SAE AMS 2486 : 2010
|
CONVERSION COATING OF TITANIUM ALLOYS FLUORIDE-PHOSPHATE TYPE |
PREN 4833 : DRAFT 2017
|
AEROSPACE SERIES - PIPE COUPLING 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) RING LOCKED FITTING - FLARELESS END - INCH SERIES - EXTRA FINE THREAD PITCH |
SAE AMS5659S : 2016
|
Steel, Corrosion-Resistant, Bars, Wire, Forgings, Rings, and Extrusions 15Cr - 4.5Ni - 0.30Cb (Nb) - 3.5Cu
|
SAE AMS QQ A 225/9 : 2014
|
ALUMINUM ALLOY 7075, BAR, ROD, WIRE, AND SPECIAL SHAPES; ROLLED, DRAWN, OR COLD FINISHED |
SAE AMS 5737 : 2012
|
STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS AND TUBING, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED, 1650 DEGREES F (899 DEGREES C), SOLUTION AND PRECIPITATION HEAT TREATED |
SAE AS 5620 : 2013
|
TITANIUM HYDRAULIC TUBING, TI-3AL-2.5V COLD WORKED AND STRESS RELIEVED, UP TO 35000 KPA (5080 PSI), REQUIREMENTS FOR QUALIFICATION TESTING AND CONTROL |
ISO 4287:1997
|
Geometrical Product Specifications (GPS) — Surface texture: Profile method — Terms, definitions and surface texture parameters |
EN 3311:2009
|
Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Bar for machining - D < 110 mm |
SAE AMS 2488 : 2000
|
ANODIC TREATMENT - TITANIUM AND TITANIUM ALLOYS SOLUTION PH 13 OR HIGHER |
ISO 2685:1998
|
Aircraft — Environmental test procedure for airborne equipment — Resistance to fire in designated fire zones |
ISO 10583:1993
|
Aerospace fluid systems — Test methods for tube/fitting assemblies |
SAE AMS 5643 : 2016
|
STEEL, CORROSION-RESISTANT, BARS, WIRE, FORGINGS, MECHANICAL TUBING, AND RINGS, 16CR - 4.0NI - 0.30CB (NB) - 4.0CU, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
SAE AMS 5743 : 2014
|
STEEL, CORROSION AND HEAT-RESISTANT, BARS AND FORGINGS 15.5CR - 4.5NI - 2.9MO - 0.10N SOLUTION HEAT TREATED, SUB-ZERO COOLED, EQUALIZED, AND OVER-TEMPERED |
PREN 3314 : 200P2
|
AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 - SOLUTION TREATED AND AGED - BAR FOR MACHINING - D <= 75 MM |
ISO 6772:2012
|
Aerospace — Fluid systems — Impulse testing of hydraulic hose, tubing and fitting assemblies |
SAE AMS 4965 : 2014
|
TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS, 6.0AL 4.0V, SOLUTION HEAT TREATED AND AGED |
SAE AMS 5734 : 2012
|
STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS, AND TUBING, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED, 1650 DEGREES F (899 DEGREES C) SOLUTION HEAT TREATED |
ISO 11218:2017
|
Aerospace Cleanliness classification for hydraulic fluids |
SAE AMS 5732 : 2012
|
STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS, TUBING AND RINGS, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED 1800 DEGREES F (982 DEGREES C), SOLUTION AND PRECIPITATION HEAT TREATED |
PREN 4836 : DRAFT 2017
|
AEROSPACE SERIES - ADAPTOR, PIPE COUPLING 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) RING-LOCKED FITTING REDUCER - FLARELESS END - INCH SERIES - EXTRA FINE THREAD PITCH |
SAE AMS 5731 : 2012
|
STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS, TUBING, AND RINGS, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED, 1800 DEGREES F (982 DEGREES C) SOLUTION HEAT TREATED |
EN 2424:2008
|
Aerospace series - Marking of aerospace products |
ISO 7257:2016
|
Aircraft Hydraulic tubing joints and fittings Rotary flexure test |
SAE AMS 2700E : 2011
|
PASSIVATION OF CORROSION RESISTANT STEELS |
ISO 7137:1995
|
Aircraft — Environmental conditions and test procedures for airborne equipment |
SAE AS 5000 : 2010
|
FITTING, PLUG-IN UNION, RING LOCKED, 24 DEGREE CONE, FLUID CONNECTION, 5080 PSI (35000 KPA), SPECIFICATION FOR |
SAE AMS 4967 : 2014
|
TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS 6.0AL - 4.0V ANNEALED, HEAT TREATABLE |
FED-STD-595 Revision C:2008
|
COLORS USED IN GOVERNMENT PROCUREMENT |
ISO 3161:1999
|
Aerospace — UNJ threads — General requirements and limit dimensions |
SAE AMS 4928 : 2016
|
TITANIUM ALLOY BARS, WIRE, FORGINGS, RINGS, AND DRAWN SHAPES, 6AL - 4V, ANNEALED |
PREN 4834 : DRAFT 2017
|
AEROSPACE SERIES - ADAPTOR, PIPE COUPLING 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) PORT FOR RING LOCKED FITTING - INCH SERIES - GEOMETRIC CONFIGURATION |
ISO 6773:1994
|
Aerospace Fluid systems Thermal shock testing of piping and fittings |