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Viewing 164041 to 164070 of 173138
1956-07-01
Standard
AMS3237A
This specification covers a butyl (IIR) rubber in the form of sheet, strip, extrusions, and molded shapes. These products have been used typically for parts, such as diaphragms, gaskets, grommets, and seals, requiring resistance to phosphate esters or low permeability to gases, but usage is not limited to such applications. The material is not suitable for use in contact with petroleum-base fluids due to excessive swell. Each application should be considered individually.
1956-07-01
Standard
AMS3356
This specification covers a silicone (VMQ) rubber in the form of sheet, strip, tubing, extrusions and molded shapes. Primarily for parts required to operate or seal from -55 to +230 degrees C (-67 to +446 degrees F), compounded especially for aircraft piston engine oil resistance, low compression set, and controlled dielectric strength. Silicone elastomer is resistant to deterioration by weathering and by high-aniline-point petroleum-base oils and remains flexible over the temperature range noted. The elastomer is not normally suitable for use in contact with gasoline or aromatic fuels and low-aniline-point petroleum-base fluids due to excessive swelling of the elastomer.
1956-07-01
Standard
AMS3345
This specification covers a silicone rubber in the form of sheet, strip, tubing, molded shapes, and extrusions. These products have been used typically for parts required to operate or seal from -90 to +205 degrees C (-130 to +400 degrees F), compounded especially for high strength, but usage is not limited to such applications. Silicone elastomer is resistant to deterioration by weathering and aircraft piston engine oil and remains flexible over the temperature range noted. This rubber is not normally suitable for use in contact with gasoline or aromatic fuels and low-aniline-point petroleum-base fluids due to excessive swelling of the elastomer.
1956-07-01
Standard
AMS3570
This specification covers two types of an open-cell, medium-flexibility polyurethane foam in the form of sheet, strip, and shapes. These products have been used typically for general interior padding, cushioning, and vibration insulation, but usage is not limited to such applications. Foam furnished to this specification shall be classified as follows: Type I - Polyurethane Foam - Easter and Type II - Polyurethane Foam - Ester. Type II shall be supplied unless Type I is ordered.
1956-07-01
Standard
AMS3615B
This specification covers one type of cotton fabric impregnated with a phenolic resin and supplied in the form of tubing. This tubing has been used typically for electrical insulation at low voltages and for protection from galvanic corrosion, but usage is not limited to such applications. This tubing has good machining qualities and good moisture resistance.
1956-07-01
Standard
AMS3675A
ABSTRACT
1956-07-01
Standard
AMS7701
This specification covers two types of magnetic nickel-iron alloy in the form of sheet and strip.
1956-07-01
Standard
AMS7702
This specification covers two types of magnetic nickel-iron alloy in the form of sheet and strip.
1956-07-01
Magazine
1956-07-01
Standard
AMS4776
This specification covers a nickel alloy in the form of wire, rod, strip, foil, and powder and a viscous mixture (paste) of the powder in a suitable binder. This filler metal has been used typically for joining corrosion and heat resistant steels and alloys requiring corrosion and oxidation resistant joints with good strength at elevated temperatures, but usage is not limited to such applications. Also may be used as a corrosion and oxidation resistant hard coating.
1956-07-01
Standard
AMS2667
This specification covers the engineering requirements for producing brazed joints in parts fabricated from austenitic corrosion and heat resistant steels, but may also be used on carbon or low-alloy steels or copper alloys, and the properties of such joints.
1956-07-01
Standard
AMS4775A
This specification covers a nickel alloy in the form of wire, rod, strip, foil, and powder and a viscous mixture (paste) of the powder in a suitable binder. This filler metal has been used typically for joining corrosion and heat resistant steels and alloys requiring corrosion and oxidation resistant joints with good strength at elevated temperatures, but usage is not limited to such applications. Also may be used as a corrosion and oxidation resistant hard coating.
1956-07-01
Standard
AMS2232C
This specification covers established inch/pound manufacturing tolerances applicable to carbon steel sheet, strip, and plate ordered to inch/pound dimensions. These tolerances apply to all conditions unless otherwise noted. The term 'excl' is used to apply only to the higher figure of the specified range. Tolerances for products sizes not listed herein shall be as agreed upon by purchaser and vendor.
1956-07-01
Standard
AMS6427B
This specification covers an aircraft quality, low alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. These products have been used typically for parts requiring a combination of high tensile strength and good ductility with relatively high impact strength and hardness, but usage is not limited to such applications. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking after heat treatment. ARP1110 recommends practices to minimize such conditions.
1956-07-01
Standard
AMS3238A
This specification covers a butyl (IIR) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
1956-07-01
Standard
AMS3346
This specification covers a silicone rubber in the form of sheet, strip, tubing, molded shapes, and extrusions. These products have been used typically for parts required to operate or seal at temperatures from -90 to +205 degrees C (-130 to +401 degrees F), compounded especially for high strength, but usage is not limited to such applications. Silicone elastomer is resistant to deterioration by weathering and aircraft piston engine oil and remains flexible over the temperature range noted. These products are not normally suitable for use in contact with gasoline or aromatic fuels and low-aniline-point petroleum-base fluids due to excessive swelling of the elastomer.
1956-07-01
Standard
AMS4941
This specification covers one grade of commercially pure titanium in the form of welded tubing.
1956-07-01
Standard
AMS2403D
This specification covers the engineering requirements for electrodeposition of nickel and the properties of the deposit.
1956-06-01
Magazine
1956-05-01
Standard
AMS3246
ABSTRACT
1956-05-01
Magazine
1956-04-01
Magazine
1956-03-15
Standard
ARP268B
The purpose of this document is to set forth the recommendations of SAE Committee S-7 relative to the location and actuation of flight deck controls. These recommendations are intended to minimize confusion and distraction and thereby reduce transition training time, crew errors, fatigue, and other factors detrimental to flight safety and efficiency. In arriving at these recommendations, the committee carefully reviewed the work of the flight deck layout panel of the Aircraft Committee of the Munitions Board, the recommendations and requirements of the Civil Aeronautics Board, the Federal Aviation Agency, the requirements of the airline operators, the aircraft manufacturers, etc. In cases where conflicting opinions existed, suitable compromises were made. The recommendations of this document apply to commercial type, multi-engine transport aircraft which utilize reciprocating or turbine type powerplants and which are operated in subsonic, transonic, or supersonic speed regimes.
1956-03-15
Standard
AS264D
No scope available.
1956-03-15
Standard
ARP467
ABSTRACT
1956-03-15
Standard
ARP476
This document describes guidelines and methods of performing the safety assessment for certification of civil aircraft. It is primarily associated with showing compliance with FAR/JAR 25.1309. The methods outlined here identify a systematic means, but not the only means, to show compliance. A subset of this material may be applicable to non-25.1309 equipment. The concept of Aircraft Level Safety Assessment is introduced and the tools to accomplish this task are outlined. The overall aircraft operating environment is considered. When aircraft derivatives or system changes are certified, the processes described herein are usually applicable only to the new designs or to existing designs that are affected by the changes. In the case of the implementation of existing designs in a new derivation, alternate means such as service experience may be used to show compliance.
1956-03-15
Standard
ARP489
This specification establishes the requirements for shielded, detachable high tension spark plug leads for reciprocating engines.
1956-03-15
Standard
ARP85C
Air Condiitioning System - General - Dealing with Design Features. Air Conditioning Equipment - Commercial Passenger - Delaing with features. Applicable only to commercial passenger carrying aircraft. Desirable Design Features - General information for use of those concerned in meeting requirements contained herein.
1956-03-15
Standard
ARP89B
The recommendations of this SAE Aerospace Recommended Practice (ARP) for aircraft compartment automatic temperature control systems are primarily intended to be applicable to occupied or unoccupied compartments of civil and military aircraft.

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