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2016-09-29
WIP Standard
ARP6328A

This document contains guidance for implementing a counterfeit mitigation program in accordance with AS5553.

The information contained in this document is intended to supplement the requirements of a higher level quality standard (e.g., AS9100) and other quality management system documents. This is not intended to stand alone, supersede, or cancel requirements found in other quality management system documents, requirements imposed by contracting authorities, or applicable laws and regulations unless an authorized exemption/variance has been obtained.

2016-09-28
WIP Standard
AS4841B
This SAE Aerospace Standard (AS) establishes the requirements for 37 degree flared tube fittings or machined internal cone fluid connection fittings for use with 37 degree external cone, spherical nose and seal ring fittings in all types of aerospace fluid systems (see Section 6).
CURRENT
2016-09-28
Standard
AS39029/84B
SCOPE IS UNAVAILABLE.
2016-09-26
WIP Standard
AS3411C
Scope is unavailable.
2016-09-26
WIP Standard
AS7460C
This procurement specification covers aircraft quality bolts and screws made of 6.0Al-4.0V titanium alloy and of 160 ksi tensile strength at room temperature.
2016-09-26
WIP Standard
MA3340C
SCOPE IS UNAVAILABLE.
CURRENT
2016-09-22
Standard
AMS6354G
This specification covers a low-alloy steel in the form of sheet, strip, and plate 4.00 inches (101.6 mm) and under in thickness.
CURRENT
2016-09-22
Standard
AMS6455L
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
CURRENT
2016-09-21
Standard
J583_201609
This SAE standard provides test procedures, performance requirements, design guidelines and installation guidelines for front fog lamps.
2016-09-19
WIP Standard
ARP5935A
Electrolytically deposited chrome plate is the current standard surface treatment for landing gear component interface surfaces that require good wear resistance and corrosion protection. Chrome plated components are typically plagued by a slight debit in fatigue performance, detrimental mud cracking surface pattern, susceptibility to scoring, wear, and seal leakage. In addition, recent changes in environmental compliance standards place further restrictions on the use of electrolytically deposited chromium. Some commercial applications have already eliminated the use of chrome plate on current and future products. As a result, a substitute for electrolytically deposited chrome plate has been sought for several years. High Velocity Oxygenated Fuel (HVOF) thermal spray coatings have been developed to the point where they are being implemented as an alternative to hard chrome plate on high strength low alloy steels for external surfaces on landing gear applications.
2016-09-18
WIP Standard
AS20218B
Scope unavailable.
2016-09-18
WIP Standard
AS6038B
This specification covers antifriction bellcrank ball bearings intended primarily for airframe use.
2016-09-16
WIP Standard
ARP5483B
This SAE Aerospace Recommended Practice establishes methods for testing airframe Rolling Element bearings. The purpose of ARP5483 and its associated slash sheets is to document test methods commonly used to evaluate airframe bearings. These test methods may be referenced in standards, purchase orders, etc. when the test is deemed appropriate to the intended use of the bearing by the end user of the bearing. These test methods are not intended to encompass every conceivable requirement for an airframe bearing. The end user of the bearing must exercise engineering judgment to determine the most appropriate standard and/or nonstandard tests for the application.
CURRENT
2016-09-16
Standard
J1654_201609
This SAE Standard covers unshielded cable intended for use at a nominal system voltage up to 600 V or 1000 V (AC rms or DC). It is intended for use in surface vehicle electrical systems.
2016-09-15
WIP Standard
AS5756/7A
SCOPE IS UNAVAILABLE.
2016-09-15
WIP Standard
AIR5575A
This SAE Aerospace Information Report (AIR) discusses the often overlooked relationship between hot stamp marking and the environmental conditions that contribute aircraft wiring problems and discusses current beliefs of military service experts, regulatory agencies and industry standard writing bodies about the potential hazards imposed by the hot stamping process.

Although prominent members of the aerospace community are taking aggressive measures to phase out the hot stamping of interconnecting wire, the process lingers on, particularly within the operations of smaller manufacturers, modification shops, and operator maintenance facilities. In recent years, non-impact marking processes have been developed that can mark virtually all of the common wire types used in aerospace interconnect applications. The purpose of this document is to encourage full conversion to non-impact marking processes in order to reduce the probability of causing damage to the wire insulation.

2016-09-14
WIP Standard
AS50861B
This specification covers polyvinyl chloride insulated single conductor electric wires made with tincoated copper conductors or silver-coated copper alloy conductors as specified in the applicable detail specification. The polyvinyl chloride insulation of these wires may be used alone or in combination with other insulating or protective materials.
2016-09-13
WIP Standard
AIR5060B
The purpose of this document is to provide reference material for establishing compatibility of electronic gas turbine engine control systems and associated components with the electromagnetic environment and achieving compliance with associated airworthiness requirements.
CURRENT
2016-09-13
Standard
AMS5648M
This specification covers a corrosion and heat-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings, and stock for forging or flash welded rings.
2016-09-12
WIP Standard
AS3209A
Scope is unavailable.
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