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Standard

Webbing, Tubular, Low Modulus Aramid 3-3/16 Wide, 2250 (10 008) Breaking Strength

2018-07-31
CURRENT
AMS3799/4D
This specification covers one width and one strength of low modulus aramid tubular webbing. This product has been used typically in construction of parachutes, but usage is not limited to such applications. 3-3/16 inches (81 mm) wide low modulus aramid tubular webbing having 2250 pounds force (10,008 N) breaking strength.
Standard

Cloth, Airplane, Mercerized Cotton 80 Pounds Force (356 N) Breaking Strength

2018-07-31
CURRENT
AMS3806G
This specification covers one strength and one weave of mercerized cotton cloth known as "airplane cloth." This cloth has been used typically for covering aircraft surfaces, such as wings, fuselage, ailerons, elevators, and other airfoil surfaces, but usage is not limited to such applications.
Standard

Fittings, Tube, Fluid Systems, Separable, Beam Seal, 3000/4000 psi, General Specification For

2018-07-31
CURRENT
AS85421B
This specification covers the design requirements and test procedures for separable beam seal fittings which includes end fittings (see 2.3.4), fitting bodies (see 2.3.7), and boss fittings (see 2.3.2) for use in aerospace fluid systems. Design requirements are for class 3000 in corrosion resistant steel (15-5 PH, 17-4 PH CRES) only and for class 4000 in titanium alloy (Ti) and corrosion and heat-resistant steel (Nickel Alloy 718 CRES) only. Definition of fittings and related terms are defined in 2.3.
Standard

Adhesives, Sealants, and Heat Transfer Materials in Battery Systems: A Primer on Applications, Manufacturing and End-Use Performance Requirements

2018-07-30
WIP
J3178
This document provides an overview of adhesives, sealants, and heat transfer materials commonly used in battery packs. Specific attention is given to the location where such materials are used within in a representative (automobile) battery pack, their basic chemical makeup, and general performance requirements during manufacturing and in end-use.
Standard

Steel, Corrosion and Heat Resistant, Bars, Wire, Forgings, Mechanical Tubing, and Rings 18Cr - 11Ni - 0.60Cb (Nb) (347) Premium Aircraft Quality, Consumable Electrode Melted Solution Heat Treated

2018-07-30
CURRENT
AMS5654G
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 over 0.50 inch (12.7 mm) in nominal diameter or least distance between parallel sides (see 8.6).
Standard

J1349 Certified Power Engine Data for GM as used in 2019 Chevrolet Blazer - Level 2

2018-07-30
CURRENT
CPGM2_19LGXBLAZ
This product includes information on the manufacturer, engine, applications, testing location, certified maximum horsepower, certified maximum torque along with the certified curves of horsepower and torque over a wide range of engine RPM speeds. In addition, this product contains complete engine information such as displacement, cylinder configuration, valve train, combustion cycle, pressure charging, charge air cooling, bore, stroke, cylinder numbering convention, firing order, compression ratio, fuel system, fuel system pressure, ignition system, knock control, intake manifold, exhaust manifold, cooling system, coolant liquid, thermostat, cooling fan, lubricating oil, fuel, fuel shut off speed, etc. Also included are all measured test parameters outlined in J2723.
Standard

Minimum Performance Standard for Airborne Multipurpose Electronic Displays

2018-07-30
CURRENT
AS8034C
This SAE Aerospace Standard (AS) specifies minimum performance standards for all types of electronic displays and electronic display systems that are intended for use in the flight deck by the flight crew in all 14 CFR Part 23, 25, 27, and 29 aircraft. The requirements and recommendations in this document are intended to apply to all installed electronic displays and electronic display systems including those that have a touch screen interface within the flight deck, regardless of intended function, criticality, or location within the flight deck, but may also be used for non-installed electronic displays. This document provides baseline requirements and recommendations (see 2.3 for definitions of “shall” and “should”). This document primarily addresses hardware requirements, such as electrical, mechanical, optical, and environmental. It does not address system specific functions.
Standard

Power Cylinder Oil Consumption: Transport Mechanisms

2018-07-27
CURRENT
J2794_201807
This document covers oil transport mechanisms from the power cylinder system which might affect oil consumption. It will not discuss in detail the oil consumption mechanisms from other systems or engine components.
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