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SAE International, 10/22/2020
Publisher: SAE
File Format: PDF
$65.00$130.00
Published:22/10/2020
File Size:1 file , 280 KB
Note:This product is unavailable in Ukraine, Russia, Belarus
This SAE Aerospace Recommended Practice (ARP) provides to the aerospace industry a procedure for the consistent and accurate calculation of fuel flow using turbine flowmeters during development, production, and post overhaul/repair gas turbine engine testing.
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, UNS S66286, 130 KSI MIN, .1900-32 UNJF-3A
$20.00 $40.00
Gland Design, O-Ring and Other Elastomeric Seals, Static Applications
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Aerospace - Deicing/Anti-Icing Self-Propelled Vehicle Functional Requirements
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Nickel Alloy, Corrosion- and Heat-Resistant, Bars, Forgings, Extrusions, Rings, and Stock for Forgings and Rings 52.5Ni - 19Cr - 3.0Mo - 5.1Cb (Nb) - 0.90Ti - 0.50Al - 18Fe Consumable Electrode or Vacuum Induction Melted 1950 °F (1066 °C) Solution Heat Treated, Precipitation Hardenable
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