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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:
AFM-570TT
Description:
ANGLE BEAM TRANSDUCER, 70° in TITANIUM, 5MHz .25" x .25" ELEMENT, CASE SIZE: .75" x .37" x .50" SUPPLIED WITH A TOP MOUNTED MICRODOT CONNECTOR. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
2
2
Tool:
AFM-575AS
Description:
ANGLE BEAM TRANSDUCER, 5MHz 75° IN ALUMINUM .25" x 25" ELEMENT, SIDE MOUNT MICRODOT CONNECTOR. CASE SIZE: (.75"L x .375"W x .50"H). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
3
3
Tool:
AFM-575AT
Description:
ANGLE BEAM TRANSDUCER, 5MHz 75° IN ALUMINUM .25" x 25" ELEMENT, TOP MOUNT MICRODOT CONNECTOR. CASE SIZE: (.75"L x .375"W x .50"H). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
4
4
Tool:
AFM-580AT
Description:
80° ALUMINUM 5 MHZ 1/4" X 1/4" TOP MOUNT TRANSDUCER
Location:
North America
Aircraft or Engine:
5
5
Tool:
AFM-590AS
Description:
90° IN ALUMINUM 5 MHz .25" X .25" SIDE MOUNT MINITURE ANGLE BEAM TRANSDUCER. CASE SIZE: .75"L x .37"W x .50"H WITH MICRODOT CONNECTOR. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
6
6
Tool:
AFM-590AT
Description:
90° IN ALUMINUM 5 MHz .25" X .25" TOP MOUNT MINITURE ANGLE BEAM TRANSDUCER. CASE SIZE: .75"L x .37"W x .50"H WITH MICRODOT CONNECTOR. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
7
7
Tool:
AFM-590SS
Description:
90° IN STEEL 5 MHz .25" X .25" SIDE MOUNT MINITURE ANGLE BEAM TRANSDUCER. CASE SIZE: .75"L x .37"W x .50"H WITH MICRODOT CONNECTOR. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
8
8
Tool:
AFM-590ST
Description:
90° IN STEEL 5 MHz .25" X .25" TOP MOUNT MINITURE ANGLE BEAM TRANSDUCER. CASE SIZE: .75"L x .37"W x .50"H WITH MICRODOT CONNECTOR. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
9
9
Tool:
AFM-650AT
Description:
50° ALUMINUM 6 MHZ 1/4" X 1/4" TOP MOUNT TRANSDUCER
Location:
North America
Aircraft or Engine:
10
10
Tool:
AFM-670AT
Description:
70° ANGLE BEAM TRANSDUCER in ALUMINUM, 6MHz .25" x .25" ELEMENT, CASE SIZE: .75" x .37" x .50" WITH TOP MOUNT MICRODOT CONNECTOR. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
11
11
Tool:
AFM-670ST
Description:
70° STAINLESS 6 MHZ 1/4" X 1/4" TOP MOUNT TRANSDUCER
Location:
North America
Aircraft or Engine:
12
12
Tool:
AFM-ADH-1
Description:
CUSTOM ULTRASONIC TRANSDUCER HOLDER #1 FOR DUAL MICRODOT AFM SERIES TRANSDUCERS FOR 747 PART 4 57-10-09 Pg.4 (AFM-570AD-1, AFM-545AD-1)
Location:
North America
Aircraft or Engine:
13
13
Tool:
AFM-ADH-2
Description:
CUSTOM ULTRASONIC TRANSDUCER HOLDER #2 FOR DUAL MICRODOT AFM SERIES TRANSDUCERS FOR 747 PART 4 57-10-09 Pg.4 (AFM-570AD-1, AFM-545AD-1)
Location:
North America
Aircraft or Engine:
14
14
Tool:
AFNDT-001/.08
Description:
2024-T351 ALUMINUM THICKNESS BLOCK 3.0" x 3.0" x .080". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
15
15
Tool:
AFNDT-001/.25
Description:
2024-T351 ALUMINUM THICKNESS BLOCK 3.0" x 3.0" x .250". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
16
16
Tool:
AFNDT-0212-1
Description:
EDDY CURRENT SURFACE REFERENCE BLOCK. 2 EDM NOTCHES ( .012"D, .020"D, x .005" W +/- .001"), INCONEL 718. SIZE: 1.0"W x 3.0"L x .25". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
17
17
Tool:
AFNDT-032/10MM
Description:
CUSTOM EDDY CURRENT CALIBRATION BLOCK 4130 or 4340 STEEL. 50mm x 50mm x 15mm with 10mm diameter hole. Corner EDM notch( 0.76mm long +/- 0.07 )x ( 0.76mm deep +/- 0.07 ) x ( 0.18mm MAX width ). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
18
18
Tool:
AFNDT-0512A
Description:
Eddy Current Hole and Surface Crack Standard: 7075-T651 Aluminum.. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
19
19
Tool:
AFNDT-0512A.
Description:
Eddy Current Surface Crack Standard. EDM Notch Size: Total of 3 Notches, 0.005, 0.010, 0.020 Deep x .005W +/- .002 per 33B-1-2 WP 402 00. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
20
20
Tool:
AFNDT-0512T
Description:
Eddy Current Hole and Surface Crack Standard: 6AL-4v Titanium.. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
21
21
Tool:
AFNDT-1000/4340
Description:
12 HOLE REFERENCE STANDARD 4340 STEEL WITH A .020" MID WALL NOTCH, .030" CORNER NOTCH, .050" CORNER NOTCH, .010" ,.020", .040: .050" SURFACE NOTCH. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
22
22
Tool:
AFNDT-1000/SA
Description:
12 HOLE REFERENCE STANDARD ALUMINUM WITH A .020" MID WALL NOTCH, .030" CORNER NOTCH, .050" CORNER NOTCH, .010" ,.020", .040: .050" SURFACE NOTCH. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
23
23
Tool:
AFNDT-1000SA-1
Description:
12 HOLE REFERENCE STANDARD ALUMINUM WITH A .020" MID WALL NOTCH, .030" CORNER NOTCH, .050" CORNER NOTCH, .010" ,.020", .040: .050" SURFACE NOTCH. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
24
24
Tool:
AFNDT-1000SS
Description:
12 HOLE REFERENCE STANDARD STAINLESS STEEL WITH A .020" MID WALL NOTCH, .030" CORNER NOTCH, .050" CORNER NOTCH, .010" ,.020", .040: .050" SURFACE NOTCH. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
25
25
Tool:
AFNDT-1000TI
Description:
12 HOLE REFERENCE STANDARD 6AL4V WITH A .020" MID WALL NOTCH, .030" CORNER NOTCH, .050" CORNER NOTCH, .010" ,.020", .040: .050" SURFACE NOTCH. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
26
26
Tool:
AFNDT-1002
Description:
CUSTOM 3 HOLE 7075-T6 ALUM. EC REFERENCE STANDARD WITH a .020x.020" CORNER NOTCH IN EACH HOLE. HOLE SIZES 1.063", .687", .625" DIA. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
27
27
Tool:
AFNDT-1002-1
Description:
CUSTOM 3 HOLE STANDARD, MATERIAL: 7075-T6 ALUMINUM, .030x.030" CORNER EDM NOTCH IN EACH HOLE. HOLE SIZES 7/16"(.437"), .1/2"(.500"), 11/16"( .687") DIAMETERS. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
28
28
Tool:
AFNDT-1003/2024-T3
Description:
CUSTOM METRIC STEP WEDGE WITH 7 1.0"x1.0" STEPS MADE OF 2024-T3 ALUMINUM. STEP SIZES ( 1.6mm, 2.4mm, 3.2mm, 4.0mm, 4.8mm, 5.6mm, 6.4mm )..+/- .05mm. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
29
29
Tool:
AFNDT-1003/5086
Description:
CUSTOM METRIC STEP WEDGE WITH 7 1.0"x1.0" STEPS MADE OF 5086 ALUMINUM. STEP SIZES ( 1.6mm, 2.4mm, 3.2mm, 4.0mm, 4.8mm, 5.6mm, 6.4mm ) +/- .05mm. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
30
30
Tool:
AFNDT-1003/7075-T6
Description:
CUSTOM METRIC STEP WEDGE WITH 7 1.0"x1.0" STEPS MADE OF 7075-T6 ALUMINUM. STEP SIZES ( 1.6mm, 2.4mm, 3.2mm, 4.0mm, 4.8mm, 5.6mm, 6.4mm )..+/- .05mm. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
31
31
Tool:
AFNDT-1004CS
Description:
ARMY STRIKER THICKNESS BLOCK 3.0"L x 1.0"W x 7.31mm. THICK. MATERIAL: 4130 CARBON STEEL. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
32
32
Tool:
AFNDT-1005
Description:
14 HOLE ROTARY STANDARD 6AL4V 5/32, 7/32, 11/32, 3/16, 5/16, 13/64, 15/64, 17/64, 19/64, 21/64, 1/4, 3/8, 1/2, 28 EDM NOTCHES .050 TOP, .030 CORNER BOTTEM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
33
33
Tool:
AFNDT-1006AL
Description:
CUSTOM 3 STEP CALIBRATION BLOCK 2024-T3 ALUMINUM, STEP SIZES 1.0" x 2.0" FACE. STEP THICKNESSES OF 0.100", 0.200" and 0.400" +/-.002". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
34
34
Tool:
AFNDT-1006CS
Description:
CUSTOM 3 STEP CALIBRATION BLOCK 4340 CARBON STEEL, STEP SIZES 1.0" x 2.0" FACE. STEP THICKNESSES OF 0.100", 0.200" and 0.400" +/-.002" PER DC-10 54-10-11 FIGURE 603 SHEET 43 PAGE 655. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
35
35
Tool:
AFNDT-1010-177SS
Description:
BOEING TOOL ST8809C LETTER CODE D 17-7 PH ANNEALED STAINLESS STEEL. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
36
36
Tool:
AFNDT-1010-ALNIBR
Description:
BOEING TOOL ST8809C LETTER CODE F Al-NI-BR. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
37
37
Tool:
AFNDT-1010A
Description:
BOEING TOOL ST8809C LETTER CODE B 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
38
38
Tool:
AFNDT-1010S
Description:
BOEING TOOL ST8809C LETTER CODE E 4340 STEEL. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
39
39
Tool:
AFNDT-1010SA
Description:
BOEING TOOL ST8809C LETTER CODE A 7075-T73 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
40
40
Tool:
AFNDT-1010TI
Description:
BOEING TOOL ST8809C LETTER CODE C 6AL-4V TITANIUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
41
41
Tool:
AFNDT-1012
Description:
Bombardier / Challenger 300 Custom UT Thickness Reference Standard Figure 2 Part 1 Section 4 page 11. Material: 2024-T351 Clad. Standard machine milling, no Chemical mill. Step Tolerance: +/-.002". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
42
42
Tool:
AFNDT-1015
Description:
EDDY CURRENT CALIBRATION BLOCK 2024-T351, WITH .020"Lx.005"W COUNTERSINK SURFACE EDM NOTCH IN EACH HOLE.0.190-0.194, countersink: 100 degrees, 0.3748-0.3819 diameter....0.203-0.207, countersink: 100 degrees, 0.3748-0.3819 diameter....0.2172-0.2182, co...
Location:
North America
Aircraft or Engine:
43
43
Tool:
AFNDT-1015-CALCS
Description:
CALIBRATION BLOCK 4140S. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
44
44
Tool:
AFNDT-1015-CALSS
Description:
CALIBRATION BLOCK 304SS. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
45
45
Tool:
AFNDT-1015-CS/MM
Description:
CUSTOM 4 STEP CALIBRATION BLOCKS CARBON STEEL , 54MM, 10MM, 15MM, 20MM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
46
46
Tool:
AFNDT-1015-INC625
Description:
CALIBRATION STANDARD INCOLNEL BLOCK 625 5X1 OAL .10,.20,.30,.40,.50. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
47
47
Tool:
AFNDT-1015-SS/MM
Description:
CUSTOM 4 STEP CALIBRATION BLOCKS STAINLESS STEEL , 54MM, 10MM, 15MM, 20MM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
48
48
Tool:
AFNDT-1015/2024
Description:
CUSTOM 4 STEP CALIBRATION BLOCK 2024-T3 ALUMINUM, STEP SIZES .75"x.75" FACE WITH STEP THICKNESSES OF .040",.060",.080",.100" +/-.001". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
49
49
Tool:
AFNDT-1016-6S-TI
Description:
CUSTOM 6 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737, 747, 757, 767 PT 6 51-00-16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6, 51-00-02 PROCEDURE 1..... Hole Sizes: .188", .250", .313", .375" .438" .500". MATERIAL: 6AL-4V Titanium. Inc...
Location:
North America
Aircraft or Engine:
50
50
Tool:
AFNDT-1017AL
Description:
Custom Eddy Current Hole Standard 7075-T7 Aluminum ( Equivalent substitute for 7010 Aluminum). Hole Sizes 1.77" and 0.58" diameter. EDM flaw size: 0.5mm(.020") x 0.1mm (0.004") +/- .002". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
51
51
Tool:
AFNDT-1025AL
Description:
Multi-Hole reference standard. Material: 7075-T6 Aluminum. 12 Holes 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 .020" x .005" Wide ± .002" Through EDM Notches in each hole. Standard also includes 3 surface EDM n
Location:
North America
Aircraft or Engine:
52
52
Tool:
AFNDT-1025TI
Description:
Multi-Hole reference standard. Material: 6Al-4v Titanium. 12 Holes 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 .020" x .005" Wide ± .002" Through EDM Notches in each hole. Standard also includes 3 surface EDM no
Location:
North America
Aircraft or Engine:
53
53
Tool:
AFNDT-1030
Description:
CUSTOM BRILE RIVET/ 100 DEGREE COUNTERSINK MULTI HOLE REFERENCE STANDARD 7075-T6 ALUMINUM. BRILE HOLE SIZES: 5/32", 3/16" and 1/4". 100 DEGREE COUNTERSINK HOLE SIZES: 5/32", 3/16", 1/4", 5/16", 3/8". .030"X.030" CORNER / COUNTERSINK EDM NOTCHES. DIM...
Location:
North America
Aircraft or Engine:
54
54
Tool:
AFNDT-1030/10MM
Description:
CUSTOM EDDY CURRENT CALIBRATION BLOCK 4130 or 4340 STEEL. 50mm x 50mm x 15mm with 10mm diameter hole. Midwall EDM notch( 9.5mm long +/- 0.95 )x ( 0.13mm deep +/- 0.01 ) x ( 0.18mm MAX width ). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
55
55
Tool:
AFNDT-1030/12MM
Description:
CUSTOM EDDY CURRENT CALIBRATION BLOCK 4130 or 4340 STEEL. 50mm x 50mm x 15mm with 12mm diameter hole. Midwall EDM notch( 9.5mm long +/- 0.95 )x ( 0.13mm deep +/- 0.01 ) x ( 0.18mm MAX width ). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
56
56
Tool:
AFNDT-1030/6MM
Description:
CUSTOM EDDY CURRENT CALIBRATION BLOCK 4130 or 4340 STEEL. 50mm x 50mm x 15mm with 6mm diameter hole. Midwall EDM notch( 9.5mm long +/- 0.95 )x ( 0.13mm deep +/- 0.01 ) x ( 0.18mm MAX width ). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
57
57
Tool:
AFNDT-1030/8MM
Description:
CUSTOM EDDY CURRENT CALIBRATION BLOCK 4130 or 4340 STEEL. 50mm x 50mm x 15mm with 8mm diameter hole. Midwall EDM notch( 9.5mm long +/- 0.95 )x ( 0.13mm deep +/- 0.01 ) x ( 0.18mm MAX width ). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
58
58
Tool:
AFNDT-1031/10MM
Description:
CUSTOM EDDY CURRENT CALIBRATION BLOCK 4130 or 4340 STEEL. 50mm x 50mm x 15mm with 10mm diameter hole. Midwall EDM notch( 1.5mm long +/- 0.15 )x ( 0.76mm deep +/- 0.07 ) x ( 0.18mm MAX width ). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
59
59
Tool:
AFNDT-1031/12MM
Description:
CUSTOM EDDY CURRENT CALIBRATION BLOCK 4130 or 4340 STEEL. 50mm x 50mm x 15mm with 12mm diameter hole. Midwall EDM notch( 1.5mm long +/- 0.15 )x ( 0.76mm deep +/- 0.07 ) x ( 0.18mm MAX width ). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
60
60
Tool:
AFNDT-1031/6MM
Description:
CUSTOM EDDY CURRENT CALIBRATION BLOCK 4130 or 4340 STEEL. 50mm x 50mm x 15mm with 6mm diameter hole. Midwall EDM notch( 1.5mm long +/- 0.15 )x ( 0.76mm deep +/- 0.07 ) x ( 0.18mm MAX width ). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
61
61
Tool:
AFNDT-1031/8MM
Description:
CUSTOM EDDY CURRENT CALIBRATION BLOCK 4130 or 4340 STEEL. 50mm x 50mm x 15mm with 8mm diameter hole. Midwall EDM notch( 1.5mm long +/- 0.15 )x ( 0.76mm deep +/- 0.07 ) x ( 0.18mm MAX width ). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
62
62
Tool:
AFNDT-1032/10MM
Description:
CUSTOM EDDY CURRENT CALIBRATION BLOCK 4130 or 4340 STEEL. 50mm x 50mm x 15mm with 10mm diameter hole. Corner EDM notch( 0.76mm long +/- 0.07 )x ( 0.76mm deep +/- 0.07 ) x ( 0.18mm MAX width ). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
63
63
Tool:
AFNDT-1032/12MM
Description:
CUSTOM EDDY CURRENT CALIBRATION BLOCK 4130 or 4340 STEEL. 50mm x 50mm x 15mm with 12mm diameter hole. Corner EDM notch( 0.76mm long +/- 0.07 )x ( 0.76mm deep +/- 0.07 ) x ( 0.18mm MAX width ). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
64
64
Tool:
AFNDT-1032/6MM
Description:
CUSTOM EDDY CURRENT CALIBRATION BLOCK 4130 or 4340 STEEL. 50mm x 50mm x 15mm with 6mm diameter hole. Corner EDM notch( 0.76mm long +/- 0.07 )x ( 0.76mm deep +/- 0.07 ) x ( 0.18mm MAX width ). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
65
65
Tool:
AFNDT-1032/8MM
Description:
CUSTOM EDDY CURRENT CALIBRATION BLOCK 4130 or 4340 STEEL. 50mm x 50mm x 15mm with 8mm diameter hole. Corner EDM notch( 0.76mm long +/- 0.07 )x ( 0.76mm deep +/- 0.07 ) x ( 0.18mm MAX width ). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
66
66
Tool:
AFNDT-1035/7075
Description:
5 hole reference standard sizes; 1/4", 5/16", 3/8", 7/16" and1/2" inch diameters.( .030" X .030" x .005" +/-.001" corner EDM notch. 7075-T6 Aluminum. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
67
67
Tool:
AFNDT-1035TI
Description:
REFERENCE STANDARD 7/16" THICK 6AL-4V. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
68
68
Tool:
AFNDT-1040
Description:
THREE HOLE CALIBRATION STANDARD. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
69
69
Tool:
AFNDT-1045
Description:
5 STEP ACRYLIC WEDGE. STEP SIZES: .250", .500",. 750", 1.00", 1.250" MATERIAL: CAST ACRYLIC. PAD SIZE: 1.0" x 1.0" TOLEREANCE = +/- .002". Includes Certification and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
70
70
Tool:
AFNDT-1046
Description:
STEP ACRYLIC WEDGE. STEP SIZES: 0.1", 0.3", 0.5", 0.7", 0.9", 1.1" MATERIAL: CAST ACRYLIC. PAD SIZE: 1.0" x 1.0" TOLEREANCE = +/- .002". Includes Certification and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
71
71
Tool:
AFNDT-1060
Description:
NON-PIPING CALIBRATION BLOCK, 3/4 X 6 1/4 X 12. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
72
72
Tool:
AFNDT-1061AL
Description:
EDDY CURRENT SURFACE BLOCK 7075-T6. 2 EDM SLOTS ( 0.2mm deep +/-0.05 & 0.12mm wide +/- 0.01),( 0.5mm deep +/- 0.01. Includes Certification Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
73
73
Tool:
AFNDT-1061CS
Description:
EDDY CURRENT SURFACE BLOCK, 4130/4140 STEEL. 2 EDM SLOTS ( 0.2mm deep +/-0.05 & 0.12mm wide +/- 0.01),( 0.5mm deep +/- 0.01. Includes Certification Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
74
74
Tool:
AFNDT-1062
Description:
NON-PIPING CALIBRATION BLOCK FIGURE T-434.2.1 ASME SECTION V Article IV, 3" X 6 1/4" X 12". MATERIAL: 1018 CARBON STEEL. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
75
75
Tool:
AFNDT-1071/2024
Description:
Custom Metric 6 Step Block. Step Thicknesses of 0.5mm, 0.6mm, 0.7mm, 0.8mm, 0.9mm and 1.0mm. (Tolerance: +/- 0.02mm). Pad Size: 19mm X 19mm, (Tolerance: +/- 0.5mm) Material: 2024 Aluminum. Includes Certification Report for step thickness and Certific
Location:
North America
Aircraft or Engine:
76
76
Tool:
AFNDT-1071/304
Description:
Custom Metric 6 Step Block. Step Thicknesses of 0.5mm, 0.6mm, 0.7mm, 0.8mm, 0.9mm and 1.0mm. (Tolerance: +/- 0.02mm). Pad Size: 19mm X 19mm, (Tolerance: +/- 0.5mm) Material: 304 Stainless Steel. Includes Certification Report for step thickness and Ce
Location:
North America
Aircraft or Engine:
77
77
Tool:
AFNDT-1071/4340
Description:
Custom Metric 6 Step Block. Step Thicknesses of 0.5mm, 0.6mm, 0.7mm, 0.8mm, 0.9mm and 1.0mm. (Tolerance: +/- 0.02mm). Pad Size: 19mm X 19mm, (Tolerance: +/- 0.5mm) Material: 4340 CRES Steel. Includes Certification Report for step thickness and Certif
Location:
North America
Aircraft or Engine:
78
78
Tool:
AFNDT-1071/7075
Description:
Custom Metric 6 Step Block. Step Thicknesses of 0.5mm, 0.6mm, 0.7mm, 0.8mm, 0.9mm and 1.0mm. (Tolerance: +/- 0.02mm). Pad Size: 19mm X 19mm, (Tolerance: +/- 0.5mm) Material: 7075 Aluminum. Includes Certification Report for step thickness and Certific
Location:
North America
Aircraft or Engine:
79
79
Tool:
AFNDT-1071/INC
Description:
Custom Metric 6 Step Block. Step Thicknesses of 0.5mm, 0.6mm, 0.7mm, 0.8mm, 0.9mm and 1.0mm. (Tolerance: +/- 0.02mm). Pad Size: 19mm X 19mm, (Tolerance: +/- 0.5mm) Material: 718 Inconel. Includes Certification Report for step thickness and Certificat
Location:
North America
Aircraft or Engine:
80
80
Tool:
AFNDT-1071/TI
Description:
Custom Metric 6 Step Block. Step Thicknesses of 0.5mm, 0.6mm, 0.7mm, 0.8mm, 0.9mm and 1.0mm. (Tolerance: +/- 0.02mm). Pad Size: 19mm X 19mm, (Tolerance: +/- 0.5mm) Material: 6AL-4V Titanium. Includes Certification Report for step thickness and Certif
Location:
North America
Aircraft or Engine:
81
81
Tool:
AFNDT-1074-3
Description:
EDDY CURRENT SURFACE BLOCK MADE OF 6AL-4V TITANIUM WITH 3 SURFACE NOTCHES ACROSS THE WIDTH OF THE BLOCK. .1mm X .005" MAX WIDTH and .2mm X .005" MAX WIDTH, .5MM X.005" MAX WIDTH. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
82
82
Tool:
AFNDT-1074/713
Description:
Custom Metric 6 Step Block. Step Thicknesses of 0.5mm, 1mm, 3mm, 5mm, 7mm, 9mm. (Tolerance: +/- 0.02mm). Pad Size: 15mm X 15mm, (Tolerance: +/- 0.5mm) Material: 713 Inconel. Includes Certification Report for step thickness and COC of material used...
Location:
North America
Aircraft or Engine:
83
83
Tool:
AFNDT-1074/718
Description:
Custom Metric 6 Step Block. Step Thicknesses of 0.5mm, 1mm, 3mm, 5mm, 7mm, 9mm. (Tolerance: +/- 0.02mm). Pad Size: 15mm X 15mm, (Tolerance: +/- 0.5mm) Material: 718 Inconel. Includes Certification Report for step thickness and COC of material used...
Location:
North America
Aircraft or Engine:
84
84
Tool:
AFNDT-1074/TI
Description:
Custom Metric 6 Step Block. Step Thicknesses of 0.5mm, 1mm, 3mm, 5mm, 7mm, 9mm. (Tolerance: +/- 0.02mm). Pad Size: 15mm X 15mm, (Tolerance: +/- 0.5mm) Material: 6AL-4V Titanium. Includes Certification Report for step thickness and COC of material ...
Location:
North America
Aircraft or Engine:
85
85
Tool:
AFNDT-1074AL
Description:
Custom Metric 6 Step Block. Step Thicknesses of 0.5mm, 1mm, 3mm, 5mm, 7mm, 9mm. (Tolerance: +/- 0.02mm). Pad Size: 15mm X 15mm, (Tolerance: +/- 0.5mm) Material: 7075-T6 Aluminum. Includes Certification Report for step thickness and COC of material...
Location:
North America
Aircraft or Engine:
86
86
Tool:
AFNDT-1075AL
Description:
ULTRASONIC TEST BLOCK .100/.500 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
87
87
Tool:
AFNDT-1075ST
Description:
ULTRASONIC TEST BLOCK .100/.500 STEEL. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
88
88
Tool:
AFNDT-1075TI
Description:
ULTRASONIC TEST BLOCK .100/.500 TITANIUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
89
89
Tool:
AFNDT-1076AL
Description:
ULTRASONIC STEP BLOCK .020", .050", .075", .100", .125" 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
90
90
Tool:
AFNDT-1076ST
Description:
ULTRASONIC STEP BLOCK .020", .050", .075", .100", .125" 4340 STEEL. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
91
91
Tool:
AFNDT-1076TI
Description:
ULTRASONIC STEP BLOCK .020", .050", .075", .100", .125" 6AL-4V TITANIUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
92
92
Tool:
AFNDT-1080-2/840
Description:
CUSTOM REFERENCE STANDARD PER SPECS. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
93
93
Tool:
AFNDT-1080/4340
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES 0.5mm, 1.0mm, 2.0mm, 3.00mm, 4.0mm, 5.0mm (.004"W +/- .002, MAX.006), 4340 STEEL 1.0"W x 7.0"L. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
94
94
Tool:
AFNDT-1085
Description:
CUSTOM MULTI-HOLE REFERECNE STANDARD, 2024-T3 WITH .030X.030 CORNER NOTCH, .020X.020 CORNER NOTCH, HOLE SIZE 5/32,11/64,3/16,13/64,9/32,17/64,1/4,7/32. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
95
95
Tool:
AFNDT-1090AL
Description:
5 STEP WEDGE .050", .100", .150", .200", .250". TOLERANCE +/-.001". MATERIAL: 2024-T3 ALUMINUM. PAD SIZE: 750" x .750" . Includes Test Report traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
96
96
Tool:
AFNDT-1090SS
Description:
5 STEP WEDGE .050", .100", .150", .200", .250". TOLERANCE +/-.001". MATERIAL: 304 STAINLESS STEEL .PAD SIZE: 750" x .750" . Includes Test Report traceable to NIST and Certificate of Conformance. ..
Location:
North America
Aircraft or Engine:
97
97
Tool:
AFNDT-1090TI
Description:
5 STEP WEDGE .050", .100", .150", .200", .250". TOLERANCE +/-.001". MATERIAL: 6AL-4V TITANIUM .PAD SIZE: 750" x .750" . Includes Test Report traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
98
98
Tool:
AFNDT-1095
Description:
8 STEP THIN WEDGE, STEP SIZES OF .030", 0.040",.050", .060", .070", .080", .090", and .100" +/- .001". PAD SIZE: .75"x.75", MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
99
99
Tool:
AFNDT-1096 15-5PH
Description:
10 STEP REFERENCE BLOCK .025,.030,.040,.050,.063,.071,.080,.090,.100,.125 15-5PH. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
100
100
Tool:
AFNDT-1096/2024T3
Description:
10 STEP REFERENCE BLOCK .025,.030,.040,.050,.063,.071,.080,.090,100,.125 2024-T3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
101
101
Tool:
AFNDT-1096/304SS
Description:
9 STEP REFERENCE BLOCK WITH ACETAL(DELRIN) HOLDING BLOCK. MATERIAL: 304 STAINLESS STEEL. STEP SIZES: .020",.050",.080", .120", .160" , .200", .300", .500", .750" +/-.010". PAD SIZE = 1.0" x 1.0". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
102
102
Tool:
AFNDT-1096/6061AL
Description:
9 STEP REFERENCE BLOCK WITH HOLDER. MATERIAL: 6061 ALUMINUM. STEP SIZES: .020",.050",.080", .120", .160" , .200", .300", .500", .750" +/-.010". PAD SIZE = 1.0" x 1.0". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
103
103
Tool:
AFNDT-1096/625
Description:
9 STEP REFERENCE BLOCK WITH ACETAL(DELRIN) HOLDING BLOCK. MATERIAL: 625 INCONEL. STEP SIZES: .020",.050",.080", .120", .160" , .200", .300", .500", .750" +/-.010". PAD SIZE = 1.0" x 1.0". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
104
104
Tool:
AFNDT-1096/6AL4V
Description:
10 STEP REFERENCE BLOCK,.030,.040,.050,.063,.071,.080,.090,100,.120 6AL4V. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
105
105
Tool:
AFNDT-1096/718
Description:
9 STEP REFERENCE BLOCK WITH ACETAL(DELRIN) HOLDING BLOCK. MATERIAL: 625 INCONEL. STEP SIZES: .020",.050",.080", .120", .160" , .200", .300", .500", .750" +/-.010". PAD SIZE = 1.0" x 1.0". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
106
106
Tool:
AFNDT-1098AL
Description:
12 HOLE REFERENCE STANDARD 2024-T3 .156, .187, .199 ,.218, .250, .281, .312, .343, .375, .406, .437, .500, .030X.030 CORNER NOTCH, .050X.050 CORNER NOTCH ( 24 EDM NOTCHES TOTAL). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
107
107
Tool:
AFNDT-1098St
Description:
12 HOLE REFERENCE STANDARD 4340 STEEL. HOLE SIZES: .156, .187, .199 ,.218, .250, .281, .312, .343, .375, .406, .437, .500, .030X.030 CORNER NOTCH, .050X.050 CORNER NOTCH (24 EDM NOTCHES TOTAL). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
108
108
Tool:
AFNDT-1098TI
Description:
12 HOLE REFERENCE STANDARD 6AL4V .156, .187, .199 ,.218, .250, .281, .312, .343, .375, .406, .437, .500, .030X.030 CORNER NOTCH, .050X.050 CORNER NOTCH (24 EDM NOTCHES TOTAL). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
109
109
Tool:
AFNDT-186A-F
Description:
CUSTOM STANDARD COMBINING 186A-F INTO ONE STANDARD. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
110
110
Tool:
AFNDT-2001-909
Description:
CUSTOM STEP WEDGE INC909, 1"X6" W/ 1" STEPS .025 -.150 IN .25 INCREMENTS. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
111
111
Tool:
AFNDT-2002AL
Description:
CALIBRATION STANDARD THREE HOLES, 1.0,1.25,1.5, CORNER NOTCH .030X.030. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
112
112
Tool:
AFNDT-2003-1AL
Description:
Contains 12 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.( .030X.030 CORNER NOTCH and 3 SURFACE NOTCHES .010", .020", .040" DEEP x .750" LONG.) 7075-T6 ALUMINUM. Includes Test Report and Certificate of C
Location:
North America
Aircraft or Engine:
113
113
Tool:
AFNDT-2003-1S
Description:
Contains 12 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. ( .030X.030 CORNER NOTCH and 3 SURFACE NOTCHES .010", .020", .040" DEEP x .750" LONG.) 4340 STEEL. Includes Test Report and Certificate of Confor
Location:
North America
Aircraft or Engine:
114
114
Tool:
AFNDT-2003-1S-1
Description:
12 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. .020 Thru EDM notches .005"(+/- .001") and 3 SURFACE NOTCHES .010", .020", .040" DEEP x .750" LONG.) 4340 Steel. Includes Test Report and Certificate...
Location:
North America
Aircraft or Engine:
115
115
Tool:
AFNDT-2003-2S
Description:
12 HOLE REFERENCE STANDARD 1018 STEEL HOLE SIZES: .187", .250" ,.312", .375", .437", .500", .562", .625", .687", .750", AND 1.0" ( .030X.030 CORNER NOTCH and 3 SURFACE NOTCHES .010", .020", .040" DEEP x .750" LONG.) 304 STAINLESS STEEL. Includes Test Repo
Location:
North America
Aircraft or Engine:
116
116
Tool:
AFNDT-2004
Description:
EDDY CURRENT SURFACE STANDARD WITH 3 EDM NOTCHES: ( .005", .010", .020" Deep x .004"Wide +/- .002 ), MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
117
117
Tool:
AFNDT-2005A
Description:
12 HOLE REFERENCE STANDARD 7075-T6 ALUMINUM. HOLE SIZES: 1/8", 5/32", 3/16", 7/32" 1/4" , 5/16", 3/8", 7/16", 1/2", 9/16" 5/8", 3/4" .030" x .030" CORNER NOTCH. .008", .020", .040" SURFACE NOTCHES. .005" +/-.001". Includes Test Report and Certificate o
Location:
North America
Aircraft or Engine:
118
118
Tool:
AFNDT-2005CS
Description:
12 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, .030X.030 Corner EDM Notches .005"(+/- .001") wide, .020" full bore thru EDM notches .005"(+/- .001") deep and 3 SURFACE NOTCHES .010", .020", .040" D...
Location:
North America
Aircraft or Engine:
119
119
Tool:
AFNDT-2005TI
Description:
12 HOLE REFERENCE STANDARD 6AL-4v TITANIUM. HOLE SIZES: 1/8", 5/32", 3/16", 7/32" 1/4" , 5/16", 3/8", 7/16", 1/2", 9/16" 5/8", 3/4" .030" x .030" CORNER NOTCH. .008", .020", .040" SURFACE NOTCHES. .005" +/-.001". Includes Test Report and Certificate of
Location:
North America
Aircraft or Engine:
120
120
Tool:
AFNDT-2006/13-8
Description:
12 HOLE REFERENCE STANDARD 13-8 PH STAINLESS STEEL (3/16, 7/32 ,1/4, 9/32, 5/16,11/32, 3/8, 7/16, 1/2, 9/16, 5/8, 3/4), .030X.030. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
121
121
Tool:
AFNDT-2006/17-4
Description:
12 HOLE REFERENCE STANDARD 17-4PH (3/16, 7/32 ,1/4, 9/32, 5/16,11/32, 3/8, 7/16, 1/2, 9/16, 5/8, 3/4), .030X.030. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
122
122
Tool:
AFNDT-2006/300M
Description:
12 HOLE REFERENCE STANDARD 300M STEEL.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"), .030" X. 030" x.005"WIDE CORNER EDM NOTCH EACH HOLE and 3 SURFACE EDM NOTCHES .750" LONG .010", .020", .040" DEEP .005" ...
Location:
North America
Aircraft or Engine:
123
123
Tool:
AFNDT-2006A
Description:
12 HOLE REFERENCE STANDARD 7075-T6 aluminum. 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"), .030" X. 030" x.004" ±.002" WIDE CORNER EDM NOTCH in EACH HOLE and 3 SURFACE EDM NOTCHES .750" LONG .010", .020",...
Location:
North America
Aircraft or Engine:
124
124
Tool:
AFNDT-2006S
Description:
12 HOLE REFERENCE STANDARD 4130 or 4340 STEEL.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"), .030" X. 030" x.005"WIDE CORNER EDM NOTCH EACH HOLE and 3 SURFACE EDM NOTCHES .750" LONG .010", .020", .040" DEE...
Location:
North America
Aircraft or Engine:
125
125
Tool:
AFNDT-2006SS
Description:
12 HOLE REFERENCE STANDARD 304 304 STAINLESS STEEL.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"), .030" X. 030" x.005"WIDE CORNER EDM NOTCH EACH HOLE and 3 SURFACE EDM NOTCHES .750" LONG .010", .020", .040...
Location:
North America
Aircraft or Engine:
126
126
Tool:
AFNDT-2006TI
Description:
12 HOLE REFERENCE STANDARD 6AL-4V.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"), .030" X. 030" x.005"WIDE CORNER EDM NOTCH EACH HOLE and 3 SURFACE EDM NOTCHES .750" LONG .010", .020", .040" DEEP .005" WIDE...
Location:
North America
Aircraft or Engine:
127
127
Tool:
AFNDT-2007AL
Description:
CUSTOM 4 STEP WEDGE. MATERIAL: 7075-T6 ALUMINUM. STEP SIZES: .020",.040",.060",.090" +/-.001. PAD SIZE: .75" x .75". Includes Test Report Traceable to NIST.
Location:
North America
Aircraft or Engine:
128
128
Tool:
AFNDT-2007AL-1
Description:
CUSTOM 4 STEP WEDGE. MATERIAL: 2024-T3 ALUMINUM. STEP SIZES: .020",.040",.060",.090" +/-.001. PAD SIZE: .75" x .75". Includes Test Report Traceable to NIST.
Location:
North America
Aircraft or Engine:
129
129
Tool:
AFNDT-2008/2024-T6
Description:
AIRCRAFT BRAKING SYSTEMS REFERENCE STANDARD PT 3 32-42-05, PROCEEDURE 1, FIGURE 11, PAGE 15 ALUMINUM 2024-T6 .. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
130
130
Tool:
AFNDT-2008/C
Description:
AIRCRAFT BRAKING SYSTEMS REFERENCE STANDARD PT 3 32-42-05, PAGES 1-7 FIGURE 2 and 3 CAST ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
131
131
Tool:
AFNDT-2008/F
Description:
AIRCRAFT BRAKING SYSTEMS REFERENCE STANDARD PT 3 32-42-05, PROCEEDURE 1, FIGURE 11, PAGE 15 ALUMINUM 2014-T6 CONDUCTIVITY RANGE 35-40 IACS.. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
132
132
Tool:
AFNDT-2008/MAG
Description:
AIRCRAFT BRAKING SYSTEMS REFERENCE STANDARD PT 3 32-42-05, PAGES 1-7 FIGURE 2 and 3. MATERIAL: MAGNESIUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
133
133
Tool:
AFNDT-2008/SS
Description:
AIRCRAFT BRAKING SYSTEMS REFERENCE STANDARD PT 3 32-42-05, PAGES 1-7 FIGURE 2 and 3 & 32-42-05 FIGURE 11 PROCEDURE 1 PAGE 15. MATERIAL: 304 STAINLESS STEEL. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
134
134
Tool:
AFNDT-2009AL
Description:
5 STEP WEDGE, 16mm, 17mm, 18mm, 19mm, 20mm, +/- .05mm. Material: 7075-T6 Aluminum. Pad Size: 20mm x 20mm square. Includes Delrin Holding Block. Includes Test Report Traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
135
135
Tool:
AFNDT-2010AL
Description:
Custom McDonnell Douglas 15 bolt hole reference standard with a .060"L x .030Dx .005" max width mid-wall notch, and .030"x.030"x.005" max width corner notch in each hole. Hole sizes (.156", .172", .188", .203", .250", .266", .281", .297", .313", .328"...
Location:
North America
Aircraft or Engine:
136
136
Tool:
AFNDT-2011/4130
Description:
10 STEP CARBON STEEL WEDGE. STEP THICKNESS OF , .019", .028", .050", .096", .148", .202", .253", .301", .350" .400" +/-.001". 1.0" x 1.0" Step Pad Face. Material: 4130 Carbon Steel. Includes Certification Report traceable to NIST.
Location:
North America
Aircraft or Engine:
137
137
Tool:
AFNDT-2011/7075
Description:
10 STEP ALUMINUM WEDGE. STEP THICKNESS OF , .019", .028", .050", .096", .148", .202", .253", .301", .350" .400" +/-.001". 1.0" x 1.0" Step Pad Face. Material: 7075-T651 Aluminum. Includes Certification Report traceable to NIST.
Location:
North America
Aircraft or Engine:
138
138
Tool:
AFNDT-2013AL
Description:
12 HOLE REFERENCE STANDARD 7075-T6 (3/16" x 2), 13/64", 7/32", 15/64" ,(1/4" x 2 ), 17/64",9/32", 19/64",5/16", 21/64" .020"x.020" and .030"x.030" x .005"W +/-.002" CORNER EDM NOTCH PER BOEING SPECIFICATION 747 PART 6 51-00-00 PAGE 8 FIGURE 3. Includes Te
Location:
North America
Aircraft or Engine:
139
139
Tool:
AFNDT-2014
Description:
CUSTOM EC STANDARD, NOTCH .060X.030X.005 TOL PER BSS7048, 304SS. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
140
140
Tool:
AFNDT-2014Ti
Description:
12 HOLE REFERENCE STANDARD IN 6AL-4v Ti; 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), .010", .020", .030", and .040" SURFACE NOTCHES. .050"x.050" CORNER EDM NOTCH and .030"x.030" CORNEREDM NOTCH, .050"Lx.030"D MID-...
Location:
North America
Aircraft or Engine:
141
141
Tool:
AFNDT-2015
Description:
CUSTOM SURFACE WAVE STANDARD, 6AL-4V. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
142
142
Tool:
AFNDT-2017-INC718
Description:
BOMBARDIER GLOBAL 5000 REFERENECE STANDARD BD-700 PT 6 57-70-001. ALSO IN 53-10-01 PART 6 PAGE 5 FIGURE 1. EDM Notches: .008", .020", .040" ( .005" W +0.00, - .002"), MATERIAL: 718 INCONEL. SIZE: 1.5"W x 3.75"L x .25". Includes Test Report and Certific
Location:
North America
Aircraft or Engine:
143
143
Tool:
AFNDT-2030/13-8
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 13-8PH STEEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
144
144
Tool:
AFNDT-2030/13-8PH
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 13-8PH MO STEEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
145
145
Tool:
AFNDT-2030/15-5PH
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 15-5PH STEEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
146
146
Tool:
AFNDT-2030/17-4
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 17-4PH STEEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
147
147
Tool:
AFNDT-2030/17-7PH
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 17-7PH STEEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
148
148
Tool:
AFNDT-2030/2014-T6
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, EDM NOTCHES .008", .020", .040" (.004W +/- .002), MATERIAL: 2014-T6 ALUMINUM. SIZE: 4.0"L x 1.0"W x .25". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
149
149
Tool:
AFNDT-2030/2014-T651
Description:
DDY CURRENT SURFACE REFERENCE STANDARD, EDM NOTCHES .008", .020", .040" (.004W +/- .002), MATERIAL: 2014-T651 ALUMINUM. SIZE: 4.0"L x 1.0"W x .25". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
150
150
Tool:
AFNDT-2030/2024
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, EDM NOTCHES .008", .020", .040" (.004W +/- .002), MATERIAL: 2024-T3 ALUMINUM. SIZE: 4.0"L x 1.0"W x .25". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
151
151
Tool:
AFNDT-2030/2024-T6
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, EDM NOTCHES .008", .020", .040" (.004W +/- .002), MATERIAL: 2024-T6 ALUMINUM. SIZE: 4.0"L x 1.0"W x .25". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
152
152
Tool:
AFNDT-2030/300M
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), MATERIAL: 300M STEEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
153
153
Tool:
AFNDT-2030/301
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002, MAX.006), CRES 301 1/2 HARD(MIL-S-5059) 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
154
154
Tool:
AFNDT-2030/304
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 304 STAINLESS STEEL 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
155
155
Tool:
AFNDT-2030/304L
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 304L STAINLESS STEEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
156
156
Tool:
AFNDT-2030/316SS
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 316 STAINLESS STEEL 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
157
157
Tool:
AFNDT-2030/4130
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 4130 STEEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
158
158
Tool:
AFNDT-2030/4340
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 4340 STEEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
159
159
Tool:
AFNDT-2030/6061-T6
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008"(0.2mm), .020"(0.5mm), .040"(1.0mm) (.004"W +/- .002), 6061-T6 ALUMINUM. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance and Material Certification.
Location:
North America
Aircraft or Engine:
160
160
Tool:
AFNDT-2030/7075-T6
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 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:
161
161
Tool:
AFNDT-2030/7075-T7
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 7075-T7 ALUMINUM. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
162
162
Tool:
AFNDT-2030/718
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 718 INCONNEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
163
163
Tool:
AFNDT-2030/I600
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 600 SERIES INCONNEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
164
164
Tool:
AFNDT-2030/MAG
Description:
Surface reference standard, Magnesium, with EDM notch depths of 0.008", 0.020" and 0.040" inches (0.2mm, 0.51mm and 1.02mm). Reference standard overall dImensions 1 X 4 X 0.25 inches (2.54cm X 10.1cm X 6.35mm). EDM notches .007" W MAX
Location:
North America
Aircraft or Engine:
165
165
Tool:
AFNDT-2030/MAR
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008"(0.2mm), .020"(0.5mm), .040"(1.0mm) (.004"W +/- .002). MATERIAL: 250 MARAGING STEEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
166
166
Tool:
AFNDT-2030/N200
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), MATERIAL: NICKEL 200. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
167
167
Tool:
AFNDT-2030/TI
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002, MAX .006"), 6AL-4v TITANIUM. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and COC
Location:
North America
Aircraft or Engine:
168
168
Tool:
AFNDT-2030CS
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002, MAX.006), 4130 or 4340 STEEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
169
169
Tool:
AFNDT-2030INC
Description:
EDDY CURRENT SURFACE REFERENCE BLOCK, EDM NOTCHES ( .008", .020", .040" x .004" W +/- .002"), INCONEL 718. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
170
170
Tool:
AFNDT-2031/4340
Description:
7 STEP REFERENCE BLOCK ..STEP PAD SIZE: 1.0" X 1.0" MATERIAL: 4340 CRES STEEL. STEP RANGE:.040", .080", .160", .250", .300", .400", .500". +/-.001". Includes certification report traceable to NIST...
Location:
North America
Aircraft or Engine:
171
171
Tool:
AFNDT-2031/6AL-4V
Description:
7 STEP REFERENCE BLOCK ..STEP PAD SIZE: 1.0" X 1.0" MATERIAL: 6AL-4V TITANIUM. STEP RANGE:.040", .080", .160", .250", .300", .400", .500" +/- .001". Includes certification report traceable to NIST...
Location:
North America
Aircraft or Engine:
172
172
Tool:
AFNDT-2031/7075
Description:
7 STEP REFERENCE BLOCK ..STEP PAD SIZE: 1.0" X 1.0" MATERIAL: 7075-T6 ALUMINUM. STEP RANGE:.040", .080", .160", .250", .300", .400", .500" +/- .001". Includes certification report traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
173
173
Tool:
AFNDT-2032/Al
Description:
5 STEP REFERENCE BLOCK ..STEP SIZES 1.0" X 1.0" 7075-T6 ALUMINUM. (400",.450",.500",.550",.600"). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
174
174
Tool:
AFNDT-2032/SS
Description:
5 STEP REFERENCE BLOCK ..STEP SIZES 1.0" X 1.0" 304 STAINLESS.(400",.450",.500",.550",.600")... Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
175
175
Tool:
AFNDT-2032/Ti
Description:
5 STEP REFERENCE BLOCK ..STEP SIZES 1.0" X 1.0" 6AL-4V Ti.(400",.450",.500",.550",.600"). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
176
176
Tool:
AFNDT-2035
Description:
6 Hole reference standard (Aluminum 7075-T6 with certifications). Hole Sizes: 1.0", 1.125", 1.250" ,1.500", 1.625", 1.750", ( .030 x .030 x .006 +/- .001) Corner EDM Notches and .010, .020, .040 Surface notches).. Includes Test Report and Certificate
Location:
North America
Aircraft or Engine:
177
177
Tool:
AFNDT-2037/7075T6
Description:
10 STEP WEDGE SUPPLIED WITH HOLDING BLOCK. STEP SIZES: .040", .080", .120", .160", .200", .240", .280", .320", .360", .400" +/-.001". Material: 7075-T6 ALUMINUM. PAD SIZE: .75" x .75". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
178
178
Tool:
AFNDT-2038AL
Description:
EDDY CURRENT CALIBRATION BLOCK 2024-T351, WITH .020"Lx.005"W COUNTERSINK SURFACE EDM NOTCH IN EACH HOLE. HOLE SIZES: .156"Ø and .187"Ø. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
179
179
Tool:
AFNDT-2039
Description:
ST8871 CARBON LAMINATE STEP WEDGE HOLDER. Includes Certificate of Conformance.
Location:
North America
Aircraft or Engine:
180
180
Tool:
AFNDT-2040AL
Description:
4 STEP WEDGE. Material: 2024-T351 Aluminum. Step Sizes: 0.5mm, 1.0mm, 1.5mm, 2.0mm, +/-0.05mm Pad Size: 19mm x 19mm. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
181
181
Tool:
AFNDT-2041/2024-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 Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
182
182
Tool:
AFNDT-2041/AL
Description:
5 STEP WEDGE 7075-T6 ALUMINUM:(.030",.060",.125",.250",.250, .375" +/-.001 Note**with additional engraving marks of metric conversions on each step.**..(0.762mm, 1.524mm, 3.175mm, 6.350mm, 9.525mm) INCLUDED WITH CERTIFICATION REPORT
Location:
North America
Aircraft or Engine:
183
183
Tool:
AFNDT-2041/AL-1
Description:
5 STEP WEDGE 2024-T3 ALUMINUM:(.030",.060",.125",.250",.250, .375" +/-.001 Note**with additional engraving marks of metric conversions on each step.** (0.762mm, 1.524mm, 3.175mm, 6.350mm, 9.525mm). IncludesTest Report Traceable to NIST and Certificate of
Location:
North America
Aircraft or Engine:
184
184
Tool:
AFNDT-2041/ST
Description:
5 STEP WEDGE 4340 steel:(.030",.060",.125",.250",.250, .375" +/-.001 Note**with additional engraving marks of metric conversions on each step.**..(0.762mm, 1.524mm, 3.175mm, 6.350mm, 9.525mm) INCLUDED WITH CERTIFICATION REPORTS
Location:
North America
Aircraft or Engine:
185
185
Tool:
AFNDT-2041/TI
Description:
5 STEP WEDGE 6al-4v TITANIUM:(.030",.060",.125",.250",.250, .375" +/-.001 Note**with additional engraving marks of metric conversions on each step.**..(0.762mm, 1.524mm, 3.175mm, 6.350mm, 9.525mm) INCLUDED WITH CERTIFICATION REPORTS
Location:
North America
Aircraft or Engine:
186
186
Tool:
AFNDT-2042/AL
Description:
CUSTOM 5 HOLE REFERENCE STANDARD MADE OF 7075-T6 ALUMINUM WITH (0.5mm X 0.5mm +/- .05mm) CORNER EDM FLAWS. HOLE SIZE : 13/64", 19/64", 23/64", 7/16" & 31/64". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
187
187
Tool:
AFNDT-2046/AL
Description:
15 HOLE REFERENCE STANDARD 7075-T6 1/8, 5/32, 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 13/32, 7/16, 15/32, 1/2, 9/16, 5/8, 15 EDM NOTCHES .030X.030 CORNER TOP. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
188
188
Tool:
AFNDT-2046/TI
Description:
15 HOLE REFERENCE STANDARD 6AL4V 1/8, 5/32, 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 13/32, 7/16, 15/32, 1/2, 9/16, 1/2, 15 EDM NOTCHES .030X.030 CORNER. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
189
189
Tool:
AFNDT-2047TI
Description:
4 STEP WEDGE. PAD SIZE 20mm X 20mm. STEP SIZES: 0.6mm, .2mm, 3mm, 4mm +/- .05mm. MATERIAL 6AL-4V
Location:
North America
Aircraft or Engine:
190
190
Tool:
AFNDT-2054AL-2
Description:
CUSTOM ALUMINUM REFERENCE STANDARD PER BOEING SPECIFICATION NDT1016-NDT1021, 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. WITH HOLE DIAMETERS: .125" .156", .187", .250",.375",.500". CORNER...
Location:
North America
Aircraft or Engine:
191
191
Tool:
AFNDT-2054CS-1
Description:
CUSTOM REFERENCE STANDARD PER BOEING SPECIFICATION NDT1040-NDT1045, 707, 727, 737, 747 PT 6 51-00-00 FIG 19, 757, 767 PT 6 51-00-17, 777 PT 6 51-00-05 PROCEDURE 2, 787 PT 6 51-00-04 PROCEDURE 1. DIAMETERS: .156",.250",.312",.375",.437",.500". CORN...
Location:
North America
Aircraft or Engine:
192
192
Tool:
AFNDT-2054CS-2
Description:
CUSTOM REFERENCE STANDARD PER BOEING SPECIFICATION NDT1040-NDT1045, 707, 727, 737, 747 PT 6 51-00-00 FIG 19, 757, 767 PT 6 51-00-17, 777 PT 6 51-00-05 PROCEDURE 2, 787 PT 6 51-00-04 PROCEDURE 1. DIAMETERS: .125", .156", .187" ,.250",.375", .500". ...
Location:
North America
Aircraft or Engine:
193
193
Tool:
AFNDT-2055
Description:
CUSTOM ROTARY BLOCK REFERENCE STANDARD. 10MM, 13MM, 15MM, 17MM , 19MM, .020X.020X.004 +/-.001, ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
194
194
Tool:
AFNDT-2056
Description:
CUSTOM CALIBRATION BLOCK, THREE SURFACE NOTCHES .008" , .020" , .040" SS. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
195
195
Tool:
AFNDT-2058/7075T6
Description:
6 STEP CALIBRATION BLOCK, CUSTOM, .030", .040", 0.60" , 0.80", .100", .150", 7075-T6 Aluminum. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
196
196
Tool:
AFNDT-2059/304SS
Description:
CUSTOM 8 STEP STANDARD, .080,.071,.063,.056,.050,.040,.030,.020, 304SS. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
197
197
Tool:
AFNDT-2059/6AL4V
Description:
CUSTOM 8 STEP STANDARD, .080,.071,.063,.056,.050,.040,.030,.020, 6AL4V. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
198
198
Tool:
AFNDT-2059/7075-T6
Description:
CUSTOM 8 STEP STANDARD, .080,.071,.063,.056,.050,.040,.030,.020, 7075-T6. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
199
199
Tool:
AFNDT-2060
Description:
CUSTOM REFERENCE STANDARD 7075-T6, NOTCH .010 +/-.001. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
200
200
Tool:
AFNDT-2061
Description:
CUSTOM 6 STEP WEDGE, 6AL-4V .3543, .2755, .1968, .1181, .0393, .0196, 4.744L X .787 W, STEP FACE .787X.787. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
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