SAE ARP4402A

Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure

SAE International, 09/22/2020

Publisher: SAE

File Format: PDF

$58.00$116.00

Description

Published:22/09/2020

Pages:23

File Size:1 file , 520 KB

Note:This product is unavailable in Ukraine, Russia, Belarus

SAE ARP4402A establishes the requirements and procedures for eddy current inspection of open fastener holes in aluminum aircraft structures.

More SAE standard pdf

SAE AMS2483C

Blackening Solution for Aluminum Touch-Up Solution

$27.00 $54.00

SAE AS5419/9B

WIRE, THERMOCOUPLE, SMOOTH SURFACE FP/POLYIMIDE/FP INSULATED, NICKEL/CHROMIUM (KP); NICKEL/ALUMINUM/MANGANESE (KN) THERMOCOUPLE EXTENSION, NORMAL WEIGHT, 260 °C (Stabilized: Jan 2021)

$38.00 $76.00

SAE AS5419/8B

WIRE, THERMOCOUPLE, SMOOTH SURFACE, FP/POLYIMIDE/FP INSULATED, NICKEL/CHROMIUM (KP); NICKEL/ALUMINUM/MANGANESE (KN) THERMOCOUPLE EXTENSION, LIGHT WEIGHT, 260 °C (Stabilized: Jan 2021)

$38.00 $76.00

SAE J2215_202101

Surface Match Verification Method for Pressure Sensitive Adhesively Attached Components (Stabilized: Jan 2021)

$30.00 $60.00