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SAE AS1241D

Current

Current

The latest, up-to-date edition.

FIRE RESISTANT PHOSPHATE ESTER HYDRAULIC FLUID FOR AIRCRAFT

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

16-09-2016

€137.83
Excluding VAT

1. SCOPE
2. APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS
4. QUALIFICATION
5. QUALITY CONTROL
6. PACKAGING AND MARKING
7. NOTES

Describes the requirements for physical and chemical properties and the minimum tests to evaluate suitability of phosphate ester hydraulic fluids for use in aircraft systems where fire resistance is required.

Committee
A-6C1
DocumentType
Standard
Pages
28
PublisherName
SAE International
Status
Current
Supersedes

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SAE AIR 5693 : 2014 COMPATIBILITY OF PTFE HOSE ASSEMBLIES WITH TYPICAL FLUIDS FOUND IN AEROSPACE APPLICATIONS
SAE AS 1501 : 1994 HOSE, AIR DUCT, FLEXIBLE, NONMETALLIC, AIRCRAFT
BS EN 3155-039:2007 Aerospace series. Electrical contacts used in elements of connection Contacts, electrical, coaxial, size 16, female, type D, solder, class R. Product standard
BS EN 3372-001:2007 Aerospace series. Connectors, electrical, circular, medium and high contact density, scoop-proof with bayonet coupling, operating temperatures -65°C to 175°C or 200°C continuous Technical specification
BS EN 3545-001:2008 Aerospace series. Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures -55°C to 175°C Technical specification
BS EN 3155-013:2006 Aerospace series. Electrical contacts used in elements of connection Contacts, electrical, triaxial, size 8, female, type D, solder, class R. Product standard
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SAE AS 5951 : 2017 HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA-ARAMID REINFORCED, 5080 PSI (35,000 KPA), 275 DEGREES F (135 DEGREES C), AIRCRAFT HYDRAULIC SYSTEMS
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SAE AS18280F FITTINGS, 24 DEGREES CONE FLARELESS, FLUID CONNECTION, 3000 PSI
ISO 9940:2015 Aerospace series Fluid, hydraulic, phosphate ester-base, fire resistant Technical specification
MIL-PRF-8805-39 Revision J:2014 SWITCHES, SENSITIVE, LIMIT, PLUNGER, 7 AMPERES, RESILIENT SEAL, FLUID RESISTANT
I.S. EN 3545-001:2008 AEROSPACE SERIES - CONNECTORS, ELECTRICAL, RECTANGULAR, WITH SEALED AND NON-SEALED REAR, PLASTIC HOUSING, LOCKING DEVICE, OPERATING TEMPERATURES -55 DEGREES C TO 175 DEGREES C - PART 001: TECHNICAL SPECIFICATION
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SAE AMS 7254 : 2014 PERFLUOROETHER ELASTOMER
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SAE ARP 1281 : 2002 ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR
01/704903 DC : DRAFT MAR 2001 PREN 3155-039 - AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 039: CONTACTS, ELECTRICAL, COAXIAL, SIZE 16, FEMALE, TYPE D, SOLDER, CLASS R - PRODUCT STANDARD
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SAE ARP 5311 : 2016 AEROSPACE-INTERFACE DEFINITION FOR MECHANICAL ACTUATION SUBSYSTEMS
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SAE AS 4510 : 2013 FITTINGS, WELD, FLUID CONNECTION, 5000 PSI
SAE AS 5000 : 2010 FITTING, PLUG-IN UNION, RING LOCKED, 24 DEGREE CONE, FLUID CONNECTION, 5080 PSI (35000 KPA), SPECIFICATION FOR
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SAE AS4623E HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA-ARAMID REINFORCED, 3,000 PSI, 275 DEGREES F, HEAVY DUTY, AIRCRAFT HYDRAULIC SYSTEMS
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SAE AS1975G Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems
SAE AMS7256B RINGS, SEALING, TETRAFLUOROETHYLENE/PROPYLENE RUBBER (FEPM) HYDRAULIC FLUID AND SYNTHETIC OIL RESISTANT 85 TO 95
SAE AS 6235 : 2015 FACE SEAL GLAND DESIGN, STATIC, O-RING AND OTHER SEALS FOR AEROSPACE HYDRAULIC AND PNEUMATIC APPLICATIONS
MIL-PRF-6164 Revision G:2012 VALVE; AIRCRAFT, PNEUMATIC, HIGH-PRESSURE CHARGING
MIL-PRF-8805-40 Revision K:2014 SWITCHES, SENSITIVE, PLUNGER, RESILIENT SEAL, FLUID RESISTANT
BS ISO 9940:2015 Aerospace series. Fluid, hydraulic, phosphate ester-base, fire resistant. Technical specification
01/704904 DC : DRAFT MAR 2001 PREN 3155-040 - AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 040 - CONTACTS, ELECTRICAL, COAXIAL, SIZE 12, MALE, TYPE D, SOLDER, CLASS R - PRODUCT STANDARD
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SAE AMS3306C RUBBER, SILICONE 1200 PSI (8.27 MPA), HIGH MODULUS 55 - 65
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SAE MA 1975 : 2015 HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE, ARAMID REINFORCED, 135 DEGREE C, STANDARD DUTY, 28000/21000 KPA, HYDRAULIC, AIRCRAFT SYSTEMS
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BS EN 3155-025:2006 Aerospace series. Electrical contacts used in elements of connection Contacts, electrical, triaxial, size 8, female, type D, crimp, class S. Product standard
BS EN 3155-059:2006 Aerospace series. Electrical contacts used in elements of connection Contacts, electrical, coaxial, size 16, female, type D, solder, class R. Product standard
BS EN 2350:1991 Circuit breakers. Technical specification
BS EN 3708-001:2006 Aerospace series. Modular interconnection systems. Terminal junction systems Technical specification
BS EN 3155-040:2007 Aerospace series. Electrical contacts used in elements of connection Contacts, electrical, coaxial, size 12, male, type D, solder, class R. Product standard
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BS EN 3155-024:2006 Aerospace series. Electrical contacts used in elements of connection Contacts, electrical, triaxial, size 8, male, type D, crimp, class S. Product standard
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EN 3708-001:2006 Aerospace series - Modular interconnection systems - Terminal junction systems - Part 001: Technical specification
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EN 3372-001:2007 Aerospace series - Connectors, electrical, circular, medium and high contact density, scoop-proof with bayonet coupling, operating temperatures - 65 °C to 175 °C or 200 °C continuous - Part 001: Technical specification
EN 3218-001:2006 Aerospace series - Connectors, rectangular, with metallic shells and screw-locking - Part 001: Technical specification
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EN 3155-013:2006 Aerospace series - Electrical contacts used in elements of connection - Part 013: Contacts, electrical, triaxial, size 8, female, type D, solder, class R - Product standard
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EN 2350:1990 Aerospace series - Circuit breakers - Technical specification
EN 3155-060:2006 Aerospace series - Electrical contacts used in elements of connection - Part 060: Contacts, electrical, coaxial, size 12, male, type D, solder, class R Product standard
EN 3545-001:2008 Aerospace series - Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures - 55 °C to 175 °C - Part 001: Technical specification
EN 3155-061:2006 Aerospace series - Electrical contacts used in elements of connection - Part 061: Contacts, electrical, coaxial, size 12, female, type D, solder, class R Product standard
EN 3155-069:2009 Aerospace series - Electrical contacts used in elements of connection - Part 069: Contacts, electrical, coaxial, size 16, female, type D, solder, class P - Product standard
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EN 3155-024:2006 Aerospace series - Electrical contacts used in elements of connection - Part 024: Contacts, electrical, triaxial, size 8, male, type D, crimp, class S - Product standard
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SAE ARP 4943 : 2008 GROUND SUPPORT EQUIPMENT HYDRAULIC SYSTEMS, DESIGN AND INSTALLATION, RECOMMENDED PRACTICES FOR
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SAE AMS 3144 : 2012 PRIMER, ANODIC ELECTRODEPOSITION FOR AIRCRAFT APPLICATIONS
ISO 23933:2006 Aerospace Aramid reinforced lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 135 degrees C/20 684 kPa (275 degrees F /3 000 psi) and 135 degrees C/21 000 kPa (275 degrees F/3 046 psi) Procurement specification
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SAE MA 4623 : 2015 Hose Assembly, Polytetrafluoroethylene, Para Aramid Reinforced Heavy-Duty, 21 000 kPa, 135 °C, Aircraft Hydraulic Systems, Metric
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SAE ARP1311D Landing Gear Structures and Mechanisms

SAE AMS QQ A 250/12 : 2013 ALUMINUM ALLOY 7075, PLATE AND SHEET
IP 71 : 1995 SECTION 1: PETROLEUM PRODUCTS - TRANSPARENT AND OPAQUE LIQUIDS - DETERMINATION OF KINEMATIC VISCOSITY AND CALCULATION OF DYNAMIC VISCOSITY - SECTION 2: GLASS CAPILLARY KINEMATIC VISCOMETERS - SPECIFICATIONS AND OPERATING INSTRUCTIONS (TWO PART SET)
ASTM D 892 : 2013-07 TEST METHOD FOR FOAMING CHARACTERISTICS OF LUBRICATING OILS
SAE AMSQQP416E PLATING, CADMIUM (ELECTRODEPOSITED)
SAE AMS6280L STEEL BARS, FORGINGS, AND RINGS, 0.50CR - 0.55NI - 0.20MO (0.28 - 0.33C) (SAE 8630)
SAE AMS4911N TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 4 V, ANNEALED
ASTM D 2155 : 2012 Standard Test Method for Determination of Fire Resistance of Aircraft Hydraulic Fluids by Autoignition Temperature
ASTM D 1217 : 2015 : REDLINE Standard Test Method for Density and Relative Density (Specific Gravity) of Liquids by Bingham Pycnometer
SAE AMS4376H PLATE, MAGNESIUM ALLOY - 3.0AL - 1.0ZN - 0.20MN (AZ31B-H26) COLD ROLLED AND PARTIALLY ANNEALED
SAE AMS T 9046 : 2002 TITANIUM AND TITANIUM ALLOY, SHEET, STRIP, AND PLATE
SAE AMSQQA250/4B ALUMINUM ALLOY 2024, PLATE AND SHEET
NAS 1613 : 2002 PACKING, PREFORMED, ETHYLENE PROPYLENE RUBBER
SAE AMS4035K ALUMINUM ALLOY, SHEET AND PLATE, 4.4CU - 1.5MG - 0.60MN (2024-0) ANNEALED; OR WHEN SPECIFIED, 'AS FABRICATED' (2024-F)
SAE AMS4045L ALUMINUM ALLOY SHEET AND PLATE 5.6ZN - 2.5MG - 1.6CU - 0.23CR 7075: (-T6 SHEET, -T651 PLATE) SOLUTION AND PRECIPITATION HEAT TREATED
SAE AMS5044J STEEL, SHEET AND STRIP, 0.15 CARBON, MAXIMUM, HALF HARD TEMPER
MIL-PRF-680 Revision C:2010 DEGREASING SOLVENT
SAE AIR1362C AEROSPACE HYDRAULIC FLUIDS PHYSICAL PROPERTIES
SAE AMS T 81533 : 2001 TRICHLOROETHANE 1, 1, 1, (METHYL CHLOROFORM) INHIBITED, VAPOR DEGREASING
ASTM B 152/B152M : 2013 : REDLINE Standard Specification for Copper Sheet, Strip, Plate, and Rolled Bar
SAE AMS4375L SHEET AND PLATE, MAGNESIUM ALLOY - 3.0AL - 1.0ZN - 0.20MN (AZ31B-0) ANNEALED AND RECRYSTALLIZED
IP 15 : 2015 PETROLEUM PRODUCTS - DETERMINATION OF POUR POINT
SAE AS 4059F : 2013 AEROSPACE FLUID POWER - CONTAMINATION CLASSIFICATION FOR HYDRAULIC FLUIDS
SAE AMS6350N STEEL SHEET, STRIP, AND PLATE, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130)
SAE AMS4944L TITANIUM ALLOY TUBING, SEAMLESS, HYDRAULIC 3.0AL - 2.5V COLD WORKED, STRESS RELIEVED
SAE AMS 4500 : 2007 COPPER, SHEET, STRIP, AND PLATE, SOFT ANNEALED

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