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SAE MA 1975 : 2015

Current
Current

The latest, up-to-date edition.

HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE, ARAMID REINFORCED, 135 DEGREE C, STANDARD DUTY, 28000/21000 KPA, HYDRAULIC, AIRCRAFT SYSTEMS
Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

27-07-2015

1 SCOPE
2 REFERENCES
3 TECHNICAL REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PREPARATION FOR DELIVERY
6 NOTES

Describes the requirements for a PTFE lined, aramid reinforced assembly suitable for use up to 135 degree C and up to 28000 kPa aircraft and missile hydraulic and pneumatic systems.

Committee
G 3
DevelopmentNote
Supersedes SAE MA 2140. (09/2004)
DocumentType
Standard
Pages
30
PublisherName
SAE International
Status
Current
Supersedes

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SAE ARP 1835 : 2013 PREPARATION FOR DELIVERY, GENERAL REQUIREMENTS FOR HOSE ASSEMBLIES
SAE ARP 603 : 1985 IMPULSE TESTING OF HYDRAULIC HOSE, TUBING, AND FITTING ASSEMBLIES
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QQ-P-35 Revision C:1988 PASSIVATION TREATMENTS FOR CORROSION-RESISTANT STEEL
ASTM B 348 : 2013 : REDLINE Standard Specification for Titanium and Titanium Alloy Bars and Billets
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SAE MA 2002 : 2013 IMPULSE TESTING OF HYDRAULIC HOSE, TUBING AND FITTING ASSEMBLIES
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SAE AIR 1228 : 2009 STANDARD IMPULSE MACHINE EQUIPMENT AND OPERATION
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SAE MA 4569 : 2015 HOSE ASSEMBLY, PTFE, ARAMID REINFORCED, STANDARD DUTY, 21000/28000 KPA, 135 DEG C, TITANIUM FITTINGS, FLARELESS, INCLUDING JUMP SIZES, STRAIGHT TO 45 DEG, METRIC
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SAE AMS 4928 : 2016 TITANIUM ALLOY BARS, WIRE, FORGINGS, RINGS, AND DRAWN SHAPES, 6AL - 4V, ANNEALED
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