SAE AS19692B
Current
Current
The latest, up-to-date edition.
Aerospace – Military Type Variable Delivery, Pressure Compensated Hydraulic Pump
Available format(s)
Hardcopy , PDF
Language(s)
English
Published date
22-06-2016
Publisher
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1. SCOPE
2. REFERENCES
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. QUALIFICATION TESTS
6. QUALITY CONFORMANCE - ACCEPTANCE TESTS
7. RELIABILITY TEST
8. PACKAGING
9. NOTES
This SAE Aerospace Standard (AS) establishes the general requirements for the design, construction, acceptance, and qualification testing of flat cut-off pressure compensated, variable delivery hydraulic pumps used in military aircraft hydraulic systems.
| Committee |
A-6C4
|
| DevelopmentNote |
Supersedes MIL P 19692 (04/2003)
|
| DocumentType |
Revision
|
| Pages |
40
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
| SAE ARP4925B | AEROSPACE DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT HELICOPTER HYDRAULIC SYSTEMS |
| SAE AS595D | AEROSPACE - CIVIL TYPE VARIABLE DELIVERY, PRESSURE COMPENSATED, HYDRAULIC PUMP |
| SAE J1779_201305 | SHIP SYSTEMS AND EQUIPMENT - HYDRAULIC SYSTEM DESIGN CRITERIA FOR MARINE VEHICLES |
| SAE AIR560C | MISSILE HYDRAULIC PUMPS |
| SAE J1776_201402 | MARINE VEHICLES - HYDRAULIC SYSTEM PUMPS AND MOTORS - DESIGN AND SPECIFICATION GUIDE |
| SAE ARP 4940 : 2014 | APPLICATION GUIDE FOR AEROSPACE HYDRAULIC MOTORS |
| SAE ARP 1383 : 2013 | AEROSPACE - IMPULSE TESTING OF HYDRAULIC COMPONENTS |
| SAE AIR 1922 : 2017 | AEROSPACE - SYSTEM INTEGRATION FACTORS THAT AFFECT HYDRAULIC PUMP LIFE |
| SAE AMS2404G | PLATING, ELECTROLESS NICKEL |
| MS3330 Base Document:1969 | Flange Accessory, 2.653 BC Square, Design Standard for |
| SAE AS567K | SAFETY CABLE, SAFETY WIRE, KEY WASHERS, AND COTTER PINS FOR PROPULSION SYSTEMS, GENERAL PRACTICES FOR USE OF |
| SAE AMSQQP416E | PLATING, CADMIUM (ELECTRODEPOSITED) |
| MIL-STD-130 Revision N:2007 | IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
| MIL-H-8890 Base Document:1961 | HYDRAULIC COMPONENTS, TYPE 111 [65 DEGREES TO PLUS 450 DEGREES F] GENERAL SPECIFICATION FOR [ASG] |
| SAE AIR 1922 : 2017 | AEROSPACE - SYSTEM INTEGRATION FACTORS THAT AFFECT HYDRAULIC PUMP LIFE |
| SAE AS4201A | PORT - RING LOCKED FLUID CONNECTION TYPE, 8000 PSI DESIGN STANDARD |
| SAE AS1300D | PORT - RING LOCKED FLUID CONNECTION TYPE, STANDARD DIMENSIONS FOR |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL-H-8891 Revision A:1978 | HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES TYPE 111 DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR |
| MIL-STD-2073-1 Revision E:2008 | STANDARD PRACTICE FOR MILITARY PACKAGING |
| SAE AMS7276H | RUBBER: FLUOROCARBON (FKM) HIGH-TEMPERATURE-FLUID RESISTANT LOW COMPRESSION SET FOR SEALS IN FUEL SYSTEMS AND SPECIFIC ENGINE OIL SYSTEMS |
| SAE AMSQQN290C | NICKEL PLATING (ELECTRODEPOSITED) |
| ASTM B 545 : 2013 : REDLINE | Standard Specification for Electrodeposited Coatings of Tin |
| SAE AIR 5872 : 2011 | AEROSPACE HYDRAULIC PUMP CONTROLS |
| MIL-HDBK-781 Revision A:1996 | RELIABILITY TEST METHODS, PLANS, AND ENVIRONMENTS FOR ENGINEERING DEVELOPMENT, QUALIFICATION AND PRODUCTION |
| SAE AS5440A | HYDRAULIC SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION REQUIREMENTS FOR |
| MS3332 Base Document:1969 | FLANGE ACCESSORY, 5,000 BC ROUND, DESIGN STANDARD FOR |
| SAE AIR1362C | AEROSPACE HYDRAULIC FLUIDS PHYSICAL PROPERTIES |
| NASM33540:2003 | SAFETY WIRING, SAFETY CABLING, COTTER PINNING, GENERAL PRACTICES FOR |
| MS3331 Base Document:1969 | Flange Accessory, 5,000 BC Square, Design Standard For |
| MIL-DTL-5541 Revision F:2006 | Chemical Conversion Coatings on Aluminum and Aluminum Alloys |
| MIL-STD-464 Revision C:2010 | ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
| SAE AMS 2460 : 2013 | PLATING, CHROMIUM |
| SAE AMS 7287 : 2012 | FLUOROCARBON ELASTOMER (FKM) HIGH TEMPERATURE/HTS OIL RESISTANT/FUEL RESISTANT LOW COMPRESSION SET/70 TO 80 HARDNESS, LOW TEMPERATURE TG -22 DEGREES F (-30 DEGREES C) FOR SEALS IN OIL/FUEL/SPECIFIC HYDRAULIC SYSTEMS |
| SAE AMS7259E | RUBBER: FLOUROCARBON (FKM), HIGH TEMPERATURE/FLUID RESISTANT, LOW COMPRESSION SET/85 TO 95 HARDNESS, FOR SEALS IN FUEL SYSTEMS AND SPECIFIC ENGINE OIL SYSTEMS |
| MIL-STD-276 Revision A:1992 | IMPREGNATION OF POROUS METAL CASTINGS AND POWDERED METAL COMPONENTS |
| MS3333 Base Document:1969 | Flange Accessory, 8,000 BC Round, Design Standard For |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MS3334 Base Document:1969 | Flange Accessory, 10,000 BC Round, Design Standard for |
| SAE AS 8775 : 1998 | HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES, GENERAL SPECIFICATION FOR |
| SAE AMS 7379 : 2008 | RUBBER: FLUOROCARBON ELASTOMER (FKM) 70 TO 80 HARDNESS, LOW TEMPERATURE SEALING TG -40 DEGREES F (-40 DEGREES C) FOR ELASTOMERIC SEALS IN AIRCRAFT ENGINE OIL, FUEL AND HYDRAULICS SYSTEMS |
| MIL F 8815 : D | FILTER AND FILTER ELEMENTS, FLUID PRESSURE, HYDRAULIC LINE, 15 MICRON ABSOLUTE AND 5 MICRON ABSOLUTE, TYPE 11 SYSTEMS; GENERAL SPECIFICATION FOR |
| SAE ARP4386C | TERMINOLOGY AND DEFINITIONS FOR AEROSPACE FLUID POWER, ACTUATION AND CONTROL TECHNOLOGIES |
| SAE AS595D | AEROSPACE - CIVIL TYPE VARIABLE DELIVERY, PRESSURE COMPENSATED, HYDRAULIC PUMP |
| MIL-DTL-15024 Revision F:1997 | Plates and Tags for Identification of Equipment, General Specification for |
| SAE ARP 1383 : 2013 | AEROSPACE - IMPULSE TESTING OF HYDRAULIC COMPONENTS |
| MIL-PRF-16173 Revision E:1993 | CORROSION PREVENTATIVE COMPOUND, SOLVENT CUTBACK, COLD-APPLICATION |
| MIL-C-11796 Revision C:1986 | CORROSION PREVENTIVE COMPOUND, PETROLATUM, HOT APPLICATION |
| MS21344 Revision A:2016 | FITTING INSTALLATION OF FLARED TUBE STRAIGHT THREADED CONNECTORS DESIGN STANDARD FOR |
| NAS847:2012 | CAPS AND PLUGS, PROTECTIVE, DUST AND MOISTURE SEAL |
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