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Recent Tool List: 2025-08-20 13:31:28
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Click on a Tool # or Description below to find the item you are interested in.
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20 Aug 2025
Tool Number
Tool Description
Location
Aircraft
or
Engine
1
1
Tool:
001U532A5100000
Description:
DORNIER 328/328 JET SE.4.48A CALIBRATION STANDARD Part 4 53-21-23 Page 11 Figure 407 Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
2
2
Tool:
019
Description:
BOEING REFERENCE STANDARD 7075-T6 ALUMINUM 7075 57-10-07 PART 6 PG.216.
Location:
North America
Aircraft or Engine:
3
3
Tool:
038
Description:
BOEING 707 REFERENCE STANDARD 2024-T3 ALUMINUM DETAIL 1 FIGURE 8 SHEET 7 BBL 70.5 SPLICE 707-300/400..PART 6, 57-30-07 PG.71
Location:
North America
Aircraft or Engine:
4
4
Tool:
039
Description:
BOEING 707 REFERENCE STANDARD 2024-T3 ALUMINUM DETAIL 3 FIGURE 8 SHEET 9 BBL 70.5 SPLICE 707-300/400..PART 6, 57-30-07 PG.73
Location:
North America
Aircraft or Engine:
5
5
Tool:
1/N-02-384
Description:
Nomad Series N22 & N24 Reference Standard. for the inspection of Wing Strut Upper Fittings, Figure 27 Page 51. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
6
6
Tool:
10-0109-00
Description:
AIRBUS REFERENCE STANDARD 51-63-01 PT 6 FIG 601, INCONEL 718, 3 EDM SLOTS (0.2mm, 0.5mm,1.0mm DEEP) x (0.05-0.25mm WIDE). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
7
7
Tool:
1002
Description:
BOEING REFERENCE STANDARD PT 6 51-00-00 Part 6 FIG 4. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
8
8
Tool:
1003
Description:
BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 14 and 51-00-06. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
9
9
Tool:
1004
Description:
BOEING REFERENCE STANDARD PT 6 51-00-0 FIG 14 PARAGRAPPH 2.C. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
10
10
Tool:
1005
Description:
BOEING REFERENCE STANDARD PT 6 51-00-00 and 51-00-06, MATERIAL: 6AL-4V TITANIUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
11
11
Tool:
10212-0501A
Description:
Reference Standard Document: 0798-10212-1000 Material: 2024-T3 or 7075-T6. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
12
12
Tool:
10212-0501B
Description:
Reference Standard Document: 0798-10212-1000 Material: 2024-T3 or 7075-T6. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
13
13
Tool:
10212-0501C
Description:
Reference Standard Document: 0798-10212-1000 Material: 2024-T3 or 7075-T6. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
14
14
Tool:
10212-0501D
Description:
Reference Standard Document: 0798-10212-1000 Material: 2024-T3 or 7075-T6. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
15
15
Tool:
10212-0501E
Description:
Reference Standard Document: 0798-10212-1000 Material: 2024-T3 or 7075-T6. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
16
16
Tool:
10212-0501F
Description:
Reference Standard Document: 0798-10212-1000 Material: 2024-T3 or 7075-T6. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
17
17
Tool:
10212-0501G
Description:
Reference Standard Document: 0798-10212-1000 Material: 2024-T3 or 7075-T6. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
18
18
Tool:
10212-0501H
Description:
Reference Standard Document: 0798-10212-1000 Material: 2024-T3 or 7075-T6. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
19
19
Tool:
10212-0501J
Description:
Reference Standard Document: 0798-10212-1000 Material: 2024-T3 or 7075-T6. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
20
20
Tool:
10212-0501K
Description:
Reference Standard Document: 0798-10212-1000 Material: 2024-T3 or 7075-T6. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
21
21
Tool:
10212-0501L
Description:
Reference Standard Document: 0798-10212-1000 Material: 2024-T3 or 7075-T6. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
22
22
Tool:
10RS-52-2-MLG-FTG-AF
Description:
MD-10 REFERENCE STANDARD FIGURE 1.3, SHEET 1&2. MATERIAL: 7075 ALUMINUM. Includes Test Report and Certificate of Conformance. MDC-99K1082
Location:
North America
Aircraft or Engine:
23
23
Tool:
10RS.01.1
Description:
BOEING REFERENCE STANDARD KC10 Page 1-6 MATERIAL: 2024-T3, 7075-T6, 6AL-4V. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
24
24
Tool:
10RS.02
Description:
BOEING REFERENCE STANDARD KC10 53.10.001, 53.10.013/.014 Page 1-8 Material: 2024-T3 and 7075-T6, 6AL-4V or Phenolic. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
25
25
Tool:
10RS.05
Description:
DC-10 REFERENCE STANDARD 53.10.025, 53.10.028, 53.10.030. Page 1-5. Material: 2024-T3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
26
26
Tool:
10RS.08
Description:
DC-10 REFERENCE STANDARD 55.10.003/.004 Page 1-12. Material: 7075-T6 and 6AL-4V. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
27
27
Tool:
10RS.10.1
Description:
DC-10 REFERENCE STANDARD 55.10.005/.006 Page 1-3. Material: 7075-T7. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
28
28
Tool:
10RS.15a
Description:
DC-10 SID REFERENCE STANDARD DETAILS -3,-5 & -7 PAGE 1-6. MATERIAL: 7075-T6 ALUMNIUM. Includes Certification Report and COC.
Location:
North America
Aircraft or Engine:
29
29
Tool:
10RS.15b
Description:
DC-10 SID REFERENCE STANDARD DETAILS -3,-5, & -5, -501 ASSEMBLY PAGE 1-6. MATERIAL: 7075-T6 ALUMNIUM. Includes Certification Report and COC.
Location:
North America
Aircraft or Engine:
30
30
Tool:
10RS.15c
Description:
DC-10 SID REFERENCE STANDARD DETAILS -7, -9 & -11, -503 ASSWMBLY PAGE 1-6. MATERIAL: 7075-T6 ALUMNIUM. Includes Certification Report and COC.
Location:
North America
Aircraft or Engine:
31
31
Tool:
10RS.17
Description:
DC-10 SID REFERENCE STANDARD DETAIL -3 & -5 PAGE 2-3. MATERIAL: 2024-T3 ALUMNIUM. Includes Certification Report and COC.
Location:
North America
Aircraft or Engine:
32
32
Tool:
10RS.17.1
Description:
DC-10 SID REFERENCE STANDARD DETAIL -3 & -5 PAGE 2-3. MATERIAL: 2024-T3 ALUMNIUM. Includes Certification Report and COC.
Location:
North America
Aircraft or Engine:
33
33
Tool:
10RS.21
Description:
DC-10 REFERENCE STANDARD DETAIL -1 PAGE 1. MATERIAL: 718 INCONEL. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
34
34
Tool:
10RS.22a
Description:
DC-10 REFERENCE STANDARD 54-10-029/.030 Page 1-2. Material: 6AL-4V. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
35
35
Tool:
10RS.23
Description:
DC-10 SID REFERENCE STANDARD 54.10.029/.030. DETAIL -1 SHEET 1 PAGE 1. MATERIAL: 6AL-4V TITANIUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
36
36
Tool:
10RS.25a
Description:
DC-10 SID REFERENCE STANDARD 57.10.029/.030. DETAIL -3 PAGE 1. MATERIAL: 7075-T7 ALUMNIUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
37
37
Tool:
10RS.25b
Description:
DC-10 SID REFERENCE STANDARD DETAIL -1 PAGE 1. MATERIAL: 7075-T7 ALUMNIUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
38
38
Tool:
10RS.25c
Description:
DC-10 SID REFERENCE STANDARD DETAIL -5 PAGE 1. MATERIAL: 7075-T7 ALUMNIUM. includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
39
39
Tool:
10RS.26.1bM
Description:
DOUGLAS DC-10 REFERENCE STANDARD 54.10.031/.032 PAGES 1-8 (SHEET1-8). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
40
40
Tool:
10RS.27b
Description:
DC-10 SID REFERENCE STANDARD DETAILS -7,-9 & -11 PAGE 1-6. MATERIAL: 7075-T6 ALUMNIUM. Includes Certification Report and COC.
Location:
North America
Aircraft or Engine:
41
41
Tool:
10RS.32
Description:
DC-10 REFERENCE STANDARD 54-10-027 Page 1-2. Material: 6AL-4V. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
42
42
Tool:
10RS.33a
Description:
DC-10 REFERENCE STANDARD 54-10-027 Page 1-2. Material: 6AL-4V. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
43
43
Tool:
10RS.33b
Description:
DC-10 REFERENCE STANDARD 54-10-027 Page 1-2. Material: 6AL-4V. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
44
44
Tool:
10RS.35
Description:
DC-10 REFERENCE STANDARD, SHEETS 1-4, PAGES 1-4. MATERIAL: 6AL-4V TITNIUM. Includes Test Report and Certificate of Conformance. 54.10.027
Location:
North America
Aircraft or Engine:
45
45
Tool:
10RS.36a
Description:
DC-10 REFERENCE STANDARD DETAIL RA11005-12-1, SHEET 1 PAGE 1&2. MATERIAL: 4130 STEEL. Includes Test Report and Certificate of Conformance. 54.10.027
Location:
North America
Aircraft or Engine:
46
46
Tool:
10RS.36aN
Description:
DC-10 REFERENCE STANDARD DETAIL RA11005-12-1, SHEET 1 PAGE 1&2. MATERIAL: 4130 STEEL. Includes Test Report and Certificate of Conformance. 54.10.027
Location:
North America
Aircraft or Engine:
47
47
Tool:
10RS.36b
Description:
DC-10 REFERENCE STANDARD DETAIL RA11005-12-2, SHEET 1 PAGE 1&2. MATERIAL: 4130 STEEL. Includes Test Report and Certificate of Conformance. 54.10.027
Location:
North America
Aircraft or Engine:
48
48
Tool:
10RS.36bN
Description:
DC-10 REFERENCE STANDARD DETAIL RA11005-12-2, SHEET 1 PAGE 1&2. MATERIAL: 4130 STEEL. Includes Test Report and Certificate of Conformance. 54.10.027.
Location:
North America
Aircraft or Engine:
49
49
Tool:
10RS.39.1
Description:
DC-10 SID REFERENCE STANDARD DETAIL -1, -3 & -5 PAGE 1-5. MATERIAL: 7075-T6 ALUMNIUM. Includes Certification Report and COC.
Location:
North America
Aircraft or Engine:
50
50
Tool:
10RS.43
Description:
DC-10 REFERENCE STANDARD PAGE 1. MATERIAL: 6AL-4V TITANIUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
51
51
Tool:
10RS.48
Description:
BOEING REFERENCE STANDARD - KC10. Page 1-23. Material: 2024-T3, 7075-T6, and 7150-T6. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
52
52
Tool:
10RS.50
Description:
DOUGLAS DC-10 REFERENCE STANDARD 54.10.031/.032 PAGES 1-5 (SHEET1-5). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
53
53
Tool:
10RS.51-MLG-FTG-FF
Description:
MD-10 REFERENCE STANDARD FIGURE 1.1, SHEET 1&2. MATERIAL: 7075 ALUMINUM. Includes Test Report and Certificate of Conformance. MDC-99K1082
Location:
North America
Aircraft or Engine:
54
54
Tool:
10RS.52-1-MLG-FTG-AF
Description:
MD-10 REFERENCE STANDARD FIGURE 1.2, SHEET 1&2. MATERIAL: 7075 ALUMINUM. INCLUDES 10RS.53-1 MLGF BUSHG and HLDR. Includes Test Report and Certificate of Conformance. MDC-99K1082
Location:
North America
Aircraft or Engine:
55
55
Tool:
10RS.53-1-MLG-FTG-CC-UPR
Description:
MD-10 REFERENCE STANDARD FIGURE 1.4, SHEET 1&2. MATERIAL: 7075 ALUMINUM. INCLUDES 10RS.53-1 MLGF BUSHG and HLDR. Includes Test Report and Certificate of Conformance. MDC-99K1082
Location:
North America
Aircraft or Engine:
56
56
Tool:
10RS.53-2-MLG-FTG-AA
Description:
MD-10 REFERENCE STANDARD FIGURE 1.5, SHEET 1&2. MATERIAL: 7075 ALUMINUM. INCLUDES 10RS.53-1 MLGF BUSHG and HLDR. Includes Test Report and Certificate of Conformance. MDC-99K1082
Location:
North America
Aircraft or Engine:
57
57
Tool:
10RS.53-3-MLG-FTG-DD
Description:
MD-10 REFERENCE STANDARD FIGURE 1.6, SHEET 1&2. MATERIAL: 7075 ALUMINUM. INCLUDES 10RS.53-1 MLGF BUSHG and HLDR. Includes Test Report and Certificate of Conformance. MDC-99K1082
Location:
North America
Aircraft or Engine:
58
58
Tool:
10RS.55-1
Description:
BOEING KC10 ET REFERENCE STANDARD. INCLUDES: -3 SKIN, -53 TEAR STRAP, -63 SHEAR CLIP. Includes Test Report Traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
59
59
Tool:
10RS.55-3
Description:
BOEING KC10 ET REFERENCE STANDARD. INCLUDES: -3 SKIN, -53 TEAR STRAP, -163 SHEAR CLIP. Includes Test Report Traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
60
60
Tool:
10RS.55-5
Description:
BOEING KC10 ET REFERENCE STANDARD. INCLUDES: -3 SKIN, -53 TEAR STRAP, -363 SHEAR CLIP. Includes Test Report Traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
61
61
Tool:
10RS.55-7
Description:
BOEING KC10 ET REFERENCE STANDARD. INCLUDES: -103 SKIN, -53 TEAR STRAP, -563 SHEAR CLIP. Includes Test Report Traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
62
62
Tool:
10RS.bN
Description:
DC-10 REFERENCE STANDARD DETAIL RA11005-12-2, SHEET 1 PAGE 1&2. MATERIAL: 4130 STEEL. Includes Test Report and Certificate of Conformance. 54.10.027
Location:
North America
Aircraft or Engine:
63
63
Tool:
123
Description:
BOEING TRANSDUCER POSITIONER FIXTURE 737 PT 4 52-10-01
Location:
North America
Aircraft or Engine:
64
64
Tool:
125
Description:
BOEING REFERENCE STANDARD 767 PT 6 -51-00-05 FIG 2 PAGE 6 & 737 pART 6 51-00-00 FIGURE 2 PAGE 6 DETAIL II. HOLE SIZES: 0.1875, 0.250, 0.3125, 0.375, 0.4375, 0.500. Material: 4130 or 4340 Cres Steel. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
65
65
Tool:
126
Description:
BOEING REFERENCE STANDARD PT 6 51-00-01 FIG 4. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
66
66
Tool:
127-0.032
Description:
BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
67
67
Tool:
127-0.036
Description:
BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
68
68
Tool:
127-0.040
Description:
BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
69
69
Tool:
127-0.050
Description:
BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
70
70
Tool:
127-0.063
Description:
BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
71
71
Tool:
127-0.071
Description:
BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
72
72
Tool:
127-0.080
Description:
BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
73
73
Tool:
127-0.090
Description:
BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
74
74
Tool:
127-0.100
Description:
BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
75
75
Tool:
127-0.110
Description:
BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
76
76
Tool:
127-0.125
Description:
BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
77
77
Tool:
127A-.032
Description:
BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
78
78
Tool:
127A-.036
Description:
BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
79
79
Tool:
127A-.040
Description:
BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
80
80
Tool:
127A-.050
Description:
BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
81
81
Tool:
127A-.063
Description:
BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
82
82
Tool:
127A-.072
Description:
BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
83
83
Tool:
127A-.080
Description:
BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
84
84
Tool:
127A-.090
Description:
BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
85
85
Tool:
127A-.100
Description:
BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
86
86
Tool:
127A-.110
Description:
BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
87
87
Tool:
127A-.125
Description:
BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
88
88
Tool:
128
Description:
BOEING REFERENCE STANDARD 767 PT 6 51-00-06 PAGE 4 FIGURE 1, MATERIAL: Aluminum Alloy. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
89
89
Tool:
130A
Description:
BOEING THICKNESS STANDARD FOR X-BAND RADOMES DETAIL IV 737 PT 6 53-50-00. MATERIAL: LUCITE. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
90
90
Tool:
130B
Description:
BOEING THICKNESS STANDARD FOR C-BAND RADOMES DETAIL V 737 PT 6 53-50-00. MATERIAL: LUCITE. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
91
91
Tool:
130C
Description:
BOEING REFERENCE STANDARD Part 6 53-50-00 Page 13 Figure 1. Material: Aluminum. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
92
92
Tool:
134
Description:
Boeing Reference Standard 707 Part 4 53-40-07 Page 12 Figure 2 (Sheet 6) Detail 3. Material: 4330M or Equivalent. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
93
93
Tool:
145-15998-001
Description:
EMBRAER REFERENCE STANDARD 54-50-00 FIG 603, 4340 STEEL
Location:
North America
Aircraft or Engine:
94
94
Tool:
145-44131-001
Description:
EMBRAER REFERENCE STANDARD 57-26-00 PT 2 FIG 601, Aluminum(7050-T745) Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
95
95
Tool:
145-44131-003
Description:
EMBRAER REFERENCE STANDARD 57-26-00 PT 2 FIG 601, Steel(15-SPH 5/8") Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
96
96
Tool:
145-44131-005
Description:
EMBRAER REFERENCE STANDARD 57-26-00 PT 2 FIG 601, Titanium(Titanium Galy US AMS2631 CLAI 1/2") Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
97
97
Tool:
145-54-0008
Description:
EMBRAER REFERENCE STANDARD 54-50-00 FIG 606, 4340 STEEL
Location:
North America
Aircraft or Engine:
98
98
Tool:
145T09065-401
Description:
EMBRAER LEGACY REFERENCE STANDARD. GSE 606 54-00-00 Page 8&9. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
99
99
Tool:
17-4PH BLOCK
Description:
17-4 PH Steel Block 110mm(3.937") x 18mm(7.09") x 15mm(.591") Block. Material: 17-4PH Steel. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
100
100
Tool:
171-00844-601 16E1
Description:
EMBRAER REFERENCE STANDARD 7075-T7 ALUMINUM.Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
101
101
Tool:
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:
102
102
Tool:
171T17973-401
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:
103
103
Tool:
17P9M2007
Description:
Douglas Reference Standard Assembly For the Ultrasonic Calibration of Upper Wing Skin to common Stringer, Figure24-4 sheets 253. Material: 7075 Aluminum. Includes Test Report Traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
104
104
Tool:
181
Description:
BOEING REFERENCE STANDARD 707 PART 6 55-10-07 PAGE 5. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
105
105
Tool:
182
Description:
BOEING REFERENCE STANDARD 707 PART 6 55-10-07 PAGE 17. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
106
106
Tool:
185
Description:
BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 13 & 777-200/300 51-00-04 PROCEDURE 1 PAGE 8. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
107
107
Tool:
186A
Description:
BOEING REFERENCE STANDARD 777 PT 6 51-00-02 Figures 1&2, Pages 6-7, HOLE SIZE 0.1875. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
108
108
Tool:
186ABCDEF
Description:
BOEING CUSTOM COMBINATION REFERENCE STANDARD 777 PT 6 51-00-02 Figures 1&2, Pages 6-7, HOLE SIZE 0.1875", .2500", .3125", .3750", .4375", .500. Each hole size marked with the corresponding Boeing Part number 186A-186F Includes Test Report and Certific...
Location:
North America
Aircraft or Engine:
109
109
Tool:
186B
Description:
BOEING REFERENCE STANDARD 777 PT 6 51-00-02 Figures 1&2, Pages 6-7, HOLE SIZE 0.2500. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
110
110
Tool:
186C
Description:
BOEING REFERENCE STANDARD 777 PT 6 51-00-02 Figures 1&2, Pages 6-7, HOLE SIZE 0.3125. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
111
111
Tool:
186D
Description:
BOEING REFERENCE STANDARD 777 PT 6 51-00-02 Figures 1&2, Pages 6-7, HOLE SIZE 0.3750. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
112
112
Tool:
186E
Description:
BOEING REFERENCE STANDARD 777 PT 6 51-00-02 Figures 1&2, Pages 6-7, HOLE SIZE 0.4375. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
113
113
Tool:
186F
Description:
BOEING REFERENCE STANDARD 777 PT 6 51-00-02 Figures 1&2, Pages 6-7, HOLE SIZE 0.5000. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
114
114
Tool:
188A
Description:
BOEING REFERENCE STANDARD PT 651-00-00-1 FIG 6. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
115
115
Tool:
189
Description:
BOEING REFERENCE STANDARD PT 6 51-00-01 FIG 4 PG.13 & 737 PT 6 51-00-00 PROCEDURE 23 PG.11 FIG.7. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
116
116
Tool:
192
Description:
BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 13. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
117
117
Tool:
194
Description:
BOEING REFERENCE STANDARD 737 PT 6 53-30-00 FIGURE 1., BOEING 757 PART 6 53-30-02 PAGE 5 FIGURE 2
Location:
North America
Aircraft or Engine:
118
118
Tool:
194A
Description:
BOEING REFERENCE STANDARD 767 PT 6 53-30-02 FIG 3 PAGE 5. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
119
119
Tool:
1TD1133D07001-2001
Description:
Seyer Industries reference standard. Material: 2024-T351 Aluminum...Chamfer EDM Notch Size: .030" x .030" x .005" +/- .002"...Bore EDM Notch Size: .030" x .030" x .005" +/- .002". Includes Test Report and Certificate of Conformance. Part Serial Number:...
Location:
North America
Aircraft or Engine:
120
120
Tool:
2-164-501
Description:
AIRBUS EDDY CURRENT CALIBRATION BLOCK 4340 STEEL, 51-10-00-250-801 and 51-63-991-001 PAGE 601 FIGURE 601. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
121
121
Tool:
2-164-551
Description:
AIRBUS CALIBRATION STANDARD, A350-A-51-90-01-01001-040A-A-NDT & 51-63-01-991-001-A PT 6 FIG 601, 2024-T351 ALUMINUM. 3 EDM SLOTS (0.2mm, 0.5mm,1.0mm DEEP) x (0.05-0.25mm WIDE). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
122
122
Tool:
2-835-01-9301
Description:
AIRBUS CALIBRATION BLOCK, STAINLESS STEEL, 0.2mm, 0.5mm, 1mm EDM SLOTS. PART 6: 51-63-01 page 601 figure 601
Location:
North America
Aircraft or Engine:
123
123
Tool:
2-835-01-9330
Description:
AIRBUS CALIBRATION BLOCK, 6AL-4v TITANIUM, 0.2mm, 0.5mm, 1mm EDM SLOTS. PART 6: 51-63-01 page 601 figure 601
Location:
North America
Aircraft or Engine:
124
124
Tool:
2-835-01-9331
Description:
AIRBUS CALIBRATION BLOCK. MATERIAL: 304 Stainless Steel, 0.2mm, 0.5mm, 1mm EDM SLOTS. PART 6: 51-63-01 page 601 figure 601 Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
125
125
Tool:
2-887-01-9313S
Description:
SPLITTED CONICAL CALIBRATION STANDARD IN 2024-T351 ALUMINUM TYPE SCCS3-7, A318 51-63-07. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
126
126
Tool:
2-887-01-9314S
Description:
SPLITTED CONICAL CALIBRATION STANDARD IN 2024-T251 ALUMINUM ..TYPE SCCS7-14, A318 51-63-07. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
127
127
Tool:
2-887-01-9315S
Description:
SPLITTED CONICAL CALIBRATION STANDARD IN 2024-T351 ALUMINUM ..TYPE SCCS14-21 , A318 51-63-06-PB1. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
128
128
Tool:
2-887-01-9316S
Description:
SPLITTED CONICAL CALIBRATION STANDARD IN 2024-T351 ALUMINUM ..TYPE SCCS21-28, A318 51-63-07. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
129
129
Tool:
2-887-01-9319S
Description:
SPLITTED CONICAL CALIBRATION STANDARD IN 6AL-4V Titanium TYPE SCCS3-7, A318/A319/A320/A321 51-63-06-991-002A. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
130
130
Tool:
2-887-01-9321S
Description:
SPLITTED CONICAL CALIBRATION STANDARD IN 6AL-4V Titanium..TYPE SCCS3-7, A318 51-63-07-991-002A. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
131
131
Tool:
2-887-01-9323S
Description:
SPLITTED CONICAL CALIBRATION STANDARD IN 6AL-4V Titanium..TYPE SCCS3-7, A318 51-63-07-991-002A. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
132
132
Tool:
2-887-01-9325S
Description:
SPLITTED CONICAL CALIBRATION STANDARD IN 6AL-4V Titanium..TYPE SCCS3-7, A318 51-63-07-991-002A. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
133
133
Tool:
2006
Description:
BOEING REFERENCE STANDARD 727 PART 6 57-10-27 FASTENER (BACB30NM7K19). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
134
134
Tool:
204-94034-1
Description:
Boeing Reference Standard- Lower Lug APE-1 Primary , D204-12769-6 ASIP Inspection Program. Material: 4340 Steel. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
135
135
Tool:
206
Description:
BOEING REFERENCE STANDARD 727 PT 6 57-10-27 FIG 19. MATERIAL 2024 ALUMINUM (FASTENERS: BACR15DG10DD14)Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
136
136
Tool:
208
Description:
BOEING REFERENCE STANDARD 727 PT 6 57-10-27 FIG 19. MATERIAL 2024 ALUMINUM (FASTENERS: BACB30PT5-10, BACN10TN5)Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
137
137
Tool:
208 FRONT SPAR
Description:
CESSNA / TEXTRON AVIATION EDDY CURRENT REFERENCE STANDARD 208 FRONT SPAR LOWER CAP. Drawing NO. 2683201
Location:
North America
Aircraft or Engine:
138
138
Tool:
208 REAR SPAR
Description:
CESSNA / TEXTRON AVIATION EDDY CURRENT REFERENCE STANDARD 208 REAR SPAR LOWER CAP. Drawing NO. 2683202
Location:
North America
Aircraft or Engine:
139
139
Tool:
212-A1325-01
Description:
AIRBUS MILITARY REFERENCE STANDARD COM 212-266 PG 13
Location:
North America
Aircraft or Engine:
140
140
Tool:
235502
Description:
CASA CN-235 EDDY CURRENT REFERENCE STANDARD PART 5 57-10-05 PAGE 510 FIGURE 504b. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
141
141
Tool:
239
Description:
BOEING REFERENCE STANDARD 727 PT 6 57-10-27 FIG 18. MATERIAL 2024 ALUMINUM (FASTENERS: BACR15DG10DD)Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
142
142
Tool:
240
Description:
BOEING REFERENCE STANDARD 727 PT 6 57-10-27 FIG 18. MATERIAL 2024 ALUMINUM (FASTENERS: BACR15DG10DD)Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
143
143
Tool:
2506F
Description:
S/B 57-200 Douglas DC-9 Reference Standard 7075-T6 Aluminum. Figure 5, 6,7
Location:
North America
Aircraft or Engine:
144
144
Tool:
262
Description:
BOEING REFERENCE STANDARD 727 PT 6 53-10-27
Location:
North America
Aircraft or Engine:
145
145
Tool:
262A
Description:
BOEING REFERENCE STANDARD 727 PT 6 53-10-27
Location:
North America
Aircraft or Engine:
146
146
Tool:
263
Description:
BOEING REFERENCE STANDARD 727 PT 6 53-10-27 PAGE 4 FIG 1. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
147
147
Tool:
2683301-1
Description:
Cessna reference standard 55-10-02-0 (Rev 1).Model 208 Inspection of Horizontal Stabilizer Spars.
Location:
North America
Aircraft or Engine:
148
148
Tool:
27-1-6033
Description:
Fokker 50/60 calibration standard Part 6 53-40-05 pages 7&8 figure 4&5. Material 2024-T3 Aluminum.
Location:
North America
Aircraft or Engine:
149
149
Tool:
27-95031-001
Description:
Fairchild METRO 23, Model SA227-CC, METRO 23, Model SA227-DC,Reference standard for inspection of the MLG and NLG Yoke Assembly. Material: 2024-T351 Aluminum. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
150
150
Tool:
272
Description:
BOEING REFERENCE STANDARD 727, PT 6 55-10-27 FIG. 2 Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
151
151
Tool:
272
Description:
Boeing Reference Standard, 727 PT 6 55-10-27 PROCEDURE 2 Figure 1 (Sheets 1- 2) Pages 4- 5. Material: 7075-T6 Aluminum and AL-NI Bronze Bushing Per AMS 4640. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
152
152
Tool:
28-0-6049
Description:
Fokker 70/100 Calibration Standard, Part 6 53-10-18 Page 12 Figure 8. Material: 2024-T351 Aluminum. Paint with Primer. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
153
153
Tool:
285
Description:
BOEING REFERENCE STANDARD 727 PART 6 57-10-27 FASTENER (BACB30NM7K23). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
154
154
Tool:
286
Description:
BOEING REFERENCE STANDARD 727 PART 6 57-10-27 FASTENER (BACB30NM7K21). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
155
155
Tool:
296
Description:
BOEING REFERENCE STANDARD 727 PT 6 53-30-27 Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
156
156
Tool:
29A028
Description:
AIRBUS REFERENCE STANDARD 51-63-01 PT 6 FIG 601. MATERIAL: 4340 STEEL. 3 EDM SLOTS (0.2mm, 0.5mm,1.0mm DEEP) x (0.05-0.25mm WIDE). Includes Test Report and Certificate of Conformance.....
Location:
North America
Aircraft or Engine:
157
157
Tool:
29A029
Description:
AIRBUS CALIBRATION STANDARD, A350-A-51-90-01-01001-040A-A-NDT & 51-63-01-991-001-A PT 6 FIG 601, 2024-T351 ALUMINUM. 3 EDM SLOTS (0.2mm, 0.5mm,1.0mm DEEP) x (0.05-0.25mm WIDE). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
158
158
Tool:
29A029YS
Description:
AIRBUS CALIBRATION STANDARD, A318/A319/A320/A321 51-63-01-991-001-A PB 1 FIG 60 & A350-A-51-90-01-01001-040A-A-NDT 1, 2024-T351 ALUMINUM. 3 EDM SLOTS (0.2mm, 0.5mm,1.0mm DEEP) x 0.13mm(.0051") WIDE. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
159
159
Tool:
29A032
Description:
AIRBUS REFERENCE STANDARD 51-63-01 PT 6 FIG 601, MATERIAL: 6AL-4V TITANIUM, 3 EDM SLOTS (0.2mm, 0.5mm,1.0mm DEEP) x (0.05-0.25mm WIDE). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
160
160
Tool:
29A047
Description:
AIRBUS REFERENCE STANDARD 51-63-01 PT 6 FIG 601, Aluminum(7075-T7)(39.5% IACS) 3 EDM SLOTS (0.2mm, 0.5mm,1.0mm DEEP) x (0.05-0.25mm WIDE). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
161
161
Tool:
29A049
Description:
AIRBUS CALIBRATION STANDARD, A350-A-51-90-01-01001-040A-A-NDT & 51-63-01-991-001-A PT 6 FIG 601, 304 stainless steel.. 3 EDM SLOTS (0.2mm, 0.5mm,1.0mm DEEP) x (0.05-0.25mm WIDE). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
162
162
Tool:
29A120
Description:
AIRBUS REFERENCE STANDARD 51-63-01 PT 6 FIG 601, MAGNESIUM. 3 EDM SLOTS (0.2mm, 0.5mm,1.0mm DEEP) x (0.05-0.25mm WIDE). Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
163
163
Tool:
3-1251
Description:
NOSE WHEEL BEAD SEAT WHEELL PROBE FOR BOEING 707
Location:
North America
Aircraft or Engine:
164
164
Tool:
301 GUIDE
Description:
BOEING REFERENCE STANDARD GUIDE PLATE KC10 FUEL COMPENSATOR CUTOUT-INSPECTION
Location:
North America
Aircraft or Engine:
165
165
Tool:
301SS
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: 301 STAINLESS . SIZE: 1.5"W x 3.75"L x .25"
Location:
North America
Aircraft or Engine:
166
166
Tool:
302 GUIDE
Description:
BOEING REFERENCE STANDARD GUIDE PLATE KC10 FUEL COMPENSATOR CUTOUT-INSPECTION
Location:
North America
Aircraft or Engine:
167
167
Tool:
305
Description:
BOEING REFERENCE STANDARD 737 PART 6 57-10-18 FIGURE 2 PAGE 6. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
168
168
Tool:
312
Description:
BOEING REFERENCE STANDARD 737 PART 6 53-10-17 PAGE 6 FIGURE 2. 2024-T3 ALUMINUM Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
169
169
Tool:
313A/313B
Description:
BOEING REFERENCE STANDARD 737 PART 6 53-10-17 PAGE 7 FIGURE 3. 2024-T3 ALUMINUM
Location:
North America
Aircraft or Engine:
170
170
Tool:
315
Description:
BOEING REFERENCE STANDARD 737 PART 4 55-30-01 FIGURE 1 PAGE 4. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
171
171
Tool:
316
Description:
BOEING REFERENCE STANDARD 737 PART 4 55-30-01 FIGURE 2 PAGE 5. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
172
172
Tool:
31A008
Description:
AIRBUS REFERENCE STANDARD 51-63-01 PT 6 FIG 601. MATERIAL: 4340 STEEL. 3 EDM SLOTS (0.2mm, 0.5mm,1.0mm DEEP) x (0.05-0.25mm WIDE). Includes Test Report and Certificate of Conformance...
Location:
North America
Aircraft or Engine:
173
173
Tool:
320
Description:
BOEING REFERENCE STANDARD 737 PART 6 55-10-19 FIGURE 2 PAGE 5. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
174
174
Tool:
321
Description:
BOEING REFERENCE STANDARD 737 PART 6 53-10-19 FIGURE 3 PAGE 6. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
175
175
Tool:
323A
Description:
BOEING REFERENCE STANDARD 737 PART 4 55-50-01 FIGURE 1 PAGE 5. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
176
176
Tool:
323B
Description:
BOEING REFERENCE STANDARD 737 PART 4 53-10-38 FIGURE 2 PAGE 6. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
177
177
Tool:
323P
Description:
BOEING ULTRASONIC TRANSDUCER SHOE 737 PART 4 53-10-38 FIGURE 3 PAGE 7. Includes Certificate of Conformance.
Location:
North America
Aircraft or Engine:
178
178
Tool:
326
Description:
BOEING REFERENCE STANDARD 737 PART 6 53-10-28 FIGURE 1 PAGE 4. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
179
179
Tool:
328A/328B
Description:
BOEING REFERENCE STANDARD 737 PART 6 53-10-38 FIGURE 2 PAGE 7.
Location:
North America
Aircraft or Engine:
180
180
Tool:
328C/328D
Description:
BOEING REFERENCE STANDARD 737 PART 6 53-10-38 FIGURE 3 PAGE 8.
Location:
North America
Aircraft or Engine:
181
181
Tool:
3320A96900-301
Description:
CONAIR EDDY CURRENT SURFACE REFERENECE STANDARD. EDM Notches: .008", .020", .040" ( .004" W ± .001"), . MATERIAL 7075-T6 ALUMINUM. SIZE: 1.5"W x 3.00"L x .25" ± .005". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
182
182
Tool:
3320A96900-303
Description:
CONAIR EDDY CURRENT SURFACE REFERENECE STANDARD. EDM Notches: .008", .020", .040" ( .004" W ± .001"), . MATERIAL 7050-T7451 ALUMINUM. SIZE: 1.5"W x 3.00"L x .25" ± .005". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
183
183
Tool:
3320A96900-305
Description:
CONAIR EDDY CURRENT SURFACE REFERENECE STANDARD. EDM Notches: .008", .020", .040" ( .004" W ± .001"), . MATERIAL 15-5PH Steel. SIZE: 1.5"W x 3.00"L x .25" ± .005". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
184
184
Tool:
3320A96900-307
Description:
CONAIR EDDY CURRENT SURFACE REFERENECE STANDARD. EDM Notches: .008", .020", .040" ( .004" W ± .001"), . MATERIAL 6Al-4v Titaniuml. SIZE: 1.5"W x 3.00"L x .25" ± .005". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
185
185
Tool:
335
Description:
BOEING REFERENCE STANDARD 737 PT 6 53-10-31. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
186
186
Tool:
336A
Description:
BOEING REFERENCE STANDARD 737 PART 6 57-30-02 FIGURE 2 PAGE 5.
Location:
North America
Aircraft or Engine:
187
187
Tool:
336B
Description:
BOEING REFERENCE STANDARD 737 PART 6 57-30-02 FIGURE 2 PAGE 5.
Location:
North America
Aircraft or Engine:
188
188
Tool:
338A
Description:
BOEING REFERENCE STANDARD 737 PART 6 53-10-35 FIGURE 1 PAGE 6. MATERIAL: 2024-T3. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
189
189
Tool:
338B
Description:
BOEING REFERENCE STANDARD 737 PART 6 53-10-35 FIGURE 1 PAGE 6. MATERIAL: 301 1/2 HARD. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
190
190
Tool:
341
Description:
BOEING REFERENCE STANDARD 737 PART 4 53-10-40 FIGURE 1 PAGE 4. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
191
191
Tool:
345
Description:
BOEING REFERENCE STANDARD 737 PART 6 57-40-01 FIGURE 2 PAGE 5. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
192
192
Tool:
349
Description:
BOEING REFERENCE STANDARD 737 PART 4 32-10-01 FIGURE 2 PAGE 5. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
193
193
Tool:
350
Description:
BOEING REFERENCE STANDARD 737 PT 4 32-20-01 FIG 2. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
194
194
Tool:
350P
Description:
BOEING POISTIONING FIXTURE 737 PT 4 32-20-01
Location:
North America
Aircraft or Engine:
195
195
Tool:
351A
Description:
BOEING REFERENCE STANDARD 737 PT 6 53-10-01
Location:
North America
Aircraft or Engine:
196
196
Tool:
351B
Description:
BOEING REFERENCE STANDARD 737 PT 6 53-10-01
Location:
North America
Aircraft or Engine:
197
197
Tool:
353ABC
Description:
BOEING REFERENCE STANDARD 737 PT6 53-10-12
Location:
North America
Aircraft or Engine:
198
198
Tool:
353D
Description:
BOEING REFERENCE STANDARD 737 PT 6 53-10-12
Location:
North America
Aircraft or Engine:
199
199
Tool:
354A
Description:
BOEING REFERENCE STANDARD 737 PT 6 57-30-04
Location:
North America
Aircraft or Engine:
200
200
Tool:
354B
Description:
BOEING REFERENCE STANDARD 737 PT 6 57-30-04
Location:
North America
Aircraft or Engine:
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