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Viewing 511 to 540 of 35878
2017-10-16
WIP Standard
AIR6965
Provide a fundamental understanding of reason for completing a bode plot on the balance machine. Discuss potential causes of a resonance within the balance process. Discuss the basis for the WN^2 requirement and how it pertains to the bode plot. Provide guidelines for the usage and interpretation of the bode plot.
2017-10-16
WIP Standard
AIR6964
Provide guidance on how balance machine vector data is captured and reported. Provide an understanding of how to transform balance machine vector data to alternate locations. Provide guidance on how vector imbalances may be used to evaluate and diagnose balance process performance.
2017-10-16
WIP Standard
AMS2368E
This specification provides a standard set of procedures for sampling and testing to meet the requirements of material specifications for wrought titanium and titanium alloy products, except forgings and forging stock. It is applicable to the extent specified in a material specification.
2017-10-16
WIP Standard
AS6070/9
Require an Ethernet cable with electrical parameters equal to the AS6070/2 or /4 with the construction parameters of the /5 or /6.
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).
2017-10-16
WIP Standard
SAE6906
The standard would include requirements for HSI management [planning, execution, coordination (internal and external) documentation, administration and quality control], including collaboration among HSI domains, coordination between HSI and other disciplines to optimize total system performance, optimize human performance, and minimize personnel-driven risks and customer ownership costs.
2017-10-14
WIP Standard
AMS3374E
This specification covers six (6) types of sealing compounds curing to elastomeric materials.
2017-10-14
WIP Standard
AS5127C
This standard describes the accepted methods used for preparing aerospace sealant test specimens for qualification and quality conformance or acceptance testing. AS5127/1 and AS5127/2 are to be used in conjunction with this document and the applicable AMS specifications.
CURRENT
2017-10-13
Standard
AMS4463A
This specification covers an aluminum alloy in the form of plate 0.750 to 1.500 inch, incl ( 19.05 to 38.10 mm, incl) in thickness (see 8.5).
CURRENT
2017-10-13
Standard
AMS4296C
This specification covers an aluminum alloy in the form of sheet and plate 0.032 to 0.310 inch, incl (0.81 to 7.87 mm, incl) in thickness, clad on both sides (see 8.4).
2017-10-13
WIP Standard
AS7510A
This SAE Aerospace Standard (AS) defines the requirements for a threadless, flexible, high conductive self-bonding coupling assembly which, when installed on defined ferrules, provides a flexible connection for joining ducting and components in pressurized fluid systems. The assembled coupling is designed to provide interchangeability of parts and components between qualified manufacturers for use from -65 to +265 °F at 130 psi nominal operating pressures and for the service life of the aircraft system.
2017-10-13
WIP Standard
AS7516A
SCOPE IS UNAVAILABLE.
CURRENT
2017-10-13
Standard
AMS6456E
This specification covers a low-alloy steel in the form of welding wire.
CURRENT
2017-10-12
Standard
AMS6328N
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
CURRENT
2017-10-12
Standard
AMS2804D
This specification covers the requirements for identification of castings.
CURRENT
2017-10-11
Standard
AS6089
This document was prepared by the SAE AS-1A2 Committee to establish techniques for validating the Network Controller (NC) complies with the NC requirements specified in AS5653, Revision B. Note that this verification document only verifies the specific requirements from AS5653 and does not verify all of the requirements invoked by documents that are referenced by AS5653. The procuring authority may require further testing to verify the requirements not explicitly defined in AS5653 and in this verification document.
CURRENT
2017-10-10
Standard
AMS4464A
This specification covers an aluminum alloy in the form of plate 0.500 to 1.500 inch, incl (12.70 to 38.10 mm, incl) in thickness (see 8.4).
CURRENT
2017-10-10
Standard
AMS4467B
This specification covers an aluminum alloy in the form of alclad sheet and plate supplied in the -T861 temper.
CURRENT
2017-10-10
Standard
AMS4206C
This specification covers an aluminum alloy in the form of plate 0.500 to 1.500 inches (12.70 to 38.10 mm) inclusive, in thickness (see 8.4).
CURRENT
2017-10-10
Standard
AIR6504
This SAE Aerospace Information Report (AIR) provides a method for assessing particle losses that occur in a sampling system of specified geometry based on the nvPM mass and number measured at the end of the sampling system. Both size dependent diffusion loss and size independent thermophoretic loss mechanisms are included in the method. The penetration function of that system must be determined by measurement and/or by computation using an analytical method as described within this report. The outcome of this line loss assessment provides estimated correction factors for nvPM mass and number concentration with associated uncertainties based upon nvPM measurement uncertainties and method assumptions. These correction factors give an estimation of nvPM mass and number values at the inlet to the sampling system.
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
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
AS18280/1C
This SAE Aerospace Standard (AS) establishes the requirements for bite type sleeves for use with 24° cone flareless fluid connection fittings per AS18280.
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.
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
AMS4329B
This specification covers an aluminum alloy in the form of plate 4.001 to 7.000 inch, incl. (101.62 to 177.80 mm, incl.) in thickness (see 8.4).
Viewing 511 to 540 of 35878