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Viewing 1 to 30 of 38109
2015-04-01
Standard
CPGM1_16LGXCAD
This product includes information on the manufacturer, engine, application, 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.
2015-04-01
Standard
CPGM1_16LGXCT6
This product includes information on the manufacturer, engine, application, 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.
2015-04-01
Standard
CPGM2_16LGXCT6
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.
2015-03-31
WIP Standard
AS50571B
This specification covers the general requirements for red and white individual instrument lights. This document has been streamlined. Appendix A to MIL-L-5057F lists those documents required for MIL-L-5057F acquisition and is a mandatory part of MIL-L-5057F. Those documents listed in Appendix A have the same status as those referenced directly in MIL-L-5057F (first tier documents). All other documents, referenced through tiering, may be used as guidance and information to supplement MIL-L-5057F. This document’s scope is limited to lamp source designs solely. Furthermore, the use of red lighting should not be considered for new design and included within this document to support requirements for existing military aircraft that still operate with this system of lighting.
2015-03-31
WIP Standard
G15AA
New AMS for Ti-6-4 Seamless, Hydraulic Tubing including Technical, Quality and Testing Requirements
2015-03-31
WIP Standard
J551/17
This SAE Standard specifies the test methods and procedures for testing passenger cars and commercial vehicles to magnetic fields generated by power transmission lines and generating stations.
2015-03-31
WIP Standard
AMS4897D
This specification covers a titanium alloy in the form of sheet and strip.
2015-03-30
WIP Standard
AMS6312J
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
2015-03-30
WIP Standard
AMS6250M
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
2015-03-30
WIP Standard
AMS6300G
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
2015-03-30
WIP Standard
AMS6413M
This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing.
2015-03-30
WIP Standard
AMS6342K
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
2015-03-30
WIP Standard
AMS6422K
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
2015-03-30
WIP Standard
AMS6437J
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
2015-03-30
WIP Standard
AMS6421G
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
2015-03-30
WIP Standard
AMS7719E
This specification covers a magnetic nickel-iron alloy in the form of sheet and strip.
2015-03-30
WIP Standard
ARP1110C
The purpose of this SAE Aerospace Recommended Practice (ARP) is to provide the aerospace industry with recommendations concerning the minimization of stress corrosion cracking in wrought heat-treatable carbon and low alloy steels and in austenitic, precipitation hardenable, and martensitic corrosion-resistant steels and alloys. The detailed recommendations are based on laboratory and field experience and reflect those design practices and fabrication procedures which should avoid in-service stress corrosion cracking.
2015-03-30
WIP Standard
AMS7717E
This specification covers a magnetically soft nickel-iron alloy in the form of sheet and strip.

These products have been used typically for parts used in magnetic circuits requiring high magnetic permeability and saturation induction with the fabricated parts to be annealed in dry hydrogen, but usage is not limited to such applications.

2015-03-30
WIP Standard
AMS6439E
This specification covers a premium-aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
2015-03-30
WIP Standard
AMS7718H
This specification covers a magnetically soft nickel-iron alloy in the form of bars, rods, forgings, mechanical tubing, and forging stock.
2015-03-30
WIP Standard
AMS1532E
This specification covers an emulsion-type cleaner in the form of a liquid.
2015-03-30
WIP Standard
AMS6356H
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
2015-03-30
WIP Standard
AMS6396F
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
2015-03-30
WIP Standard
AMS6357L
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
2015-03-30
WIP Standard
AMS6370P
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.
2015-03-29
Standard
AS4311A
SCOPE IS UNAVAILABLE.
2015-03-29
Standard
AS4309D
SCOPE IS UNAVAILABLE.
2015-03-29
Standard
AS4310A
SCOPE IS UNAVAILABLE.
2015-03-29
Standard
AIR4176A
The purpose of this SAE Aerospace Information Report (AIR) is to provide information that would be useful to potential users/operators and decision makers for evaluating and quantifying the benefits of an Engine Monitoring Systems (EMS) versus its cost of implementation. This document presents excerpts from reports developed to analyze "actual aircraft cost/benefits results". These are presented as follows: a. First, to outline the benefits and cost elements pertaining to EMS that may be used in performing a cost versus benefits analysis. b. Second, to present considerations for use in conducting the analysis. c. Third, to provide examples of analyses and results as they relate to the user/operator and decision-maker community. The document encompasses helicopters and fixed wing aircraft and distinguishes between civilian and military considerations.
2015-03-29
WIP Standard
AMS4944L
This specification covers a titanium alloy in the form of seamless tubing.
Viewing 1 to 30 of 38109

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