SAE ARP699E
Current
The latest, up-to-date edition.
High Temperature Pneumatic Duct Systems for Aircraft
Hardcopy , PDF
English
09-11-2015
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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.
| DocumentType |
Standard
|
| Pages |
103
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
This Recommended Practice is intended to outline 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. These recommendations are to be considered as currently applicable and necessarily subject to revision from time to time, as a result of the rapid development of the industry.
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| 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 AMS5545F | 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 Treated Precipitation Heat Treatable |
| SAE AMS5548P | Steel, Corrosion and Heat-Resistant, Sheet and Strip 16.5Cr - 4.5Ni - 2.9Mo - 0.10N 1850 to 1975 °F (1010 to 1079 °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 °F (968 °C) Solution Heat Treated |
| SAE AMS4901T | Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 70.0 ksi (485 MPa) |
| SAE AMS4900P | Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 55 ksi (379 MPa) Yield Strength |
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