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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:
NRK-3AL-6061
Description:
CUSTOM NAVY BLOCK 6061-T6,20 FASTENER HOLES (.156-.750) CONTAINING A TOTAL OF 71 EDM NOTCHES. Includes Test Report and Certificate of Confromance.
Location:
North America
Aircraft or Engine:
2
2
Tool:
NRK-3AST
Description:
CUSTOM NAVY BLOCK SET, 3 Blocks Total. Materials: 7075-T6 Aluminum, 4340 Cres Steel and 6AL-4V Titanium. Each Standard Includes 20 Fastener Holes (.156-.750) Containing a total of 71 EDM Notches. All Standards Manufactured in Accordance with U.S.A.F. ...
Location:
North America
Aircraft or Engine:
3
3
Tool:
NRK-3I
Description:
CUSTOM NAVY BLOCK. MATERIAL: 718 INCONEL CONTAINING 20 FASTENER HOLES (.156-.750) WITH A TOTAL OF 71 EDM NOTCHES. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
4
4
Tool:
NRK-3MAG
Description:
CUSTOM NAVY BLOCK AZ 31 MAGNESIUM, 20 FASTENER HOLES (.156-.750) CONTAINING A TOTAL OF 71 EDM NOTCHES. Includes Test Report and Certificate of Confromance.
Location:
North America
Aircraft or Engine:
5
5
Tool:
NRK-3S/17-4
Description:
CUSTOM NAVY REFERENCE STANDARD. MATERIAL: 17-4PH TH1050 STAINLESS STEEL. CONTAINS 20 FASTENER HOLES (.156-.750) WITH A TOTAL OF 71 EDM NOTCHES. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
6
6
Tool:
NRK-3S/17-7
Description:
CUSTOM NAVY REFERENCE STANDARD. MATERIAL: 17-7PH STAINLESS STEEL. CONTAINS 20 FASTENER HOLES (.156-.750) WITH A TOTAL OF 71 EDM NOTCHES. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
7
7
Tool:
NRK-3S/400SS
Description:
CUSTOM NAVY EDDY CURRENT BLOCK. Material: 400 Stainless Steel. 3 Plate assembly measuring 4" x 7" x .875", Contains 20 fastener holes with diameters ranging from .156" – .750"., 71 EDM notches in various locations (notch depth & lengths vary), Widths for
Location:
North America
Aircraft or Engine:
8
8
Tool:
NRK-3S/HX
Description:
CUSTOM NAVY EDDY CURRENT BLOCK. Material: Hastelloy X, 3 Plate assembly measuring 4" x 7" x .875", Contains 20 fastener holes with diameters ranging from .156" – .750"., 71 EDM notches in various locations (notch depth & lengths vary), Widths for all notc
Location:
North America
Aircraft or Engine:
9
9
Tool:
NRK-3SS
Description:
CUSTOM NAVY BLOCK. MATERIAL: 304 STAINLESS STEEL ,CONTAINING 20 FASTENER HOLES (.156-.750) WITH A TOTAL OF 71 EDM NOTCHES NOTCHES. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
10
10
Tool:
NRK-3ST
Description:
CUSTOM NAVY EDDY CURRENT BLOCK. Material: 4340 Cres Steel. 3 Plate assembly measuring 4" x 7" x .875", Contains 20 fastener holes with diameters ranging from .156" – .750"., 71 EDM notches in various locations (notch depth & lengths vary), Widths for all
Location:
North America
Aircraft or Engine:
11
11
Tool:
NRK-3T
Description:
CUSTOM NAVY EDDY CURRENT BLOCK. Material: 6AL-4V Titanium 3 Plate assembly measuring 4" x 7" x .875", Contains 20 fastener holes with diameters ranging from .156" – .750"., 71 EDM notches in various locations (notch depth & lengths vary), Widths for all n
Location:
North America
Aircraft or Engine:
12
12
Tool:
P564A
Description:
BOEING TRANSDUCER POSITIONER PT 4 57-50-01
Location:
North America
Aircraft or Engine:
13
13
Tool:
P564B
Description:
BOEING TRANSDUCER POSITIONER PT 4 57-50-01
Location:
North America
Aircraft or Engine:
14
14
Tool:
P6020A
Description:
BOEING TRANSDUCER POSITIONER 767 PART 4 57-50-14 PAGE 9 FIGURE 2. Includes Certificate of Conformance.
Location:
North America
Aircraft or Engine:
15
15
Tool:
P6020B
Description:
BOEING TRANSDUCER POSITIONER 767 PART 4 57-50-14 PAGE 9 FIGURE 2. Includes Certificate of Conformance.
Location:
North America
Aircraft or Engine:
16
16
Tool:
P6021A
Description:
BOEING TRANSDUCER POSITIONER 767 PART 4 57-50-14 PAGE 10 FIGURE 3. Includes Certificate of Conformance.
Location:
North America
Aircraft or Engine:
17
17
Tool:
P6021B
Description:
BOEING TRANSDUCER POSITIONER 767 PART 4 57-50-14 PAGE 10 FIGURE 3. Includes Certificate of Conformance.
Location:
North America
Aircraft or Engine:
18
18
Tool:
P6021C
Description:
BOEING TRANSDUCER POSITIONER 767 PART 4 57-50-14 PAGE 10 FIGURE 3. Includes Certificate of Conformance.
Location:
North America
Aircraft or Engine:
19
19
Tool:
PDL 1030J
Description:
HERCULES C-130 UT CALIBRATION STANDARD FIGURE 17 SHEETS 1&2 20-40-00. FASTENER (HL18PB6-8, HL18PB6-6, HL70-6). Includes Test Report Traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
20
20
Tool:
PDL 1034J/1040J
Description:
CALIBRATION STANDARD 20-40-00 FIG 18 7075-T6 ALUMINUM
Location:
North America
Aircraft or Engine:
21
21
Tool:
PDL 1035J
Description:
KINGPIN RISER TRANSDUCER, C130 SMP-C-NDI 20-40-00: FIG 19, PG.28
Location:
North America
Aircraft or Engine:
22
22
Tool:
PDL 1036
Description:
C-130 TRUSS MOUNT UPPER LUG INSPECTION TRANSDUCER, 5MHz., "A" & "B" SMP 515-C INSPECTION PROCEDURE FOR WINGS CHAPTER 57. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
23
23
Tool:
PDL 1037AJ
Description:
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 PAGE 30 FIG 20, 7075-T6 ALUMINUM
Location:
North America
Aircraft or Engine:
24
24
Tool:
PDL 1037BJ
Description:
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 PAGE 31 FIG 21, 7075-TG ALUMINUM
Location:
North America
Aircraft or Engine:
25
25
Tool:
PDL 1155
Description:
CALIBRATION STANDARD FIGURE 3 FASTENER (BACB30NX12K11, BACB30NX14K8, HL1012-12)
Location:
North America
Aircraft or Engine:
26
26
Tool:
PDL 1214J
Description:
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 22
Location:
North America
Aircraft or Engine:
27
27
Tool:
PDL 1215J
Description:
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 23 PAGE 33, 7075-T6 ALUMINUM
Location:
North America
Aircraft or Engine:
28
28
Tool:
PDL 1217AJ
Description:
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 24 PAGES 34, 7075-T6 ALUMINUM
Location:
North America
Aircraft or Engine:
29
29
Tool:
PDL 1217BJ
Description:
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 25 PAGE 35, CAST ACRYLIC SHEET
Location:
North America
Aircraft or Engine:
30
30
Tool:
PDL 1217CJ
Description:
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 26 PAGE 36, CAST ACRYLIC SHEET
Location:
North America
Aircraft or Engine:
31
31
Tool:
PDL 1253
Description:
CALIBRATION STANDARD FIGURE 20-49 FASTENER (HLT114-6-8 + KFN542-3)
Location:
North America
Aircraft or Engine:
32
32
Tool:
PDL 1254J
Description:
HERCULES C-130 UT CALIBRATION STANDARD FIGURE 21 SHEETS 1-4 20-40-00. FASTENER (HLT116 HI-LOCK FASTENERS WITH SELF LOCKING NUTS). Includes Test Report Traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
33
33
Tool:
PDL 389J
Description:
LOCKHEED C-130 CALIBRATION STANDARD 7075-T6 ALUMINUM FIGURE 1
Location:
North America
Aircraft or Engine:
34
34
Tool:
PDL 419J
Description:
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 2 PAGE 4, 2024-T3 ALUMINUM
Location:
North America
Aircraft or Engine:
35
35
Tool:
PDL 447J
Description:
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 4, 7075-T6 ALUMINUM
Location:
North America
Aircraft or Engine:
36
36
Tool:
PDL 449J
Description:
LOCKHEED C-130 CALIBRATION STANDARD FIGURE 5, 7075-T6 ALUMINUM
Location:
North America
Aircraft or Engine:
37
37
Tool:
PDL 457AJ
Description:
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 6 PAGES 8&9 SHEET 1&2, 7075-T6 ALUMINUM
Location:
North America
Aircraft or Engine:
38
38
Tool:
PDL 457SJ
Description:
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 6 PAGES 8&9 SHEET 1&2, 4340 STEEL
Location:
North America
Aircraft or Engine:
39
39
Tool:
PDL 457SS
Description:
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 6 PAGES 8&9 SHEET 1&2 304 STAINLESS STEEL
Location:
North America
Aircraft or Engine:
40
40
Tool:
PDL 459J
Description:
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 7 PAGE 10, 7075-T6 ALUMINUM
Location:
North America
Aircraft or Engine:
41
41
Tool:
PDL 601J
Description:
CALIBRATION STANDARD FIGURE 20-29
Location:
North America
Aircraft or Engine:
42
42
Tool:
PDL 843J
Description:
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 9 FASTENER (HL21-6-4 + TLN 1030.3)
Location:
North America
Aircraft or Engine:
43
43
Tool:
PDL 874
Description:
CALIBRATION STANDARD 20-40-00 FIG 10
Location:
North America
Aircraft or Engine:
44
44
Tool:
PDL 917
Description:
LOCKHEED C 130 CALIBRATION STANDARD FIGURE 2 PAGE 14. 7075-T6 ALUMINUM OR EQUIVALENT.
Location:
North America
Aircraft or Engine:
45
45
Tool:
PDL 919
Description:
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 11 SHEET 1&2, 7075-T6 ALUMINUM, FASTENERS (HL64PB-10-9, HLT114-6-8, HLT18PB-12, HL70)
Location:
North America
Aircraft or Engine:
46
46
Tool:
PDL 919J
Description:
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 11 SHEET 1&2, 7075-T6 ALUMINUM, FASTENERS (HL64PB-10-9, HLT114-6-8, HLT18PB-12, HL70)
Location:
North America
Aircraft or Engine:
47
47
Tool:
PDL 920
Description:
CALIBRATION STANDARD FIGURE 12 FASTENER (HLT114-6-8, HLPB8-8, HL18PB10-8, HL 206-4)
Location:
North America
Aircraft or Engine:
48
48
Tool:
PDL 920J
Description:
CALIBRATION STANDARD FIGURE 12 FASTENER (HLT114-6-8, HLPB8-8, HL18PB10-8, HL 206-4)
Location:
North America
Aircraft or Engine:
49
49
Tool:
PDL 941J
Description:
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 13 PAGE 19, 7075-T6 ALUMINUM
Location:
North America
Aircraft or Engine:
50
50
Tool:
PDL 943J
Description:
CALIBRATION STANDARD FIGURE 14 PG.20 FASTENER (HL54-6-6, HL54-6-5, COLLAR (HL70-6) SMP-515-C NDI; 20-40-00, 7075-T6 ALUMINUM
Location:
North America
Aircraft or Engine:
51
51
Tool:
PDL 944-2J
Description:
CALIBRATION STANDARD FIGURE 15 FASTENER (HL40-6-5 + HL70-6, NAS6208-11 + KFN5428), 7075-T6 ALUMINUM
Location:
North America
Aircraft or Engine:
52
52
Tool:
PDL 944-J
Description:
CALIBRATION STANDARD FIGURE 15 FASTENER (HL40-6-5 + HL70-6, NAS6208-11 + KFN5428), 7075-T6 ALUMINUM
Location:
North America
Aircraft or Engine:
53
53
Tool:
PDL 958
Description:
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 PAGE 23 FIGURE 16 2024-T3 ALUMINUM
Location:
North America
Aircraft or Engine:
54
54
Tool:
PDL 980
Description:
C-130 Lower Engine Mount Longeron-Fwd End Calibration Standard. 7075-T6 Aluminum...
Location:
North America
Aircraft or Engine:
55
55
Tool:
PN-925-7/2MHZ
Description:
RIGID SURFACE PROBE 90 DEG .250" DROP 7.0" LONG MICRODOT CONNNECTOR 1-3MHz .125" TIP
Location:
North America
Aircraft or Engine:
56
56
Tool:
PN-95-7FX/2MHZ
Description:
FLEXIBLE SURFACE PROBE 90 DEG .500" DROP 7.0" LONG MICRODOT CONNNECTOR 1-3MHz .125" TIP
Location:
North America
Aircraft or Engine:
57
57
Tool:
PPG-125/5
Description:
PENCIL PROBE GUIDE, .750"Ø x .500" H FOR .125"Ø PROBE TIPS. MATERIAL: DELRIN OR EQUIVALENT.
Location:
North America
Aircraft or Engine:
58
58
Tool:
PROBE GUIDE S41-G1A
Description:
BOEING PROBE GUIDE. MATERIAL: POLYETHYLENE or EQUIVALENT.
Location:
North America
Aircraft or Engine:
59
59
Tool:
PROBE GUIDE S41-G1B
Description:
BOEING PROBE GUIDE. MATERIAL: POLYETHYLENE or EQUIVALENT.
Location:
North America
Aircraft or Engine:
60
60
Tool:
PROBE GUIDE S43-G1A,G1B, G1C
Description:
BOEING PROBE GUIDE. MATERIAL: POLYETHYLENE or EQUIVALENT.
Location:
North America
Aircraft or Engine:
61
61
Tool:
PSP 396
Description:
BOMBARDIER CALIBRATION STANDARD, CL-215T PART 6 FIGURE 5 PAGE 8. A TOTAL OF 15 HOLE SIZES: 4mm THRU 18mm MATERIAL: 2024T3 ALUMINUM. Includes Certification Report Traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
62
62
Tool:
PSR5-15R20
Description:
5MHZ, .590"Ø(15 mm) ACTIVE ELEMENT (HIGH DAMPED), REPLACEABLE DELAY TRANSDUCER SIDE MOUNT MICRODOT CONNECTOR. Delay Tip length = (.790")20mm. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
63
63
Tool:
PT.24
Description:
SUFACE PROBE 90° DEGREES .063" DROP .100"Ø SHAFT DIAMETER BENT 15° DEGREES, 10.0" LONG WITH TRIAX FISCHER CONNECTOR. FREQUENCY 500KHz-2MHz. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
64
64
Tool:
PT.27
Description:
DC-10 ANGLE BEAM TRANSDUCER 60°, 5MHz .187" x .187" ELEMENT. CASE SIZE: .690" x .310" x .560". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
65
65
Tool:
PT.28
Description:
DC-10 ANGLE BEAM TRANSDUCER 70°, 5MHz .187" x .187" ELEMENT. CASE SIZE: .690" x .310" x .560". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
66
66
Tool:
PT.29A
Description:
CUSTOM 45 DEGREE LUCITE WEDGE
Location:
North America
Aircraft or Engine:
67
67
Tool:
PT.29B
Description:
CUSTOM 11 DEGREE LUCITE WEDGE
Location:
North America
Aircraft or Engine:
68
68
Tool:
PT.30
Description:
QUICK CHANGE TRANSDUCER 5MHz .25" ELEMENT 3/8-32 THREAD
Location:
North America
Aircraft or Engine:
69
69
Tool:
PT.30a
Description:
CUSTOM 45 DEGREE LUCITE SHEAR WAVE WEDGE FOR TITANIUM INSPECTION USED WITH RS.22
Location:
North America
Aircraft or Engine:
70
70
Tool:
PT.30b
Description:
CUSTOM 20 DEGREE LUCITE "L" WAVE WEDGE WITH 1.220" RADIUS FOR TITANIUM INSPECTION USED WITH RS.22
Location:
North America
Aircraft or Engine:
71
71
Tool:
PT.31.1
Description:
CUSTOM 45 DEGREE 5MHz .187"x.187" SHEAR WAVE TRANSDUCER WITH HANDLE BENT AT 5 DEGREES AWAY. MICRODOT CONNECTOR.
Location:
North America
Aircraft or Engine:
72
72
Tool:
PT.34
Description:
STRAIGHT BEAM (LONGITUDINAL) TRANSDUCER, 10MHz .125"Ø ELEMENT. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
73
73
Tool:
PT.53
Description:
LOW FREQUENCY REFLECTION SPOT PROBE .750"Ø DIAMETER, 2.0" TALL WITH TRIAX FISCHER CONNECTOR. 100Hz-10KHz. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
74
74
Tool:
PT.56/A
Description:
DC-10 TRANSDUCER INCIDENT ANGLE 8° RADIUS 1.8
Location:
North America
Aircraft or Engine:
75
75
Tool:
PT.56/B
Description:
DC-10 TRANSDUCER INCIDENT ANGLE 6° RADIUS 2.1
Location:
North America
Aircraft or Engine:
76
76
Tool:
PT.56/C
Description:
DC-10 TRANSDUCER INCIDENT ANGLE 13° RADIUS 2.25
Location:
North America
Aircraft or Engine:
77
77
Tool:
PT.59
Description:
DC-10 ANGLE BEAM TRANSDUCER 45°, 5MHz .187" x .187" ELEMENT, END MOUNT MICRODOT CONNECTOR. CASE SIZE: .690" x .310" x .560". Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
78
78
Tool:
PT.60
Description:
TRANSDUCER SHEARWAVE 10MHZ .125ELEMENT, 34°
Location:
North America
Aircraft or Engine:
79
79
Tool:
PWA28403
Description:
PRATT & WHITTNEY 1ST STAGE FAN BLADE CALIBRATION STANDARD WITH HOLDING BLOCK . Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
80
80
Tool:
PWA28403B
Description:
PRATT & WHITTNEY 1ST STAGE FAN BLADE CALIBRATION STANDARD. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
81
81
Tool:
PWA75909
Description:
ENGINE BLADE PROBE, DIFFERENTIAL 1-4 MHz, ATTACHED CABLE 6.0' FEET LONG WITH 16 PIN LEMO CONNECTOR FOR NOTEC SERIES INSTRUMENTS. DIFFERENTIAL 1-4 MHz. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
82
82
Tool:
PZT-15MHz
Description:
.25" Dia. 15MHz K-81 MATERIAL PIEZOELECTRIC ELEMENT
Location:
North America
Aircraft or Engine:
83
83
Tool:
QCX45
Description:
45° IN ALUMINUM LUCITE (PLEXIGLASS) WEDGE FOR .25" DIAMETER TRANSDUCER. 3/8-32 THREAD
Location:
North America
Aircraft or Engine:
84
84
Tool:
QFW35A/40
Description:
35 DEGREE LUCITE WEDGE FOR QUICK FIT TRANSDUCER
Location:
North America
Aircraft or Engine:
85
85
Tool:
QO-QTS-TI-03-001
Description:
Air Force reference standard Detail#1. Material 7075-T6 Aluminum. EDM Notch size: .050" x .050" x .005" Max Width, 10 Flaws total. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
86
86
Tool:
RA-RA-4
Description:
ROTARY (RA SCANNER) ADAPTOR EXTENSION: MALE 4 PIN STEP LEMO TO FEMALE 4 PIN STEP LEMO . 4 INCHES LONG. Includes Certificate of Conformance.
Location:
North America
Aircraft or Engine:
87
87
Tool:
RA-RAFX-6
Description:
FLEX SHAFT ADAPTER FOR RECHII SCANNER MALE CONNECTOR TO RECHII RA PROBE, (4PIN STEP LEMO RECEPTACLE FEMALE CONNECTOR) WITH SLIDING COLLAR, 6.0" LONG. Includes Test Report and Certificate of Conformance
Location:
North America
Aircraft or Engine:
88
88
Tool:
RA-UR
Description:
ADAPTER FOR UNIVERSAL PROBE (4 PIN FISCHER) TO RECHII RA SCANNER, (4PIN STEP LEMO)
Location:
North America
Aircraft or Engine:
89
89
Tool:
RA-UR/12FX
Description:
FLEXIBLE ADAPTER FOR UNIVERSAL PROBE (4 PIN FISCHER) TO RECHII RA SCANNER, (4PIN STEP LEMO) 12.0 " LONG.
Location:
North America
Aircraft or Engine:
90
90
Tool:
RA-UR/4
Description:
ROTARY (RA SCANNER) ADAPTOR: MALE 4 PIN STEP LEMO TO FEMALE 4 PIN FISCHER. 4 INCHES LONG. Includes Certificate of Conformance.
Location:
North America
Aircraft or Engine:
91
91
Tool:
RA-URFX-12
Description:
FLEXIBLE ROTARY PROBE ADAPTOR MALE 4 PIN STEP LEMO TO RECEPTACLE (FEMALE) 4-PIN FISCHER CONNECTOR 12.0" WORKING LENGTH
Location:
North America
Aircraft or Engine:
92
92
Tool:
Radius Shoe .500R
Description:
Boeing Custom Contact Radius Shoe 201 with a 0.500" radius with no thru hole. Material: Black ABS. Includes Certificate of Conformance.
Location:
North America
Aircraft or Engine:
93
93
Tool:
Radius Shoe 201
Description:
Boeing Custom Contact Radius Shoe 201 with a 0.100" radius. Material: Black Delrin(Acetal).
Location:
North America
Aircraft or Engine:
94
94
Tool:
Radius Shoe 202
Description:
Boeing Custom Contact Radius Shoe 202 with a 0.150" radius. Material: Black Delrin(Acetal).
Location:
North America
Aircraft or Engine:
95
95
Tool:
Radius Shoe 203
Description:
Boeing Custom Contact Radius Shoe 203 with a 0.200" radius. Material: Lucite/Cast Acrylic.
Location:
North America
Aircraft or Engine:
96
96
Tool:
RD11-01A
Description:
MD-11 REFERENCE STANDARD MDC-K5225 SECTION 2-1 PAGES 1-2, FIG 1.3 SHEETS 1&2. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
97
97
Tool:
RD11-02
Description:
MD REFERENCE STANDARD MDC-K5225 SECTION 2-1 FIG 1.6
Location:
North America
Aircraft or Engine:
98
98
Tool:
RD11-03
Description:
MD11 REFERENCE STANDARD MDC-K5225 SECTION 2-1
Location:
North America
Aircraft or Engine:
99
99
Tool:
RS-502
Description:
ASTRA G100 REFERENCE STANDARD, PG.613: 04-00-00 FIG.605
Location:
North America
Aircraft or Engine:
100
100
Tool:
RS-502-C
Description:
ASTRA G100 REFERENCE STANDARD, 2 EDM FATIGUE CRACKS 2.4mm X 1.2mm (PG.613: 04-00-00 FIG.605)
Location:
North America
Aircraft or Engine:
101
101
Tool:
RS9000-1
Description:
DC9 REFERENCE STANDARD PER BOEING SB DC9-54A031 PAGE 16 FIGURE 1. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
102
102
Tool:
RSDC6-5
Description:
BOEING REFERENCE STANDARD DC6
Location:
North America
Aircraft or Engine:
103
103
Tool:
S-17-1
Description:
BOEING CUSTOM NDI TEST REFERENCE STANDARD ASSEMBLY DASH NO. 1, MATERIAL 2024-T3, STRINGER=7075-T6
Location:
North America
Aircraft or Engine:
104
104
Tool:
S-17-2
Description:
BOEING CUSTOM NDI TEST REFERENCE STANDARD ASSEMBLY DASH NO. 2, MATERIAL 2024-T3, STRINGER=7075-T6
Location:
North America
Aircraft or Engine:
105
105
Tool:
S-17-3
Description:
BOEING CUSTOM NDI TEST REFERENCE STANDARD ASSEMBLY DASH NO. 3, MATERIAL 2024-T3, STRINGER=7075-T6
Location:
North America
Aircraft or Engine:
106
106
Tool:
S-17-4
Description:
BOEING CUSTOM NDI TEST REFERENCE STANDARD ASSEMBLY DASH NO. 4, MATERIAL 2024-T3, STRINGER=7075-T6
Location:
North America
Aircraft or Engine:
107
107
Tool:
S-17-5
Description:
BOEING CUSTOM NDI TEST REFERENCE STANDARD ASSEMBLY DASH NO. 5, MATERIAL 2024-T3, STRINGER=7075-T6
Location:
North America
Aircraft or Engine:
108
108
Tool:
S-17-6
Description:
BOEING CUSTOM NDI TEST REFERENCE STANDARD ASSEMBLY DASH NO. 6, MATERIAL 2024-T3, STRINGER=7075-T6
Location:
North America
Aircraft or Engine:
109
109
Tool:
S-17-7
Description:
BOEING CUSTOM NDI TEST REFERENCE STANDARD ASSEMBLY DASH NO. 7, MATERIAL 2024-T3, STRINGER=7075-T6
Location:
North America
Aircraft or Engine:
110
110
Tool:
S-17-8
Description:
BOEING CUSTOM NDI TEST REFERENCE STANDARD ASSEMBLY DASH NO. 8, MATERIAL 2024-T3, STRINGER=7075-T6
Location:
North America
Aircraft or Engine:
111
111
Tool:
S0143
Description:
Fokker 50/60 Reference Standard PART 6 53-30-03 PAGE 9. Material: 2024-T3 Alclad Aluminum.
Location:
North America
Aircraft or Engine:
112
112
Tool:
S41-E1A
Description:
BOEING CUSTOM REFERENCE STANDARD MCU ESM S41-E1A NDI REF STD PER DRAWING SK667-00011.
Location:
North America
Aircraft or Engine:
113
113
Tool:
S41-E1C
Description:
BOEING CUSTOM REFERENCE STANDARD MCU ESM S41-E1C NDI REF STD PER DRAWING SK667-00012.
Location:
North America
Aircraft or Engine:
114
114
Tool:
S41-F1B
Description:
BOEING CUSTOM REFERENCE STANDARD MCU ESM S41-F1B NDI REF STD PER DRAWING SK667-00010.
Location:
North America
Aircraft or Engine:
115
115
Tool:
S46-C2
Description:
BOEING REFERENCE STANDARD S42-C6 FIGURE 2. MATERIAL: 2024-T3 CLAD. RIVET: BACR15CE6. Includes Test Report and Certificate of Conformance
Location:
North America
Aircraft or Engine:
116
116
Tool:
S46-G1A/G2A
Description:
BOEING REFERENCE STANDARD FIGURE 2. MATERIAL: 2024-T3 ALUMINUM. FASTENERS: BACR15CE6D 2 PLACES. Includes Certification Report.
Location:
North America
Aircraft or Engine:
117
117
Tool:
S520 BLOCK
Description:
British Aerospace test block. Material: mild steel 4130, 4140 or 4340 cres .128: thick. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
118
118
Tool:
S53-10-103.3/1
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 53-10-25 PT 4 FIGURE 3&4 PAGES 7&8. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
119
119
Tool:
S57-10-105.2/1
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 57-10-58 PT 6 FIGURE 7-9 PAGES 13-15. Material: 2024-T3 Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
120
120
Tool:
S57-10-105.2/2
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 57-10-58 PT 6 FIGURE 7-9 PAGES 13-15. Material: 2024-T3 Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
121
121
Tool:
SAAB 5341-151-01I
Description:
REFERENCE STANDARD SAAB 340 FIG.1 5341-151-01I PART 4 PAGE 5. MATERIAL: 4140 CRES STEEL. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
122
122
Tool:
SAAB 5512-332-03I
Description:
SAAB 340 REFERENCE STANDARD 5512-332-03I FIGURE 1 PAGE 2, 55-10-00 PART 6 PAGE 3. MATERIAL: 2024-T351 ALUMINUM WITH 4 HL10 VAP-6-7 HI-LOK FASTENERS.. Includes Test Reprort and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
123
123
Tool:
SB 146/53-167/2
Description:
BAE SYSTEMS REFERENCE STANDARD, AVRO 146-RJ, ISB.53-167AP2
Location:
North America
Aircraft or Engine:
124
124
Tool:
SB 146/53-167/2
Description:
BAE 146-RJ SERIES REFERENCE STANDARD ISB.53-167 APPENDIX 2 DRAWING 15, PAGE 23&24. Material: Substitute 2024-T3 Clad for 2014A-T4 Aluminum. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
125
125
Tool:
SB 57-3329 FIG.9
Description:
Raytheon 12 Hole Standard Calibration Block Figure 9 Page 20, Service Bulletin SB 57-3329. Hole sizes 9/64, 11/64,3/16 and 13/64. Material: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
126
126
Tool:
SB09530016-5/303SS
Description:
DOUGLAS REFERENCE STANDARD 53-253, 303/SS
Location:
North America
Aircraft or Engine:
127
127
Tool:
SB09530016-5/AL
Description:
DOUGLAS REFERENCE STANDARD 53-253, 7075-t651
Location:
North America
Aircraft or Engine:
128
128
Tool:
SB09530016-5/TI
Description:
DOUGLAS REFERENCE STANDARD 53-253, TITANIUM
Location:
North America
Aircraft or Engine:
129
129
Tool:
SB09540030-5
Description:
DC9 SURFACE REFERENCE REFERENCE STANDARD DC9-54-030. MATERIAL: 17-7 PH STAINLESS STEEL. EDM NOTCH: 0.002"-0.010" WIDE x 0.030" DEEP.
Location:
North America
Aircraft or Engine:
130
130
Tool:
SB09550023-17
Description:
Douglas Reference Standard Assembly 55-23 Figure1 sheets 1-5, Pages 31-35. Material: 2024-T3 Aluminum. Includes Test Report Traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
131
131
Tool:
SB10270203-5
Description:
Douglas Reference Standard Inboard Slat Drive Arm. Bulletin A27-203. Figure1 sheet 11, Pages 31-35. Material: HY-TUF or 4000 Series Steel CAD Plated. Includes Test Report Traceable to NIST and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
132
132
Tool:
SB10550016-147
Description:
DC-10 SERVICE BULLETIN REFERENCE STANDARD FIGURE 1 PAGE 14, SHEET 1. MATERIAL: 7075-T6 ALUMNIUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
133
133
Tool:
SB11530001-5
Description:
DOUGLAS MD-11 REFERENCE STANDARD. MD11-53-001 FIGURE 1 SHEET 1. MATERIAL: 7075-T6 ALUMINUM
Location:
North America
Aircraft or Engine:
134
134
Tool:
SCRIBE STANDOFF
Description:
FOR HS410 SENSOR
Location:
North America
Aircraft or Engine:
135
135
Tool:
SE.4.44
Description:
328JET CALIBRATION STANDARD (SE.4.44); 51-60-01 PAGE 9/10 FIG.605 EDDY CURRENT
Location:
North America
Aircraft or Engine:
136
136
Tool:
SLS-123456-SS304
Description:
BOEING REFERENCE STANDARD PER DRAWING STD-1. MATERIAL: 304 STAINLESS STEEL. CHEMICAL CONVERSION COATING PER MIL-DTL-5541, CLASS 1A. Includes Certification Traceable to NIST and Material Certs.
Location:
North America
Aircraft or Engine:
137
137
Tool:
SLS-IN718-201-010793B2
Description:
BOEING REFERENCE STANDARD, 0.030 x 0.030 x .005" +/- 002" CORNER EDM NOTCH. MATERIAL: 718 INCONEL
Location:
North America
Aircraft or Engine:
138
138
Tool:
SN09530004-3
Description:
DOUGLAS REFERENCE STANDARD
Location:
North America
Aircraft or Engine:
139
139
Tool:
SN10280002
Description:
DOUGLAS REFERENCE STANDARD FIGURE 2 SHEETS 2-8. INCLUDES GANG CHANNEL PART NUMBER RMG9421-3-7-2. Test Report and Certificate of Conformance included.
Location:
North America
Aircraft or Engine:
140
140
Tool:
SN10550000
Description:
BOEING REFERENCE STANDARD SHEETS 1-4. DETAIL -3,-5,-7. MATERIAL: 7075-T7 & 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
141
141
Tool:
SN90570006
Description:
BOEING REFERENCE STANDARD
Location:
North America
Aircraft or Engine:
142
142
Tool:
SO111-7
Description:
Custom FOKKER F28 Horizontal Stab. Drive Junction Fitting Eddy Current Standard per drawing # 28. 0-3210/2610-Material: 7075-T6. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
143
143
Tool:
SORFIT 146/151/1
Description:
BAE REFERENCE STANDARD 146 SERIES / AVRO-RJ SERIES PART 4 53-20-96 PG 14&15 FIGURE 5&6. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
144
144
Tool:
SORFIT 146/151/2
Description:
BAE REFERENCE STANDARD 146 SERIES / AVRO-RJ SERIES PART 4 53-20-96 PG 14&15 FIGURE 5&6. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
145
145
Tool:
SORFIT 146/154/1
Description:
BAE REFERENCE STANDARD 146 SERIES / AVRO-RJ SERIES PART 6 53-20-95 PG 11 FIG 5. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
146
146
Tool:
SORFIT 146/164/1
Description:
BAE REFERENCE STANDARD 146 SERIES / AVRO-RJ SERIES PART 4 53-20-19 PG 9 FIG 5. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
147
147
Tool:
SORFIT 146/166/1
Description:
BAE REFERENCE STANDARD 146-RJ 53-238 53-30-15 PT 6 FIGURE 5&6 PAGES 9&10. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
148
148
Tool:
SORFIT 146/166/2
Description:
BAE REFERENCE STANDARD 146-RJ 53-238 53-30-16 PT 6 FIGURE 4-6 PAGES 8-10. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
149
149
Tool:
SP-078
Description:
CALIBRATION STANDARD BATS
Location:
North America
Aircraft or Engine:
150
150
Tool:
SP-096
Description:
CALIBRATION STANDARD BATS 53-30-30
Location:
North America
Aircraft or Engine:
151
151
Tool:
SP-115
Description:
CALIBRATION STANDARD BATS
Location:
North America
Aircraft or Engine:
152
152
Tool:
SP-265
Description:
LOCKHEED C-130 STEP BLOCK. PROCEEDURE SMP 515-C. PAGE 9 MATERIAL: 7075-T6 ALUMINUM.
Location:
North America
Aircraft or Engine:
153
153
Tool:
SRSM-51020S/WLD
Description:
urface reference standard, 4340 Steel, with EDM notch depths of 0.5mm", 1.0" and 2.0mm +/-1.3mm1 (0.2mm, 0.51mm and 1.02mm), Notch Width: .18mm Max. Depth: +/- .03mm. Reference standard overall dImensions 25.4mm X 101.6mm X 6.4mm). Includes Test Report a
Location:
North America
Aircraft or Engine:
154
154
Tool:
SS TYPE 301
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:
155
155
Tool:
SS TYPE 304
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: 304 STAINLESS STEEL. SIZE: 1.5"W x 3.75"L x .25"
Location:
North America
Aircraft or Engine:
156
156
Tool:
SSI 55-11-115/1
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 55-11-10 PT 6 FIGURE 6&7 PAGES 12&13. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
157
157
Tool:
SSI 57-20-151/152A/153A/1
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 57-20-50 PT 6 FIGURE 6&7 PAGES 10&11. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
158
158
Tool:
SSI57-20-151/152A/153A/2
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 57-20-50 PT 6 FIGURE 8&9 PAGES 12&13. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
159
159
Tool:
SSID S57-51-117.1
Description:
BAE GUIDE MANDREL 146 SERIES / AVRO-RJ SERIES PART 6 57-51-10 PG 6 FIG 2. Includes Certificate of Conformance.
Location:
North America
Aircraft or Engine:
160
160
Tool:
ST4130
Description:
BOMBARDIER / CANADAIR EDDY CURRENT SURFACE REFERENCE STANDARD PART 6 55-20-001, NOTCHES .008", .020", .040" (.005" Wide +000 / - .002 and +/- .001" Depth), MATERIAL: 4130 STEEL. Includes certification Report and Certificate of Conformance(COC)...
Location:
North America
Aircraft or Engine:
161
161
Tool:
ST4330
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: 4330 or 4340 STEEL. SIZE: 1.5"W x 3.75"L x .25". Includes certification Rep
Location:
North America
Aircraft or Engine:
162
162
Tool:
ST4340
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: 4340 STEEL. SIZE: 1.5"W x 3.75"L x .25". Includes certification Report ...
Location:
North America
Aircraft or Engine:
163
163
Tool:
ST8870-1
Description:
BOEING COMPOSITE REFERENCE STANDARD 51-04-00, PAGE 20 FIGURE 7. GR/EP SKIN/NOMEX CORE DISBOND DEFECT
Location:
North America
Aircraft or Engine:
164
164
Tool:
ST8870-4
Description:
BOEING COMPOSITE REFERENCE STANDARD 51-04-00, PAGE 19 FIGURE 6. GR/EP SKIN/NOMEX CORE DISBOND DEFECT
Location:
North America
Aircraft or Engine:
165
165
Tool:
ST8870-7
Description:
BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE( 1-10 PLY), PT 1 51-04-00, PAGE 21 FIGURE 8. SUPPLIED WITH HOLDING BLOCK
Location:
North America
Aircraft or Engine:
166
166
Tool:
ST8870-8
Description:
BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE( 11-20 PLY), PT 1 51-04-00, PAGE 21 FIGURE 8. SUPPLIED WITH HOLDING BLOCK
Location:
North America
Aircraft or Engine:
167
167
Tool:
ST8870-9
Description:
BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE( 21-30 PLY), PT 1 51-04-00, PAGE 19 FIGURE 8. SUPPLIED WITH HOLDING BLOCK
Location:
North America
Aircraft or Engine:
168
168
Tool:
ST8870B-7
Description:
BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE WITH HOLDING PLATE. MATERIAL: BMS8-79 FIBERGLASS( 1-10 PLY), PT 1 51-04-00, PAGE 27 FIGURE 8. B737 NDT Part 1, 51-04-00. Includes C-Scan, Certification Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
169
169
Tool:
ST8870B-8
Description:
BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE WITH HOLDING PLATE. MATERIAL: BMS8-79 FIBERGLASS( 11-20 PLY), PT 1 51-04-00, PAGE 27 FIGURE 8. B737 NDT Part 1, 51-04-00. Includes C-Scan, Certification Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
170
170
Tool:
ST8870B-9
Description:
BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE WITH HOLDING PLATE. MATERIAL: BMS8-79 FIBERGLASS( 21-30 PLY), PT 1 51-04-00, PAGE 27 FIGURE 8. B737 NDT Part 1, 51-04-00. Includes C-Scan, Certification Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
171
171
Tool:
ST8870C-7
Description:
BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE WITH HOLDING PLATEBMS8-139 FIBERGLASS( 1-10 PLY), PT 1 51-04-00, PAGE 28 FIGURE 8. Includes C-Scan, Certification Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
172
172
Tool:
ST8870C-8
Description:
BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE WITH HOLDING PLATEBMS8-139 FIBERGLASS( 11-20 PLY), PT 1 51-04-00, PAGE 28 FIGURE 8. Includes C-Scan, Certification Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
173
173
Tool:
ST8870C-9
Description:
BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE WITH HOLDING PLATEBMS8-139 FIBERGLASS( 21-30 PLY), PT 1 51-04-00, PAGE 28 FIGURE 8. Includes C-Scan, Certification Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
174
174
Tool:
ST8870D
Description:
BOEING PERFORATED BONDED REFERENCE STANDARD ALUMINUM HONEYCOMB ALL PT4 78-30-01; PG.18 FIG.3
Location:
North America
Aircraft or Engine:
175
175
Tool:
ST8871
Description:
COMPOSITE 10 STEP WEDGE SOLID LAMINATE, 777 PT 4 51-00-06 PAGE 7 FIGURE 1. BMS 8-276 FABRIC MATERIAL TYPE 35 CL3 GRADE190. STEP SIZES: .050, .100, .200, .300, .400, .500, .600, .700, .800, .900.
Location:
North America
Aircraft or Engine:
176
176
Tool:
ST8871D
Description:
BOEING COMPOSITE REFERENCE STANDARD 5-10-15 PLY 737 PT 4; 78-30-02 PG.10 FIGURE 4 & 777 PT 4 78-30-03
Location:
North America
Aircraft or Engine:
177
177
Tool:
STANDARD-A1
Description:
.050" 7075-T6 ALUMINUM WITH THREE FLAT BOTTOM HOLES (2/64", 3/64", and 5/64") DRAWING "A" (PS21211.3 FOR F/A-18 OUTER WING FORWARD SPAR)
Location:
North America
Aircraft or Engine:
178
178
Tool:
STANDARD-A2
Description:
.080" 7075-T6 ALUMINUM WITH THREE FLAT BOTTOM HOLES (2/64", 3/64", and 5/64") DRAWING "A" (PS21211.3 FOR F/A-18 OUTER WING FORWARD SPAR)
Location:
North America
Aircraft or Engine:
179
179
Tool:
STANDARD-A3
Description:
.125" 7075-T6 ALUMINUM WITH THREE FLAT BOTTOM HOLES (2/64", 3/64", and 5/64") DRAWING "A" (PS21211.3 FOR F/A-18 OUTER WING FORWARD SPAR)
Location:
North America
Aircraft or Engine:
180
180
Tool:
STANDARD-B
Description:
2/64" FLAT BOTTOM HOLE EQUIVALENT SURFACE NOTCH STANDARD (*ABOVE DESCRIPTION MUST BE ENGRAVED ON THE REFERENCE STANDARD) ..DRAWING "B" (PS21211.3 FOR F/A-18 OUTER WING FORWARD SPAR) MATERIAL=7075-T6
Location:
North America
Aircraft or Engine:
181
181
Tool:
STANDARD-C
Description:
MIL-STD-2154A, STANDARD ULTRASONIC TEST BLOCK FOR AGNLE BEAM EXAMINATION, 7075-t6
Location:
North America
Aircraft or Engine:
182
182
Tool:
STD-00107021
Description:
Avcon Industries LFEC Calibration Reference Standard. BNC Document: 00107021, Rev. B Figure 7 Page 22. Material: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
183
183
Tool:
STD-1--AL
Description:
Custom Radius Channel Standard Material: 7075-T651 ALUMINUM. Standard to include a total of 62 EDM flaws identified as A, B,C, D, E, and F in the drawing. Includes test report traceable to NIST standards which comply with MIL-Q-9858A, Mil-4-45208A.
Location:
North America
Aircraft or Engine:
184
184
Tool:
STD-1-TI
Description:
Custom Radius Channel Standard Material: 6AL-4V Titanium. Standard to include a total of 62 EDM flaws identified as A, B,C, D, E, and F in the drawing. Includes test report traceable to NIST standards which comply with MIL-Q-9858A, Mil-4-45208A.
Location:
North America
Aircraft or Engine:
185
185
Tool:
STR/146/RIT/5089
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 53-20-26 PT 6 FIGURE 6&7 PAGES 12&13. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
186
186
Tool:
STR/146/RP/5139
Description:
BAE 146-RJ SERIES REFERENCE STANDARD 57-55-09 PT 6 FIGURE 6&7 PAGES 12&13. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
187
187
Tool:
T.53.03
Description:
SHORTS REFERENCE STANDARD Shorts SD 3-30, 53 pages 3-8. Material: 2024-T3 or 2014 AluminumIncludes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
188
188
Tool:
TB-16
Description:
NORTEC EDDY CURRENT STANDARD
Location:
North America
Aircraft or Engine:
189
189
Tool:
TBLFC.030-6
Description:
BLADE PROBE, .030 THICK, 6" LONG, STRAIGHT, 50-500KHZ, TRIAX FISCHER CONNECTOR, 737 PT 6 57-30-09. Includes test report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
190
190
Tool:
TEFLON TAPE/ 2.0
Description:
PTFE TEFLON TAPE ROLL, 2.0" WIDE, .003"(1MIL) THICK.
Location:
North America
Aircraft or Engine:
191
191
Tool:
TEFLON TAPE/.250
Description:
PTFE TEFLON TAPE ROLL .250" WIDE, .002"-.003" THICK
Location:
North America
Aircraft or Engine:
192
192
Tool:
TEFLON TAPE/.500
Description:
PTFE TEFLON TAPE ROLL .500" WIDE, .002"-.003" THICK
Location:
North America
Aircraft or Engine:
193
193
Tool:
TEFLON TAPE/1.0
Description:
PTFE TEFLON TAPE ROLL 1.0" WIDE, .003"(1MIL) THICK
Location:
North America
Aircraft or Engine:
194
194
Tool:
TI-6AL-4V
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: 6AL-4V TITANIUM. SIZE: 1.5"W x 3.75"L x .25"
Location:
North America
Aircraft or Engine:
195
195
Tool:
Ti-6AL-4V BLOCK
Description:
Titanium Block 110mm(3.937") x 18mm(7.09") x 15mm(.591") Block. Material: 6AL-4V. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
196
196
Tool:
Ti-6AL-6V-2sn
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: TI-6AL-6V-2SN TITANIUM. SIZE: 1.5"W x 3.75"L x .25"
Location:
North America
Aircraft or Engine:
197
197
Tool:
TP54
Description:
AIRBUS REFERENCE STANDARD A318-A321 51-63-07-PB1, PAGE 2 SHEET 01. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
198
198
Tool:
TP54-02-1
Description:
AIRBUS REFERENCE STANDARD, NTM 53-41-86, A300-600 PT 6 51-10-01, A318-A321 51-63-07-PB1, PAGE 2 SHEET 01. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
199
199
Tool:
TP54-07-1
Description:
AIRBUS SPLIT CALIBRATION REFERENCE STANDARD A318-A321 51-63-07-991-002 PB1. MATERIAL: 6AL-4V TITANIUM. Includes Test Report and Certificate of Conformance.
Location:
North America
Aircraft or Engine:
200
200
Tool:
TRS-6-12A
Description:
Custom 6 Step Wedge .020", .040", .080", .150" ,0.300", 0.600" +/-.001", Per Drawing Specification TXX003503. Material: 2219-T81 Aluminum. Includes Teflon Base.
Location:
North America
Aircraft or Engine:
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