SAE ARP699E
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
09-11-2015
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.
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 AIR744C | 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 ARP85F | 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 ARP292C | ENVIRONMENTAL CONTROL SYSTEMS FOR HELICOPTERS |
| SAE ARP85F:2019 | Air Conditioning Systems for Subsonic Airplanes<br> |
| SAE AS4073B:2019 | Air Cycle Air Conditioning Systems for Air Vehicles |
| 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 AMS4911N | TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 4 V, ANNEALED |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| SAE AMS5599H | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 62NI - 21.5CR - 9.0MO - 3.7 CB (NB), ANNEALED |
| SAE AMS5512L | STEEL, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 18CR - 10.5NI - 0.80CB (SAE 30347), SOLUTION HEAT TREATED |
| SAE AMS5542N | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 72NI - 15.5CR - 0.95CB(NB) - 2.5TI - 0.70AL - 7.0FE, ANNEALED |
| SAE AMS5595G | STEEL, CORROSION RESISTANT, SHEET, STRIP, AND PLATE, 9.0MN - 20CR - 6.5NI - 0.28N, SOLUTION HEAT TREATED |
| SAE AMS5526J | 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 AMS5510S | 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 AMS4910R | 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 AMS5528H | 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 AMS4916K | TITANIUM ALLOY SHEET, STRIP, AND PLATE 8AL - 1MO - 1V DUPLEX ANNEALED |
| SAE AMS5596L | 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 AMS4900P | TITANIUM SHEET, STRIP, AND PLATE, COMMERCIALLY PURE, ANNEALED, 55.0 KSI (379 MPA) YIELD STRENGTH |
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