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This SAE Aerospace Standard (MA) defines the requirements for a convoluted polytetrafluoroethylene (PTFE) lined, metallic reinforced, hose assembly suitable for use in aircraft fluid systems at temperatures of 55 to 204 degrees C and at operating pressures per Table 1.
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This specification covers an aluminum alloy in the form of hand forgings procured to metric dimensions. AMS 4247 is the inch/pound version of this MAM.These forgings have been used typically for parts requiring a combination of high strength and resistance to stress-corrosion cracking and for parts requiring stability during machining, but usage is not limited to such applications.
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The NBIC recognizes three important areas of post-construction activities where information, understanding,and following specific requirements will promote public and personal safety. These areas include:
The NBIC provides rules, information, and guidance for post-construction activities, but does not providedetails for all conditions involving pressure-retaining items. Where complete details are not provided in thiscode, the code user is advised to seek guidance from the Jurisdiction and from other technical sources.
The words shall, should, and may are used throughout the NBIC and have the following intent:
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This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of June 2007, and has been superseded by AMS 2253. The requirements of the latest issue of AMS 2253 shall be fulfilled whenever reference is made to the cancelled MAM 2253. By this action, this document will remain listed in the Numerical Section of the Index of the Aerospace Materials Specifications noting that is it superseded by AMS 2253.This specification covers established metric manufacturing tolerances applicable to carbon and alloy steel tubing ordered to metric dimensions. These tolerances apply to all conditions unless otherwise noted.
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Properties for type AY oils are not addressed in this document.
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SAE USCAR12-5 gives specific and measurable design criteria to be applied at a design review prior to tooling. Thespecification is formatted as a checklist to aid in its use. The requirements do not apply in all situations so engineeringjudgment must be used. This is a specification for design criteria; applicable performance specifications (USCAR-2, etc.)must still be performed.
This specification covers the grain flow pattern requirements in headed bolts, screws, and studs. The heading practice in the manufacture of the bolt, screw, or stud sets the grain flow pattern, but it is also greatly influenced by the fastener design.
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This SAE metric Aerospace Recommended Practice (MAP) lists wrenching surface sizes and tolerances for fluid fittings which utilize machined or unmachined hex bar dimensions and machined or forged wrenching surfaces across the center body section of shape fittings.