• Your shopping cart is empty!

  • SAE ARP1947B
Provide PDF Format

Learn More

SAE ARP1947B

  • Dendrite Arm Spacing of Structural Aircraft Quality D357 Aluminum Alloy Castings, Determination and Acceptance of
  • standard by SAE International, 08/01/2007
  • Publisher: SAE

$37.00$74.00


This document covers the recommended practice for determining the acceptability of the dendrite arm spacing (DAS) of D357-T6 aluminum alloy castings required to have tensile strength not lower than 50,000 psi (345 MPa). To apply this method, at least two coupons used for DAS measurement and tensile testing, shall be attached to the casting in locations as defined by the cognizant engineering organization. Areas of the casting which require DAS control must be accessible for surface DAS measurements.

Product Details

Published:
08/01/2007
File Size:
1 file , 510 KB

Related Products

SAE MA3388A

SAE MA3388A

STUD, STEPPED - 2.0 DIA ENGAGEMENT, A286, MJ METRIC 6 X 1 - 5 X 0.8 (Stabilized: Jan 2015)..

$37.00 $74.00

SAE AS1337A

SAE AS1337A

Selected Aerospace Diameter Pitch Combinations of Metric 60° Screw Threads for Nuts and Bolts..

$37.00 $74.00

SAE J 1033

SAE J 1033

Procedure for Measuring Bore and Face Runout of Flywheels, flywheel housings and Flywheel Housing Ad..

$37.00 $74.00

SAE AS17108A

SAE AS17108A

Bearing, Ball, Annular, Primarily for Aircraft Generators and Motor-Generators, Wide Cartridge, Type..

$37.00 $74.00