ISO 2964:1985
Current
The latest, up-to-date edition.
Aerospace — Tubing — Outside diameters and thicknesses — Metric dimensions
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English, French
21-03-1985
Includes the external diameters and thicknesses of tubes, for all metallic materials, to be selected for all uses in aircraft structural and system design. They shall be selected from those specified in the table. The tolerances shall be specified in the relevant standard appropriate to the material and intended application.
DevelopmentNote |
Also numbered as BS 2M46(1986). (11/2003)
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DocumentType |
Standard
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Pages |
2
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PublisherName |
International Organization for Standardization
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Status |
Current
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Supersedes |
Standards | Relationship |
NFL 15 611 : 1973 | Similar to |
DIN ISO 2964:1986-12 | Identical |
SAC GB/T 30207 : 2013 | Identical |
NF ISO 2964 : 1987 | Identical |
NFL 12 610 : 1968 | Similar to |
PN 92/L-01464 : 1992 | Identical |
NFL 15 670 : 1978 | Similar to |
NFL 15 612 : 1973 | Similar to |
NFL 15 620 : 1978 | Similar to |
NFL 15 621 : 1969 | Similar to |
PNE 28582 | Identical |
96/702220 DC : 0 | PREN 4223 - AEROSPACE SERIES - PIPE COUPLINGS 60 DEGREES; IN ANODIZED ALUMINIUM ALLOY INTERFACE FOR FLEXIBLE TUBES - GEOMETRICAL CONFIGURATION |
14/30301503 DC : 0 | BS ISO 8575 - AEROSPACE - FLUID SYSTEMS - HYDRAULIC SYSTEM TUBING |
PREN 2672 : 200P1 | AEROSPACE SERIES - DESIGN AND CONSTRUCTION OF PIPELINES FOR FLUIDS IN LIQUID OR GASEOUS CONDITION - DESIGN OF RIGID LINES |
PREN 3504 : 200P2 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - CIRCULAR TUBES FOR FLUIDS - CLOSE TOLERANCES - DIAMETER 3.2 MM <= D <= 50 MM - THICKNESS 0.25 MM <= A <= 2 MM - DIMENSIONS |
PREN 4180 : 200P1 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - CIRCULAR TUBES FOR FLUIDS - LARGE TOLERANCES - DIAMETER 4 MM <= D <= 40 MM - THICKNESS 0.4 MM <= A <= 2 MM - DIMENSIONS |
NF EN 3717 : 2008 | AEROSPACE SERIES - TUBES - SELECTION FOR ENGINES FLUID SYSTEMS |
BS ISO 8575:2016 | Aerospace. Fluid systems. Hydraulic system tubing |
I.S. EN 3717:2008 | AEROSPACE SERIES - TUBES - SELECTION FOR ENGINES FLUID SYSTEMS |
ISO 14625:2007 | Space systems — Ground support equipment for use at launch, landing or retrieval sites — General requirements |
DIN 65178-6:1987-01 | AEROSPACE; CONFIGURATION AND DESIGN OF FLUID PIPELINES; HOSE ASSEMBLIES, MANUFACTURE |
BS ISO 7257:2016 | Aircraft. Hydraulic tubing joints and fittings. Rotary flexure test |
96/702218 DC : 0 | PREN 4149 - AEROSPACE SERIES - PIPE COUPLINGS 60 DEGREES; IN ANODIZED ALUMINIUM ALLOY; INTERFACES FOR FLUID SYSTEMS |
BS Z 100:1999 | Space systems. Ground support equipment for use at launch, landing, or retrieval sites. General requirements |
SAE AIR 2000 : 2000 | AEROSPACE FLUID SYSTEM STANDARDS, METRIC, NATIONAL AND INTERNATIONAL |
ISO 8575:2016 | Aerospace — Fluid systems — Hydraulic system tubing |
ISO 7257:2016 | Aircraft Hydraulic tubing joints and fittings Rotary flexure test |
BS ISO 14625:2007 | Space systems. Ground support equipment for use at launch, landing or retrieval sites. General requirements |
14/30264731 DC : DRAFT JUNE 2014 | BS ISO 7257 - AIRCRAFT - HYDRAULIC TUBING JOINTS AND FITTINGS - ROTARY FLEXURE TEST |
BS EN 3717:2008 | Aerospace series. Tubes. Selection for engines fluid systems |
PREN 2621 : 200P2 | AEROSPACE SERIES - CIRCULAR STRUCTURAL TUBES SEAMLESS, IN LOW ALLOY STEEL - 4 <= D 100 MM - 0,5 <= A <= 10 MM - DIMENSIONS |
TR 2678 : 1 | AEROSPACE SERIES - DESIGN AND CONSTRUCTION OF PIPELINES FOR FLUIDS IN LIQUID OR GASEOUS CONDITION - DESIGN OF RIGID LINES |
DIN 9004:1985-06 | AEROSPACE; BENDING RADII FOR TUBES; APPROXIMATE VALUES FOR COLD WORKING |
BS EN 4180:2002 | Aerospace series. Circular tubes, for fluids in titanium and titanium alloys. Wide tolerances. Diameter 4 mm ≤ D ≤ 40 mm. Dimensions |
EN 4180:2001 | Aerospace series - Circular tubes, for fluids in titanium and titanium alloys - Wide tolerances<br /><br />Diameter 4 mm < D < 40 mm - Dimensions |
EN 3717:2008 | Aerospace series - Tubes - Selection for engines fluid systems |
DIN 9370:1985-04 | AEROSPACE; TUBES; CLASSIFICATION, PRESSURE TERMS, CALCULATION AND DESIGN CRITERIA |
DIN ISO 8575:1998-10 | AEROSPACE - FLUID SYSTEMS - HYDRAULIC SYSTEM TUBING |
PREN 3717 : 200P1 | AEROSPACE SERIES - TUBES - SELECTION FOR ENGINES FLUID SYSTEMS |
SAE MA2003 | Rotary Flexure Testing of Hydraulic Tubing Joints and Fittings |
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