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SAE ARP 699 : 2015

SAE ARP 699 : 2015

Current

Current

The latest, up-to-date edition.

HIGH TEMPERATURE PNEUMATIC DUCT SYSTEMS FOR AIRCRAFT

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

11-09-2015

Publisher

SAE International

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

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.

Committee
AC-9
DocumentType
Standard
Pages
103
PublisherName
SAE International
Status
Current
Supersedes

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

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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Hardcopy - English
PDF - English
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