
Standard
ARP5718B
This document describes: a. the preparatory steps to test experimental Type II, III, and IV fluids according to AMS1428; b. the recommendations for the preparation of samples for endurance time testing according to ARP5485; c. a short description of wind tunnel testing; d. a short description of the recommended field spray test; e. the protocol to generate draft holdover time guidelines from endurance time data obtained from ARP5485; f. 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; g. the role of the SAE G-12 Aircraft Deicing Fluids Committee; h. the role of the SAE G-12 Holdover Time Committee; and i. 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 requirements for AMS1424 Type I fluids (these are provided in ARP6207).
CURRENT
2017-12-05
Standard
AS5498A
This document contains Minimum Operational Performance Specification (MOPS) of ACTIVE on-board INFLIGHT Icing Detection Systems (FIDS). This MOPS specifies FIDS Operational Performance which is the minimum necessary to satisfy regulatory requirements for the design and manufacture of the equipment to a minimum standard and guidance towards acceptable means of compliance when installed on an AIRCRAFT. Detection of ICE accreted on the AIRCRAFT during ground operations is not considered in this document. This MOPS was written for the use of FIDS on AIRCRAFT as defined in 1.3 and 2.3. Expected minimum performance specifications for FIDS and their FUNCTIONS are provided in Section 3. The minimum performance requirements as defined in Section 3 do not consider SYSTEM performance as installed on the AIRCRAFT. Performance in excess of the minimum performance may be required by the SYSTEM installed on an AIRCRAFT in order to meet regulatory or operational requirements.
2017-12-01
WIP Standard
ARP1176B
This SAE Aerospace Recommended Practice (ARP) provides recommended practices for cleaning aircraft oxygen equipment such as tubing, pieces, parts (including regulator and valve parts), cylinders and ground-based equipment that may be used to support aircraft oxygen systems. This revision introduces a cleanliness coding scheme that can be referenced as a requirement, and/or referenced to identify compliance to meeting such a requirement. These methods may apply to gaseous and liquid oxygen equipment. This document specifies work area details, methods to select suitable cleaning agents, cleaning methods, test methods to verify cleanliness level, and methods of packaging the components and parts after cleaning. Technicians designated to clean oxygen equipment must be qualified and trained to clean oxygen equipment. This ARP is applicable to metallic and non-metallic parts.
CURRENT
2017-11-30
Standard
ARP6539
This SAE Aerospace Recommended Practice (ARP) provides a process for the verification and validation of monitors used in highly-integrated and complex aircraft flight control and related systems.
CURRENT
2017-11-30
Standard
AIR1213A
The scope of this report is limited to a discussion of candidate radioisotope power systems which are presently in varying stages of development, and is oriented principally towards aerospace applications.
2017-11-10
WIP Standard
SAE5145A
This SAE Aerospace Information Report (AIR) lists whole body anthropometric surveys and provides current sources for the survey raw data and summary statistics. The purpose of this directory is to provide a single source for accessing anthropometric survey data for human modelers, human factors specialists, and other interested in anthropometric data. It is not meant to provide detailed data on each survey, but to provide readers with enough information to allow them to make a decision about which surveys are of possible application to their work. The reader can then obtain further information and actual data from the listed points of contact.
CURRENT
2017-11-09
Standard
ARP594F
The requirements presented in this document address the key considerations for thermal safety in aircraft fuel pump design. Document sections focus on understanding safety relative to an electrically motor driven fuel pump assembly acting as an ignition source for explosive fuel vapors within the airplane tank.
CURRENT
2017-11-09
Standard
ARP991C
This document recommends design objectives for navigation, position, and anticollisionlight systems for visual detection and collision avoidance between airplanes in flight and on the ground. Customers for new airplanes or lighting components, and designers or manufacturers may take advantage of this document in specifying the initial requirements that, in most cases, significantly exceed the applicable minimum intensities as shown in the Federal Aviation Regulations as well provide better stability, longer life and lower operating costs.
2017-10-26
WIP Standard
ARP6812
This SAE Aerospace Recommended Practice (ARP) covers the functional, design, construction, and test requirements for Brake Temperature Monitoring Systems (BTMS), and sometimes referred to as Brake Temperature Indication Systems (BTIS). The BTMS is limited to aircraft where a dispatch indication and brake temperature indication is required. The scope of this BTMS equipment shall be limited to the 1) brake temperature sensor or indicator, 2) temperature reference measurement, if required, and 3) processing and communication of brake temperature. This recommended practice will not address cockpit ergonomics and aircraft operating procedures.
2017-10-25
WIP Standard
ARP1840C
This document establishes two types of engine transport devices: Type A: For split engine pack transport (mainly lower deck) Type B: For full engine transport (mainly main deck)
2017-10-25
WIP Standard
ARP4166A
This Aerospace Recommended Practice (ARP) defines and establishes design, construction, and performance requirements for a flexible, reusable, water-vaporproof cover for environmental protection of internal combustion engines, major components, and other military and commercial items.
2017-10-25
WIP Standard
ARP4898A
This SAE Aerospace Recommended Practice (ARP) recommends design and test criteria for reusable shipping and storage stands for aircraft engines. An optional hard cover (enclosure) is also specified.
2017-10-25
WIP Standard
ARP4732A
This SAE Aerospace Recommended Practice (ARP) defines and establishes design, construction, and performance requirements for a flexible nonreuseqble waterproof cover for shipment of aircraft engines, major components, and other military and commercial items not intended for storage; items to be removed within fourteen (14) days.
2017-10-25
WIP Standard
AS18013A
No scope available.
2017-10-25
WIP Standard
AS5135A
This SAE Aerospace Standard (AS) describes the characteristics of a desiccant port installed through the flat wall of a shipping and storage container. With the cover removed, the desiccant port shall provide access to the interior of the container for installation and removal of desiccant.
2017-10-25
WIP Standard
AS5017A
This SAE Aerospace Standard (AS) describes the characteristics of an air filling valve used in reusable shipping and storage containers.
2017-10-25
WIP Standard
ARP726B
This recommended practice covers a self-contained detection system which is capable of pressurizing a closed system up to 70 psig with halogen (tracer) gas and up to 3500 psig with nitrogen. An external tracer gas supply may be used to increase the capacity of the system. The detector shall be capable of detecting leaks as small as .05 ounce of tracer gas per year, with a system pressure of 70 psig or less. The purpose of this document is to provide a recommended practice for the design of a universal leak detector which will pressurize a closed system with a mixture of inert and tracer gas and provide a probe and detector to indicate location and rate of system leakage with a high degree of accuracy.
CURRENT
2017-10-25
Standard
ARP60493
This guide provides detailed information, guidance, and methods for demonstrating electromagnetic compatibility (EMC) on civil aircraft. This guide addresses aircraft EMC compliance for safety and functional performance of installed electrical and electronic systems. The EMC guidance considers conducted and radiated electromagnetic emissions and transients generated by the installed electrical and electronic systems which may affect other installed electrical and electronic systems on the aircraft. Application of appropriate electrical and electronic equipment EMC requirements are discussed. Methods for aircraft EMC tests and analysis are described. This guide does not address aircraft compatibility with the internal electromagnetic environments of portable electronic devices (PED) or with the external electromagnetic environments, such as high-intensity radiated fields (HIRF), lightning, and precipitation static.
2017-10-23
WIP Standard
AMS1435D
This specification covers deicing and anti-icing materials in the form of a fluid. This deicing/anti-icing fluid has been used typically on runways, taxiways, and other aircraft maneuvering areas for the prevention and removal of frozen deposits of frost and ice. Fluids must not be used to deice/anti-ice aircraft.
2017-10-22
WIP Standard
ARP6001A
This SAE Aerospace Recommended Practice (ARP) provides general requirements for a generic “passive” side stick that could be used for fly by wire transport and business aircraft. It addresses the following: - The functions to be implemented - The geometric and mechanical characteristics - The mechanical and electrical interfaces - The safety and certification requirements
2017-10-20
WIP Standard
AS4108C
This specification defines the requirements for A286 cres T-bolts and eye bolts, with room temperature tensile strength of a minimum of 160000 psi, for use with clamps and V-band couplings at 1000 °F maximum ambient temperature.
2017-10-20
WIP Standard
AIR5128B
This SAE Aerospace Information Report (AIR) is limited to the subject of aircraft fuel systems and the questions concerning the requirements for electrical bonding of the various components of the system as related to Static Electric Charges, Fault Current, Electromagnetic Interference (EMI) and Lightning Strikes (Direct and Indirect Effects). This AIR contains engineering guidelines for the design, installation, testing (measurement) and inspection of electrical bonds.
2017-10-16
WIP Standard
ARP6448A
This document provides an industry-recommended framework for establishing agreements to ensure that seats with integrated electronic components (e.g., actuation system, reading light, inflatable restraint, IFE, etc.) meet the seat TSO Minimum Performance Standard. These agreements will allow Seat Suppliers to build and ship completed, integrated and approved seat assemblies under TSOA with electronics included. The document presents the roles, responsibilities and accontibilities of the Electronics Manufacturer, the Seat Supplier, and the Seat Installer/Electronics Activator in the context of AC 21-49 Section 7.b ‘ Type Certification using TSO-approved seat with electronic components defined in TSO design’. This document applies to all FAA seat TSOs (C39(), C127()…etc).
2017-10-13
WIP Standard
AS7516A
SCOPE IS UNAVAILABLE.
CURRENT
2017-10-10
Standard
ARP5945A
The purpose of this Aerospace Recommended Practice (ARP) is to provide the sample selection criteria and endurance time test procedures for SAE Type I aircraft deicing/anti-icing fluids, required for the generation of endurance time data of acceptable quality for review by the SAE G-12 Holdover Time Committee. A significant body of previous research and testing has indicated that all Type I fluids formulated with conventional glycols, as defined in 3.1.1 of AMS1424, perform in a similar manner from an endurance time perspective. This applies to Type I deicing/anti-icing fluids formulated with propylene glycol, ethylene glycol, and diethylene glycol only. As a result, Type I deicing/anti-icing fluids containing these glycol bases no longer require testing for endurance times.
CURRENT
2017-10-10
Standard
ARP5485B
The purpose of this Aerospace Recommended Practice (ARP) is to provide the sample selection and endurance time test procedures for SAE Type II, III, and IV aircraft deicing/anti-icing fluids, required for the generation of endurance time data of acceptable quality for review by the SAE G-12 Holdover Time Committee. The related standard ARP5718 provides the process by which endurance time data is converted to holdover times for publication by regulators and subsequent use by aircraft operators.
CURRENT
2017-10-10
Standard
ARP6207
This document describes: the preparatory steps to test experimental Type I fluids according to AMS1424; the recommendations for the preparation of samples for endurance time testing according to ARP5945; a short description of the recommended field spray test; the protocol to demonstrate that Type I fluid can be used with the Type I holdover time guidelines published by the FAA and Transport Canada, including endurance time data obtained from ARP5945; the protocol for inclusion of Type I fluids on the FAA and Transport Canada lists of fluids; the protocol for updating the FAA and Transport Canada lists of fluids; the role of the SAE G-12 Aircraft Deicing Fluids Committee; the role of the SAE G-12 Holdover Time Committee; and the process for the publication of Type I holdover time guidelines. This document does not describe laboratory-testing procedures. This document does not include the qualification requirements for AMS1428 Type II, III, and IV fluids (these are provided in ARP5718).
CURRENT
2017-10-10
Standard
ARP6385
The requirements presented in this document address the key considerations for mechanical and electrical safety in aircraft fuel pump design. Document sections focus on understanding safety relative to an electrically motor driven fuel pump assembly acting as an ignition source for explosive fuel vapors within the airplane tank.
2017-10-05
WIP Standard
AIR6811
Provide guidance for applying aircraft equipment electromagnetic, electrical, and mechanical qualification standards, including RTCA/DO-160, MIL-STD-461, MIL-STD-810, and MIL-STD-704, to civil aircraft certification intended for military use and for military aircraft equipment installed on civil aircraft. The guidance will identify where the equipment environmental qualification standards meet the intent of the civil or military aircraft certification requirements. Conversely, the guidance will identify where the equipment environmental qualification standards have differences that do not meet the intent of the civil or military aircraft certification requirements and when these differences matter based on equipment criticality.
Viewing 1 to 30 of 3743

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