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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:
354C
Description:
BOEING REFERENCE STANDARD 737 PT 6 57-30-04
Location:
North America
Aircraft or Engine:
2
2
Tool:
355A
Description:
BOEING REFERENCE STANDARD 737 PT 6 57-30-04
Location:
North America
Aircraft or Engine:
3
3
Tool:
355B
Description:
BOEING REFERENCE STANDARD 737 PT 6 57-30-04
Location:
North America
Aircraft or Engine:
4
4
Tool:
355C
Description:
BOEING REFERENCE STANDARD 737 PT 6 57-30-04
Location:
North America
Aircraft or Engine:
5
5
Tool:
356
Description:
BOEING REFERENCE STANDARD 737 53-30-04 PART 6 PAGE 4 FIGURE 1. Includes test report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
6
6
Tool:
363
Description:
BOEING REFERENCE STANDARD PART 6 53-30-03 FIGURE 1 PAGE 6. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
7
7
Tool:
365
Description:
BOEING REFERENCE STANDARD 737 PART 4 71-20-01 PG.4 FIGURE 1 DETAIL I. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
8
8
Tool:
365G
Description:
BOEING TRANSDUCER GUIDE 737 PART 4 71-20-01 PG.4 FIGURE 1 DETAIL II. Includes Certificate of Conformance.
Location:
North America
Aircraft or Engine:
9
9
Tool:
367
Description:
BOEING REFERENCE STANDARD 737 PT 6 71-20-01 Figure 4, PG. 10-12 (Sheets 1-3) Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
10
10
Tool:
369
Description:
BOEING REFERENCE STANDARD 727 Part 6 53-30-27 & 737 Part 6 53-30-05. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
11
11
Tool:
370
Description:
BOEING REFERENCE STANDARD 737 PT 4 53-30-02 FIG 1. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
12
12
Tool:
375
Description:
BOEING REFERENCE STANDARD 737 PT 4 55-10-02. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
13
13
Tool:
3765A96919-301
Description:
CONAIR EDDY CURRENT SURFACE REFERENECE STANDARD. DHC-8-Q400 FOR INSPECTION OF OUTSIDE FUSELAGE CTS. ALL ALUMINUM PARTS ALODINED. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
14
14
Tool:
3765A96919-303
Description:
CONAIR EDDY CURRENT SURFACE REFERENECE STANDARD. DHC-8-Q400 FOR INSPECTION OF OUTSIDE FUSELAGE CTS. ALL ALUMINUM PARTS ALODINED. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
15
15
Tool:
3765A96919-305
Description:
CONAIR EDDY CURRENT SURFACE REFERENECE STANDARD. DHC-8-Q400 FOR INSPECTION OF OUTSIDE FUSELAGE CTS. ALL ALUMINUM PARTS ALODINED. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
16
16
Tool:
378
Description:
BOEING REFERENCE STANDARD 737 PT 6 53-10-44 PAGE 5 FIGURE 2. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
17
17
Tool:
382-57-74 82-688
Description:
HERCULES CALIBRATION BLOCK 382-57-74 82-688
Location:
North America
Aircraft or Engine:
18
18
Tool:
383
Description:
BOEING REFERENCE STANDARD 737 PART 6 53-30-07 FIGURE 2 PAGE 7. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
19
19
Tool:
4004
Description:
BOEING REFERENCE STANDARD 747 PART 4 53-40-01 PAGE 10 FIGURE 6. Includes Test Report and Certificate of Confromance.
Location:
North America
Aircraft or Engine:
20
20
Tool:
401
Description:
BOEING REFERENCE STANDARD 747 PT 4 57-10-01 Page 4 Figure 1. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
21
21
Tool:
402
Description:
BOEING REFERENCE STANDARD 747 PT 4 57-10-04 Page 5 Figure 1. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
22
22
Tool:
4028
Description:
BOEING REFERENCE STANDARD 747 PART 4 57-40-03 FIGURE 3 PAGE 6.MATERIAL: 4340 STEEL. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
23
23
Tool:
4028G
Description:
BOEING TRANSDUCER GUIDE 747 57-40-03 FIGURE 2 PAGE 5. MATERIAL: LUCITE. Includes Certificate of Conformance.
Location:
North America
Aircraft or Engine:
24
24
Tool:
4028P
Description:
BOEING TRANSDUCER POSITIONER 747 57-40-03 FIGURE 1 PAGE 4A. MATERIAL: ALUMINUM. Includes Certificate of Conformance.
Location:
North America
Aircraft or Engine:
25
25
Tool:
4029
Description:
BOEING REFERENCE STANDARD 747 PART 4 55-50-01 FIGURE 1 PAGE 4.MATERIAL: 2024-T3 or 7075-T6 Aluminum. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
26
26
Tool:
403
Description:
BOEING REFERENCE STANDARD PT 4 57-10-04 FIG 2, PAGE 6. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
27
27
Tool:
4036
Description:
BOEING REFERENCE STANDARD 747 PART 4 57-40-05 FIGURE 3 PAGE 6.MATERIAL: 4340 STEEL. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
28
28
Tool:
4036G
Description:
BOEING TRANSDUCER GUIDE 747 PART 4 57-40-05 FIGURE 2 PAGE 4.MATERIAL: LUCITE ( CAST ACRYLIC ). Includes Certificate of Conformance.
Location:
North America
Aircraft or Engine:
29
29
Tool:
403A/403B
Description:
BOEING REFERENCE STANDARD 747 PT 4 57-10-04 Page 6 Figure 2. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
30
30
Tool:
404
Description:
BOEING 747 REFERENCE STANDARD PART 6 57-10-08 FIGURE 2 PAGE 5. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
31
31
Tool:
405
Description:
BOEING REFERENCE STANDARD 747 PT 4 57-10-02 Page 5 Figure 2. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
32
32
Tool:
4057
Description:
BOEING REFERENCE STANDARD 747 PT 6 53-30-03
Location:
North America
Aircraft or Engine:
33
33
Tool:
4059
Description:
BOEING 747 REFERENCE STANDARD PART 4 57-10-12 FIGURE 1 PAGE 5. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
34
34
Tool:
406
Description:
BOEING REFERENCE STANDARD 747 PT 6 57-10-09 Page 6 Figure 2. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
35
35
Tool:
4070
Description:
BOEING REFERENCE STANDARD 747, PT 6 53-30-07. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
36
36
Tool:
4072
Description:
BOEING REFERENCE STANDARD 747 PT 6 53-30-05. Material 2024-T3 Aluminum. Fasteners BACR15CE5D5, BACR15CE6D5. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
37
37
Tool:
4072C
Description:
BOEING OPTICAL CENTER 747 PT 6 53-30-05. Material Plexiglass. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
38
38
Tool:
408
Description:
BOEING REFERENCE STANDARD PT 4 57-10-03 FIG 2, PAGE 5. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
39
39
Tool:
410
Description:
BOEING REFERENCE STANDARD 747 PT 4 57-10-05 Page 6 Figure 3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
40
40
Tool:
411
Description:
BOEING REFERENCE STANDARD PT 6 55-10-04 FIG 1, PAGE 4. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
41
41
Tool:
412
Description:
BOEING REFERENCE STANDARD PT 6 55-10-01 FIG 1, PAGE 3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
42
42
Tool:
412B5MHZ35R41FE
Description:
CUSTOM 5MHz 35° TRANSVERSE WAVE TRANSDUCER WITH A 41mm (1.614") RADIUS WITH END MOUNT MICRODOT CONNECTOR. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
43
43
Tool:
412B5MHZ35R48FE
Description:
CUSTOM 5MHz 35° TRANSVERSE WAVE TRANSDUCER WITH A 48mm(1.890") RADIUS WITH END MOUNT MICRODOT CONNECTOR. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
44
44
Tool:
412B5MHZ35R80FE
Description:
CUSTOM 5MHz 35° TRANSVERSE WAVE TRANSDUCER WITH END MOUNT MICRODOT CONNECTOR WIT A 80mm RADIUS. USED WITH AIRBUS REFERENCE STANDARD PART NUMBER 98A54003096 Includes Test Report and Certificate of Conformance. REFERENCE: AIRBUS A300-600 PART 4 54-50-20
Location:
North America
Aircraft or Engine:
45
45
Tool:
412B5MHZ40R75FE
Description:
CUSTOM 5MHz 40° TRANSVERSE WAVE TRANSDUCER WITH END MOUNT MICRODOT CONNECTOR WIT A 75mm RADIUS. USED WITH AIRBUS REFERENCE STANDARD PART NUMBER 98A54003069 Includes Test Report and Certificate of Conformance. REFERENCE: AIRBUS A300-600 PART 4 54-50-20
Location:
North America
Aircraft or Engine:
46
46
Tool:
412B5MHZ45FE
Description:
CUSTOM 5MHz 45° TRANSVERSE WAVE TRANSDUCER WITH END MOUNT MICRODOT CONNECTOR. Includes Test Report and Certificate of Conformance. REFERENCE: AIRBUS A300-600 PART 4 54-50-15
Location:
North America
Aircraft or Engine:
47
47
Tool:
412E5MHZ60FE
Description:
CUSTOM 5MHz 60° IN FE TRANSVERSE WAVE BACKSHOOTING TRANSDUCER WITH A SIDE MOUNTED MICRODOT CONNECTOR. CASE SIZE: .690" x .354" x .354 Includes Test Report and Certificate of Conformance. REFERENCE STANDARD: 98A54003077
Location:
North America
Aircraft or Engine:
48
48
Tool:
423
Description:
BOEING 747 REFERENCE STANDARD PART 6 57-10-17 FIGURE 2 PAGE 8. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
49
49
Tool:
424
Description:
BOEING 747 REFERENCE STANDARD PART 6 57-10-17 FIGURE 3 PAGE 9. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
50
50
Tool:
426
Description:
BOEING REFERENCE STANDARD PT 4 55-10-01 FIG 1, PAGE 4. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
51
51
Tool:
431
Description:
BOEING REFERENCE STANDARD PT 6 53-10-19 FIG 1, PAGE 6. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
52
52
Tool:
432
Description:
BOEING REFERENCE STANDARD 747 PT 6 57-30-02 Page 4 Figure 1. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
53
53
Tool:
4340-3-0050
Description:
DC9 REFERENCE STANDARD S/B 57-118 SERVICE SKETCH 2671 SHEET 4 OF 7. MATERIAL: 4340 STEEL.
Location:
North America
Aircraft or Engine:
54
54
Tool:
435
Description:
BOEING 747 REFERENCE STANDARD PART 6 57-10-20 FIGURE 3 PAGE 7. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
55
55
Tool:
436
Description:
BOEING 747 REFERENCE STANDARD PART 6 57-10-20 FIGURE 4 PAGE 8. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
56
56
Tool:
437
Description:
BOEING REFERENCE STANDARD 747 53-10-01 PART 4 PAGE 11 FIGURE 2. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
57
57
Tool:
438
Description:
BOEING REFERENCE STANDARD 747 53-10-01 PART 4 PAGE 11 FIGURE 2. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
58
58
Tool:
439
Description:
BOEING 747 REFERENCE STANDARD PART 6 57-10-22 FIGURE 2 PAGE 5. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
59
59
Tool:
440
Description:
BOEING REFERENCE STANDARD 747 PT 4 57-10-11 Page 5 Figure 2. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
60
60
Tool:
441
Description:
BOEING REFERENCE STANDARD 747 PT 4 57-10-10 Page 9 Figure 2. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
61
61
Tool:
442
Description:
BOEING REFERENCE STANDARD PT 4 53-10-02 FIG 2, PAGE 5. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
62
62
Tool:
443
Description:
BOEING REFERENCE STANDARD PT 4 53-10-02 FIG 2, PAGE 5. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
63
63
Tool:
446
Description:
BOEING REFERENCE STANDARD 747 PT 4 57-10-13 Page 5 Figure 2. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
64
64
Tool:
447
Description:
BOEING REFERENCE STANDARD 747 PT 4 57-10-13 Page 5 Figure 2. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
65
65
Tool:
448
Description:
BOEING REFERENCE STANDARD 747 PT 4 57-10-13 Page 5 Figure 2. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
66
66
Tool:
449
Description:
BOEING REFERENCE STANDARD 747 PT 4 57-10-13 Page 5 Figure 2. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
67
67
Tool:
45-127-1
Description:
Custom Probe Locating Bushing Tool Figure 1 Page 6 Item #1. Material 2024-T3 Aluminum.
Location:
North America
Aircraft or Engine:
68
68
Tool:
45-127-2
Description:
Custom Probe Locating Bushing Tool Figure 1 Page 6 Item #2. Material 2024-T3 Aluminum.
Location:
North America
Aircraft or Engine:
69
69
Tool:
45-128
Description:
Custom 8 Hole Calibration Standard Test Coupon Assembly Figure 5 Page 10 to include the following Pieces. Figure 2 Page 7. Material .071" 2024-T3 Clad Aluminum, 7 EDM Flaws total. Figure 3 Page 8 .250" 4130or4340 Steel 0 EDM Flaws total and Figure 4...
Location:
North America
Aircraft or Engine:
70
70
Tool:
45-128-1
Description:
Custom 8 Hole Calibration Standard Test Coupon. Figure 1 Page 7. Material .071" 2024-T3 Clad Aluminum. 7 EDM Flaws total.
Location:
North America
Aircraft or Engine:
71
71
Tool:
45-128-2
Description:
Custom 8 Hole Calibration Standard Test Coupon. Figure 3 Page 8. Material .250" 4130/4340 Steel. 0 EDM Flaws total.
Location:
North America
Aircraft or Engine:
72
72
Tool:
45-128-3
Description:
Custom 8 Hole Calibration Standard Test Coupon. Figure 4 Page 9. Material .125" 2024-T3 Clad Aluminum. 0 EDM Flaws total.
Location:
North America
Aircraft or Engine:
73
73
Tool:
460
Description:
BOEING REFERENCE STANDARD 747 PART 6 57-10-28, PAGE 3 FIGURE 1. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
74
74
Tool:
471
Description:
BOEING REFERENCE STANDARD 747 PT 4 57-30-02 Page 4 Figure 1. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
75
75
Tool:
474
Description:
BOEING REFERENCE STANDARD PT 6 53-10-20 FIG 1, PAGE 5. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
76
76
Tool:
475
Description:
BOEING 747 REFERENCE STANDARD PART 6 57-10-27 FIGURE 1 PAGE 4. Material: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
77
77
Tool:
476
Description:
BOEING REFERENCE STANDARD PT 6 53-10-18 FIG 3, PAGE 6. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
78
78
Tool:
477
Description:
BOEING REFERENCE STANDARD PT 6 53-10-18 FIG 3, PAGE 6. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
79
79
Tool:
478
Description:
BOEING REFERENCE STANDARD PT 6 5-10-18 FIG 3 PAGE 6. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
80
80
Tool:
482
Description:
BOEING 747 REFERENCE STANDARD PART 6 55-10-08 FIGURE 3 PAGE 7. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
81
81
Tool:
483
Description:
BOEING 747 REFERENCE STANDARD PART 6 55-10-08 FIGURE 3 PAGE 7. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
82
82
Tool:
484
Description:
BOEING 747 REFERENCE STANDARD PART 6 55-10-25 FIGURE 1 PAGE 4. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
83
83
Tool:
490
Description:
BOEING REFERENCE STANDARD 747 PT 4 57-30-06 Page 5 Figure 2. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
84
84
Tool:
497
Description:
BOEING REFERENCE STANDARD 767 PT 6 53-00-05 FIG 1. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
85
85
Tool:
497C
Description:
BOEING PLEXIGLASS OPTICAL CENTER 767 PT 6 53-00-04 FIG 4
Location:
North America
Aircraft or Engine:
86
86
Tool:
497G
Description:
BOEING PLEXIGLASS PROBE HOLDER GUIDE 767 PT 6 53-00-04 FIG 3
Location:
North America
Aircraft or Engine:
87
87
Tool:
497P
Description:
BOEING PLEXIGLASS PROBE HOLDER 767 PT 6 53-00-04 FIG 2
Location:
North America
Aircraft or Engine:
88
88
Tool:
506
Description:
BOEING REFERENCE STANDARD 757 PT 4 57-40-01 FIG 3 Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
89
89
Tool:
5290020-4
Description:
Cessna Model 401/402 Calibration Standard Figure 4 part 2 & 3 Inspection. Plate A - 7075-T6 Aluminum and Plate B - 2024-T3 Aluminum.
Location:
North America
Aircraft or Engine:
90
90
Tool:
53-10-110A
Description:
Raytheon 125 Series Calibration Standard. Material: 4340 Cres Steel. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
91
91
Tool:
53-10-126/1
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 53-10-0126/1 PT 6 FIGURE 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
92
92
Tool:
53-10-130/158/1
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 53-10-01 PT 6 FIGURES 5&6 PAGES 10&11. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
93
93
Tool:
53-10-137
Description:
BAE 146-RJ SERIES REFERENCE STANDARD SET OF 8 UNITS, 53-10-12 PT 6 FIGURE 7 PAGES 907-910. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
94
94
Tool:
53-10-153/155/175/193/194/1
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 53-10-08 PT 6 FIGURES 5&6 PAGES 9&10. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
95
95
Tool:
53-10-153/155/175/194/1
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 53-10-06 PT 6 FIGURES 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
96
96
Tool:
53-10-189/1
Description:
BAE 146-RJ SERIES PROBE GUIDE 53-10-15 PT 6 PAGES 1&2. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
97
97
Tool:
53-10-192/1
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 53-10-25 PT 6 FIGURES 6&7 PAGES 10&11. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
98
98
Tool:
53-20-104/1
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 53-00-86 PT 6 FIGURES 7&8 PAGES 14&15. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
99
99
Tool:
53-20-140A/1
Description:
BAE REFERENCE STANDARD 146 SERIES / AVRO-RJ SERIES PART 4 53-20-26 PG 10 FIG 5. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
100
100
Tool:
53-20-140A/2
Description:
BAE REFERENCE STANDARD 146 SERIES / AVRO-RJ SERIES PART 4 53-20-26 PG 10 FIG 5. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
101
101
Tool:
53-20-145/1
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 53-20-03 PT 6 FIGURE 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
102
102
Tool:
53-20-148/1
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 53-20-01 PT 6 FIGURES 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
103
103
Tool:
53-20-149/1
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 53-20-65 PT 6 FIGURE 11&12 PAGES 16&17. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
104
104
Tool:
53-20-155/1/1
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 53-10-36 PT 6 FIGURES 7&8 PAGES 13&14. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
105
105
Tool:
53-20-155/1/2
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 53-10-36 PT 6 FIGURES 9&10 PAGES 15&16. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
106
106
Tool:
53-20-155/1/3
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 53-10-36 PT 6 FIGURES 11&12 PAGES 17&18. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
107
107
Tool:
53-20-155/1/4
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 53-10-36 PT 6 FIGURES 13&14 PAGES 19&20. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
108
108
Tool:
53-20-157/2
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 53-20-84 PT 6 FIGURE 8 PAGE 12. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
109
109
Tool:
53-20-165
Description:
BAE 146 BRITISH AIRCRAFT PT 4 53-20-14, 2024-T6
Location:
North America
Aircraft or Engine:
110
110
Tool:
53-20-165/2
Description:
RADIUSED ULTRASONIC PROBE SHOE USED WITH K5K AND REFERENCE STANDARD 53-20-165/1 (BAe 146 Series)
Location:
North America
Aircraft or Engine:
111
111
Tool:
53-20-167/1
Description:
BAE REFERENCE STANDARD 146-RJ 53-238 53-20-21 PT 4 FIGURE 4 PAGE 519. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
112
112
Tool:
53-20-167/2
Description:
BAE PROBE RADIUSED SHOE, 146-RJ 53-238 53-20-21 PT 4 FIGURE 4&5 PAGE 519 & 512. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
113
113
Tool:
53-20-169/1
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 53-20-21 PT 4 FIGURE 3 PAGES 505. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
114
114
Tool:
53-20-169/2
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 53-20-21 PT 4 FIGURE 3 PAGES 505. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
115
115
Tool:
53-20-171/1
Description:
BAE REFERENCE STANDARD 146 SERIES / AVRO-RJ SERIES PART 4 53-20-21 PG 512 FIG 5. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
116
116
Tool:
53-20-171/2
Description:
RADIUSED ULTRASONIC PROBE SHOE USED WITH K5K(AFC-525-7S) AND REFERENCE STANDARD 53-20-165/1 (BAe 146 Series). Includes Certificate of Conformance.
Location:
North America
Aircraft or Engine:
117
117
Tool:
53-20-179/2
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 53-30-14 PT 6 FIGURE 5&6 PAGES 10&11. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
118
118
Tool:
53-20-180/3
Description:
BAE REFERENCE STANDARD 146-RJ 53-20-88 FIG 4&5, PAGES 8&9. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
119
119
Tool:
53-30-126/1
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 53-30-02 PT 6 FIGURE 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
120
120
Tool:
53-30-131/1
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 53-30-01 PT 6 FIGURE 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
121
121
Tool:
53-30-174/177/179/1
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 53-30-03 PT 6 FIGURE 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
122
122
Tool:
53-30-174/177/179/2
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 53-30-04 PT 6 FIGURE 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
123
123
Tool:
53-40-125/1
Description:
BAE REFERENCE STANDARD 146-RJ 53-238 53-40-06 PT 6 FIGURE 5&6 PAGES 9&10. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
124
124
Tool:
53-41-04-991-002-A
Description:
Airbus Reference standard 53-41-04-991-002-A Sheet 01 part 6 page 11. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
125
125
Tool:
55-31-105/1
Description:
BAE REFERENCE STANDARD 146 SERIES / AVRO-RJ SERIES PART 4 55-31-42 PG 7 FIG 3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
126
126
Tool:
55-31-109/2
Description:
BAE REFERENCE STANDARD 146 SERIES / AVRO-RJ SERIES PART 4 55-31-43 PG 8 FIG 4. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
127
127
Tool:
55-31-NDT 1
Description:
BAE REFERENCE STANDARD 146-RJ 53-238 55-20-11 PT 6 FIGURE 5 PAGE 9. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
128
128
Tool:
55-33-101/1
Description:
BAE REFERENCE STANDARD 146 SERIES / AVRO-RJ SERIES PART 4 55-33-10 PG 7/8 FIG 3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
129
129
Tool:
55-33-101/2
Description:
BAE REFERENCE STANDARD 146 SERIES / AVRO-RJ SERIES PART 4 55-33-10 PG 7/8 FIG 3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
130
130
Tool:
55-33-101/3
Description:
BAE REFERENCE STANDARD 146 SERIES / AVRO-RJ SERIES PART 4 55-33-10 PG 7/8 FIG 3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
131
131
Tool:
57-10-035/044/1
Description:
BAE JETSTREAM SERIES 4100 57-10-36 PT 6
Location:
North America
Aircraft or Engine:
132
132
Tool:
57-10-102/1
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 57-10-12 PT 4 FIGURE 6&7 PAGES 11&12. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
133
133
Tool:
57-10-102/2
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 57-10-12 PT 4 FIGURE 6&7 PAGES 11&12. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
134
134
Tool:
57-10-107/1
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 57-10-52 PT 6 FIGURE 5&6 PAGES 11&12. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
135
135
Tool:
57-10-107/2
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 57-10-52 PT 6 FIGURE 6&7 PAGES 12&13. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
136
136
Tool:
57-10-111/1
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 57-10-55 PT 6 FIGURE 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
137
137
Tool:
57-10-111/2
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 57-10-55 PT 4 FIGURE 5&6 PAGES 8&9. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
138
138
Tool:
57-10-117/1
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 57-10-50 PT 6 FIGURE 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
139
139
Tool:
57-10-117/2
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 57-10-48 PT 6 FIGURE 3&4 PAGES 7&8. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
140
140
Tool:
57-10-119/1
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 57-10-42 PT 6 FIGURES 4&5 PAGE 7&8. Material: 7075-T6 & 2014A-T6 Aluminum. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
141
141
Tool:
57-20-148A/1
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 57-20-24 PT 6 FIGURES 5&6 PAGE 9&10. Material: 2024-T3 & 2024-T6 Aluminum. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
142
142
Tool:
57-20-163/1
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 57-20-28 PT 6 FIGURES 4&5 PAGE 9&10. Material: 2024-T3 & 2024-T6 Aluminum. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
143
143
Tool:
57-20-179/1
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 57-20-10 PT 4 FIGURES 4 PAGE 8. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
144
144
Tool:
57-54-103C
Description:
CUSTOM BOEING REFERENCE STANDARD 7075-T6 ALUMINUM
Location:
North America
Aircraft or Engine:
145
145
Tool:
57-54-103C-POS
Description:
CUSTOM TRANSDUCER POSITIONER FOR 57-54-103C REFERENCE STANDARD
Location:
North America
Aircraft or Engine:
146
146
Tool:
602
Description:
BOEING REFERENCE STANDARD 767 PT 4 32-10-01 FIG 2 Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
147
147
Tool:
603
Description:
BOEING REFERENCE STANDARD 767 PT 4 55-10-01 FIG 1. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
148
148
Tool:
604A
Description:
BOEING REFERENCE STANDARD 767 PT 6 53-60-01 FIG 1
Location:
North America
Aircraft or Engine:
149
149
Tool:
604B
Description:
BOEING REFERENCE STANDARD 767 PT 6 53-60-01 FIG 1
Location:
North America
Aircraft or Engine:
150
150
Tool:
605
Description:
BOEING REFERENCE STANDARD 767 PT 6 22-10-01 FIG 2. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
151
151
Tool:
605A
Description:
BOEING REFERENCE STANDARD 767 PT 6 22-10-01
Location:
North America
Aircraft or Engine:
152
152
Tool:
6061 AL BLOCK
Description:
Aluminum Block 110mm(3.937") x 18mm(7.09") x 15mm(.591") Block. Material: 6061-T6 Aluminum. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
153
153
Tool:
608
Description:
BOEING REFERENCE STANDARD 767 PT 4 27-80-01 FIG 4 Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
154
154
Tool:
608P1
Description:
TRANSDUCER WEDGE
Location:
North America
Aircraft or Engine:
155
155
Tool:
608P2
Description:
TRANSDUCER WEDGE
Location:
North America
Aircraft or Engine:
156
156
Tool:
610
Description:
BOEING REFERENCE STANDARD 767 PT 4 32-20-01 FIG 2. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
157
157
Tool:
6583103-1
Description:
Cessna Model 500 Calibration Standard 53-30-03-0 Rev. 14 Figure 4 Sheet 1 Inspection. Material: 2024-T3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
158
158
Tool:
6AL-6V-2SN-Ti
Description:
EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" +/-.001 DEEP, (MAX WIDTH .005"), 6AL-6V-2SNTi
Location:
North America
Aircraft or Engine:
159
159
Tool:
71658-10-42
Description:
DOUGLAS DC-10 HORIZONTAL STABILIZER REFERENCE STANDARD 4130 or 4340 STEEL, SB A55-17 PAGE 21 FIG.1(SHEET 3) BOLT IDENTIFICATION 71658-10-42 (5/8" X 4.1")
Location:
North America
Aircraft or Engine:
160
160
Tool:
71658-10-46
Description:
DOUGLAS DC-10 HORIZONTAL STABILIZER REFERENCE STANDARD 4130 or 4340 STEEL, SB A55-17 PAGE 21 FIG.1(SHEET 3) BOLT IDENTIFICATION 71658-10-46 (5/8" X 4.4")
Location:
North America
Aircraft or Engine:
161
161
Tool:
71658-14-45
Description:
DOUGLAS DC-10 HORIZONTAL STABILIZER REFERENCE STANDARD 4130 or 4340 STEEL, SB A55-17 PAGE 21 FIG.1(SHEET 3) BOLT IDENTIFICATION 71658-14-45 (7/8" X 4.8")
Location:
North America
Aircraft or Engine:
162
162
Tool:
71658-14-50
Description:
DOUGLAS DC-10 HORIZONTAL STABILIZER REFERENCE STANDARD 4130 or 4340 STEEL, SB A55-17 PAGE 21 FIG.1(SHEET 3) BOLT IDENTIFICATION 71658-14-50 (7/8" X 5.1")
Location:
North America
Aircraft or Engine:
163
163
Tool:
71658-16-55
Description:
DOUGLAS DC-10 HORIZONTAL STABILIZER REFERENCE STANDARD 4130 or 4340 STEEL, SB A55-17 PAGE 21 FIG.1(SHEET 3) BOLT IDENTIFICATION 71658-16-55 (1.0" X 6.0")
Location:
North America
Aircraft or Engine:
164
164
Tool:
71658-18-53/2&3
Description:
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 CARBON STEEL, 54-10-11 PAGE 651 FIG.603 SHEET 39
Location:
North America
Aircraft or Engine:
165
165
Tool:
71658-18-59
Description:
DOUGLAS DC-10 HORIZONTAL STABILIZER REFERENCE STANDARD 4130 or 4340 STEEL, SB A55-17 PAGE 21 FIG.1(SHEET 3) BOLT IDENTIFICATION 71658-8-59 (1 1/8" X 6.25")
Location:
North America
Aircraft or Engine:
166
166
Tool:
71658-18-64
Description:
DOUGLAS DC-10 HORIZONTAL STABILIZER REFERENCE STANDARD 4130 or 4340 STEEL, SB A55-17 PAGE 21 FIG.1(SHEET 3) BOLT IDENTIFICATION 71658-18-64 (1 1/8" X 6.5")
Location:
North America
Aircraft or Engine:
167
167
Tool:
71658-20-68
Description:
DOUGLAS DC-10 HORIZONTAL STABILIZER REFERENCE STANDARD 4130 or 4340 STEEL, SB A55-17 PAGE 21 FIG.1(SHEET 3) BOLT IDENTIFICATION 71658-20-68 (1 1/4" X 7.0")
Location:
North America
Aircraft or Engine:
168
168
Tool:
71658-7-35/1&4
Description:
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 CARBON STEEL, 54-10-11 PAGE 651 FIG.603 SHEET 39
Location:
North America
Aircraft or Engine:
169
169
Tool:
717RS1
Description:
717-200 REFERENCE STANDARD ISOLATOR LUG. FIG. 1.1 SHEET 1, PAGE 1. MATERIAL: 4340 NORMALIZED STEEL PER MIL-S-5000. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
170
170
Tool:
717RS10-C
Description:
717-200 REFERENCE STANDARD FOR THE LOWER CENTER WING SKIN PANELS AT STRINGER 16 &18. PAGES 1-11. MATERIAL: 2024-T3, 7075-T6 &7075-T7 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
171
171
Tool:
717RS12
Description:
717-200 REFERENCE STANDARD...FIG. 1.16 SHEET 1-5, PAGES 1-5. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
172
172
Tool:
717RS15
Description:
717-200 REFERENCE STANDARD...FIG. 1.4 SHEET 1-4, PAGES 1-4. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
173
173
Tool:
717RS20
Description:
717-200 REFERENCE STANDARD...FIG. 1.21 SHEET 1-3, PAGES 1-3. MATERIAL: 2014-T6 and 7075-T7 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
174
174
Tool:
717RS23
Description:
717-200 REFERENCE STANDARD...FIG. 1.8 SHEET 1-5, PAGES 1-5. MATERIAL: 2024-T3 and 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
175
175
Tool:
717RS2A
Description:
717-200 REFERENCE STANDARD...FIG. 1.12 SHEET 1-4, PAGES 1-4. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
176
176
Tool:
717RS2B
Description:
717-200 REFERENCE STANDARD...FIG. 1.13 SHEET 1-4, PAGES 1-4. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
177
177
Tool:
717RS2C
Description:
717-200 REFERENCE STANDARD...FIG. 1.14 SHEET 1-4, PAGES 1-4. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
178
178
Tool:
717RS2D
Description:
717-200 REFERENCE STANDARD...FIG. 1.15 SHEET 1-4, PAGES 1-4. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
179
179
Tool:
717RS4
Description:
717-200 REFERENCE STANDARD FIGURE 1.17 SHEETS (1-4 ), PAGES 1-4. MATERIAL: 2024-T3 and 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
180
180
Tool:
717RS7
Description:
717-200 REFERENCE STANDARD...FIG. 1.22 SHEET 1-7, PAGES 1-7. MATERIAL: 2024-T3 and 7075-T7 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
181
181
Tool:
717RS8
Description:
717-200 REFERENCE STANDARD...FIG. 1.23 SHEET 1-6, PAGES 1-3. MATERIAL: 2024-T3 and 7075-T7 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
182
182
Tool:
717RS9
Description:
BOEING 717-200 REFERENCE STANDARD FIGURE 1.24. MATERIAL: 6AL-4V. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
183
183
Tool:
717RST5
Description:
717-200 REFERENCE STANDARD...FIG. 1.18 SHEET 1-3, PAGES 1-3. MATERIAL: 2024-T3 and 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
184
184
Tool:
717RST6
Description:
717-200 REFERENCE STANDARD...FIG. 1.19 SHEET 1-3, PAGES 1-3. MATERIAL: 2024-T3 and 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
185
185
Tool:
7637987-17
Description:
A53-142 Douglas DC-9 Probe Holding Fixture and alignment 2024-T3 Clad Aluminum. Figure 1, Sheet 4
Location:
North America
Aircraft or Engine:
186
186
Tool:
7637987-19
Description:
CUSTOM SPO-2664 SLIDING PROBE FIXTURE USED WITH DC-10 REFERENCE STANDARD 7637987-15 Includes Certificate of Conformance
Location:
North America
Aircraft or Engine:
187
187
Tool:
7637987-9
Description:
A53-142 Douglas DC-9 7637987-9 Reference Standard Assembly 2024-T3 Clad Aluminum. Figure 1, Sheets 2&3
Location:
North America
Aircraft or Engine:
188
188
Tool:
7947479-10
Description:
Air Force General Purpose Eddy Current Standard. Standard is a three (3) plate assembly measuring 4" x 7" x 1.06". Contains twenty (20) fastener holes with diameters from 0.156 to 0.750", two (2) screw holes, and two (2) dowel pins holes. Standard also co
Location:
North America
Aircraft or Engine:
189
189
Tool:
7947479-10 I
Description:
Air Force General Purpose Eddy Current Standard. Standard is a three (3) plate assembly measuring 4" x 7" x 1.06". Contains twenty (20) fastener holes with diameters from 0.156 to 0.750", two (2) screw holes, and two (2) dowel pins holes. Standard also co
Location:
North America
Aircraft or Engine:
190
190
Tool:
7947479-10 S
Description:
Air Force General Purpose Eddy Current Standard. Standard is a three (3) plate assembly measuring 4" x 7" x 1.06". Contains twenty (20) fastener holes with diameters from 0.156 to 0.750", two (2) screw holes, and two (2) dowel pins holes. Standard also co
Location:
North America
Aircraft or Engine:
191
191
Tool:
7947479-10 Ti
Description:
Air Force General Purpose Eddy Current Standard. Standard is a three (3) plate assembly measuring 4" x 7" x 1.06". Contains twenty (20) fastener holes with diameters from 0.156 to 0.750", two (2) screw holes, and two (2) dowel pins holes. Standard also co
Location:
North America
Aircraft or Engine:
192
192
Tool:
7947479-10/17-4PH
Description:
Air Force General Purpose Eddy Current Standard. Standard is a three (3) plate assembly measuring 4" x 7" x 1.06". Contains twenty (20) fastener holes with diameters from 0.156 to 0.750", two (2) screw holes, and two (2) dowel pins holes. Standard also co
Location:
North America
Aircraft or Engine:
193
193
Tool:
7947479-10/304SS
Description:
Air Force General Purpose Eddy Current Standard. Standard is a three (3) plate assembly measuring 4" x 7" x 1.06". Contains twenty (20) fastener holes with diameters from 0.156 to 0.750", two (2) screw holes, and two (2) dowel pins holes. Standard also co
Location:
North America
Aircraft or Engine:
194
194
Tool:
80RS10
Description:
MD-80 REFERENCE STANDARD SECTION 2-1 FIGURE13
Location:
North America
Aircraft or Engine:
195
195
Tool:
80RS11
Description:
MD-80 REFERENCE STANDARD 57.80.007
Location:
North America
Aircraft or Engine:
196
196
Tool:
80RS12
Description:
MD-80 REFERENCE STANDARD
Location:
North America
Aircraft or Engine:
197
197
Tool:
80RS13
Description:
MD-80 REFERENCE STANDARD 57.80.012
Location:
North America
Aircraft or Engine:
198
198
Tool:
80RS14
Description:
717-200 REFERENCE STANDARD...FIG. 1.6 SHEET 1-4, PAGES 1-4. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
199
199
Tool:
80RS16
Description:
MD-80 REFERENCE STANDARD
Location:
North America
Aircraft or Engine:
200
200
Tool:
80RS18
Description:
717-200 REFERENCE STANDARD...FIG. 1.5 SHEET 1-5, PAGES 1-5. MATERIAL: 7075-T6 CLAD ALUMINUM, 2014-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.53.80.003
Location:
North America
Aircraft or Engine:
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