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Items (212,183)
This specification covers a non-phenolic, non-chromated, thickened paint remover in the form of a solvent-base liquid.
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers an alkaline cleaner in the form of a liquid for use above 65 °C (154 °F).
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a water-base cleaner in the form of a concentrated liquid.
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a beryllium aluminum alloy in the form of investment castings.
AMS G Titanium and Refractory Metals Committee
This specification covers chromium-molybdenum (4130) seamless and welded steel tubing of aircraft quality.
AMS E Carbon and Low Alloy Steels Committee
This specification covers a mold release agent in the form of a liquid.
AMS P17 Polymer Matrix Composites Committee
This specification covers honeycomb core made of polyamide paper sheets in a non-hexagonal, flexible cell configuration and supplied in the form of blocks, slices, and ordered shapes.
AMS P17 Polymer Matrix Composites Committee
This specification covers a foaming-type, heat-curing, resin-base adhesive in the form of paste or sheet.
AMS P17 Polymer Matrix Composites Committee
This report revises ARD50015 document to the AIR format. This report, as was the original, is intended to complement ARP1420C and AIR1419C documents issued by the SAE S-16 Committee on spatial total-pressure distortion. These previous documents addressed only total-pressure distortion and excluded total temperature distortion. The subject of inlet total temperature distortion is addressed in this report with some background and identification of the problem area. The status of past efforts is reviewed, and an attempt is made to define where we are today. Deficiencies, voids, and limitations in knowledge and test techniques for total temperature distortion are identified.
S-16 Turbine Engine Inlet Flow Distortion Committee
This specification covers expanded honeycomb core made of glass cloth impregnated with polyimide resin and supplied in the form of blocks, slices, and ordered shapes.
AMS P17 Polymer Matrix Composites Committee
This specification establishes the acceptance criteria and inspection requirements for adhesive-bonded sandwich structures including the metal-to-metal bonding found in these structures, but usage is not limited to such applications and each application should be considered individually.
AMS P17 Polymer Matrix Composites Committee
This specification and its supplementary detail specifications cover organic fibers in the form of cloth impregnated with epoxy resin, the resin to be supplied in a "B" stage condition.
AMS P17 Polymer Matrix Composites Committee
This specification covers a thermally stable aramid fabric in the form of cloth.
AMS P17 Polymer Matrix Composites Committee
This specification and its supplementary detail specifications cover interleaf carrier materials in the form of polyethylene film or coated paper tape or sheeting.
AMS P17 Polymer Matrix Composites Committee
This specification covers continuous filaments consisting of boron deposited on a tungsten substrate by the hydrogen reduction of boron trichloride.
AMS P17 Polymer Matrix Composites Committee
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