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MODUK - DEF STAN 02-388 - REQUIREMENTS FOR THE PERIODIC INSPECTION, TESTING AND MAINTENANCE OF HYDRAULIC ACCUMULATORS - ISSUE 1: 04.00; INCORPORATING NES 388 CATEGORY 2: ISSUE 1: 10.97 Organization: MODUK
Date: 2000-04-01
Description: This NES specifies the requirements for the periodic inspection, testing and maintenance of Naval Standard Hydraulic Accumulator Shells. It is applicable to the following range of accumulators currently in use in the hydraulic systems of surface ships and submarines: Chromium-molybdenum steel and duplex stainless steel bladder type accumulators of metric capacities (4,10,20a nd 37 litre) with a working pressure of 207 bar g.
GOST 14064 - HYDRAULIC ACCUMULATORS. BASIC PARAMETERS Organization: GOST
Date: 1968-11-20
NPFC - MIL-DTL-5498 - ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT Organization: NPFC
Date: 2013-04-22
Description: This aircraft hydraulic accumulator is intended for use in aircraft for both type I and type II hydraulic systems specified in SAE AS5440.
SAE ARP4379 - (R) AEROSPACE - ACCUMULATOR, HYDRAULIC, CYLINDRICAL, PISTON SEPARATED Organization: SAE
Date: 2016-04-01
Description: This SAE Aerospace Recommended Practice (ARP) is a guide for defining the requirements for aerospace piston hydraulic accumulators, including details pertinent to the design, fabrication, performance and testing of the accumulator.
SAE ARP4553 - (R) AEROSPACE - ACCUMULATOR, HYDRAULIC, SELF-DISPLACING Organization: SAE
Date: 2008-12-01
Description: Purpose This SAE Aerospace Recommended Practice (ARP) is intended to provide design and qualification requirements for selfdisplacing hydraulic accumulators. These requirements are intended be included in the Procurement Specification for the accumulator.
NPFC - QPL-5498 - ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT Organization: NPFC
Date: 2017-02-03
Description: QUALIFIED PRODUCT LIST OF PRODUCTS QUALIFIED UNDER PERFORMANCE SPECIFICATION MIL-DTL-5498 Accumulators, Hydraulic, Cylindrical 3000 PSI, Aircraft This list has been prepared for use by or for the Government in the acquisition of products covered by the subject specification and such listing is not intended to and does not connote endorsement of the product by the Department of Defense.
GOST 16769 - HYDRAULIC ACCUMULATORS. GENERAL TECHNICAL REQUIREMENTS Organization: GOST
Date: 1984-01-01
GOST 26496 - HYDRAULIC ACCUMULATORS. ACCEPTANCE RULES AND TEST METHODS Organization: GOST
Date: 1985-03-26
AIR FORCE - AN6218 REV 3 - FITTINGS - HYDRAULIC ACCUMULATOR AIR PRESSURE GAGE Organization: AIR FORCE
Date: 1954-06-01
SAE ARP4378 - (R) ACCUMULATOR, HYDRAULIC, WELDED BELLOWS, FACTORY PRE-CHARGED Organization: SAE
Date: 2017-01-01
Description: This SAE Aerospace Recommended Practice (ARP) provides design and test requirements for high pressure, factory pre-charged, welded bellows hydraulic accumulators. Purpose The requirements contained in this ARP are compiled for inclusion in a Procurement Specification for this type of accumulator.
NPFC - MIL-A-52689 - ACCUMULATORS; HYDRAULIC Organization: NPFC
VDI 3282 - CHARACTERISTIC QUANTITIES OF OIL-HYDRAULIC DEVICES; HYDRAULIC ACCUMULATORS Organization: VDI
Date: 1963-09-01
SPI AN-108 - RECOMMENDED GUIDELINE - HYDRAULIC ACCUMULATORS ON INJECTION MOLDING MACHINES - TO PURCHASE CALL 1-800-854-7179 USA/CANADA OR 303-397-7956 WORLDWIDE Organization: SPI
FAA - AD 98-09-05 - CORROSION OF THE BRAKE HYDRAULIC ACCUMULATORS\BRITISH AEROSPC (ENGLAND)\ATP Organization: FAA
FAA - AD 97-NM-226 - CORROSION OF THE BRAKE HYDRAULIC ACCUMULATORS\BRITISH AEROSPC\ATP SERIES Organization: FAA
ARMY - MIL-A-62158 CANC NOTICE 1 - ACCUMULATOR, HYDRAULIC, VEHICULAR Organization: ARMY
Date: 1976-12-17
ARMY - MIL-A-62158 - ACCUMULATOR, HYDRAULIC, VEHICULAR Organization: ARMY
Date: 1972-10-30
AIR FORCE - AND10309 REV 2 CANC - ACCUMULATOR INSTALLATION - HYDRAULIC Organization: AIR FORCE
Date: 1959-06-08
FAA - AD 97-NM-104 - CORROSION OF THE CYLINDER TUBE OF THE MAIN HYDRAULIC ACCUMULATOR\BRITISH AEROSPACE\ATP SERIES Organization: FAA
FAA - AD 70-10-04 - HYDRAULIC ACCUMULATOR END CAP FAILURE\SPRAGUE ENGINEERING\A-200-25\A-200-50 Organization: FAA

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