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Standard

Calibration Fluid for Diesel Injection Equipment

2018-07-27
WIP
J967
This SAE Standard defines the requirements of a calibration fluid recommended for flow bench testing, calibration, and flushing of fuel injection equipment, in production facilities, in laboratories, and in service establishments.
Standard

Plating, Silver, Nickel Strike, High Bake

2018-07-27
CURRENT
AMS2410L
This specification covers the requirements for electrodeposited silver on other metals, usually with a nickel strike between the basis metal and the silver.
Standard

J1349 Certified Power Engine Data for 2019 Dodge Challenger SC HEMI (Hellcat) - Level 2

2018-07-26
CURRENT
CPFC2_19DODCHHM
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

J1349 Certfied Power Engine Data for FCA as used in 2019 Dodge Challenger SRT HO - Level 2

2018-07-26
CURRENT
CPFC2_19CHALLHO
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

Modules and Basic Racks of Metric Spur and Helical Gears

2018-07-25
WIP
AS1560B
This SAE Aerospace Standard (AS) establishes the standard modules for aerospace metric involute gear teeth and establishes the tooth dimensions of aerospace metric involute gear teeth in terms of the conjugate rack type cutter whose counterpart reference profile is called the basic rack profile of the generated gear, having the tooth dimensions expressed in terms proportional to the module.
Standard

Limits, Table of Limits and Lubrication Charts

2018-07-25
WIP
AS176D
The Table of Limits and the corresponding Limits and Lubrication Charts covered by this specification are to be used in connection with inspection, repair and assembly operations of aircraft engines. Included are such items as fits, clearances, backlashes, spring loads, and the methods of tightening threaded parts such as torque, angle of turn, or bolt stretch. The Lubrication Charts, if furnished, are to be used for tracing the oil flow through the engine.
Standard

Operating Instructions for Aircraft Engines (Preparation of)

2018-07-25
WIP
AS177C
The operating instructions covered by this specification are published for the purpose of providing a background of engine operating information with which a pilot and his crew should be familiar when operating an aircraft powered by a particular engine model. Operating instructions also contain engine operational procedures which serve as a guide for: (1) the preparation of the right manual by the aircraft manufacturer, (2) operating an engine prior to the publication of the aircraft right manual, and (3) instructional purposes. This specification covers the requirements for format and outline of contents of operating instructions in published form or in manuscript from suitable for publication.
Standard

External Hydraulic Fluid Leakage Definition for Landing Gear Shock Absorbers

2018-07-25
CURRENT
ARP6408
The purpose of this SAE Aerospace Recommended Practice (ARP) is to provide a practical definition of external hydraulic fluid leakage exhibited by landing gear shock absorbers/struts. The definition will outline normal (acceptable weepage) and excessive leakage (unacceptable leakage) of shock absorbers/struts that is measurable. The definition of leakage is applicable to new gear assemblies, refurbished/remanufactured (overhauled) shock absorbers/struts, leakage of shock absorbers/struts encountered during acceptance flights, newly delivered and in-service aircraft. This ARP is intended to provide guidelines for acceptable leakage of landing gear shock absorbers/struts between the ambient temperatures of 65 °F (-54 °C) and 130 °F (54 °C) and to outline the procedure for measuring such leakage. The specific limits that are applied to any particular aircraft shall be adjusted by the aircraft manufacturer before inclusion in the applicable maintenance manual.
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