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This specification covers an alkaline permanganate oxide conditioner in the form of a water-soluble powder or a liquid for dilution with water
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers an alkaline-type, water-base cleaner in the form of a liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a coconut-oil-base hand soap in the form of a liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers inert, fluorochemical, liquid heat transfer agents
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a tank-type cleaner in the form of a liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers an acidic oxide remover compound in the form of a ready-to-use liquid, liquid concentrate, or water-soluble powder for dilution with water or for dilution with mineral acid as defined by the compound manufacturer
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers the requirements for removers used on amine-cured epoxy coating systems (see 6.1
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers the requirements for one grade of remover of various organic coatings from aircraft parts
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers one type of a biodegradable, deactant-type deodorizer in the form of an aerosol-packaged liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a cleaner for plastics in the form of a liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a solvent-emulsion cleaner in the form of a solvent-base liquid concentrate
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers materials in the form of a liquid used to remove smut from aluminum surfaces treated with etch-type oxidation and corrosion removers
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers two types of paint remover in the form of a liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers powdered materials, solutions of which are used to remove smut from aluminum surfaces treated with etch-type oxidation and corrosion removers
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a process for removal of aluminide protective coatings from cobalt alloys
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a terpene base solvent cleaner in the form of a liquid, which forms a transient emulsion with water
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers an alkaline aqueous cleaner compound in the form of a liquid concentrate or a water-soluble powder for dilution with water
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a rust-inhibiting compound in the form of a liquid concentrate or a water soluble powder
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a carbon soil and paint remover compound in the form of a liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a cleaner in the form of a liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers vacuum-arc-cast molybdenum in the form of wrought round bars
AMS G Titanium and Refractory Metals Committee
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of October, 1991
AMS B Finishes Processes and Fluids Committee
This specification covers a water-miscible, low-foaming cleaner in the form of a liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
The task of chemical process operator in the parts cleaning area is generally considered unskilled labor and in the past, little or no training had been provided or recommended. Since overhaul cleaning is a critical process step prior to visual and fluorescent penetrant inspection processes, consideration must be given to minimum levels of training for these process operators. It is the responsibility of the department supervisor to ensure that all personnel within the department are trained to acceptable level in all general aspects of health and safety and basic operating procedures. This document is intended to augment the local quality control system which will control the application and frequency of the guidelines stated within
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers an aluminum-base alloy in the form of hand forgings and forging stock
AMS D Nonferrous Alloys Committee
This SAE Aerospace Information Report (AIR) establishes guidance for the specification of formulated lubricant properties which contribute to the lubricating function in bearings, gears, clutches, and seals of aviation propulsion and drive systems
E-34 Propulsion Lubricants Committee
This specification covers two types of semi-processed silicon steel in the form of sheet and strip supplied in coils or cut lengths
AMS E Carbon and Low Alloy Steels Committee
This specification covers a corrosion and heat resistant steel in the form of welded tubing
AMS F Corrosion and Heat Resistant Alloys Committee
This specification establishes the requirements for cleaning compounds, used in parts washers and spray cabinets for cleaning aircraft components
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers an emulsion-type, foam-on, pressure-spray cleaner in the form of a liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This SAE Aerospace Recommended Practice (ARP) covers a laboratory procedure for determining the cleaning efficiency of aircraft turbine engine gas path cleaners. Results are indicative of cleaning compound performance in the compressor sections of installed aircraft turbine engines, when used in a starter crank/soak/rinse application
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a paint remover in the form of a liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a water-miscible, foam-on, pressure spraying cleaner in the form of a liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This SAE Recommended Practice specifies graphic symbols for operator controls, gauges, tell-tales, indicators, instructions, and warning against risks in small craft and for engines and other equipment intended to be used in small craft
Marine Technical Steering Committee
This specification covers filled, resinous, thermosetting compounds capable of being applied and cured in place between the surfaces of mechanically fastened (joined) structures
AMS P Polymeric Materials Committee
This specification covers an alkaline-type, thickened paint remover in the form of a liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a ready-mixed thixotropic compound in the form of a stable film-forming compound suitable for application by brushing or spraying
AMS J Aircraft Maintenance Chemicals and Materials Committee
The Environmental Control Analysis SYstem (EASY) computer program is summarized in this report. Development of this computer program initially was sponsored by the U.S. Air Force Flight Dynamics Laboratory. (See References 1, 2, 3, and 4.) It provides techniques for determination of steady state and dynamic (transient) ECS performance, and of control system stability; and for synthesis of optimal ECS control systems. The program is available from the U.S. Air Force, or as a proprietary commercial version. General uses of a transient analysis computer program for ECS design and development, and general features of EASY relative to these uses, are presented. This report summarizes the nine analysis options of EASY, EASY program organization for analyzing ECS, data input to the program and resulting data output, and a discussion of EASY limitations. Appendices provide general definitions for dynamic analysis, and samples of input and output for EASY
AC-9 Aircraft Environmental Systems Committee
Traditional methods of photometry rely on the use of a goniometer to rotate the test item around two axes at right angles. This method is satisfactory for most situations but has certain disadvantages: a Point-by-point measurements with a goniometer may be slow. With more advanced requirements, particularly for headlamps, where the entire beam pattern is of concern, isocandela measurements are becoming increasingly needed. Such testing can be very time consuming. b For production quality assurance, the speed of a goniometer may not allow testing to keep pace with the production line if a large quantity of lamps must be sampled. c High Intensity Discharge (HID) lamps are becoming commonly used. Such lamps are orientation sensitive, changing in both lumen output and intensity distribution when tilted. This can introduce significant inaccuracies in test results when testing is performed using a goniometer. There is a need for alternative test techniques which can achieve very high speed
Test Methods and Equipment Stds Committee
The scope of this SAE Recommended Practice includes practical applications, theory, process management, audit and control recommendations, limitations, additional considerations, and process documentation
EG-1A Balancing Committee
This Aerospace Standard (AS) defines the test requirements for determining that bus monitors meet the requirements of MIL-STD-1553B, Digital Time Division Command/Response Multiplex Data Bus
AS-1A Avionic Networks Committee
Primarily to provide recommendations concerning minimizing stress-corrosion cracking in wrought titanium alloy products
AMS G Titanium and Refractory Metals Committee
This test method provides procedures for exposing specimens of elastomer material (slab form) representative to those used in gas turbine engines to aviation lubricants under extended duration and engine relevant thermal conditions. For AS5780 requirements the time is at least 1800 hours and temperatures are 100 °C to 160 °C. Positive volume change is an indication of specimen swell and subsequent negative volume change is an indication of specimen deterioration, both properties are important in the evaluation of the compatibility of the lubricant with elastomers used in the construction of the gas turbine
E-34 Propulsion Lubricants Committee
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