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Recent Tool List: 2025-08-20 13:31:28
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20 Aug 2025
Tool Number
Tool Description
Location
Aircraft
or
Engine
1
1
Tool:
AFNDT-3472AL
Description:
Custom Eddy Current Bolt Hole Calibration Standard Manufactured in Accordance with Boeing Specification 51-00-00. Total of 14 with 28 EDM Notches. Hole Sizes: Diameters 13.5mm(.531"), 14.1mm(.555"), 14.3mm(.563"), 15.0mm(.591"), 15.9mm(.625"), 16.7mm(...
Location:
North America
Aircraft or Engine:
2
2
Tool:
AFNDT-3474AL
Description:
12 Hole reference standard. Material: 7075-T6 Aluminum. Contains 12 hole sizes; 1/8 inch (3.175mm), 5/32 inch (3.96mm), 3/16 inch (4.74mm), 1/4 inch (6.35mm), 5/16 inch (7.92mm), 3/8 inch (9.52mm), 7/16 inch (11.09mm), 1/2 inch (12.7mm), 9/16 inch (14....
Location:
North America
Aircraft or Engine:
3
3
Tool:
AFNDT-3474CS
Description:
12 Hole reference standard. Material: 4130 or 4340 Steel. Contains 12 hole sizes; 1/8 inch (3.175mm), 5/32 inch (3.96mm), 3/16 inch (4.74mm), 1/4 inch (6.35mm), 5/16 inch (7.92mm), 3/8 inch (9.52mm), 7/16 inch (11.09mm), 1/2 inch (12.7mm), 9/16 inch (1...
Location:
North America
Aircraft or Engine:
4
4
Tool:
AFNDT-3474CS
Description:
12 Hole reference standard. Material: 4130 or 4340 Steel. Contains 12 hole sizes; 1/8 inch (3.175mm), 5/32 inch (3.96mm), 3/16 inch (4.74mm), 1/4 inch (6.35mm), 5/16 inch (7.92mm), 3/8 inch (9.52mm), 7/16 inch (11.09mm), 1/2 inch (12.7mm), 9/16 inch (14.2
Location:
North America
Aircraft or Engine:
5
5
Tool:
AFNDT-3474TI
Description:
12 Hole reference standard. Material: 6AL-4v Titanium. Contains 12 hole sizes; 1/8 inch (3.175mm), 5/32 inch (3.96mm), 3/16 inch (4.74mm), 1/4 inch (6.35mm), 5/16 inch (7.92mm), 3/8 inch (9.52mm), 7/16 inch (11.09mm), 1/2 inch (12.7mm), 9/16 inch (14.2...
Location:
North America
Aircraft or Engine:
6
6
Tool:
AFNDT-3476CS
Description:
CUSTOM 6 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION..737 PART 6 51-00-00 FIG.3 PG. 8, 757 PT 6 51-00-17 PAGE 7 FIG 3 and 767 PT 6 51-00-16 PAGE 7 FIG 3. Includes Test Report and Certificate of Conformance..... Hole Sizes: .188", .250", .313", .3...
Location:
North America
Aircraft or Engine:
7
7
Tool:
AFNDT-3477AL
Description:
METRIC 10 STEP ALUMINUM CALIBRATION BLOCK, 1mm, 2mm, 3mm, 4mm, 5mm, 6mm, 7mm, 8mm, 9mm, 10mm ± .05mm. Pad Size: 25mm X 25mm. Material: 2024-T3 Aluminum Supplied with a Delrin Holding Block. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
8
8
Tool:
AFNDT-3477CS
Description:
METRIC 10 STEP CARBON STEEL CALIBRATION BLOCK, 1mm, 2mm, 3mm, 4mm, 5mm, 6mm, 7mm, 8mm, 9mm, 10mm ± .05mm. Pad Size: 25mm X 25mm. Material: 1018 or 4340 Carbon Steel Supplied with a Delrin Holding Block. Includes Test Report and Certificate of Conform...
Location:
North America
Aircraft or Engine:
9
9
Tool:
AFNDT-3477TI
Description:
METRIC 10 STEP TITANIUM CALIBRATION BLOCK, 1mm, 2mm, 3mm, 4mm, 5mm, 6mm, 7mm, 8mm, 9mm, 10mm ± .05mm. Pad Size: 25mm X 25mm. Material: 6AL-4V Titanium Supplied with a Delrin Holding Block. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
10
10
Tool:
AFNDT-3478TI
Description:
5 STEP WEDGE .024", .040", .060", .080", .100". TOLERANCE +/-.002". ..MATERIAL: 6AL-4V TITANIUM . PAD SIZE: 75" x .75" .Supplied with Delrin Holding Block. Includes Test Report traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
11
11
Tool:
AFNDT-3479TI
Description:
7 STEP CALIBRATION BLOCK. MATERIAL: 6AL-4V TITANIUM. STEP THICKNESS: 0.024", 0.040", 0.060", 0.800", 0.100", .150" 0.200" +/- .001". STEP PAD SIZE: .75" x .75". Note: The first and last pad is 1.0" long. Supplied With Delrin Holding Block Includes certi
Location:
North America
Aircraft or Engine:
12
12
Tool:
AFNDT-3481AL
Description:
Metric Aluminum Multi-hole reference standard. Material: 2024-T3 Aluminum. Contains 28 holes; 3.6mm, 4.0mm, 4.4mm, 4.8mm, 5.2mm, 5.6mm, 6.0mm, 6.4mm, 6.8mm, 7.2mm, 7.6mm, 8.0mm, 8.4mm, 8.8mm, 9.2mm, 9.6mm, 10.0mm, 10.4mm, 10.8mm, 11.0mm, 11.4mm, 11.8mm...
Location:
North America
Aircraft or Engine:
13
13
Tool:
AFNDT-3482AL
Description:
5 STEP CALIBRATION BLOCK, 7075-T6 ALUMINUM. STEP SIZES: .098", .197", .295", .394", .492" ± .001". PAD SIZE: 1.0" x 1.0". Supplied with Delrin Holding Block. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
14
14
Tool:
AFNDT-3482AL-1
Description:
5 STEP CALIBRATION BLOCK, 7075-T6 ALUMINUM. STEP SIZES: .020", .039", .059", .079", .098" ± .001". PAD SIZE: 1.0" x 1.0". Supplied with Delrin Holding Block. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
15
15
Tool:
AFNDT-3483AL
Description:
BOEING 2 STEP CALIBRATION BLOCK, PT 4 51-00-00 PAGE 6 FIGURE 2, MATERIAL: 7075-T6 Aluminum. Step Size: 0.150" and 0.300" ±.0.002. PAD SIZE: 1.0" X 1.0". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
16
16
Tool:
AFNDT-3483CS
Description:
BOEING 2 STEP CALIBRATION BLOCK, PT 4 51-00-00 PAGE 6 FIGURE 2, MATERIAL: LOW CARBON STEEL SUCH AS 1018, 4130 or 4340. Step Size: 0.150" and 0.300" ±.0.002. PAD SIZE: 1.0" X 1.0". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
17
17
Tool:
AFNDT-3484AL
Description:
Eddy Current Bolt Hole Calibration standard, 5 Hole Sizes. Material: 7075-T6 Aluminium, Hole diameters: .750", .875",1.00" 1.125" 1.187", .030" x .030" x .005" ± .001" Corner EDM Notch in each hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
18
18
Tool:
AFNDT-3485AL
Description:
Eddy Current Bolt Hole Calibration standard, 3 Hole Sizes. Material: 7075-T6 Aluminium, Hole diameters: 1.250" 1.375", 1.500", .030" x .030" x .005" ± .001" Corner EDM Notch in each hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
19
19
Tool:
AFNDT-3486/15-5PH
Description:
8 STEP WEDGE, STEP SIZES: 0.125", 0.150", 0.289", 0.300", 0.350", 0.476", 0.500", 0.650" +/- .001". PAD SIZE: 1.0" x 1.0". MATERIAL: 15-5PH STAINLESS STEEL SUPPLIED WITH DELRIN HOLDING BLOCK. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
20
20
Tool:
AFNDT-3487/4130
Description:
5 STEP WEDGE .050", .100", .200", .400", .500". TOLERANCE +/-.001". MATERIAL: 4130 STEEL SUPPLIED WITH HOLDING BLOCK. PAD SIZE: 1.0" x 1.0" . Includes Test Report traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
21
21
Tool:
AFNDT-3487/TI
Description:
5 STEP WEDGE .050", .100", .200", .400", .500". TOLERANCE +/-.001". MATERIAL: 6AL-4V TITANIUM SUPPLIED WITH HOLDING BLOCK. PAD SIZE: 1.0" x 1.0" . Includes Test Report traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
22
22
Tool:
AFNDT-3488/AL
Description:
5 STEP WEDGE .032", .064", .128", .256", .500". TOLERANCE +/-.001". MATERIAL: 7075-T6 ALUMINUM SUPPLIED WITH HOLDING BLOCK. PAD SIZE: 1.0" x 1.0" . Includes Test Report traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
23
23
Tool:
AFNDT-3489/AL
Description:
9 STEP WEDGE: .010", .020" .032", .040", .050", .064", .128", .256", .500". TOLERANCE +/-.001". MATERIAL: 2024-T3 ALUMINUM SUPPLIED WITH HOLDING BLOCK. PAD SIZE: 1.0" x 1.0" . Includes Test Report traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
24
24
Tool:
AFNDT-3491AL
Description:
METRIC 6 STEP WEDGE. STEP SIZE: 0.6mm, 1mm, 3mm, 7mm, 13mm, 20mm +/- .03mm. Material: 7075-T6 Aluminum. Pad Size: 20mm x 20mm square Supplied With Acetal(Delrin) Holding Block Includes Test Report Traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
25
25
Tool:
AFNDT-3492AL
Description:
METRIC 5 STEP WEDGE: STEP SIZE: 2mm, 5mm, 10mm, 15mm, 20mm +/- .03mm. Material: 7075-T6 Aluminum. Pad Size: 20mm x 20mm square Includes Test Report Traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
26
26
Tool:
AFNDT-3493AL
Description:
7 STEP REFERENCE BLOCK ..STEP PAD SIZE: 1.0" X 1.0" MATERIAL: 7075-T6 ALUMINUM. STEP RANGE:.100", .200", .300", .400", .500", .600", .700" +/- .001". Includes certification report traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
27
27
Tool:
AFNDT-3496CS
Description:
8 STEP WEDGE, STEP SIZES: .020", .025", .030", .040", .050", .060", .080", and .100" +/- .001". PAD SIZE: .75" x .75" Supplied With Delrin Holding Block. MATERIAL: 4340 Steel . Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
28
28
Tool:
AFNDT-3496TI
Description:
8 STEP WEDGE, STEP SIZES: .020", .025", .030", .040", .050", .060", .080", and .100" +/- .001". PAD SIZE: .75" x .75" Supplied With Delrin Holding Block. MATERIAL: 6AL-4V TITANIUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
29
29
Tool:
AFNDT-3497/2024-T3
Description:
5 STEP WEDGE 2024-T351, Step Sizes: 0.5mm, 1.0mm, 1.5mm, 2.0mm, 2.5mm, +/-0.05mm Pad Size: 25mm x 25mm. Includes Certification Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
30
30
Tool:
AFNDT-3499
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD. Low Hydrogen Embrittlement Cadmium-Titaniium Alloy Plating per BAC5804. 4 EDM FLAWS ON BOTH SIDES. ONE SIDE UNPLATED(BARE). NOTCH DEPTHS : .005", .010", .020", .050". NOTCH WIDTH: (.007" +/- .002"). MATERIAL: 4...
Location:
North America
Aircraft or Engine:
31
31
Tool:
AFNDT-3500/MAG
Description:
Surface reference standard, Magnesium, with EDM notch depths of 0.008", 0.020", 0.030 and 0.040" inches (0.2mm, 0.51mm, 0.76mm and 1.02mm). Reference standard overall dImensions 1 X 5 X 0.25 inches (2.54cm X 12.7cm X 6.35mm). EDM notches .007" W MAX Inclu
Location:
North America
Aircraft or Engine:
32
32
Tool:
AFNDT-3502AL
Description:
4 HOLE ALUMINUM CALIBRATION STANDARD. ....2 HOLE SIZES AT 2.38mm DIAMETER WITH A CONER EDM NOTCH .030" x .030" X .005" WIDE ± .001" IN ONE HOLE. NO EDM NOTCH IN THE SECOND HOLE.....2 COUNTERSINK HOLES AT .0937mm DIAMETER WITH AN EDM NOTCH IN ONE OF T...
Location:
North America
Aircraft or Engine:
33
33
Tool:
AFNDT-3503AL
Description:
Aluminum Multi-hole reference standard. Material: 7075-T6 Aluminum. Contains 12 hole sizes; .154" (3.9mm), .189" (4.8mm) .217"(5.50mm), .248"(6.3mm), .281"(7.13mm), .312"(7.92mm), .344" (8.71mm), .375"(9.52mm), .437" (11.09mm), .500"(12.7mm), .562" (...
Location:
North America
Aircraft or Engine:
34
34
Tool:
AFNDT-3504TI
Description:
12 HOLE REFERENCE STANDARD MANUFACTURED TO SPECIFICATION USAF T.O. 33-B-1-1. MATERIAL: 6AL-4V TITANIUM. HOLE SIZES: 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 7/16", 1/2", 9/ 16" 5/8", 3/4" 0.020" x 0.004" +/-.001" Wide thru EDM NOTCHES. 4 tot...
Location:
North America
Aircraft or Engine:
35
35
Tool:
AFNDT-3505/6061-T4
Description:
METRIC 10 STEP CALIBRATION BLOCK, 0.5mm, 1mm, 1.5mm, 2mm, 2.5mm, 3mm, 3.5mm, 4mm, 4.5mm, 5mm ± .05mm. Pad Size: 20mm X 20mm. Material: 6061-T4 Aluminum. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
36
36
Tool:
AFNDT-3506
Description:
SINGLE HOLE REFERENCE STANDARD, HOLE SIZE 3.0", EDM CORNER NOTCH: .030" x .030" x .005 ± .002", MID-WALL NOTCH:.060" x .030" DEEP +/-.002". MATERIAL: 7075-T6 DIMENSIONS: 4.0" x 4.0" x 0.5" Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
37
37
Tool:
AFNDT-3507
Description:
Custom 2 hole BOEING REFERENCE STANDARD MANUFACTURED PER 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Includes Test Report and Certificate of Conformance. ....HOLE SIZES: 0.344" (11/32''),0.562"...
Location:
North America
Aircraft or Engine:
38
38
Tool:
AFNDT-3508/6061
Description:
METRIC 5 STEP CALIBRATION BLOCK, 6061-T4 ALUMINUM. STEP SIZES: .5mm, 1.0mm, 1.5mm, 2.0mm, 2.5mm. PAD SIZE: 1.0" x 1.0". PROVIDED WITH A DELRIN HOLDER.Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
39
39
Tool:
AFNDT-3509
Description:
SINGLE HOLE REFERENCE STANDARD, HOLE SIZE 27.7mm(1.090"), EDM CORNER NOTCH: .030" x .030" x .005 ± .002", MATERIAL: 7075-T6 DIMENSIONS: 3.0" x 3.0" x 0.5" Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
40
40
Tool:
AFNDT-3510/2024T3
Description:
Contains 12 hole sizes; 187", .203", .218", .234", .250", .265", .281", .296", .312", .328", .343" and .359" diameters. ( .030" x .030" Corner EDM Notch and 3 Surface EDM Notches .010", .020", .040" Deep x .750" Long.) Material: 2024-T3 Aluminum. Inclu...
Location:
North America
Aircraft or Engine:
41
41
Tool:
AFNDT-3510/6AL4V
Description:
Contains 12 hole sizes; 187", .203", .218", .234", .250", .265", .281", .296", .312", .328", .343" and .359" diameters. ( .030" x .030" Corner EDM Notch and 3 Surface EDM Notches .010", .020", .040" Deep x .750" Long.) Material: 6AL-4V Titanium. Includ...
Location:
North America
Aircraft or Engine:
42
42
Tool:
AFNDT-3512AL
Description:
MISTRAS 3 HOLE EDDY CURRENT TEST STANDARD, HOLE SIZES: .250", .375", .500" DIAMETERS, EDM CORNER NOTCH: .025" x .025" x .005 ± .002", MID-WALL NOTCH:.080" x .025" DEEP +/-.002" per BSS7048. 1 SURFACE EDM NOTCH .150" LONG x .030" DEEP. ALL NOTCHES TO B...
Location:
North America
Aircraft or Engine:
43
43
Tool:
AFNDT-3513AL
Description:
SAFRAN MESSIER -BUGATTI-DOWTY REFERENCE STANDARD Material aluminum 7075-T6; Thickness 1/2"...- Number of holes 11;..- hole diameters: 14.0mm, 14.2mm, 14.4mm, 14.6mm, 15.6mm, 15.8mm, 16.1mm, 16.2mm, 16.3mm, 16.6mm, 16.9mm...EDM notch in each hole: thru ...
Location:
North America
Aircraft or Engine:
44
44
Tool:
AFNDT-3514AL
Description:
5 STEP WEDGE .075", .150", .225", .300", .375". TOLERANCE +/-.001". MATERIAL: 7050-T7 ALUMINUM. PAD SIZE: 1.0" x 1.0" . Includes Test Report traceable to NIST and Certificate of Conformance. Meets ASTM E797/797M
Location:
North America
Aircraft or Engine:
45
45
Tool:
AFNDT-3515AL
Description:
5 STEP WEDGE .050", .125", .200", .275", .350". TOLERANCE +/-.001". MATERIAL: 7050-T7 ALUMINUM. PAD SIZE: 1.0" x 1.0" . Includes Test Report traceable to NIST and Certificate of Conformance. Meets ASTM E797/797M
Location:
North America
Aircraft or Engine:
46
46
Tool:
AFNDT-3516/15-5PH
Description:
6 STEP CALIBRATION BLOCK, MATERIAL: 15-5PH STEEL. PAD SIZE: .75" x .75". STEP SIZES: .030", .100", .200", .300", .400", .500" ± .001". Includes certification Report Traceable to NIST.
Location:
North America
Aircraft or Engine:
47
47
Tool:
AFNDT-3517/2024
Description:
10 STEP WEDGE. STEP THICKNESS OF , .025", .050", .100", .200", .300", .400", .500", .600", .800" 1.000" +/-.03mm Pad Size: 12.5mm" x 25mm" . Material: 2024-T3 Aluminum. Includes Certification Report traceable to NIST.
Location:
North America
Aircraft or Engine:
48
48
Tool:
AFNDT-3517/7075
Description:
10 STEP WEDGE. STEP THICKNESS OF , .025", .050", .100", .200", .300", .400", .500", .600", .800" 1.000" +/-.03mm Pad Size: 12.5mm" x 25mm" . Material: 7075-T6 Aluminum. Includes Certification Report traceable to NIST.
Location:
North America
Aircraft or Engine:
49
49
Tool:
AFNDT-3517MAG
Description:
10 STEP WEDGE. STEP THICKNESS OF , .025", .050", .100", .200", .300", .400", .500", .600", .800" 1.000" +/-.03mm. Pad Size: 12.5mm" x 25mm" . Material: AZ91E Magnesium. Includes Certification Report traceable to NIST.
Location:
North America
Aircraft or Engine:
50
50
Tool:
AFNDT-3517SS
Description:
10 STEP WEDGE. STEP THICKNESS OF , .025", .050", .100", .200", .300", .400", .500", .600", .800" 1.000" +/-.03mm Pad Size: 12.5mm" x 25mm" . Material: 304 Stainless Steel. Includes Certification Report traceable to NIST.
Location:
North America
Aircraft or Engine:
51
51
Tool:
AFNDT-3517TI
Description:
10 STEP WEDGE. STEP THICKNESS OF , .025", .050", .100", .200", .300", .400", .500", .600", .800" 1.000" +/-.03mm Pad Size: 12.5mm" x 25mm" . Material: 6AL-4V Titanium. Includes Certification Report traceable to NIST.
Location:
North America
Aircraft or Engine:
52
52
Tool:
AFNDT-3518AL
Description:
12 Hole Standard - Hole Sizes; 3/16 inch (4.74mm) 7/32 inch (5.53mm) 1/4 inch (6.35mm) 9/32 inch (7.13mm) 5/16 inch (7.92mm) 11/32 inch (8.71mm) 3/8 inch (9.52mm) 7/16 inch (11.09mm) 1/2 inch (12.7mm) 9/16 inch (14.27mm) 5/8 inch (15.87mm) 3/4 inch (19...
Location:
North America
Aircraft or Engine:
53
53
Tool:
AFNDT-3519SS
Description:
6 HOLE REFERENCE STANDARD IN 304 STAINLESS STEEL; HOLE SIZES: (1/8, 5/32, 3/16, 7/32, 1/4, 9/32), WITH .030"x.030" CORNER EDM NOTCH IN EACH HOLE. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
54
54
Tool:
AFNDT-3520MAG
Description:
16 STEP WEDGE. STEP THICKNESS OF , .0625", .125", .187", .250", .312", .375", .437", .500", .562" .625", 687", .750", .812", .875", .937", 1.00" +/-.002". Pad Size: .620" x 1.5" . 9.20" Long x 1.5" Wide Finished Size. Material: AZ91E Magnesium. Includes
Location:
North America
Aircraft or Engine:
55
55
Tool:
AFNDT-3521AL
Description:
5 STEP METRIC WEDGE , 2mm, 4mm, 6mm, 8mm, 10mm, +/- .05mm. Material: 7075-T6 Aluminum. Pad Size: 19mm x 19mm square Supplied with Delrin Holding Block. Includes Test Report Traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
56
56
Tool:
AFNDT-3522AL
Description:
CUSTOM EDDY CURRENT SURFACE REFERENCE STANDARD, 3 EDM SLOTS .008",.020",.040" .006" ±.001". MATERIAL: 7075-T6 ALUMINUM. SIZE: .312" THICK x 1.375 WIDE x 3.156". Includes Test Report and Certifictate of Conformance.
Location:
North America
Aircraft or Engine:
57
57
Tool:
AFNDT-3522SS
Description:
CUSTOM EDDY CURRENT SURFACE REFERENCE STANDARD, 3 EDM SLOTS .008",.020",.040" .006" ±.001". MATERIAL: 304 STAINLESS STEEL. SIZE: .312" THICK x 1.375 WIDE x 3.156". Includes Test Report and Certifictate of Conformance.
Location:
North America
Aircraft or Engine:
58
58
Tool:
AFNDT-3522ST
Description:
CUSTOM EDDY CURRENT SURFACE REFERENCE STANDARD, 3 EDM SLOTS .008",.020",.040" .006" ±.001". MATERIAL: 4340 STEEL. SIZE: .312" THICK x 1.375 WIDE x 3.156". Includes Test Report and Certifictate of Conformance.
Location:
North America
Aircraft or Engine:
59
59
Tool:
AFNDT-3523AL
Description:
4 Step Calibration Block, 1.250", 1.500", 1.750", 2.000". Tolerance= ± .002" MATERIAL: 7075-T6 Aluminum. Pad Size: 1.0" x 1.0" Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
60
60
Tool:
AFNDT-3523CS
Description:
4 Step Calibration Block, 1.250", 1.500", 1.750", 2.000". Tolerance= ± .002" MATERIAL: 4340 Carbon Steel. Pad Size: 1.0" x 1.0" Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
61
61
Tool:
AFNDT-3523MAG
Description:
4 Step Calibration Block, 1.250", 1.500", 1.750", 2.000". Tolerance= ± .002" MATERIAL: Magnesium. Pad Size: 1.0" x 1.0" Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
62
62
Tool:
AFNDT-3523SS
Description:
4 Step Calibration Block, 1.250", 1.500", 1.750", 2.000". Tolerance= ± .002" MATERIAL: 304 Stainless Steel. Pad Size: 1.0" x 1.0" Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
63
63
Tool:
AFNDT-3523TI
Description:
4 Step Calibration Block, 1.250", 1.500", 1.750", 2.000". Tolerance= ± .002" MATERIAL: 6AL-4v Titanium. Pad Size: 1.0" x 1.0" Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
64
64
Tool:
AFNDT-3524AL
Description:
4 HOLE REFERENCE STANDARD. Material: 7075-T6 Aluminum 10" x 3.5" x .375" , HOLE SIZES: 1.25", 1.50", 1.75", 2.00". EDM NOTCH: .030" x .030" x .005 ± .001" CORNER NOTCH IN EACH HOLE. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
65
65
Tool:
AFNDT-3524CS
Description:
4 HOLE REFERENCE STANDARD. Material: 4130 or 4340 Carbon Steel 10" x 3.5" x .375" , HOLE SIZES: 1.25", 1.50", 1.75", 2.00". EDM NOTCH: .030" x .030" x .005 ± .001" CORNER NOTCH IN EACH HOLE. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
66
66
Tool:
AFNDT-3524SS
Description:
4 HOLE REFERENCE STANDARD. Material: 304 Stainless Steel 10" x 3.5" x .375" , HOLE SIZES: 1.25", 1.50", 1.75", 2.00". EDM NOTCH: .030" x .030" x .005 ± .001" CORNER NOTCH IN EACH HOLE. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
67
67
Tool:
AFNDT-3524TI
Description:
4 HOLE REFERENCE STANDARD. Material: 6AL-4v Titanium 10" x 3.5" x .375" , HOLE SIZES: 1.25", 1.50", 1.75", 2.00". EDM NOTCH: .030" x .030" x .005 ± .001" CORNER NOTCH IN EACH HOLE. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
68
68
Tool:
AFNDT-3525MAG-1
Description:
2 HOLE REFERENCE STANDARD. Material: Magnesium 5.0" x 3.5" x .375" , HOLE SIZES: 1.25", 1.50". EDM NOTCH: .030" x .030" x .005 ± .001" CORNER NOTCH IN EACH HOLE. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
69
69
Tool:
AFNDT-3525MAG-2
Description:
2 HOLE REFERENCE STANDARD. Material: Magnesium 5.0" x 3.5" x .375" , HOLE SIZES: 1.75", 2.00". EDM NOTCH: .030" x .030" x .005 ± .001" CORNER NOTCH IN EACH HOLE. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
70
70
Tool:
AFNDT-3526ST
Description:
12 HOLE REFERENCE STANDARD, 15 Total EDM Notches. Hole Sizes; 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 7/16, 1/2, 9/16, 5/8 and 3/4 inch diameters. Material: 4340 Steel. .030" x .030" x .005" ± .001" Corner Notch in each hole, .008" ,.020", .040" x .0...
Location:
North America
Aircraft or Engine:
71
71
Tool:
AFNDT-3527/2024T3
Description:
12 Hole Calibration Standard, 27 Total EDM Notches. Hole Sizes; 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 7/16, 1/2, 9/16, 5/8 and 3/4 inch diameters. ( .030 x .030 and .020 x .020 ± .002" Corner EDM Notches in each Hole. 3 surface EDM Notches .008”,.020”
Location:
North America
Aircraft or Engine:
72
72
Tool:
AFNDT-3528TI
Description:
12 HOLE REFERENCE STANDARD, 15 Total EDM Notches. Hole Sizes; 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 7/16, 1/2, 9/16, 5/8 and 3/4 inch diameters. Material: 6AL-4V Titanium. .050" x .050" x .005" ± .001" Corner Notch in each hole, .008" ,.020", .040"...
Location:
North America
Aircraft or Engine:
73
73
Tool:
AFNDT-3529AL
Description:
4 Step Calibration Block, .750", 1.000", 1.250", 1.500". Tolerance= ± .002" MATERIAL: 2024-T3 Aluminum. Pad Size: 1.0" x 1.0" Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
74
74
Tool:
AFNDT-3530TI
Description:
METRIC 5 STEP WEDGE, 1mm, 3mm, 7mm, 12mm, 15mm +/- .05mm. Material: 6Al-4v Titanium. Pad Size: 25mm x 25mm square. Includes Test Report Traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
75
75
Tool:
AFNDT-3531/2014-T6
Description:
13 HOLE REFERENCE STANDARD, 2014-T6 Aluminum. HOLE SIZES: 5/32", 3/16", 7/32" 1/4", 9/32", 5/16", 11/32", 3/8", 7/16", 1/2", 9/16" 5/8", 3/4", MId-Wall EDM Notch = .060"L x .030D x .004" ± .001". Manufactured in accordance to Aircraft Braking System...
Location:
North America
Aircraft or Engine:
76
76
Tool:
AFNDT-3532
Description:
6 STEP WEDGE, .045", .005", .015", .025", .035", .045" ± .001". Material: 6061-T6 Aluminum. Pad Size: 1.0" x 1.0" square with .500" Steps on the ends. Includes Test Report Traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
77
77
Tool:
AFNDT-3533
Description:
6 STEP WEDGE, .045", .010", .020", .030", .040", .045" ± .001". Material: 6061-T6 Aluminum. Pad Size: 1.0" x 1.0" square with .500" Steps on the ends. Includes Test Report Traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
78
78
Tool:
AFNDT-3534/2024T3
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .010"(0.254mm), .020"(0.5mm), .030"(.762mm) (.004"W +/- .002), 2024-T3 ALUMINUM. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
79
79
Tool:
AFNDT-3536AL
Description:
METRIC 5 STEP WEDGE. STEP SIZES: 12.5mm, 16mm, 20mm, 25mm, 30mm STEP TOLERANCE +/-.03mm(.00118"). MATERIAL: 7075-T6 ALUMINUM .PAD SIZE: 25mm x .25mm. Includes Test Report traceable to NIST, Mill Certificate for Material and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
80
80
Tool:
AFNDT-3537AL
Description:
METRIC 5 STEP WEDGE. STEP SIZES: 0.40mm, 0.65mm, 1.3mm, 2.0mm, 2.5mm STEP TOLERANCE +/-.03mm(.00118"). MATERIAL: 2024-T3 ALUMINUM .PAD SIZE: 25mm x .25mm. Supplied with Delrin Holding Block. Includes Test Report traceable to NIST, Mill Certificate f...
Location:
North America
Aircraft or Engine:
81
81
Tool:
AFNDT-3541AL
Description:
EDDY CURRENT SURFACE STANDARD MANUFACTURED TO BSS 7698,..3 EDM NOTCHES: ( .010", .020", .030" Deep x .005" Wide ± .001 ), MATERIAL: 7075-T6 Aluminum. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
82
82
Tool:
AFNDT-3541ST
Description:
EDDY CURRENT SURFACE STANDARD MANUFACTURED TO BSS 7698,.. 3 EDM NOTCHES: ( .010", .020", .030" Deep x .005" Wide ± .001 ), MATERIAL: 4340 Steel. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
83
83
Tool:
AFNDT-3541TI
Description:
EDDY CURRENT SURFACE STANDARD MANUFACTURED TO BSS 7698, ..3 EDM NOTCHES: ( .010", .020", .030" Deep x .005" Wide ± .001 ), MATERIAL: 6AL-4V Titanium. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
84
84
Tool:
AFNDT-3542AL
Description:
METRIC 5 STEP WEDGE 0.6mm(.024"),5.44mm( .214"),10.26mm( .404"),15.09mm( .594"), 20mm(.787"). TOLERANCE +/-.001". MATERIAL: 7075-T6 ALUMINUM .PAD SIZE: 75" x .75". Supplied with Delrin Holding Block. Includes Test Report traceable to NIST and Certif...
Location:
North America
Aircraft or Engine:
85
85
Tool:
AFNDT-3544/2219-T8
Description:
10 STEP REFERENCE BLOCK .038, .045, .055, .065, .080, .100, .125, .150", .175", .200", ± .001" Supplied with Delrin Holding Block... Pad Size: .800" x .800" ± 0.010" Material: 2219-T8. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
86
86
Tool:
AFNDT-3545AL
Description:
Custom 4 Step Flat Bottom Hole CRS. Step Thicknesses of 2mm, 3mm, 6mm, 15mm. 12 total Flat Bottom Holes 1.2mm(.047")Ø (Tolerance: ± 3% ). Pad Size: WIDTH 40mm ± 1mm x LENGTH 60mm ± 0.2mm. Material: 7075-T6 Aluminum anodized for corrosion protection....
Location:
North America
Aircraft or Engine:
87
87
Tool:
AFNDT-3545TI
Description:
Custom 4 Step Flat Bottom Hole CRS. Step Thicknesses of 2mm, 3mm, 6mm, 15mm. 12 total Flat Bottom Holes 1.2mm(.047")Ø (Tolerance: ± 3% ). Pad Size: WIDTH 40mm ± 1mm x LENGTH 60mm ± 0.2mm. Material: 6AL-4v Titanium. Includes Certification Report and...
Location:
North America
Aircraft or Engine:
88
88
Tool:
AFNDT-3546AL
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHE SIZES: .005"(.127mm) , .020"(0.5mm), .050"(1.27mm) (.005"W +/- .001). MATERIAL: 7075-T6 ALUMINUM. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
89
89
Tool:
AFNDT-3547CS
Description:
5 STEP WEDGE, .020", .030", .040", .050", .060". TOLERANCE +/-.001". MATERIAL: 4340 Steel . PAD SIZE: .75" x .75". Supplied with Delrin Holding Block. Includes Test Report traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
90
90
Tool:
AFNDT-3548/7075
Description:
5 STEP WEDGE, 1mm, 3mm, 5mm, 7mm, 10mm, +/- .05mm. Material: 7075-T6 Aluminum. Pad Size: 20mm x 20mm square supplied with Delrin Holding Block. Includes Test Report Traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
91
91
Tool:
AFNDT-3549
Description:
Custom 4 hole standard. Material 17-4PH or 17-7PH Stainless. Size: 6.0" x 4.65" x .375" Thick. Hole Diameters: 1.125",1.190",1.250", and..1.3750" EDM Corner Notch .030" x .030" x .005" ± .001" in each hole. Includes Test Report and Certificate of C...
Location:
North America
Aircraft or Engine:
92
92
Tool:
AFNDT-3550
Description:
Custom Bolt Hole Standard. Material: .250" Thick 718 Inconel. Hole size .320"Ø with a .030" x .030" EDM corner notch. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
93
93
Tool:
AFNDT-3551CS
Description:
7 HOLE REFERENCE STANDARD in 4340 Steel; Hole Sizes: .875", 1.000", 1.100", 1.200", 1.300", 1.400", 1.500"), With a .030" x .030" x .004" ± .001" Corner EDM Notch in top and bottom of each hole in the top plate. 14 Notches Total. Includes Engraving, ...
Location:
North America
Aircraft or Engine:
94
94
Tool:
AFNDT-3552TI
Description:
5 Step calibration block (0.100", 0.250", 0.500", 0.750" and 1.000"; . Step pad size: .75” x .75”. Material: 6AL-4V Titanium. Includes Test Report and Certificate of Conformance.....Reference: B777 NTM Part4 51-00-10
Location:
North America
Aircraft or Engine:
95
95
Tool:
AFNDT-3554
Description:
CUSTOM 4 HOLE STANDARD IN 2024-T351 ALUMINUM PER BOEING PART NUMBER NDT1084. EDM CORNER NOTCH SIZES: .020" x .020" x .005" +/- .002 " and .030" x .030" x .005" +/- .002" HOLE SIZES: .875"(7/8"), .937" (15/16"), 1.0", 1.125". Includes Test Report and ...
Location:
North America
Aircraft or Engine:
96
96
Tool:
AFNDT-3555
Description:
CUSTOM 5 HOLE STANDARD IN 2024-T351 ALUMINUM PER BOEING PART NUMBER NDT1084. EDM CORNER NOTCH SIZES: .020" x .020" x .005" +/- .002 " and .030" x .030" x .005" +/- .002" HOLE SIZES: .531" (17/32"), .625" (5/8"), .750" (3/4"), .875"(7/8"), .906"(29/32...
Location:
North America
Aircraft or Engine:
97
97
Tool:
AFNDT-3556AL
Description:
8 STEP WEDGE, STEP SIZES OF .060", .070",.085", .100", .120", .145", .175", and .210" +/- .001". PAD SIZE: .80"x.80", MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
98
98
Tool:
AFNDT-3557AL
Description:
8 STEP WEDGE, STEP SIZES OF .018", .021",.025", .030", .035", .040", .045", and .050" +/- .001". PAD SIZE: .80"x.80", MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
99
99
Tool:
AFNDT-3558/7075T6
Description:
10 STEP WEDGE SUPPLIED WITH DELRIN HOLDING BLOCK. STEP SIZES: .020", .040", .60", .80", .100", .120", .140", .160", .180", .200" +/-.001". Material: 7075-T6 ALUMINUM. PAD SIZE: .75" x .75". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
100
100
Tool:
AFNDT-3559AL-3
Description:
15 HOLE REFERENCE STANDARD, Material: 7075-T6 Aluminum. Hole Sizes: 1/8, 3/16, 1/4, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8, 11/16, 3/4, 13/16, 7/8, 15/16, 1.0. A Total 15 Mid-bore notch @ 0.030" deep x 0.004" wide x 0.060" long in each hole. 3 Surface EDM No...
Location:
North America
Aircraft or Engine:
101
101
Tool:
AFNDT-3560A
Description:
Corrosion Reference Standard used for verifying function of low frequency corrosion probes. It is 0.100” thick with simulated 5%, 10% and 20% material loss. Overall size: 7.50” x 3.50” (190 x 89 mm). Material: 2024-T3 Aluminum. Includes Certification.
Location:
North America
Aircraft or Engine:
102
102
Tool:
AFNDT-3560B
Description:
Corrosion Reference Standard used for verifying function of low frequency corrosion probes. It is 0.100” thick with simulated 5%, 10% and 20% material loss. Overall size: 7.50” x 3.50” (190 x 89 mm). Material: 7075-T6 Aluminum. Includes Certification.
Location:
North America
Aircraft or Engine:
103
103
Tool:
AFNDT-3561AL
Description:
CUSTOM 3 STEP CALIBRATION BLOCK, 2024-T3 ALUMINUM... STEP PAD SIZE: 25.0mm x 25.0mm. STEP THICKNESSES: 0.3mm, 0.5mm and 0.8mm ± 0.03mm. Supplied with Protective Acetal Holding Block. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
104
104
Tool:
AFNDT-3562/321SS
Description:
CUSTOM 3 STEP CALIBRATION BLOCK 321 Stainless, STEP SIZES .75" x .75" FACE. STEP THICKNESSES OF 0.025", 0.040" and 0.060" +/-.001". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
105
105
Tool:
AFNDT-4010/2024T3
Description:
6 STEP WEDGE: 0.030 in. (0.762 mm), 0.050 in. (1.27 mm), 0.100 in.(2.54 mm), 0.150 in (3.81 mm), 0.300 in. (7.62 mm), and 0.500 in. (12.70 mm) +/-.001", Material: 2024-T3 Aluminum. Pad Size: 0.75" x 0.75" , BLOCK SIZE: 4.50" L x .750"W SUPPLIED WITH D
Location:
North America
Aircraft or Engine:
106
106
Tool:
AFNDT-4010/7075T6
Description:
6 STEP WEDGE: 0.030 in. (0.762 mm), 0.050 in. (1.27 mm), 0.100 in.(2.54 mm), 0.150 in (3.81 mm), 0.300 in. (7.62 mm), and 0.500 in. (12.70 mm) +/-.001", Material: 7075-T6 Aluminum. Pad Size: 0.75" x 0.75" , BLOCK SIZE: 4.50" L x .750"W SUPPLIED WITH D
Location:
North America
Aircraft or Engine:
107
107
Tool:
AFNDT-40244
Description:
CUSTOM ETHER NDE TEST BLOCK, PER SPEC
Location:
North America
Aircraft or Engine:
108
108
Tool:
AFNDT-4072G
Description:
PROBE GUIDE FOR BOEING 747 PT 6 53-30-05. Material Delrin. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
109
109
Tool:
AFNDT-5000
Description:
COMPOSITE STEP WEDGE SOLID CFRP TAPE, BMS 8-276 Cytec. PAD SIZE: 3.0" WIDE by 2.0" LONG. STEP SIZES .100” to 1.0” in INCREMENTS of .100".
Location:
North America
Aircraft or Engine:
110
110
Tool:
AFNDT-7003TI
Description:
12 HOLE REFERENCE STANDARD. MATERIAL: 6AL-4V Titanium.Hole Sizes: (3/16", 7/32" ,1/4", 9/32", 5/16",11/32", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4"), .020" X .005" WIDE +/-.001" THROUGH EDM NOTCH IN EACH HOLE. Includes Test Report, Conductivity and Certi...
Location:
North America
Aircraft or Engine:
111
111
Tool:
AFNDT-7075DAA19
Description:
ASTM DISTANCE AMPLITUDE SET OF 19 7075-T6 ALUMINUM (CASE INCL) 3/34", 5/64" and 8/64" FLAT BOTTOM HOLES
Location:
North America
Aircraft or Engine:
112
112
Tool:
AFNDT-AL-6061
Description:
CUSTOM REFERENCES STANDARD PER AMS4083
Location:
North America
Aircraft or Engine:
113
113
Tool:
AFNDT-CFRP20-4
Description:
Custom 20 ply 12" x 12" CFRP Test Panel with 4 random defects(grafoil delaminations) between the ply layup in random locations. Autoclave cured per Boeing Specification BAC 5317. Includes C-Scan image to identify defects and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
114
114
Tool:
AFNDT-CHOKE BLOCK-70/30
Description:
CALIBRATION BLOCK 70/30 COPPER-NICKEL
Location:
North America
Aircraft or Engine:
115
115
Tool:
AFNDT-CHOKE BLOCK-C
Description:
CALIBRATION BLOCK 1018 CARBON STEEL
Location:
North America
Aircraft or Engine:
116
116
Tool:
AFNDT-CHOKE BLOCK-DUP
Description:
CALIBRATION BLOCK 2205 SS (DUPLEX)
Location:
North America
Aircraft or Engine:
117
117
Tool:
AFNDT-CHOKE BLOCK-S
Description:
CALIBRATION BLOCK 303 STAINLESS STEEL
Location:
North America
Aircraft or Engine:
118
118
Tool:
AFNDT-CRJ200/CRS
Description:
SURFACE REFERENCE STANDARD, ALUMINUM, .005W x .008", .020", .040" EDM NOTCH DEPTHS . MATERIAL 2024-T3 AL...CRJ200 PART1 51-20-06 PG.9
Location:
North America
Aircraft or Engine:
119
119
Tool:
AFNDT-DELRIN BLOCKS
Description:
DELRIN BLOCKS W/ TOE CLAMPS .500-.030 STEP BLOCKS
Location:
North America
Aircraft or Engine:
120
120
Tool:
AFNDT-ECRC82040
Description:
Eddy Current Crack Standard Magnesium AZ-31
Location:
North America
Aircraft or Engine:
121
121
Tool:
AFNDT-FBH30AL
Description:
Used for determining resolution and sensitivity capabilities and for producing area amplitude and distance amplitude plots for normal beam transducers. Contains ten flat-bottom holes at 3/64” diameter, ten at 5/64”, and ten at 8/64”. Metal travel dista...
Location:
North America
Aircraft or Engine:
122
122
Tool:
AFNDT-FBH30CS
Description:
Used for determining resolution and sensitivity capabilities and for producing area amplitude and distance amplitude plots for normal beam transducers. Contains ten flat-bottom holes at 3/64” diameter, ten at 5/64”, and ten at 8/64”. Metal travel dista...
Location:
North America
Aircraft or Engine:
123
123
Tool:
AFNDT-IIW-01-CASE
Description:
Form Fitted Wood Case for IIW Type 1 Calibration Block
Location:
North America
Aircraft or Engine:
124
124
Tool:
AFNDT-IIW-01AL
Description:
ALUM. IIW TYPE 1 TEST BLOCK.. Aluminum Ultrasonic IIW Type 1 Test Block 7075-T6 Aluminum. 1 "x 4"x 12". Contains 2" diameter hole and 4" radius. Also, 1/8" x 1" radius alternate reflector and 1/16" deep on echo side. Meets ASTM-E-164, MIL-STD-2154 a...
Location:
North America
Aircraft or Engine:
125
125
Tool:
AFNDT-IIW-01CS
Description:
IIW TYPE 1 TEST BLOCK.. Aluminum Ultrasonic IIW Type 1 Test Block 1018 Carbon Steel. 1 "x 4"x 12". Contains 2" diameter hole and 4" radius. Also, 1/8" x 1" radius alternate reflector and 1/16" deep on echo side. Meets ASTM-E-164, MIL-STD-2154 and AW...
Location:
North America
Aircraft or Engine:
126
126
Tool:
AFNDT-MX3502
Description:
Meets AS-5282 and ASTM E1444 requirements. 12 Pre-drilled holes simulate subsurface discontinuities Verifies magnetic particle system performance when actual test parts with discontinuities are not available Forms surface indications at various magnet...
Location:
North America
Aircraft or Engine:
127
127
Tool:
AFNDT-PLUG
Description:
PLUG - 54-10-33
Location:
North America
Aircraft or Engine:
128
128
Tool:
AFNDT-PR-T-2521/22
Description:
CUSTOM EDDY CURRENT SURFACE CALIBRATION BLOCK. PER CUSTOMER SUPPLIED DRAWING. MATERIAL: 7075-T6 Aluminum. EDM Notch size 1mm (.040') , .76mm(.030"), .2mm(.008") deep x .1mm(.004") wide +/- .002". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
129
129
Tool:
AFNDT-ROMPAS-7075-T6
Description:
ROMPAS BLOCK, 7075-T6 ALUMINUM ½" (12.5mm) or 1" (25.4 mm) thick, 1" radius opposite 2" radius, with 5/64" diameter side drilled hole (3/4" deep flat bottom hole in 1" thick version). SPECIFICATION: ASTM E-164. (Includes wooden case)
Location:
North America
Aircraft or Engine:
130
130
Tool:
AFNDT-SA227
Description:
FAIRCHILD REFERENCE STARDARD FOR THE SA227 DOOR use fastener MS2042AD4-10
Location:
North America
Aircraft or Engine:
131
131
Tool:
AFNDT-SRS-082A-1
Description:
EDDY CURRENT SURFACE BLOCK 7075-T6 ALUMINUM. 2 EDM SLOTS ( 0.2mm deep +/-0.05mm & 0.12mm wide +/- 0.01mm). EDM NOTCH#1 ( 0.5mm deep +0.06/-0.04 & 0.12 wide +0.01/-0.02 ), and EDM NOTCH #2 ( 1.0mm deep +0.06mm/-0.04mm & 0.12mm wide +0.01mm/-0.02mm). Inc...
Location:
North America
Aircraft or Engine:
132
132
Tool:
AFNDT-SRS-082S-1
Description:
EDDY CURRENT SURFACE BLOCK 4130 STEEL. 2 EDM SLOTS ( 0.2mm deep +/-0.05mm & 0.12mm wide +/- 0.01mm). EDM NOTCH#1 ( 0.5mm deep +0.06/-0.04 & 0.12 wide +0.01/-0.02 ), and EDM NOTCH #2 ( 1.0mm deep +0.06mm/-0.04mm & 0.12mm wide +0.01mm/-0.02mm). Includes ...
Location:
North America
Aircraft or Engine:
133
133
Tool:
AFNDT-SRS-4A
Description:
SURFACE STANDARD ALUMINUM(2024-T351) 1 EDM SLOT (0.040 DEEP)
Location:
North America
Aircraft or Engine:
134
134
Tool:
AFNDT-SRS-4S
Description:
SURFACE STANDARD STEEL 4340 1 EDM SLOT (0.40 DEEP)
Location:
North America
Aircraft or Engine:
135
135
Tool:
AFNDT-SRS-4T
Description:
SURFACE STANDARD TITANIUM 1 EDM SLOT (0.40 DEEP)
Location:
North America
Aircraft or Engine:
136
136
Tool:
AFNDT-SS304
Description:
CUSTOM REFERENCES STANDARD PER AMSS5564
Location:
North America
Aircraft or Engine:
137
137
Tool:
AFNDT-VL769-1A
Description:
TITANIUM VERTICAL(INBOARD LUG) ULTRASONIC REFERENCE STANDARD(.800"THICK, 3.56" OUTSIDE RADIUS WITH A 1.312" BORE DIAMETER. COPPER BERYLLIUM NON FLANGED BUSHING WITH A 1.128 BORE DIA. ( 2 EACH .100" x .100" CORNER NOTCHES)
Location:
North America
Aircraft or Engine:
138
138
Tool:
AFNDT-VL769-2A
Description:
TITANIUM VERTICAL(INBOARD LUG) ULTRASONIC REFERENCE STANDARD(1.500" THICK, 3.56" OUTSIDE RADIUS WITH A 1.312" BORE DIAMETER. COPPER BERYLLIUM NON FLANGED BUSHING WITH A 1.128 BORE DIA. ( 2 EACH .100" x .100" CORNER NOTCHES)
Location:
North America
Aircraft or Engine:
139
139
Tool:
AFNDT1016-12S-2024
Description:
CUSTOM 12 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: .188", .219", .250",.282", 313", .344", .375" .438" .500",.563", .
Location:
North America
Aircraft or Engine:
140
140
Tool:
AFNDT1016-12S-7075
Description:
CUSTOM 12 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: .188", .219", .250",.282", 313", .344", .375" .438" .500",.563", .6
Location:
North America
Aircraft or Engine:
141
141
Tool:
AFP-080/TIP
Description:
.080" THREADED DELAY TIP FOR THE AFP SERIES PENCIL TRANSDUCERS
Location:
North America
Aircraft or Engine:
142
142
Tool:
AFP-1012
Description:
10 MHZ .125" dia focused Straight shaft pencil transducer with a .080" Replaceable tip. Standard microdot connector
Location:
North America
Aircraft or Engine:
143
143
Tool:
AFP-1012/90
Description:
10 MHZ 90° .125"Ø diameter focused pencil transducer with a .060" Replaceable tip. Standard microdot connector. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
144
144
Tool:
AFP-1512
Description:
15 MHZ .125" dia focused Straight shaft pencil transducer with a .080" Replaceable tip. Standard microdot connector
Location:
North America
Aircraft or Engine:
145
145
Tool:
AFP-1512/45
Description:
15 MHZ .125"Ø dia focused 45° shaft pencil transducer with a .060" Replaceable tip, supplied with a microdot connector. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
146
146
Tool:
AFP-1512/90
Description:
15 MHZ 90° SHAFT .125" dia focused pencil transducer with a .060" Replaceable tip. Standard microdot connector
Location:
North America
Aircraft or Engine:
147
147
Tool:
AFP-7512
Description:
7.5MHZ .125" dia. High Resolution focused Straight shaft pencil transducer with a .080" Replaceable tip. Standard microdot connector. ( K-PEN style )
Location:
North America
Aircraft or Engine:
148
148
Tool:
AFP-7512/90
Description:
7.5MHZ 90° angle head. High Resolution .125" dia focused pencil transducer with a .080" Replaceable tip. Standard microdot connector. K-PEN Style
Location:
North America
Aircraft or Engine:
149
149
Tool:
AFPT-080
Description:
.080"Ø DELAY TIP FOR AFP SERIES PENCIL TRANSDUCERS. 1/4-36 THREAD. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
150
150
Tool:
AFPT60
Description:
.060" DELAY TIP FOR AFP SERIES SONOPEN TYPE PENCIL TRANSDUCERS. 1/4-36 THREAD. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
151
151
Tool:
AFRR.156SE
Description:
HOLE PROBE 100KHZ - 2 MHZ, 1.1" WL
Location:
North America
Aircraft or Engine:
152
152
Tool:
AFS-0204-70AT
Description:
70° ANGLE BEAM TRANSDUCER in ALUMINUM, 2.25MHz .25" x .25" ELEMENT, CASE SIZE( .550"L x .310"W x .675" H) SUPPLIED WITH A TOP MOUNT MICRODOT CONNECTOR. Includes Test Report and Certificate of conformance.
Location:
North America
Aircraft or Engine:
153
153
Tool:
AFS-0500L
Description:
5MHZ 28° SHEAR WAVE IN TI, 1.97 LEFT SIDE
Location:
North America
Aircraft or Engine:
154
154
Tool:
AFS-0500R
Description:
5MHZ 28° SHEAR WAVE IN TI, 1.97 RIGHT SIDE
Location:
North America
Aircraft or Engine:
155
155
Tool:
AFS-0501L
Description:
35° SHEAR WAVE IN TI, 1.97 RIGHT SIDE SCANNING
Location:
North America
Aircraft or Engine:
156
156
Tool:
AFS-0501R
Description:
35° SHEAR WAVE IN TI, 1.97 RIGHT SIDE SCANNING
Location:
North America
Aircraft or Engine:
157
157
Tool:
AFS-0503-45S
Description:
STAVELEY 45 DEGREES IN ALUMINUM SHEAR WAVE TRANSDUCER 5MHz 187" x .187" ELEMENT SIDE MOUNT MICRODOT CONNECTOR
Location:
North America
Aircraft or Engine:
158
158
Tool:
AFS-0503-45T
Description:
Mini Angle Beam Transducer, 5.0MHz, 0.187" x 0.187" Element, 45° Shear in Aluminum, Top Mount Microdot Connector. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
159
159
Tool:
AFS-0503-70S
Description:
Mini Angle Beam Transducer, 5.0MHz, 0.187" x 0.187" Element, 70° Shear in Aluminum, Side Mount Microdot Connector. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
160
160
Tool:
AFS-0503-70T
Description:
Mini Angle Beam Transducer, 5.0MHz, 0.187" x 0.187" Element, 70° Shear in Aluminum, Top Mount Microdot Connector. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
161
161
Tool:
AFS-0503-90SS
Description:
Mini Angle Beam Transducer, 5.0MHz, 0.187" x 0.187" Element, 90° Shear in Steel, Side Mount Microdot Connector. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
162
162
Tool:
AFS-0503L
Description:
5MHZ 28° REFRACTED L WAVE 1.125" R. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
163
163
Tool:
AFS-0504-40AT
Description:
60° ANGLE BEAM TRANSDUCER in ALUMINUM, 5MHz .187" x .25" ELEMENT, CASE SIZE( .47"L x .31"W x .55" H) TOP MOUNT MICRODOT CONNECTOR. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
164
164
Tool:
AFS-0504-45AS
Description:
OLYMPUS 45° DEGREES IN ALUMINUM SHEAR WAVE TRANSDUCER 5MHz .25" x .25" ELEMENT SIDE MOUNT MICRODOT CONNECTOR. CASE SIZE: .550" L x .310" W x .675"H. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
165
165
Tool:
AFS-0504-45AT
Description:
OLYMPUS 45° DEGREES IN ALUMINUM SHEAR WAVE TRANSDUCER 5MHz .25" x .25" ELEMENT TOP MOUNT MICRODOT CONNECTOR. CASE SIZE: .550" L x .310" W x .675"H. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
166
166
Tool:
AFS-0504-45SS
Description:
OLYMPUS 45° DEGREES IN STEEL SHEAR WAVE TRANSDUCER 5MHz .25" x .25" ELEMENT SIDE MOUNT MICRODOT CONNECTOR. CASE SIZE: .550" L x .310" W x .675"H. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
167
167
Tool:
AFS-0504-45ST
Description:
OLYMPUS 45° DEGREES IN STEEL SHEAR WAVE TRANSDUCER 5MHz .25" x .25" ELEMENT TOP MOUNT MICRODOT CONNECTOR. CASE SIZE: .550" L x .310" W x .675"H. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
168
168
Tool:
AFS-0504-60AS
Description:
60° ANGLE BEAM TRANSDUCER in ALUMINUM, 5MHz .25" x .25" ELEMENT, CASE SIZE( .550"L x .310"W x .675" H) SIDE MOUNT MICRODOT CONNECTOR. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
169
169
Tool:
AFS-0504-70AS
Description:
70° ANGLE BEAM TRANSDUCER in ALUMINUM, 5MHz .25" x .25" ELEMENT, CASE SIZE( .550"L x .310"W x .675" H) SIDE MOUNT MICRODOT CONNECTOR. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
170
170
Tool:
AFS-0504-70ST
Description:
70° ANGLE BEAM TRANSDUCER in STEEL, 5MHz .25" x .25" ELEMENT, CASE SIZE( .550"L x .310"W x .675" H) SUPPLIED WITH A TOP MOUNT MICRODOT CONNECTOR. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
171
171
Tool:
AFS-0504-70ST-SM
Description:
70° ANGLE BEAM TRANSDUCER in STEEL, 5MHz ..187" x .25" ELEMENT, CASE SIZE( .550"L x .310"W x .675" H) TOP MOUNT MICRODOT CONNECTOR. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
172
172
Tool:
AFS-0504S
Description:
5MHZ 28° REFRACTED SHEAR WAVE 1.125" R. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
173
173
Tool:
AFS-0506
Description:
5MHZ 51° SHEAR WAVE IN ALUMINUM. CASE SIZE .50" W x .80"L x .37"H, REFERENCE STANDARD NDT624
Location:
North America
Aircraft or Engine:
174
174
Tool:
AFS-0507
Description:
5MHZ 32° SHEARWAVE IN ALUMINUM. CASE SIZE .50"X.80"L. HEIGHT TAPERS FROM .20"H FRONT TO .32" H BACK. REFERENCE STANDARD IS NDT624
Location:
North America
Aircraft or Engine:
175
175
Tool:
AFS-0508
Description:
5MHZ BACKSHOOTER IN TI .25" ELEMENT, CASE SIZE .300HX.300WX.500L
Location:
North America
Aircraft or Engine:
176
176
Tool:
AFS-0515L
Description:
50° TITANIUM HARDWIRED CABLE. MODIFIED VERSION OF AFS-0501L
Location:
North America
Aircraft or Engine:
177
177
Tool:
AFS-0515R
Description:
50° TITANIUM HARDWIRED CABLE. MODIFIED VERSION OF AFS-0501R
Location:
North America
Aircraft or Engine:
178
178
Tool:
AFS-0516L
Description:
5MHZ 45° SHEARWAVE. SCANS TOWARDS THE LEFT. LOW PROFILE TRANSDUCER
Location:
North America
Aircraft or Engine:
179
179
Tool:
AFS-0516R
Description:
5MHZ 45° SHEARWAVE. SCANS TOWARDS THE RIGHT. LOW PROFILE TRANSDUCER
Location:
North America
Aircraft or Engine:
180
180
Tool:
AFS-0517L
Description:
5MHZ 45° SHEARWAVE WITH 34° COMPOUND ANGLE. SCANS TOWARDS THE LEFT. LOW PROFILE TRANSDUCER
Location:
North America
Aircraft or Engine:
181
181
Tool:
AFS-0517R
Description:
5MHZ 45° SHEARWAVE WITH 34° COMPOUND ANGLE. SCANS TOWARDS THE RIGHT. LOW PROFILE TRANSDUCER
Location:
North America
Aircraft or Engine:
182
182
Tool:
AFS-0519
Description:
CUSTOM BOEING ANGLE BEAM TRANSDUCER, 50°, 5MHz, .187" x.187" ELEMENT WITH TOP MOUNTED MICRODOT CONNECTOR. .550" x .26" x .450" USED WITH NDT596 . Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
183
183
Tool:
AFS-0520
Description:
10 MHz .187x.187 element L-Wave transducer 19 degree incident angle, 1.569R. Case size: .50Lx.26Wx.425H top mount connector
Location:
North America
Aircraft or Engine:
184
184
Tool:
AFS-0521
Description:
CUSTOM ANGLE BEAM TRANSDUCER 5MHZ 45° in Al .25"X.25"ELEMENT. 690"L x .590"H x .300"W WITH END MOUNT MICRODOT CONNECTOR. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
185
185
Tool:
AFS-0522
Description:
5MHZ 45° CUSTOM TRANSDUCER, AL, 2.9"LX.900"WX1.75"H
Location:
North America
Aircraft or Engine:
186
186
Tool:
AFS-0524
Description:
5 MHz shear wave transducer .25" x .25" square element. 1.025 radius top mount connector. used with NDT3238 ref. standard
Location:
North America
Aircraft or Engine:
187
187
Tool:
AFS-0525
Description:
5 MHz COMPOUND SHEARWAVE TRANSDUCER USED FOR LEFT SIDE EDM BORE NOTCH ON NDT3242
Location:
North America
Aircraft or Engine:
188
188
Tool:
AFS-0526
Description:
5 MHz COMPOUND ANGLE SHEARWAVE TRANSDUCER WITH A 2.275 INCH RADIUS. USED TO SCAN NEAR SIDE EDM NOTCH ON NDT3243
Location:
North America
Aircraft or Engine:
189
189
Tool:
AFS-0527
Description:
5 MHz SHEARWAVE TRANSDUCER USED TO SCAN MID BORE EDM NOTCH ON NDT3242 and NDT3243, 35° INCIDENT ANGLE
Location:
North America
Aircraft or Engine:
190
190
Tool:
AFS-0528
Description:
42.5° SHEAWAVE TRANSDUCER, 5MHZ OUTER LUG INSPECTION, LOW PROFILE SIDE MOUNT CONNECTOR
Location:
North America
Aircraft or Engine:
191
191
Tool:
AFS-0529
Description:
33.5° 5MHZ SHEARWAVE TRANSDUCER, NOSE AERA OF LUG, LOW PROFILE SIDE MOUTN TRANSDUCER
Location:
North America
Aircraft or Engine:
192
192
Tool:
AFS-0530-4
Description:
5MHz 45 deg in steel angle beam transducer. ( .500"L x .300"W x .425"H)
Location:
North America
Aircraft or Engine:
193
193
Tool:
AFS-0530-6
Description:
5MHz 60 deg in steel angle beam transducer. ( .500"L x .300"W x .425"H)
Location:
North America
Aircraft or Engine:
194
194
Tool:
AFS-0531
Description:
CUSTOM ANGLE BEAM TRANSDUCER. 5MHz 45 DEG. IN ALUMINUM TOP MOUNT CONNECTOR. CASE SIZE(.230"L x .350"W x .500"H)
Location:
North America
Aircraft or Engine:
195
195
Tool:
AFS-0532
Description:
CUSTOM MULTI SHOE TRANSDUCER 45 DEG. IN ALUMINUM 5MHz. (15, 0, 15, DEGREE OFF SETS)
Location:
North America
Aircraft or Engine:
196
196
Tool:
AFS-0536
Description:
5MHZ SHEARWAVE TRANSDUCER, 45°, STEEL, .187" x .250" ELEMENT. CASE SIZE .380"L,x .300"WX.500H,
Location:
North America
Aircraft or Engine:
197
197
Tool:
AFS-0537
Description:
5MHZ SHEARWAVE TRANSDUCER, 60°, STEEL, .187" x .500"ELEMENT. CASE SIZE, .380"Lx.300"WX.500H
Location:
North America
Aircraft or Engine:
198
198
Tool:
AFS-0538L
Description:
CUSTOM SHEARWAVE TRANSDUCER, 5MHZ, LEFT SIDE, FOR NDT6052
Location:
North America
Aircraft or Engine:
199
199
Tool:
AFS-0538R
Description:
CUSTOM SHEARWAVE TRANSDUCER, 5MHZ, RIGHT SIDE, FOR NDT6052
Location:
North America
Aircraft or Engine:
200
200
Tool:
AFS-0539
Description:
Custom 5MHz 45 degree shearweave ring transducer which features both right and left scanning directions. Ref. Standard NDT796
Location:
North America
Aircraft or Engine:
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