Overview

Reference standards should be used in every application and are available in many configurations.

Standard references availabe for the following:

Standard references manufactured from the follwing materials:

Olympus can manufacture reference standards for any aircraft manufacturer or any other eddy current applicaiton.

Reference Standards

Standard Type	Description	Reference	Part ID	Item Number
Surface Crack	Aluminum Surface Crack Standard	.008 in., .020 in., .040 in. Notch Depths	SRS-0824A	U8860536
Surface Crack	Carbon Steel Crack Standard	.008 in., .020 in., .040 in. Notch Depths	SRS-0824S	U8860546
Surface Crack	Stainless Steel Crack Standard	.008 in., .020 in., .040 in. Notch Depths	SRS-0824SS	U8860549
Surface Crack	Titanium Crack Standard	.008 in., .020 in., .040 in. Notch Depths	SRS-0824T	U8860550
Surface Crack	Magnesium Crack Standard	.008 in., .020 in., .040 in. Notch Depths	SRS-0824M	U8860545
Hole	Mulitple Hole Standard - Number of holes-Version-Material-Notch type	EC Reference Standard with Cert	MHS-12-1A-0	U8860405
Hole	Mulitple Hole Standard - Number of holes-Version-Material-Notch type	EC Reference Standard with Cert	MHS-29-1A-0	U8860423
Hole	Reference standard Aluminum 7075-T651 / 7075-T73	(NRK-3AL)	1920166	U8861513
Hole	Reference Standard Stainless Steel	(NRK-3SS)	NRK-3SS	U8861604
Hole	Reference Standard Titanium	(NRK-3T)	1920167	U8860227
Hole	Reference Standard 4340 Steel	(NRK-3ST)	1920168	U8880206
Fastener	SPO-3932 Sliding Probe Crack Standard 2nd Layer Aluminum	SPO-3932	1916915	U8860199
Thickness	Thickness Reference Standard. 5 Step Aluminum 7075-T6	with 0.020 in., 0.040 in., 0.060 in., 0.080 in., 0.100 in. thickness steps with 0.75 in. square pads.	TRS-5-8A-7075-T6	U8861613
Training	New Training Standard	Training	NEC-6151-SD	U8861706

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