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This AIR provides information about the specific requirements for missile hydraulic pumps and their associated power sources.
This SAE Recommended Practice establishes uniform test procedures for friction based parking brake components used in conjunction with hydraulic service braked vehicles with a gross vehicle weight rating greater than 4500 kg (10 000 lb). The components covered in this document are the primary actuation and the foundation park brake. Various peripheral devices such as application dashboard switches or indicators are not included.
SCOPE IS UNAVAILABLE.
SCOPE IS UNAVAILABLE.
This specification covers a corrosion-resistant steel in the form of wire.
This SAE Aerospace Recommended Practice (ARP) establishes the overall component and system function guidelines and minimum performance levels for a TPMS. These guidelines include, but are not limited to: Design recommendations for system components, which: Monitor tire inflation Are located in/on the tire/wheel assembly, landing gear axle, and/or aircraft avionics compartment Recommended performance and safety guidelines for a TPMS.
This SAE Aerospace Information Report (AIR) provides technical information to assist the development of specific cleaning methods for those filter elements which are designated as "cleanable" and cannot be cleaned by simple and obvious procedures.
Incidents where a piece of ground support equipment or personnel damages an aircraft under the control of ground or maintenance operations that requires corrective action by aircraft maintenance personnel. Operations include, but are not limited to servicing, line maintenance, heavy maintenance, and aircraft movement, e.g., marshalling/pushback/tow/reposition/taxi.
To establish design recommendations that will provide a basis for safe and reliable connections to threaded screw-type or stud-type electrical equipment terminations. These recommendations are directed primarily, but not solely, to the aerospace and ground support equipment industries. Since individual design criteria may alter the details as outlined, it is therefore important that this SAE Aerospace Information Report (AIR) not be considered mandatory but be used only as a design guidance.
This specification covers an aluminum alloy in the form of sheet and plate 0.006 to 3.000 inches (0.15 to 76.20 mm), inclusive, in nominal thickness (see 8.5).
This specification covers two styles of glass cloth impregnated with a polyester resin system, the resin being processed to a “B” stage condition. Either style of glass may be used.
This specification covers an aluminum alloy in the form of drawn seamless tubing in the annealed (O) condition. This specification covers products from 0.018 to 0.500 inch (0.46 to 12.70 mm) in wall thickness (see 8.6).
This specification covers a prepolymer in the form of an epoxy cresol novolac (ECN) resin.
This specification covers a resin-impregnated glass fabric honeycomb core in the form of flat or contoured sandwich structures.
This specification covers polytetrafluoroethylene resin in the form of asbestos-fiber-reinforced sheet.
This specification covers synthetic-rubber-coated nylon in the form of flat braid.
This specification covers a glass cloth impregnated with a heat-curable epoxy resin system, the resin being processed to a “B” stage condition, and furnished in the form of continuous rolls.
This specification and its supplementary detail specifications cover flame resistant cloth woven from various fibers.
This specification covers one type of polyamide fiber in the form of knitted cloth.
This specification covers carbon in the form of hollow microspheres.
This specification covers one type of glass cloth impregnated with a heat-reactive, thermosetting, hot-melt, addition-type, polyimide resin system, furnished in continuous rolls of full width material.
This specification covers a silicone (VMQ) rubber in the form of sheet, strip, tubing, molded shapes, and extrusions.
This specification covers paper base honeycomb material having a cell size of 0.330 or 0.440 in. (8.38 or 11.18 mm). Unless otherwise ordered, size 0.440 in. (11.18 mm) be supplied.
This specification covers a loosely-woven cotton in the form of wipes supplied in rolls or cut sheets.
This specification covers a synthetic rubber in the form of a nonrigid, smooth bore, noncollapsing-type hose.
This specification covers a corrosion and heat-resistant, air-melted, nickel alloy in the form of investment castings.
This specification covers one type of woven glass cloth treated with a chrome-silane finish. a chrome-silane finish.
This specification covers aluminum in the form of foil and light gage sheet.
This specification covers a polyester resin in the form of a film clad on one or both sides with copper foil.
This specification covers a silica fiber insulation in the form of felted pads, flat or in rolls, as ordered.
This specification covers one type of methyl methacrylate resin in the form of extrusions, compression moldings, and injection moldings.
This specification covers a corrosion-resistant steel in the form of investment castings.
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.
This specification covers a corrosion-resistant steel in the form of investment castings.
This specification covers one type of continuous multifilament carbon fibers in the form of a tow or yarn (when twisted). The weight per unit length of the tow or yarn is governed by the filament count which is identified by the supplier's grade or material designation.
This specification covers a corrosion and heat-resistant steel in the form of investment castings.
This specification covers a ductile (nodular) iron in the form of sand castings.
This specification covers low-carbon steel in the form of bars, forgings, mechanical tubing, sheet, strip, plate, and forging stock.
This specification covers a corrosion-resistant steel in the form of investment castings.
This specification covers an aluminum alloy in the form of sheet and plate clad on one side with a different aluminum alloy.
This specification covers a chloroprene rubber (CR) that can be used to manufacture product in the form of sheet, strip, tubing, extrusions, and molded shapes such as window channels, bumper pads, chafing strips, etc. For molded rings, compression seals, molded O-ring cord, and molded-in-place gaskets for aeronautical and aerospace applications, use the equivalent AMS7XXX specification.
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