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CURRENT
2017-01-03
Standard
AMS5664F
This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, flash welded rings 10 inches (254 mm) and under in least nominal cross-sectional dimension, and stock of any size for forging or flash welded rings (see 8.5).
CURRENT
2017-01-03
Standard
AMS4779H
This specification covers a nickel alloy in the form of wire, rod, strip, foil, and powder and a viscous mixture (paste) of the powder in a suitable binder.

This filler metal has been used typically for joining corrosion and heat resistant steels and alloys requiring corrosion and oxidation resistant joints with good strength at elevated temperatures, but usage is not limited to such applications. This filler metal may also be used as a corrosion and oxidation resistant hard coating.

CURRENT
2017-01-03
Standard
AMS5132L
This specification covers a high-carbon steel in the form of bars.
CURRENT
2017-01-03
Standard
ARP6852B
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.
2016-12-31
WIP Standard
ARP4048A
The purpose of this document is to delineate the technical specifications for horizontal rotating type, hard-bearing balancing machines for measuring the amount and angle of unbalance corrections required in one or more than one transverse planes to balance gas turbine rotors.
2016-12-29
WIP 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 the recommended field spray test; d. the protocol to generate draft holdover time guidelines from endurance time data obtained from ARP5485; e. 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; f. the role of the SAE G-12 Aircraft Deicing Fluids Committee; g. the role of the SAE G-12 Holdover Time Committee; h. 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 process for AMS1424 Type I fluids.
2016-12-28
WIP Standard
AS8049D

This SAE Aerospace Standard (AS) defines minimum performance standards, qualification requirements, and minimum documentation requirements for passenger and crew seats in civil rotorcraft, transport aircraft, and general aviation aircraft. The goal is to achieve comfort, durability, and occupant protection under normal operational loads and to define test and evaluation criteria to demonstrate occupant protection when a seat/occupant/restraint system is subjected to statically applied ultimate loads and to dynamic impact test conditions set forth in the applicable Federal Regulations 14 CFR 23, 25, 27, or 29.

Guidance for test procedures, measurements, equipment, and interpretation of results is also presented to promote uniform techniques and to achieve acceptable data.

While this document addresses system performance, responsibility for the seating system is divided between the seat supplier and the installation applicant.

CURRENT
2016-12-27
Standard
AMS3892/10B
This specification covers one type of carbon fiber in the form of tow.
2016-12-24
WIP Standard
TAHB0009A
This handbook provides "how to" guidance to industry and government for the reliability Activities and Methods contained in ANSI/GEIA-STD-0009 for developing reliable products and systems, successfully demonstrating them during test and evaluation, and sustaining them throughout the system/product life cycle. ANSI/GEIA-STD-0009 requires the developers and customer/users working as a team to plan and implement a reliability program that provides systems/products that satisfy the user's requirements and expectations using a systems engineering approach. The four Objectives of ANSI/GEIA-STD-0009 are listed below: Objective 1: Understand Customer/User Requirements and constraints. The team (developer, customer, and user), includes the Activities necessary to ensure that the user's requirements and product needs are fully understood and defined, so that a comprehensive design specification and Reliability Program Plan are generated. Objective 2: Design and redesign for reliability.
2016-12-21
WIP Standard
ARP6915
This Aerospace Recommended Practice (ARP) offers best practice regarding the implementation of IVHM systems taking into account Human Factors, both the vehicle crew and the maintenance staff. The document will include considerations regarding both military and civil fixed wing aircraft. Safety implications will also be addressed.
2016-12-21
WIP Standard
AMS2808E
This specification covers requirements for identification of forgings, including die forgings, hand forgings, and rolled rings.
CURRENT
2016-12-21
Standard
AS6070/2A
SCOPE IS UNAVAILABLE.
2016-12-21
WIP Standard
AS81765A
This specification covers requirements for material used in electrical insulating heat shrinkable components. The continuous operating temperature of these materials shall range from -75°C to +200°C (-103°F to +392°F).

Classification: The properties of heat shrinkable molded components shall be as specified in the applicable specification sheet.

2016-12-21
WIP Standard
AMS2800E
This specification covers the requirements for identification of finished parts.
2016-12-21
WIP Standard
AMS3582B
This specification covers a crosslinked polyvinyl chloride plastic in the form of flexible, thin-wall, heat-shrinkable tubing. Primarily for use as a flexible, electrical insulation tubing whose diameter can be reduced to a predetermined size by heating to 175 degrees C (345 degrees F) or higher. This tubing is stable for continuous exposure from -20 to +105 degrees C (-5 to +220 degrees F).
2016-12-21
WIP Standard
AMS3579E
This specification covers a non-crosslinked polyvinyl chloride plastic in the form of flexible, thin-wall, heat-strinkable tubing with a low recovery temperature.

These products have been used typically as a flexible, electrical insulation tubing whose diameter can be reduced to a predetermined size by heating to 150 degrees C (302 degrees F) or higher, but usage is not limited to such applications. This tubing is stable for continuous exposure from -20 to +105 degrees C (-4 to 221 degrees F).

2016-12-21
WIP Standard
AMS3593B
This specification covers an irradiated, thermally-stabilized, flame-resistant, modified-polyvinylidene-fluoride plastic in the form of extra-thin-wall tubing. Primarily for use as a semi-rigid, electrical insulation tubing and marker sleeves in short lengths whose diameter can be reduced to a predetermined size by heating to temperatures of 175 degrees C (347 degrees F) or higher.
Viewing 91 to 120 of 43606