SAE MAM6415C

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This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock procured in SI (Metric) units.

AMS 6415 is the inch/pound version of this MAM.

These products have been used typically for parts, 90 millimeters and under in nominal thickness at time of heat treatment, requiring a through-hardening steel capable of developing a minimum hardness of 40 HRC when properly hardened and tempered and also for parts of greater thickness but requiring proportionately lower hardness, but usage is not limited to such applications.

Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking after heat treatment; ARP 1110 recommends practices to minimize such conditions.

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Published:
03/12/2003
File Size:
1 file , 75 KB

SAE USCAR20

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This life test for underhood/passenger/trunk connector systems may be used in place of Section 5.8.6 (Connector System Electrical Test Flow Chart) of SAE/USCAR-2. All other requirements of SAE/USCAR-2 remain applicable even when this test is used. Refer to SAE/USCAR-2 and Connector/Terminal Supplier for appropriate power rating and current cycle Testing.

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Published:
12/01/2001
File Size:
1 file , 72 KB

SAE USCAR33

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This specification is a general level subsystem light source specification that establishes test requirements of Light Emitting Diode (LED) components and modules for use in automotive lighting systems. The completed test data to this test specification is intended to be provided to the OEM by the Tier I lamp set maker as part of the lamp assembly PPAP. Re-testing shall be required if any portion of the approved LED modules experiences a design, manufacturing or component change. This document shall be applied to systems that meet the requirements for design, performance and validation established by government standards. The LED module is defined as the LED devices and any electronics required to properly energize the LEDs using vehicle electrical power system along with any associated electrical wiring, connectors and thermal management system. Samples shall be tested as a subsystem and considered one test sample for the entire test sequence. A failure of any component in the test sample shall constitute a failure of the entire sample. If other manufactures components are intended to be approved for use in the LED modules, then those possible combinations of components shall be considered a new LED module and shall also be tested. Additional testing may be required by individual OEM’s to meet specific EMC, quality, reliability and durability objectives. The following tests are to be performed under the following conditions: • New sample • Design or process change made to an existing module • Completion of one calendar year as noted in the “ANNUAL TESTS” Table shown in the Appendix. (Note: Production process control data, collected at a shorter interval per an approved control plan, may be substituted if approved by customer’s responsible engineer and purchasing representative.)

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Published:
02/19/2013
File Size:
1 file , 1.1 MB

NBBI NB23-2011

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NBBI NB23-2011

An American National Standard providing rules and guidelines for inservice inspection, repair, and alteration of pressure-retaining items, the National Board Inspection Code (NBIC) is required in many United States and Canadian jurisdictions.

NBBI NB23 is softcover / 3-hole punched. Binders are not included.

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Published:
2011
ANSI:
ANSI Approved
File Size:
3 files , 12 MB

SAE MA4534A

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This document has been declared “Stabilized” and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist.

This SAE Aerospace Standard covers high strength commercial sockets and universal sockets which posses the strength, clearances, and internal wrenching design so configured that, when mated with hexagon (6 point) fasteners, they shall transmit torque to the fastener without bearing on the outer 5% of the fastener’s wrenching points. this document provides additional requirements beyond ANSI B107.5 appropriate for aerospace use.

Inclusion of dimensional data in this document is not intended to imply all of the products described therein are stock production sizes. Consumers are requested to consult with manufacturers concerning lists of stock production sizes

Product Details

Published:
02/10/2013
File Size:
1 file , 2.7 MB