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Standard

Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Procurement Specification

2018-10-24
CURRENT
AS1650F
This SAE Aerospace Standard (AS) defines the requirements for a threadless, flexible, self-bonding coupling assembly which, when installed on machined fixed-cavity ferrules, provides a flexible connection for joining tubing and components in aircraft fuel, vent, or other systems. This assembled coupling, hereafter referred to as the assembly, is designed for use from -65 to +400 °F and at 125 psig nominal operating pressure. AS1650 was not designed for the new certification requirements for flammable leakage zones and fuel tanks for lightning protection and assembly redundancy. As such, their use and installation may require additional efforts and equipment to support new FAA CFR compliance. The AS7510 flexible coupling should be the preferred coupling for use in flammable leakage zones and fuel tanks that require service life and functionality for lightning protection and part redundancy.
Standard

Solid Runway Deicing/Anti-Icing Product

2018-10-24
CURRENT
AMS1431E
This specification covers a runway deicing and anti-icing product in the form of a solid. Unless otherwise stated, all specifications referenced herein are latest (current) revision.
Standard

Laser-Powder Bed Fusion (L-PBF) Produced Parts, 17-4PH H1025 Alloy

2018-10-24
WIP
AMS7016
his specification covers a corrosion and heat-resistant steel alloy in the form of parts produced by laser-powder bed fusion (L-PBF) that are subjected to a solution anneal and precipitation heat treat operations. Parts may require subsequent machining or surface finishing to meet specific application requirements.
Standard

Methods and Processes for Evaluation of Aerodynamic Effects of SAE-Qualified Aircraft Ground Deicing/Anti-Icing Fluids

2018-10-24
CURRENT
ARP6852C
This document describes methods that are known to have been used by aircraft manufacturers to evaluate aircraft aerodynamic performance and handling effects following application of aircraft ground deicing/anti-icing fluids (“fluids”), as well as methods under development. Guidance and insight based upon those experiences are provided, including: Similarity analyses Icing wind tunnel tests Flight tests Computational fluid dynamics and other numerical analyses This document also describes: The history of evaluation of the aerodynamic effects of fluids The effects of fluids on aircraft aerodynamics The testing for aerodynamic acceptability of fluids for SAE and regulatory qualification performed in accordance with AS5900 Additionally, Appendices A to E present individual aircraft manufacturers’ histories and methodologies which substantially contributed to the improvement of knowledge and processes for the evaluation of fluid aerodynamic effects
Standard

Identification and Assessment for Damage to Composite Aircraft Structures Training Document

2018-10-23
WIP
AIR6825
Individuals who complete this course will be able to define the type of damage, define the extent of damage, determine if further inspection is required, and provide accurate documentation of the damage. The intended outcome of the training is increased safety such that no aircraft is released with unknown damage and that the aircraft meets continued airworthiness requirements. The goal is to change the culture from damage discovery to damage reporting while also reducing or eliminating flight delays due to incorrect or insufficient information.
Standard

Aircraft Tire Inspection - In-Service Removal Criteria

2018-10-23
WIP
ARP6225A
This document is for establishing tire removal criteria of on-wing civil aircraft tires only. This document is primarily intended for use with commercial aircraft but may be used on other categories of civil aircraft as applicable. The criteria are harmonized with the Care and Service Manuals of the tire manufacturers for both radial and bias tires.
Standard

SAE-1001 Application Guide

2018-10-23
WIP
SAE1001/1
The Application Guide will provide additional information on the application and use of SAE1001, including different development approaches, specialties and domains, as well as scalability to different project and system scope. (SAE-1001/1 - Information Report)
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