We noticed you’re not on the correct regional site. Switch to our AMERICAS site for the best experience.
  • SAE ARP 699 : 2015

    Current The latest, up-to-date edition.
    Add to Watchlist
    This Standard has been added successfully to your Watchlist.
    Please visit My Watchlist to see all standards that you are watching.
    Please log in or to add this standard to your Watchlist.
    We could not add this standard to your Watchlist.
    Please retry or contact support for assistance.
    You need to be logged in to add this standard to your Watchlist.
    Please log in now or create an account to add.
    You already added this Product in the Watchlist.

    HIGH TEMPERATURE PNEUMATIC DUCT SYSTEMS FOR AIRCRAFT

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  09-11-2015

    Publisher:  SAE International

    Add to Watchlist

    Add To Cart

    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 : A AIR VEHICLE SUBSYSTEMS (JOINT SERVICE SPECIFICATION GUIDE)
    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 : G 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 : A 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 : D 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
    • Access your standards online with a subscription

      Features

      • Simple online access to standards, technical information and regulations
      • Critical updates of standards and customisable alerts and notifications
      • Multi - user online standards collection: secure, flexibile and cost effective