SAE AS 5202 : 2005
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
PORT OR FITTING END, INTERNAL STRAIGHT THREAD, DESIGN STANDARD
Superseded date
10-08-2020
Superseded by
Published date
01-01-2005
Publisher
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| Committee |
G-3
|
| DevelopmentNote |
Supersedes MS 33649 (C). (09/2002) Supersedes SAE AS 33649. (09/2005)
|
| DocumentType |
Standard
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| MIL-PRF-5503 Revision G:2013 | ACTUATORS: AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
| MIL-DTL-9395-50 Base Document:2014 | SWITCH, PRESSURE, ABSOLUTE TYPE 1, 5 AMPERES, 28.5 +/- .5 INCHES HG |
| MS21959 Revision D:2011 | Body,Cluster Fitting, Two-Way, 90 Degrees, Internal Boss |
| SAE AS4073A | Air Cycle Air Conditioning Systems for Military Air Vehicles |
| MS21958 Revision D:2011 | Body, Cluster Fitting, Two-Way, 180 Degrees, Internal Boss |
| MIL-PRF-83419 Revision F:2016 | ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
| MIL-DTL-9395-6 Revision C:2006 | SWITCHES, PRESSURE (ABSOLUTE), TYPE 1, SPDT, 3 AMPERES |
| SAE ARP5543 | Aircraft Wheel Inflation Valves Incorporating an Inflation Pressure Gauge |
| MIL-DTL-32106 Base Document:2003 | INITIATORS, ELECTRICAL, FOR ROCKET MOTOR IGNITERS |
| MIL-DTL-5523 Revision E:2011 | VALVE; RELIEF, HYDRAULIC PRESSURE |
| MIL-DTL-5099 Revision C:2011 | INDICATOR, CABIN AIR PRESSURE, 1-7/8 INCH DIAL, TYPE MA-1 |
| MS28882 Revision G:2009 | VALVE, FUEL CHECK, LOW PRESSURE, GASKET SEAL STRAIGHT THREAD CONNECTION |
| NASA SSTD 8070 0044 : 2012 | STANDARD FOR CARBON STEEL PIPING SYSTEMS |
| MIL-PRF-27197 Revision F:2017 | INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED |
| SAE AS4875A | Fittings, Straight Threaded Boss or Flanged, Fluid Connection |
| MIL-DTL-81716 Revision A:2009 | PACKING, PREFORMED, STRAIGHT THREADED TUBE FITTING BOSS, TYPE 2 HYDRAULIC (-65 DEGREES F TO +275 DEGREES F) |
| MIL-PRF-38135 Revision D:2014 | INDICATOR, INDICATED AIRSPEED AVU-19A, STANDBY |
| SAE ARP4925B | Aerospace Design and Installation of Commercial Transport Helicopter Hydraulic Systems |
| SAE AS4841B | Fittings, 37° Internal Flare, Fluid Connection, Procurement Specification |
| MIL-PRF-81975 Revision C:2008 | COUPLINGS, REGULATED, AERIAL PRESSURE REFUELING TYPE MA-2, TYPE MA-3 AND TYPE MA-4 |
| SAE AMSP5510A | O-Ring, Preformed, Straight Thread Tube Fitting Boss, Type I Hydraulic (-65 to 160 °F) |
| MIL-DTL-9395-49 Base Document:2014 | SWITCH, PRESSURE, ABSOLUTE TYPE 1, 5 AMPERES, 24.5 +/- .5 INCHES HG |
| MIL-DTL-9395-1 Revision D:2006 | SWITCHES, PRESSURE (GAGE), TYPE 2, SPDT, 3 AMPERES |
| MIL-DTL-7891 Revision G:2008 | FILLER VALVE, AIRCRAFT OXYGEN |
| MS21345 Revision B:2016 | FITTINGS - INSTALLATION OF UNIVERSAL ELBOW |
| MIL-DTL-25308 Revision C:2010 | GAGE, PRESSURE, DIAL INDICATING, HYDRAULIC, TYPE ME-1 |
| SAE AS4875/1A | Fittings, Straight Thread Boss or Flanged 37° Flared, Fluid Connection |
| MS21946 Revision F:2012 | Body, Cluster Fitting, One-Way, Internal Boss |
| MIL-PRF-6164 Revision G:2012 | VALVE; AIRCRAFT, PNEUMATIC, HIGH-PRESSURE CHARGING |
| NASA SSTD 8070 0126 : 2014 | TUBING SYSTEMS FOR FACILITY SYSTEMS, SPECIAL TEST EQUIPMENT, AND AEROSPACE HARDWARE |
| NASA SSTD 8070 0069 : 2008 | LOW PRESSURE VACUUM JACKETED PIPE |
| NASA SSTD 8070 0047 : 2016 | STANDARD FOR STAINLESS STEEL PIPING SYSTEMS AA, ACK1, ACK4, ACK6, B, BCK1, BCK3, BCK4, BCK6, BCK10, C, EE, G, H, JJ, K3, L1, L2, NCK1, NCK2, NCK3, NCK10, NCK11, P, R, T, AND Z |
| MIL-DTL-38394 Revision E:2009 | Transmitter, Pressure TRU-81/A, Oil, 0-500 PSI |
| MIL-DTL-5498 Revision G:2013 | ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT |
| SAE AS4941B | Aerospace - General Requirements for Commercial Aircraft Hydraulic Components |
| JSSG-2009 Revision A:2013 | Air Vehicle Subsystems |
| MIL-PRF-25435 Revision D:2008 | TRANSMITTERS, PRESSURE, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-DTL-9395-48 Revision C:2006 | SWITCH, PRESSURE, ABSOLUTE TYPE 1, 5 AMPERES |
| SAE AS683D | Installation Procedures and Torques for Fluid Connections |
| SAE ARP4752B | Aerospace - Design and Installation of Commercial Transport Aircraft Hydraulic Systems |
| SAE ARP4763 | Aerospace - General Requirements for Hydraulic Relief Valves |
| MIL-DTL-5508 Revision C:2007 | FUSES, AIRCRAFT AUTOMATIC QUANTITY-MEASURING, HYDRAULIC |
| AN6248 Revision 3:2011 | PUMP - HYDRAULIC HAND, TYPE 3000 |
| SAE ARP5555 | Recommendations for Installation of Seals in Standard Glands |
| SAE AS5586 | Aerospace - General Requirements for Hydraulic System Reservoirs |
| MIL-DTL-9395-32 Revision D:2006 | SWITCHES, PRESSURE, DIFFERENTIAL (TYPE 3), 4 AMPERES |
| MS21960 Revision D:2011 | Body, Cluster Fitting, Three-Way, Internal Boss |
| MIL-DTL-9395-30 Revision H:2012 | Switches, Pressure, (Gage), Type II 5 Amperes |
| SAE AS4875/3A | Fittings, Straight Thread Port or Flanged to 24° Cone Flareless, Fluid Connection |
| 11/30250206 DC : 0 | BS EN 6140 - AEROSPACE SERIES - PLUG, PROTECTIVE, NON METALLIC FOR FITTING ENDS <= 3000 PSI HYDRAULIC SYSTEMS |
| SAE AS4073B:2019 | Air Cycle Air Conditioning Systems for Air Vehicles |
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