SAE AMS STD 2175 : 1998
Withdrawn
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.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
Available format(s)
Hardcopy , PDF
Withdrawn date
07-14-2003
Language(s)
English
Published date
01-01-1998
Publisher
DocumentType |
Standard
|
Pages |
31
|
PublisherName |
SAE International
|
Status |
Withdrawn
|
Standards | Relationship |
MIL-STD-2175 Revision A:1993 | Similar to |
SAE AMS 4962 : 2016 | TITANIUM ALLOY, INVESTMENT CASTINGS, 6 AL - 4 V HOT ISOSTATICALLY PRESSED |
SAE AS 4073 : 2013(R2018) | AIR CYCLE AIR CONDITIONING SYSTEMS FOR MILITARY AIR VEHICLES |
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 AMS 5376 : 2013 | ALLOY, CORROSION AND HEAT RESISTANT, INVESTMENT CASTINGS, 30FE - 21CR - 20NI - 20CO - 3.0MO - 2.5W - 1.0CB - 0.15N, AS CAST |
SAE ARP 4945 : 2013 | 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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