SAE AMSSTD2175
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
Castings, Classification and Inspection of
Hardcopy , PDF
14-07-2003
English
01-07-1998
Important note : Users cannot be edited or removed once added to your Multi user PDF.| DocumentType |
Standard
|
| Pages |
30
|
| PublisherName |
SAE International
|
| Status |
Withdrawn
|
The purpose of this military standard is to prescribe the non-destructive testing acceptance criteria for the inspection of metal castings that are classified (see 1.3) in accordance with this standard.
| Standards | Relationship |
| MIL-STD-2175 Revision A:1993 | Similar to |
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| SAE AMS 4289 : 2013 | ALUMINUM ALLOY CASTINGS, 7.0SI - 0.55MG - 0.12TI (F357.0-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| SAE AS 8056 : 2004(R2016) | MINIMUM DESIGN AND PERFORMANCE OF AIRPLANE GALLEY IN-FLIGHT CARTS, CONTAINERS, AND ASSOCIATED COMPONENTS |
| MIL-DTL-9479 Revision E:1999 | |
| MIL-HDBK-454 Revision B:2007 | GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT |
| SAE AS 94900 : 2007 | AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR |
| SAE ARP 1281 : 2002 | ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR |
| SAE ARP 4058 : 2017 | GENERAL SPECIFICATION GUIDE FOR MECHANICAL GEARED ROTARY ACTUATORS |
| MIL-PRF-7032 Revision H:2010 | INVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR |
| SAE AMS5376G | ALLOY, CORROSION AND HEAT RESISTANT, INVESTMENT CASTINGS, 30FE - 21CR - 20NI - 20CO - 3.0MO - 2.5W - 1.0CB - 0.15N, AS CAST |
| SAE ARP4945A | AEROSPACE-SOLENOID VALVE, HYDRAULIC, THREE WAY, TWO POSITION, DIRECT ACTING |
| SAE AMS 4288 : 2016 | ALUMINUM ALLOY CASTINGS, 7.0SI - 0.58MG - 0.15TI (E357.0-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
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