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  • SAE ARP 699 : 2015

    Current The latest, up-to-date edition.

    HIGH TEMPERATURE PNEUMATIC DUCT SYSTEMS FOR AIRCRAFT

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  09-11-2015

    Publisher:  SAE International

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    Table of Contents - (Show below) - (Hide below)

    1. SCOPE
    2. REFERENCES
    3. TERMINOLOGY
    4. INSTALLATION CRITERIA AND LIMITATIONS
    5. DUCT SYSTEM AND DUCT COMPONENT
       DESIGN CRITERIA
    6. FIELD MAINTENANCE AND INSPECTION CRITERIA

    Abstract - (Show below) - (Hide below)

    Specifies the design, installation, testing, and field maintenance criteria for a high temperature metal pneumatic duct system, for use as a guide in the aircraft industry.

    General Product Information - (Show below) - (Hide below)

    Committee AC-9
    Document Type Standard
    Publisher SAE International
    Status Current
    Supersedes

    Standards Referenced By This Book - (Show below) - (Hide below)

    SAE AIR 744 : 2015 AEROSPACE AUXILIARY POWER SOURCES
    SAE AIR 806 : 2015 AIR CONDITIONING OF AIRCRAFT CARGO
    SAE AS 1895 : 2016 COUPLING ASSEMBLY, V-RETAINER, HIGH PRESSURE, HIGH TEMPERATURE, PNEUMATIC TUBE
    SAE ARP 217 D : 2016 TESTING OF AIRPLANE INSTALLED ENVIRONMENTAL CONTROL SYSTEMS (ECS)
    JSSG-2009 Revision A:2013 Air Vehicle Subsystems
    SAE ARP 85 : 2012 AIR CONDITIONING SYSTEMS FOR SUBSONIC AIRPLANES
    SAE AIR 869 : 2014 V-COUPLINGS, INCLUDING V-BAND AND V-RETAINER COUPLING ASSEMBLIES, FLANGE AND SEAL DESIGN, APPLICATION OF
    SAE ARP 1796 : 2015 ENGINE BLEED AIR SYSTEMS FOR AIRCRAFT
    SAE J 1775 : 2015 BLEED-AIR PNEUMATIC SYSTEMS FOR GAS TURBINE EQUIPPED MARINE AND AMPHIBIOUS CRAFT
    SAE ARP 292 : 2014 ENVIRONMENTAL CONTROL SYSTEMS FOR HELICOPTERS

    Standards Referencing This Book - (Show below) - (Hide below)

    SAE AMS 4912 : NONCURRENT SHEET AND STRIP, 4A1 3MO 1V, SOLUTION HEAT TREATED
    SAE AMS 5525 : 2012 STEEL, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, 1800 DEGREE F (982 DEGREE C) SOLUTION HEAT TREATED
    SAE AMS 4911 : 2014 TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 4 V, ANNEALED
    MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    SAE AMS 5599 : 2016 NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 62NI - 21.5CR - 9.0MO - 3.7 CB (NB), ANNEALED
    SAE AMS 5512 : 2012 STEEL, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 18CR - 10.5NI - 0.80CB (SAE 30347), SOLUTION HEAT TREATED
    SAE AMS 5542 : 2012 NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 72NI - 15.5CR - 0.95CB(NB) - 2.5TI - 0.70AL - 7.0FE, ANNEALED
    SAE AMS 5595 : 2014 STEEL, CORROSION RESISTANT, SHEET, STRIP, AND PLATE, 9.0MN - 20CR - 6.5NI - 0.28N, SOLUTION HEAT TREATED
    SAE AMS 5526 : 1989 STEEL SHEET, STRIP, AND PLATE, CORROSION AND HEAT RESISTANT, 19.5CR - 9.5NI - 1.4MO - 1.4W - 0.42(CB+TA) - 0.22TI, SOLUTION HEAT TREATED
    SAE AMS 5510S : 2014 STEEL, CORROSION AND HEAT-RESISTANT, SHEET, STRIP AND PLATE, 18CR - 10.5NI - 0.40TI (SAE 30321) SOLUTION HEAT TREATED
    SAE AMS 5603 : 2001 SHEET AND STRIP-15CR 8.4NI 2.2MO 1.1AL, VAC. INDUCT. MELTED, SOLUTION HEAT TREATED
    MIL W 27664 : NOTICE 1 WELDING, SPOT, INERT-GAS SHIELDED ARC
    SAE AMS 4910 : 2017 TITANIUM ALLOY, SHEET, STRIP, AND PLATE 5AL - 2.5SN ANNEALED
    SAE AMS 5545 : 2010 NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 54NI - 19CR - 11CO - 9.8MO - 3.2TI - 1.5AL - 0.006B, VACUUM INDUCTION AND CONSUMABLE ELECTRODE MELTED, SOLUTION HEAT TREATABLE, PRECIPITATION HEAT TREATED
    SAE AMS 5548 : 2012 STEEL, CORROSION AND HEAT-RESISTANT, SHEET AND STRIP, 16.5CR - 4.5NI - 2.9MO - 0.10N, 1850 TO 1975 DEGREES F (1010 TO 1079 DEGREES C) ANNEALED
    MIL-W-8611 Revision A:1957 WELDING, METAL ARC AND GAS STEELS AND CORROSION AND HEAT RESISTANT ALLOYS PROCESS FOR
    SAE AMS 5528 : 2012 STEEL, CORROSION-RESISTANT, SHEET, STRIP, AND PLATE, 17CR - 7.1NI - 1.1AL, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE
    MIL-W-6858 Revision D:1978 WELDING RESISTANCE, SPOT AND SEAM
    SAE AMS 4916 : 2014 TITANIUM ALLOY SHEET, STRIP, AND PLATE 8AL - 1MO - 1V DUPLEX ANNEALED
    SAE AMS 5596 : 2016 NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, FOIL AND PLATE, 52.5NI - 19CR - 3.0MO - 5.1CB (NB) - 0.90TI - 0.50AL - 18FE, CONSUMABLE ELECTRODE REMELTED OR VACUUM INDUCTION MELTED, 1775 DEGREES F (968 DEGREES C) SOLUTION HEAT TREATED
    SAE AMS 4901 : 2015 TITANIUM SHEET, STRIP, AND PLATE, COMMERCIALLY PURE, ANNEALED, 70.0 KSI (485 MPA)
    SAE AMS 4900 : 2014 TITANIUM SHEET, STRIP, AND PLATE, COMMERCIALLY PURE, ANNEALED, 55.0 KSI (379 MPA) YIELD STRENGTH
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