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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:
BM5-196LN-6
Description:
Mini microdot Coaxial Cable. BNC to 5-44 thread mini-microdot, RG196 low noise 50 Ohm 6.0 feet long.
Location:
North America
Aircraft or Engine:
2
2
Tool:
BN-MD-6
Description:
BNC TO MICRODOT CABLE
Location:
North America
Aircraft or Engine:
3
3
Tool:
BUTTON HEAD CAL STD
Description:
BOEING BUTTON HEAD CALIBRATION STANDARD
Location:
North America
Aircraft or Engine:
4
4
Tool:
C-130 FIXTURE
Description:
Custom C-130 Blade Inside Bushing Probe Fixture per Drawing No. 201757983. Material: ABS Plastic machined not 3D Printed.
Location:
North America
Aircraft or Engine:
5
5
Tool:
C-130-WR
Description:
C-130 Outer Wing Rainbow Fitting Bolt Hole Standard C-130, 2 Layers, 3 HOLES, 3/4", 7/8" and 1.0" with .004" X .030" X .030" EDM Notches in each hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
6
6
Tool:
C12-DEL-3C1N
Description:
REPAIR REFERENCE STANDARD GR/EP LAMINATE STEP DELAM DEFECT. ALL BOEING AIRCRAFT MODELS PART 1 51-01-01. Includes C-SCAN Certification and Certificate of Conformance...
Location:
North America
Aircraft or Engine:
7
7
Tool:
C12-DIS-3C1N
Description:
REPAIR REFERENCE STANDARD GR/EP LAMINATE STEP DISBOND and CORE LAMINATE INTERFACE. ALL BOEING AIRCRAFT MODELS PART 1 51-01-01. Includes C-SCAN Certification and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
8
8
Tool:
C12-PCS-3C1N
Description:
REPAIR REFERENCE STANDARD GR/EP LAMINATE STEP POTTED HOLE and SPLICE CORE DEFECT. ALL BOEING AIRCRAFT MODELS PART 1 51-01-01. Includes C-SCAN Certification and Certificate of Conformance...
Location:
North America
Aircraft or Engine:
9
9
Tool:
C12-POT-3C1N
Description:
REPAIR REFERENCE STANDARD GR/EP LAMINATE STEP POTTED CORE and CORE DEFECT. ALL BOEING AIRCRAFT MODELS PART 1 51-01-01. Includes C-SCAN Certification and Certificate of Conformance...
Location:
North America
Aircraft or Engine:
10
10
Tool:
C13/C33
Description:
PEMCO REPAIR COUPON #25 FIGURE 2. MATERIAL: 2024-T3 CLAD ALUMINUM. RIVETS: MS20426DD6. EDM NOTCH LENGTH: .26"(.66mm) and .280"(.71mm) BOTH SIDES OF FASTENER HOLE. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
11
11
Tool:
C130-CW-012
Description:
C-130 CALIBRATION STANDARD. MATERIAL:7075-T6 ALUMINUM 5 PIECE STACK. FASTENER (HLT114-6-8 + NUT P/N: KFN542-3) 6 PLACES. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
12
12
Tool:
C130-CW-013
Description:
C-130 CALIBRATION STANDARD. MATERIAL:7075-T6 ALUMINUM 5 PIECE STACK. FASTENER (HLT114-6-8 + NUT P/N: KFN542-3) 6 PLACES. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
13
13
Tool:
C130-CWOW-019
Description:
LOCKHEED C-130 CALIBRATION STANDARD LOWER SURFACE PANEL. MATERIAL: 7075-T6 ALUMINUM
Location:
North America
Aircraft or Engine:
14
14
Tool:
C130-OW-016
Description:
LOCKHEED C-130 CALIBRATION STANDARD FIGURE 9-4 No.1 and No. 4 Truss Mount Upper Lugs. Material: 7075-T6 Aluminum Sulfuric Acid Anodized Per MIL-A-8625 or Equivalent. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
15
15
Tool:
C130-UT-17-1
Description:
C-130 CALIBRATION STEP STANDARD. MATERIAL:7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
16
16
Tool:
C3/C29
Description:
PEMCO REPAIR COUPON #25 FIGURE 2. MATERIAL: 2024-T3 CLAD ALUMINUM. RIVETS: MS20426DD6. EDM NOTCH LENGTH: .125"(.031mm) and .180"(.45mm) BOTH SIDES OF FASTENER HOLE. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
17
17
Tool:
CA12-1508A
Description:
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 7075-T7 ALUMINUM, 54-10-11 PAGE 634A FIG.603 SHEET 21B
Location:
North America
Aircraft or Engine:
18
18
Tool:
CA12-1683A
Description:
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 STEEL, 54-10-11 PAGE 632C FIG.603 SHEET 20C
Location:
North America
Aircraft or Engine:
19
19
Tool:
CA235-235502
Description:
AIRBUS MILITARY REFERENCE STANDARD 53-30-10 FIG 505, PAGE 508.
Location:
North America
Aircraft or Engine:
20
20
Tool:
CB-LM-532048
Description:
REFERENCE BLOCK FIGURE 5. MATERIAL: 2024-T351 ALUMINUM WITH PRIMER. EDM NOTCH: 3mm X 3mm X .15mm ± .05mm. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
21
21
Tool:
CBM-6
Description:
CABLE - BNC TO MICRODOT 6' LONG
Location:
North America
Aircraft or Engine:
22
22
Tool:
CE1331699-003
Description:
8 STEP THICKNESS CALIBRATION STANDARD. STEP SIZES: .025", .030", .035", .040", .045", .055", .060", .068" +/-.001". PAD SIZE 1.0" x 1.25" TYP. MATERIAL: 7475-T7351 ALUMINUM, CHROMIC ACID ANODIZED. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
23
23
Tool:
CE1617528
Description:
CALIBRATION STANDARD, BOMBARDIER TEST REFERENCE ULTRA SONIC NDI. MATERIAL: 7475-T7351 and 7040-T7451 ALUMINUM. MS90254U0805D FASTENERS. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
24
24
Tool:
CE1617529
Description:
CALIBRATION STANDARD, BOMBARDIER TEST REFERENCE ULTRA SONIC NDI. MATERIAL: 7475-T7351 and 7040-T7451 ALUMINUM. MS90254U0805D FASTENERS. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
25
25
Tool:
CFM56 9970-958-579
Description:
EDDY CURRENT SURFACE REFERENCE BLOCK. 2 EDM NOTCHES .012" Deep x .004" Wide and .020" Deep x .004" Wide. Tolerance on Width (.004" W +/- .002"), Material: Inconel 600 Series. Reference: CFM56-5B S/B 72-0620 PAGE 14. Includes Test Report and Certificate
Location:
North America
Aircraft or Engine:
26
26
Tool:
COUPON 12
Description:
PEMCO WORLD AIR SERVICES EDDY CURRENT LOW FREQUENCY STANDARD. COUPON FOR USE WITH INSPECTION ED-3. 05-30-10 PG.193. Includes Certification Report Tracable to NIST.
Location:
North America
Aircraft or Engine:
27
27
Tool:
COUPON 2
Description:
PEMCO WORLD AIR SERVICES EDDY CURRENT LOW FREQUENCY STANDARD. COUPON FOR USE WITH INSPECTION ED-4. 05-30-10 PG.190. Includes Certification Report Tracable to NIST.
Location:
North America
Aircraft or Engine:
28
28
Tool:
COUPON 25
Description:
PEMCO LOW FREQUENCY EDDY CURRENT STANDARD FOR INSPECTION UJ-1. 05-30-10 PAGE 194. EDM NOTCH: .030 MAX WIDTH x .240" LONG. Includes Certification Report Tracable to NIST.
Location:
North America
Aircraft or Engine:
29
29
Tool:
COUPON 29
Description:
PEMCO WORLD AIR SERVICES EDDY CURRENT LOW FREQUENCY STANDARD. COUPON FOR USE WITH INSPECTION ED-3 and ED-4. 05-30-10 PG.195. Includes Certification Report Tracable to NIST.
Location:
North America
Aircraft or Engine:
30
30
Tool:
COUPON 3
Description:
PEMCO WORLD AIR SERVICES EDDY CURRENT LOW FREQUENCY STANDARD. COUPON FOR USE WITH INSPECTION ED-3. 05-30-10 PG.191. Includes Certification Report Tracable to NIST.
Location:
North America
Aircraft or Engine:
31
31
Tool:
COUPON 31
Description:
PEMCO WORLD AIR SERVICES EDDY CURRENT LOW FREQUENCY STANDARD. COUPON FOR USE WITH INSPECTION ED-5. 05-30-10 PG.196. Includes Certification Report Tracable to NIST.
Location:
North America
Aircraft or Engine:
32
32
Tool:
COUPON 6
Description:
PEMCO WORLD AIR SERVICES EDDY CURRENT LOW FREQUENCY STANDARD. COUPON FOR USE WITH INSPECTION ED-5. 05-30-10 PG.192. Includes Certification Report Tracable to NIST.
Location:
North America
Aircraft or Engine:
33
33
Tool:
CRES 17-4PH
Description:
BOMBARDIER CHALLENGER EDDY CURRENT SURFACE BLOCK CRES 17-4PH STEEL. PART6 78-30-06 PAGE 27, 0.008", 0.020" and 0.040" EDM NOTCHES. Includes Certification Report Tracable to NIST.
Location:
North America
Aircraft or Engine:
34
34
Tool:
CRS 1 AL6061
Description:
6 STEP CALIBRATION BLOCK. STEP THICKNESS: 0.020", 0.040", 0.060", 0.100", 0.150", 0.200" +/- .001". STEP PAD SIZE: 1.0" x 1.0". MATERIAL: 6061-T6 ALUMINUM. Includes certification Report Traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
35
35
Tool:
CRS 2 AL6061
Description:
6 STEP CALIBRATION BLOCK. STEP THICKNESS: 0.100", 0.250", 0.400", 0.600", 0.800", 1.000" +/- .001". STEP PAD SIZE: 1.0" x 1.0". MATERIAL: 6061-T6 ALUMINUM. Includes certification Report Traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
36
36
Tool:
CRS AL2024
Description:
5 STEP CALIBRATION BLOCK. STEP THICKNESS: 0.200", 0.400", 0.600", 0.800", 1.000" +/- .001". STEP PAD SIZE: 1.0" x 1.0". MATERIAL: 2024-T351 ALUMINUM. Includes certification Report Traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
37
37
Tool:
CW-23 OW-47
Description:
C-130 CALIBRATION STANDARD. MATERIAL:7075-T7 or Equivalent Aluminum. FASTENER (NAS517-3-2) 2 Places. Includes Test Report and Certificate of Conformance For Standard and Certification for material and Fasteners.
Location:
North America
Aircraft or Engine:
38
38
Tool:
D3-MD-6
Description:
CABLE 3 PIN DIN TP MICRODOT 6FT LONG A320 53-41-56 53-41-33, USE WITH DEFECTOMETER
Location:
North America
Aircraft or Engine:
39
39
Tool:
DAC ETBS AL-1T 2024-T3 0.063
Description:
MD-80 REFERENCE STANDARD ETFL PROCEDURE 5, 06-10-02.005. MATERIAL: 2024-T3 ALUMINUM 0.063". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
40
40
Tool:
DAC ETBS AL-1T/ 0.032
Description:
MD-80 REFERENCE STANDARD ETFL PROCEDURE 5 Part 6 06-10-02 Page F1 Figure 1. Material: 7075-T7 ALUMINUM .032". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
41
41
Tool:
DAC ETBS AL-1T/ 0.071
Description:
MD-80 REFERENCE STANDARD ETFL PROCEDURE 5 Part 6 06-10-02 Page F1 Figure 1. Material: 2024-T3 ALUMINUM .071". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
42
42
Tool:
DAC ETBS AL-1T/ 0.090
Description:
MD-80 REFERENCE STANDARD ETFL PROCEDURE 5 Part 6 06-10-02 Page F1 Figure 1. Material: 7075-T6 ALUMINUM .090". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
43
43
Tool:
DAC ETBS AL-1T/0.080
Description:
MD-80 REFERENCE STANDARD ETFL PROCEDURE 5 Part 6 06-10-02 Page F1 Figure 1. Material: 2024-T3 ALUMINUM .080". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
44
44
Tool:
DAC ETOH AL
Description:
Multi Purpose Calibration Standard. 13 Basic Hole Sizes; 1/8, 5/32, 3/16, 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 x .005 Corner EDM Notches in each Hole, .020 x .005 Thru EDM Notch in holes less than 3/16. Mat
Location:
North America
Aircraft or Engine:
45
45
Tool:
DAC ETOH FE
Description:
Multi Purpose Calibration Standard. 13 Basic Hole Sizes; 1/8, 5/32, 3/16, 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 x .005 Corner EDM Notches in each Hole, .020 x .005 Thru EDM Notch in holes less than 3/16. Mat
Location:
North America
Aircraft or Engine:
46
46
Tool:
DAC ETOH TI
Description:
Multi Purpose Calibration Standard. 13 Basic Hole Sizes; 1/8, 5/32, 3/16, 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 x .005 Corner EDM Notches in each Hole, .020 x .005 Thru EDM Notch in holes less than 3/16. Mat
Location:
North America
Aircraft or Engine:
47
47
Tool:
DAC ETOH-AL-1/2
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Aluminum. 1/2 (0.500) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
48
48
Tool:
DAC ETOH-AL-1/4
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Aluminum. 1/4 (0.250) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
49
49
Tool:
DAC ETOH-AL-1/8
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Aluminum. 1/8 (0.125) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
50
50
Tool:
DAC ETOH-AL-11/16
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Aluminum. 11/16 (0.6875) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
51
51
Tool:
DAC ETOH-AL-3/16
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Aluminum. 3/16 (0.1875) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
52
52
Tool:
DAC ETOH-AL-3/4
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Aluminum. 3/4 (0.750) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
53
53
Tool:
DAC ETOH-AL-3/8
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Aluminum. 3/8 (0.375) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
54
54
Tool:
DAC ETOH-AL-5/16
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Aluminum. 5/16 (0.3125) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
55
55
Tool:
DAC ETOH-AL-5/8
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Aluminum. 5/8 (0.625) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
56
56
Tool:
DAC ETOH-AL-7/16
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Aluminum. 7/16 (0.4375) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
57
57
Tool:
DAC ETOH-AL-9/16
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Aluminum. 9/16 (0.5625) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
58
58
Tool:
DAC ETOH-AL.04
Description:
717-200 OPEN HOLE REFERENCE STANDARD. FIG. 1.20, PAGE 1. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
59
59
Tool:
DAC ETOH-FE-1/2
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Steel. 1/2 (0.500) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
60
60
Tool:
DAC ETOH-FE-1/4
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Steel. 1/4 (0.250) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
61
61
Tool:
DAC ETOH-FE-1/8
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Steel. 1/8 (0.125) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
62
62
Tool:
DAC ETOH-FE-11/16
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Steel. 11/16 (0.6875) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
63
63
Tool:
DAC ETOH-FE-3/16
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Steel. 3/16 (0.1875) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
64
64
Tool:
DAC ETOH-FE-3/4
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Steel. 3/4 (0.750) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
65
65
Tool:
DAC ETOH-FE-3/8
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Steel. 3/8 (0.375) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
66
66
Tool:
DAC ETOH-FE-5/16
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Steel. 5/16 (0.3125) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
67
67
Tool:
DAC ETOH-FE-5/8
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Steel. 5/8 (0.625) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
68
68
Tool:
DAC ETOH-FE-7/16
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Steel. 7/16 (0.4375) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
69
69
Tool:
DAC ETOH-FE-9/16
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Steel. 9/16 (0.5625) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
70
70
Tool:
DAC ETOH-FE.08
Description:
717-200 REFERENCE STANDARD...FIG. 1.9, PAGE 1. MATERIAL: 4340 STEEL PER MIL-S-5000. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
71
71
Tool:
DAC ETOH-IT-1/2
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Titanium. 1/2 (0.500) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
72
72
Tool:
DAC ETOH-IT-1/4
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Titanium. 1/4 (0.250) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
73
73
Tool:
DAC ETOH-IT-1/8
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Titanium. 1/8 (0.125) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
74
74
Tool:
DAC ETOH-IT-11/16
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Titanium. 11/16 (0.6875) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
75
75
Tool:
DAC ETOH-IT-3/16
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Titanium. 3/16 (0.1875) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
76
76
Tool:
DAC ETOH-IT-3/4
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Titanium. 3/4 (0.750) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
77
77
Tool:
DAC ETOH-IT-3/8
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Titanium. 3/8 (0.375) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
78
78
Tool:
DAC ETOH-IT-5/16
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Titanium. 5/16 (0.3125) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
79
79
Tool:
DAC ETOH-IT-5/8
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Titanium. 5/8 (0.625) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
80
80
Tool:
DAC ETOH-IT-7/16
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Titanium. 7/16 (0.4375) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
81
81
Tool:
DAC ETOH-IT-9/16
Description:
McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Titanium. 9/16 (0.5625) Inch Hole. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
82
82
Tool:
DAC GSET-AL
Description:
MCDONNELL DOUGLAS REFERENCE STANDARD 06-20-01 7075-T6
Location:
North America
Aircraft or Engine:
83
83
Tool:
DAC GSET-AL.01
Description:
MCDONNELL DOUGLAS REFERENCE STANDARD 06-20-01 FIG.1 SHEETS 1-3. MATERIAL: 7075-T6 ALUMINUM PER QQ-Q-250/12.
Location:
North America
Aircraft or Engine:
84
84
Tool:
DAC GSET-FE
Description:
MCDONNELL DOUGLAS REFERENCE STANDARD 06-20-01 4340
Location:
North America
Aircraft or Engine:
85
85
Tool:
DAC GSET-FE.01
Description:
MCDONNELL DOUGLAS REFERENCE STANDARD 06-20-01 FIG.1 SHEETS 1-3. MATERIAL: 4340 STEEL PER MIL-S-5000
Location:
North America
Aircraft or Engine:
86
86
Tool:
DAC GSET-MG
Description:
MCDONNELL DOUGLAS REFERENCE STANDARD 06-20-01 ALUMINUM BRONZE
Location:
North America
Aircraft or Engine:
87
87
Tool:
DAC GSET-SS.01
Description:
MCDONNELL DOUGLAS REFERENCE STANDARD 06-20-01 FIG.1 SHEETS 1-3. MATERIAL: 303SE CRES or 301 1/2 HARD CRES STEEL.
Location:
North America
Aircraft or Engine:
88
88
Tool:
DAC GSET-TI.01
Description:
MCDONNELL DOUGLAS REFERENCE STANDARD 06-20-01 FIG.1 SHEETS 1-3. MATERIAL: 6AL-4V TITANIUM PER AMS 491 or MIL-T-9046
Location:
North America
Aircraft or Engine:
89
89
Tool:
DAPT 09-0052-00
Description:
DOWTY AEROSPACE PROPELLERS PROBE GUIDE FIXTURE, SF340-61-A42
Location:
North America
Aircraft or Engine:
90
90
Tool:
DC-10 FIG603/15C
Description:
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 628B FIG.603 SHEET 15C
Location:
North America
Aircraft or Engine:
91
91
Tool:
DC-10 FIG603/15E/4340
Description:
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 CARBON STEEL, 54-10-11 PAGE 628D FIG.603 SHEET 15E
Location:
North America
Aircraft or Engine:
92
92
Tool:
DC-10 FIG603/15E/Ti
Description:
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 628D FIG.603 SHEET 15E
Location:
North America
Aircraft or Engine:
93
93
Tool:
DC-10 FIG603/15G
Description:
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 CARBON STEEL, 54-10-11 PAGE 628F FIG.603 SHEET 15G
Location:
North America
Aircraft or Engine:
94
94
Tool:
DC-10 FIG603/23
Description:
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 7075-T6 ALUMINUM, 54-10-11 PAGE 635 FIG.603 SHEET 23
Location:
North America
Aircraft or Engine:
95
95
Tool:
DC-10 FIG603/24-Al
Description:
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 636C FIG.603 SHEET 24
Location:
North America
Aircraft or Engine:
96
96
Tool:
DC-10 FIG603/24-Ti
Description:
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 636C FIG.603 SHEET 24
Location:
North America
Aircraft or Engine:
97
97
Tool:
DC-10 FIG603/25
Description:
DOUGLAS DC-10 WING CLEVIS REFERENCE STANDARD 6AL-6V or 6AL-4 TITANIUM, 54-10-11 PAGE 637 FIG.603 SHEET 25
Location:
North America
Aircraft or Engine:
98
98
Tool:
DC-10 FIG603/27Al
Description:
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 639 FIG.603 SHEET 27
Location:
North America
Aircraft or Engine:
99
99
Tool:
DC-10 FIG603/27Ti
Description:
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 639 FIG.603 SHEET 27
Location:
North America
Aircraft or Engine:
100
100
Tool:
DC-10 FIG603/28LOWER/Al
Description:
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 640 FIG.603 SHEET 28 (LOWER)
Location:
North America
Aircraft or Engine:
101
101
Tool:
DC-10 FIG603/28LOWERTi
Description:
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 640 FIG.603 SHEET 28 (LOWER)
Location:
North America
Aircraft or Engine:
102
102
Tool:
DC-10 FIG603/28UPPER/Al
Description:
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 640 FIG.603 SHEET 28 (UPPER)
Location:
North America
Aircraft or Engine:
103
103
Tool:
DC-10 FIG603/28UPPER/Ti
Description:
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 640 FIG.603 SHEET 28 (UPPER)
Location:
North America
Aircraft or Engine:
104
104
Tool:
DC-10 FIG603/28WEDGE
Description:
CUSTOM TRANSDUCER WEDGE 9 DEGREE INCIDENT ANGLE WITH A 1.80"RADIUS FOR BOTH UPPER AND LOWER ULTRASONIC SCANS, DC-10 54-10-11 FIGURE 603 SHEET 28 PAGE 640
Location:
North America
Aircraft or Engine:
105
105
Tool:
DC-10 FIG603/29Al
Description:
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 641 FIG.603 SHEET 29
Location:
North America
Aircraft or Engine:
106
106
Tool:
DC-10 FIG603/29Ti
Description:
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 641 FIG.603 SHEET 29
Location:
North America
Aircraft or Engine:
107
107
Tool:
DC-10 FIG603/30-AL
Description:
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 7075-T6 ALUMINUM, 54-10-11 PAGE 642 FIG.603 SHEET 30
Location:
North America
Aircraft or Engine:
108
108
Tool:
DC-10 FIG603/39-1
Description:
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4130 or 4340, 54-10-11 PAGE 651 FIG.603 SHEET 39, BOLT IDENTIFICATION 71658-7-35 #1
Location:
North America
Aircraft or Engine:
109
109
Tool:
DC-10 FIG603/39-2
Description:
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4130 or 4340, 54-10-11 PAGE 651 FIG.603 SHEET 39, BOLT IDENTIFICATION 71658-18-53 #2
Location:
North America
Aircraft or Engine:
110
110
Tool:
DC-10 FIG603/39-3
Description:
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4130 or 4340, 54-10-11 PAGE 651 FIG.603 SHEET 39, BOLT IDENTIFICATION 71658-18-53 #3
Location:
North America
Aircraft or Engine:
111
111
Tool:
DC-10 FIG603/39-4
Description:
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4130 or 4340, 54-10-11 PAGE 651 FIG.603 SHEET 39, BOLT IDENTIFICATION 71658-7-35 #4
Location:
North America
Aircraft or Engine:
112
112
Tool:
DC-10 FIG603/43
Description:
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 655 FIG.603 SHEET 43
Location:
North America
Aircraft or Engine:
113
113
Tool:
DC-10 FIG603/5
Description:
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 CARBON STEEL, 54-10-11 PAGE 617 FIG.603 SHEET 5
Location:
North America
Aircraft or Engine:
114
114
Tool:
DC-9/MD-80-1 FIG 21
Description:
Boeing DC-9/MD-80 Reference Standard Design (1- Assembly) Figure 21, Sheet 1-5 Page 31-35, 7-5. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
115
115
Tool:
DC3-1
Description:
DC-3 REFERENCE STANDARD ..SECTION 3 PAGE 2 FIGURE 1.1
Location:
North America
Aircraft or Engine:
116
116
Tool:
DHC 29116-001
Description:
deHAVILLAND DASH 8 LFEC CALIBRATION STANDARD. PART 6 53-30-31 PAGE 7 FIGURE 3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
117
117
Tool:
DHC 29117-001
Description:
deHAVILLAND DASH 8 LFEC CALIBRATION STANDARD. PART 6 53-10-21 PAGE 5 FIGURE 3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
118
118
Tool:
DLH-2
Description:
Polystyrene 12.7 mm(0.5 in.), Diameter = 14mm (0.551 in.), Length= 12.7 mm(0.5in.)
Location:
North America
Aircraft or Engine:
119
119
Tool:
DLT-10M
Description:
DELAY TIPS FOR 10mm(.394") DIAMETER DELAY TRANSDUCERS
Location:
North America
Aircraft or Engine:
120
120
Tool:
DLT-125
Description:
DELAY TIPS FOR .125" ARD SERIES TRANSDUCERS
Location:
North America
Aircraft or Engine:
121
121
Tool:
DLT-2MMR
Description:
CUSTOM DELAY TIPS 2MM" RADIUS FOR REPLACEABLE DELAY TRANSDUCERS.
Location:
North America
Aircraft or Engine:
122
122
Tool:
DLT.187-P
Description:
Persplex(Lucite) Delay Tip(Standoff) for MRD-1501-HR Transducer.
Location:
North America
Aircraft or Engine:
123
123
Tool:
DLT125-5
Description:
.50" LONG DELAY TIP FOR .125"Ø ARD SERIES TRANSDUCERS.
Location:
North America
Aircraft or Engine:
124
124
Tool:
DLT125-75
Description:
.750" LONG DELAY TIP FOR .125"Ø ARD SERIES TRANSDUCERS.
Location:
North America
Aircraft or Engine:
125
125
Tool:
DLT25
Description:
DELAY TIPS FOR .25" DIAMETER ARD SERIES DELAY TRANSDUCERS
Location:
North America
Aircraft or Engine:
126
126
Tool:
DLT25-1.0
Description:
1.0" LONG DELAY TIP FOR .25" DIAMETER ARD/ TRD SERIES DELAY TRANSDUCERS.
Location:
North America
Aircraft or Engine:
127
127
Tool:
DLT25-75
Description:
.750" LONG DELAY TIP FOR .25" DIAMETER ARD/ TRD SERIES DELAY TRANSDUCERS.
Location:
North America
Aircraft or Engine:
128
128
Tool:
DLT5-10
Description:
10 DEGREE ANGLE DELAY SHOE, 16.8mmØ
Location:
North America
Aircraft or Engine:
129
129
Tool:
DLT50
Description:
DELAY TIPS FOR .500" ARD SERIES DELAY TRANSDUCERS.
Location:
North America
Aircraft or Engine:
130
130
Tool:
DLT50-13M
Description:
DELAY TIPS FOR ARD-1050/13MM DIAMETER DELAY TRANSDUCERS.
Location:
North America
Aircraft or Engine:
131
131
Tool:
DRR-25
Description:
DELAY TIP
Location:
North America
Aircraft or Engine:
132
132
Tool:
DRT74469
Description:
ALUMINUM BLOCK 2024-T3 3/64" FLAT BOTTOM HOLE, 2.0"LX2.0"HX.375"W
Location:
North America
Aircraft or Engine:
133
133
Tool:
DRT90592G
Description:
DOWTY AEROSPACE PROPELLERS GUIDE FOR DRT90592
Location:
North America
Aircraft or Engine:
134
134
Tool:
E190 57-001
Description:
EMBRAER 190/195 REFERENCE STANDARD, 190:00335-99999 OR POST-MOD SB 190-57-0031/02. PART 6 57-50-00, FIGURE 1-SHEET 1&2.
Location:
North America
Aircraft or Engine:
135
135
Tool:
E53-002A
Description:
EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad Aluminum. Single Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .031"..Doubler = .040"..Filler = .031"..Stringer = .063"
Location:
North America
Aircraft or Engine:
136
136
Tool:
E53-002A.
Description:
EMBRAER 170/175 REFERENCE STANDARD PT 6 51-06-00 pages 7-10. Material: 2024-T3 Alclad Aluminum. Dual Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .031"..Doubler 1 = .040"..Doubler 2 = .063"..Filler = ....
Location:
North America
Aircraft or Engine:
137
137
Tool:
E53-002B
Description:
EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad Aluminum. Single Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .047"..Doubler = .050"..Filler = .047"..Stringer = .063"
Location:
North America
Aircraft or Engine:
138
138
Tool:
E53-002B.
Description:
EMBRAER 170/175 REFERENCE STANDARD PT 6 51-06-00 pages 7-10. Material: 2024-T3 Alclad Aluminum. Dual Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .047"..Doubler 1 = .050"..Doubler 2 = .063"..Filler = ....
Location:
North America
Aircraft or Engine:
139
139
Tool:
E53-002C
Description:
EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad Aluminum. Single Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .055"..Doubler = .063"..Filler = .055"..Stringer = .063"
Location:
North America
Aircraft or Engine:
140
140
Tool:
E53-002C.
Description:
EMBRAER 170/175 REFERENCE STANDARD PT 6 51-06-00 pages 7-10. Material: 2024-T3 Alclad Aluminum. Dual Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .055"..Doubler 1 = .063"..Doubler 2 = .063"..Filler = ....
Location:
North America
Aircraft or Engine:
141
141
Tool:
E53-002D
Description:
EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad Aluminum. Single Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .071"..Doubler = .080"..Filler = .071"..Stringer = .063"
Location:
North America
Aircraft or Engine:
142
142
Tool:
E53-002D.
Description:
EMBRAER 170/175 REFERENCE STANDARD PT 6 51-06-00 pages 7-10. Material: 2024-T3 Alclad Aluminum. Dual Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .071"..Doubler 1 = .080"..Doubler 2 = .063"..Filler = ....
Location:
North America
Aircraft or Engine:
143
143
Tool:
E53-002E
Description:
EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad Aluminum. Single Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .080"..Doubler = .098"..Filler = .080"..Stringer = .063"
Location:
North America
Aircraft or Engine:
144
144
Tool:
E53-002E.
Description:
EMBRAER 170/175 REFERENCE STANDARD PT 6 51-06-00 pages 7-10. Material: 2024-T3 Alclad Aluminum. Dual Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .080"..Doubler 1 = .098"..Doubler 2 = .063"..Filler = ....
Location:
North America
Aircraft or Engine:
145
145
Tool:
E53-002F
Description:
EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad Aluminum. Single Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .098"..Doubler = .110"..Filler = .098"..Stringer = .063"
Location:
North America
Aircraft or Engine:
146
146
Tool:
E53-002F.
Description:
EMBRAER 170/175 REFERENCE STANDARD PT 6 51-06-00 pages 7-10. Material: 2024-T3 Alclad Aluminum. Dual Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .098"..Doubler 1 = .110"..Doubler 2 = .063"..Filler = ....
Location:
North America
Aircraft or Engine:
147
147
Tool:
E53-003A
Description:
EMBRAER 170/175 REFERENCE STANDARD DUAL DOUBLER CONFIGURATION PT 6 53-06-00 pages 6-10 REV.1, Material: 2024-T3 Alclad. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
148
148
Tool:
E53-003B
Description:
EMBRAER 170/175 REFERENCE STANDARD DUAL DOUBLER CONFIGURATION PT 6 53-06-00 pages 6-10 REV.1, Material: 2024-T3 Alclad. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
149
149
Tool:
E53-003C
Description:
EMBRAER 170/175 REFERENCE STANDARD DUAL DOUBLER CONFIGURATION PT 6 53-06-00 pages 6-10 REV.1, Material: 2024-T3 Alclad. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
150
150
Tool:
E53-003D
Description:
EMBRAER 170/175 REFERENCE STANDARD DUAL DOUBLER CONFIGURATION PT 6 53-06-00 pages 6-10 REV.1, Material: 2024-T3 Alclad. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
151
151
Tool:
E53-003E
Description:
EMBRAER 170/175 REFERENCE STANDARD DUAL DOUBLER CONFIGURATION PT 6 53-06-00 pages 6-10 REV.1, Material: 2024-T3 Alclad. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
152
152
Tool:
E53-003F
Description:
EMBRAER 170/175 REFERENCE STANDARD DUAL DOUBLER CONFIGURATION PT 6 53-06-00 pages 6-10 REV.1, Material: 2024-T3 Alclad. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
153
153
Tool:
E53-004
Description:
EMBRAER 190/195 REFERENCE STANDARD PT 6 53-23-00 pages 1-13. Material: 2024-T3 Alclad Aluminum. Repair Doubler Configuration. Includes Test Report and Certificate of Conformance. Repair Doubler = .125" Fus Skin Thickness = .098" Filler = .098" In
Location:
North America
Aircraft or Engine:
154
154
Tool:
E54-003
Description:
EMBRAER 170/175 CALIBRATION STANDARD PT 4 54-50-00 Embraer 170 NDT 1967 Rev. 49, pages 11-13 and Embraer 175 NDT 5893 Rev. 25, pages 10-12. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
155
155
Tool:
EC SHIM SET
Description:
9 PIECE EDDY CURRENT SHIM THICKNESS SET. COLOR COATED THICKNESS RANGE FROM .0005"-.010
Location:
North America
Aircraft or Engine:
156
156
Tool:
ELT TEMPLATE-1
Description:
EDDY CURRENT CIRCLE TEMPLATE, 0.750"Ø. 3 HOLE SIZES: .749", .750",.751". MATERIAL: 2024-T351, 0.063"
Location:
North America
Aircraft or Engine:
157
157
Tool:
ELT TEMPLATE-2
Description:
EDDY CURRENT CIRCLE TEMPLATE, 0.201"Ø. 3 HOLE SIZES: .200", .201",.202". MATERIAL: 2024-T351, 0.063"
Location:
North America
Aircraft or Engine:
158
158
Tool:
ELT TEMPLATE-3
Description:
EDDY CURRENT CIRCLE TEMPLATE, SELECT RIVET SIZES. 12 HOLE SIZES: .125", .156",.187", .218", .250", .281", .312", .343", .375", .437", .500", .562". MATERIAL: 2024-T351, 0.063"
Location:
North America
Aircraft or Engine:
159
159
Tool:
EM145NDI540043A
Description:
EMBRAER REFERENCE STANDARD 54-50-00 PT 2 FIG 606
Location:
North America
Aircraft or Engine:
160
160
Tool:
EM145NDI540047A
Description:
EMBRAER REFERENCE STANDARD 54-50-00 PT 2 FIG 615
Location:
North America
Aircraft or Engine:
161
161
Tool:
EO13829.001/1
Description:
Aeronautical Engineers Australia Reference Standard Fig.2 Page 5 DOC NO: MMS13829.001/1 and REF EO: EO13829.001/1
Location:
North America
Aircraft or Engine:
162
162
Tool:
ET-55C-2
Description:
BOMBARDIER / CHALLENGER 604 10 STEP ALUMINUM WEDGE, ET-53-30-012 PT 6 FIG. 2 . STEP THICKNESSES:, .024", .028", .031", .035", .039", .044", .048", .052", .056" .059" +/-0.002, . PAD SIZE: 1.0" x 1.0" +/-0.010", Material: 2024-T3 ALUMINUM. Chromic ano
Location:
North America
Aircraft or Engine:
163
163
Tool:
ET-55C-3
Description:
BOMBARDIER / CHALLENGER 604 10 STEP ALUMINUM WEDGE, ET-53-30-012 PT 6 FIG. 2 . STEP THICKNESSES:, .024", .028", .031", .035", .039", .044", .048", .052", .056" .059" +/-0.002, . PAD SIZE: 1.0" x 1.0" +/-0.010", Material: 2124-T8 or 7075-T7 ALUMINUM.
Location:
North America
Aircraft or Engine:
164
164
Tool:
ET002
Description:
BRANTLY CALIBRATION STANDARD
Location:
North America
Aircraft or Engine:
165
165
Tool:
ET002
Description:
BRANTLY B2 MAIN ROTOR BLADE ROOT SKIN CALIBRATION STANDARD PG.2. MATERIAL: 2024-T3 ALUMINUM BARE & CLAD. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
166
166
Tool:
ET6018
Description:
CUSTOM SIKORSKY S61-N FLAT BOTTOM HOLE AFT REAR FUSELAGE REFERENCE STANDARD 51-10-05 FIGURE 7 (SHEETS 1-5). MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certiicate of Conformance.
Location:
North America
Aircraft or Engine:
167
167
Tool:
ETBS AL-1T/2024-T3 0.032
Description:
MD REFERENCE STANDARD ETFL PROCEDURE 5 06-10-02
Location:
North America
Aircraft or Engine:
168
168
Tool:
ETD2015-145-108529
Description:
CUSTOM EDDY CURRENT STANDARD, 2024-T351 ALUMINUM .063"/.050". MS20426AD5 CSK RIVET 2 PLACES
Location:
North America
Aircraft or Engine:
169
169
Tool:
F12-DEL-3C1N
Description:
REPAIR REFERENCE STANDARD GR/EP FIBERGLASS STEP DELAM DEFECT. ALL BOEING AIRCRAFT MODELS PART 1 51-01-01. Includes C-SCAN Certification and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
170
170
Tool:
F12-DIS-3C1N
Description:
REPAIR REFERENCE STANDARD GR/EP FIBERGLASS STEP DISBOND and CORE FIBERGLASS INTERFACE. ALL BOEING AIRCRAFT MODELS PART 1 51-01-01. Includes C-SCAN Certification and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
171
171
Tool:
F15-AL-UT-0 125
Description:
F15 REFERENCE STANDARD, 2124-T821, 1F-15A-36-2-65
Location:
North America
Aircraft or Engine:
172
172
Tool:
F15-AL-UT-0 175
Description:
F15 REFERENCE STANDARD, 2124-T821, 1F-15A-36-2-65
Location:
North America
Aircraft or Engine:
173
173
Tool:
F15-AL-UT-0 225
Description:
F15 REFERENCE STANDARD, 2124-T821, 1F-15A-36-2-65
Location:
North America
Aircraft or Engine:
174
174
Tool:
F15-AL-UT-0 275
Description:
F15 REFERENCE STANDARD, 2124-T821, 1F-15A-36-2-65
Location:
North America
Aircraft or Engine:
175
175
Tool:
F15-AL-UT-0.175-2
Description:
F15 REFERENCE STANDARD. MATERIAL: 2024-T3, OUTBOARD TORQUE BOX REAR SPAR, 68A115101, LOWER FLANGE FASTENER HOLES. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
176
176
Tool:
F15-TI-UT-.175
Description:
F15 REFERENCE STANDARD,6AL-4V 1F-15A-36
Location:
North America
Aircraft or Engine:
177
177
Tool:
F15-TI-UT-0.175
Description:
F15 REFERENCE STANDARD,6AL-4V
Location:
North America
Aircraft or Engine:
178
178
Tool:
FF171-5234
Description:
BOEING REFERENCE STANDARD. MATERIAL: 6AL-4V TITANIUM ROUND 2.50" DIAMETER O.D. / 1.125" DIAMETER I.D. EDM CORNER NOTCH: .030" x .030" +0.00/-0.002 WIDE
Location:
North America
Aircraft or Engine:
179
179
Tool:
Figure 4.E.-4
Description:
Honeywell Positioning Plate and Spacers, 32-49-01 page 4.E.-5. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
180
180
Tool:
FOKKER-50/60
Description:
FOKKER 50/60 CALIBRATION STANDARD PART 6 53-30-09 PAGE 6 FIGURE 3. MATERIAL: 2024-T3 ALUMINUM. NOTE: ***DOES NOT INCLUDE 3M BELLY PROTECTIVE TAPE 8641
Location:
North America
Aircraft or Engine:
181
181
Tool:
GSE 450
Description:
EMBRAER190/195 REFERENCE STANDARD PART 6 57-50-00 PAGE 5 FIGURE 1. Material: 6AL-4v Titanium. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
182
182
Tool:
GSE 503
Description:
EMBRAER 190/195 REFERENCE STANDARD PT 4 53-10-00 pages 1-12 Embraer 190-NDT 2824, 270-801-B. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
183
183
Tool:
GSE 503/171T17969-401
Description:
EMBRAER 170/175 REFERENCE STANDARD PT 6 53-10-00 pages 4-11. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
184
184
Tool:
GSE 506
Description:
EMBRAER 170/175/190/195 CALIBRATION STANDARD. PART NUMBER 171T17973-401. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
185
185
Tool:
HOLDER ASSEMBLY
Description:
DELRIN HOLDER ASSEMBLY
Location:
North America
Aircraft or Engine:
186
186
Tool:
Holding Block No.1
Description:
Honeywell Holding Block No.1, 32-49-01 page 4.E.-3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
187
187
Tool:
Holding Block No.2
Description:
Honeywell Holding Block No.2, 32-49-01 page 4.E.-4. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
188
188
Tool:
HOLDING FIXTURE
Description:
LEFT AND RIGHT REAR SPAR MOUNT TOOL MODIFICATION W/ 10 DRILLED HOLES
Location:
North America
Aircraft or Engine:
189
189
Tool:
Honeywell ET Standard
Description:
Honeywell Eddy Current Wheel Surface Standard. Material:2024-T6 Forged Aluminum. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
190
190
Tool:
KC10-7025-3 ASSEMBLY
Description:
CUSTOM MANUFACTURED BOEING REFERENCE STANDARD FOR ULTRASONIC INSPECTION 101/201
Location:
North America
Aircraft or Engine:
191
191
Tool:
KC10-7027
Description:
BOEING REFERENCE STANDARD KC10 FUEL COMPENSATOR CUTOUT-INSPECTION.( 301 GUIDE AND 302 GUIDE ARE PART OF INSPECTION AND SOLD SEPARATELY)
Location:
North America
Aircraft or Engine:
192
192
Tool:
KT56778
Description:
MESSIER-DOWTY REFERENCE STANDARD 631-32-181 2024-T3
Location:
North America
Aircraft or Engine:
193
193
Tool:
L00-MD-6
Description:
CABLE ADAPTER
Location:
North America
Aircraft or Engine:
194
194
Tool:
L72 BLOCK
Description:
British Aerospace test block. Material: 2024-T3 Aluminum .128: thick. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
195
195
Tool:
LINEAR MOUNT PLATE
Description:
BOEING CUSTOM PLATE
Location:
North America
Aircraft or Engine:
196
196
Tool:
Lucite Wedge 120P
Description:
Custom Lucite Wedge for Reference Standard 1. Material: Lucite/Cast Acrylic
Location:
North America
Aircraft or Engine:
197
197
Tool:
M346 SPAR 4 STD-1
Description:
CUSTOM REFERENCE STANDARD, H346 SPAR 4 STD-1 HOLE INTERFACE WITH FLAPS HINGE REWORK. MATERIAL: 7050-T7451 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
198
198
Tool:
MAB-CS
Description:
ROMPAS BLOCK, 7075-T6 or 7075-T73 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). Note:
Location:
North America
Aircraft or Engine:
199
199
Tool:
MB01-10
Description:
CABLE - BNC to Microdot 10' Feet Long. Includes Certificate of Conformance.
Location:
North America
Aircraft or Engine:
200
200
Tool:
MBBQCX35-2
Description:
Cast Acrylic transducer wedge with a 33 degree sound path, 3/8-32 thread 80mm(3.15") radius
Location:
North America
Aircraft or Engine:
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