| Part Number | Description | Sources Available | Tool Request Qty |
|---|---|---|---|
| 31300-00000-100 | DRAWING | 1 | |
| 856A3926G01 | DRAWING | 1 | |
| PWC80505 | DRAWING | 1 | |
| SE05000901 | DRAWING | 1 | |
| SE05252902 | DRAWING | 1 | |
| SE251021131 | DRAWING | 1 | |
| SE35102182 | DRAWING | 1 | |
| SE35102192 | DRAWING | 1 | |
| SE35812101 | DRAWING | 1 | |
| SE45807901 | DRAWING | 1 |
Partial Match
| Part Number | Description | Sources Available | Tool Request Qty |
|---|---|---|---|
| 0180-3010000 | HELI-COIL WITHDRAWING TOOL | 3 | |
| 0781314007 | HINGE PIN / SCREW, DRAWING ITEM -20 | 1 | |
| 10/3641 | FISHPOLE HOIST KIT DRAWING NO 10/3641 CONFIG.3 | 2 | |
| 105-14101 W1 | H145 DRAWING TOOL | 1 | |
| 10C2428P01 | DRAWING TOOLING | 1 | |
| 2000DD10980-1 | Aluminum CAL Standard, United Airlines Drawing No. 2000DD10980 REV D | 1 | |
| 2000DD10980-3 | Steel CAL Standard, United Airlines Drawing No. 2000DD10980 REV D | 1 | |
| 2000DD10980-5 | Titanium CAL Standard, United Airlines Drawing No. 2000DD10980 REV D | 1 | |
| 208 FRONT SPAR | CESSNA / TEXTRON AVIATION EDDY CURRENT REFERENCE STANDARD 208 FRONT SPAR LOWER CAP. Drawing NO. 2683201 | 1 | |
| 208 REAR SPAR | CESSNA / TEXTRON AVIATION EDDY CURRENT REFERENCE STANDARD 208 REAR SPAR LOWER CAP. Drawing NO. 2683202 | 1 | |
| 262A | Boeing Standard, 727 PART6 53-10-27, Drawing No. Fig 11 Sheet 7 | 1 | |
| 2801787 | DEFACTOMETER 1.837 AIRBUS HFEC INSPECTION KIT DRAWING NO . 1.837.69-0038 | 1 | |
| 2PRE65B94003 | PLUG - TURBINE REVERSER EXIT NOZZLE, CF6-50 ENGINE (SPECIFICATION DRAWING) | 1 | |
| 3727073-1 | CARBON SEAL DRAWING TOOL | 1 | |
| 407-XMSN | 407 TRANSMISSION SHIMS PER BELL'S ORIGINAL SHIM DRAWING, $1000 PER SET OF FOUR (4) | 1 | |
| 601967-9 | NO DRAWING *A.S.I.* | 1 | |
| 65C28106 | REPAIR DRAWING | 1 | |
| 708-666 | MAIN DRAWING CRIMPING TOOL | 1 | |
| 82700011-001-138 | TOOL-AILERON RIGGING (DRAWING AND MYLAR TEMPLATE) | 1 | |
| 83707 | FLUSH CART - ENGINE IDG COOLING SYSTEM, PER BOEING SPEC. DRAWING A71040 | 1 | |
| 85517021-001-138 | TOOL-LEFT ELEVATOR RIGGING (DRAWING AND MYLAR TEMPLATE) | 4 | |
| 85517021-002-138 | TOOL-RIGHT ELEVATOR RIGGING (DRAWING AND MYLAR TEMPLATE) | 4 | |
| 856A2953 | Partial drawing | 2 | |
| 856A3724G02 | Sighting Tool Set- ( only have G01 drawings) | 8 | |
| 85740007-S901-138 | TOOL-AILERON TRIM TAB RIGGING (DRAWING AND MYLAR TEMPLATE) | 2 | |
| 85740007-S903-138 | TOOL-L/H GEAR TAB RIGGING (DRAWING AND MYLAR TEMPLATE) | 1 | |
| 85740007-S904-138 | TOOL-R/H GEAR TAB RIGGING (DRAWING AND MYLAR TEMPLATE) | 1 | |
| 85740009-S903-138 | TOOL-TRIM TAB RIGGING (DRAWING AND MYLAR TEMPLATE) | 2 | |
| 85741000-001-138 | TOOL-AILERON RIGGING (DRAWING AND MYLAR TEMPLATE) | 2 | |
| 85741000-003-138 | TOOL-LEFT GEAR TAB RIGGING (DRAWING AND MYLAR TEMPLATE) | 2 | |
| 85741000-004-138 | TOOL-RIGHT GEAR TAB RIGGING (DRAWING AND MYLAR TEMPLATE) | 2 | |
| 8DK4354 - 001 | DRAWING KIT RUDDER ACTUATOR BRACS NUTS INSPECTION AND RECTIFICATION | 1 | |
| 8DK4354-001 | DRAWING KIT RUDDER ACTUATOR BRACS NUTS INSPECTION AND RECTIFICATION | 1 | |
| 9829-0012 | FLUSH CART - ENGINE IDG COOLING SYSTEM, PER BOEING SPEC. DRAWING A71040 | 1 | |
| 98A57103017000 | Airbus Standard, A300-600 FIG4 see drawing provided | 1 | |
| 98D28108658000 | TEST TOOL - PRESSURE, ACT( replaces 98D28108417000)- No Drawing !!!!!!!!!!!!! | 11 | |
| 98D71203500.213 | KNURLED NUT, DRAWING ITEM -21 | 1 | |
| 98F29208217018 | SPRING AS PER DRAWING | 1 | |
| 98S21305000000 | DRAWING PARTS 98S21305000000 ATR | 1 | |
| 98S53005021-000 | ATR72 Calibration Standard Drawing PT6 53-51-01 PG 608, Figure 601 | 3 | |
| 98S57105015 | Calibration Standard Drawing 57-14-03, Figure 401 | 1 | |
| 98S57105032-200 | ATR72 Calibration Standard Drawing PT4 57-12-12 PG 404, Figure 401 | 3 | |
| 98S57105032-202 | ATR72 Calibration Standard Drawing PT4 57-12-12 PG 405, Figure 402 | 3 | |
| 98S57105033-200 | ATR42 CALIBRATION STANDARD DRAWING PT4 57-12-11 PG 404, FIGURE 401 | 1 | |
| 98S57205030-004 | COMPOSITE LIGHTNING REFERENCE STANDARD..FOR ATR72 PT 4 51-40-00: REFERENCE DRAWING | 5 | |
| 98S57205030.001 | COMPOSITE LIGHTNING REFERENCE STANDARD..FOR ATR72 PT 4 51-40-00: REFERENCE DRAWING | 4 | |
| 98S57205030.004 | COMPOSITE LIGHTNING REFERENCE STANDARD..FOR ATR72 PT 4 51-40-00: REFERENCE DRAWING | 5 | |
| 98S57205030001 | CALIBRATION STANDARD, ATR72, DRAWING REF: 22S57213396 | 4 | |
| 98S57205030003 | CALIBRATION STANDARD, ATR72, DRAWING REF: 22S5721 | 2 | |
| 98S57205030004 | CALIBRATION STANDARD, ATR72, DRAWING REF: 22S57213396 | 5 | |
| A25012-19 | ELECTRICAL TEST EQUIPMENT - OFF-WING ESCAPE SLIDE SYSTEM (LIMITED APPLICABILITY ON A25012-19 PER A25012 GSE DRAWING) | 2 | |
| A25012-29 | ELECTRICAL TEST EQUIPMENT - OFF-WING ESCAPE SLIDE SYSTEM (LIMITED APPLICABILITY ON A25012-19 PER A25012 GSE DRAWING) | 2 | |
| A26001-131 | ADAPTER CABLE - ENGINE/APU FIRE BOTTLE SQUIB (REFER TO USAGE TABLE IN THE A26001 TOOL DRAWING FOR REQUIRED CABLES) | 6 | |
| A26001-134 | ADAPTER CABLE - CARGO FIRE BOTTLE SQUIB (REFER TO USAGE TABLE IN THE A26001 TOOL DRAWING FOR THE REQUIRED CABLE(S)) | 5 | |
| A26001-135 | ADAPTER CABLE - ENGINE/APU FIRE BOTTLE SQUIB (REFER TO USAGE TABLE IN THE A26001 TOOL DRAWING FOR REQUIRED CABLES) | 7 | |
| A26001-136 | ADAPTER CABLE - ENGINE FIRE BOTTLE SQUIB (REFER TO USAGE TABLE IN THE A26001 TOOL DRAWING FOR REQUIRED CABLES) | 4 | |
| A26001-137 | ADAPTER CABLE - ENGINE/APU FIRE BOTTLE SQUIB (REFER TO USAGE TABLE IN THE A26001 TOOL DRAWING FOR REQUIRED CABLES) | 6 | |
| A26001-138 | ADAPTER CABLE - ENGINE/APU FIRE BOTTLE SQUIB (REFER TO USAGE TABLE IN THE A26001 TOOL DRAWING FOR REQUIRED CABLES) | 5 | |
| A26001-139 | ADAPTER CABLE - ENGINE/APU FIRE BOTTLE SQUIB (REFER TO USAGE TABLE IN THE A26001 TOOL DRAWING FOR REQUIRED CABLES) | 6 | |
| A26001-144 | ADAPTER CABLE - ENGINE FIRE BOTTLE SQUIB (REFER TO USAGE TABLE IN THE A26001 TOOL DRAWING FOR REQUIRED CABLES) | 4 | |
| A26001-145 | ADAPTER CABLE - ENGINE FIRE BOTTLE SQUIB (REFER TO USAGE TABLE IN THE A26001 TOOL DRAWING FOR REQUIRED CABLES) | 4 | |
| A26001-148 | ADAPTER CABLE - CARGO FIRE BOTTLE SQUIB (REFER TO USAGE TABLE IN THE A26001 TOOL DRAWING FOR THE REQUIRED CABLE(S)) | 5 | |
| A26001-175 | ADAPTER CABLE - ENGINE FIRE BOTTLE SQUIB (REFER TO USAGE TABLE IN THE A26001 TOOL DRAWING FOR REQUIRED CABLES) | 6 | |
| A26001-176 | ADAPTER CABLE - ENGINE FIRE BOTTLE SQUIB (REFER TO USAGE TABLE IN THE A26001 TOOL DRAWING FOR REQUIRED CABLES) | 5 | |
| A26001-192 | ADAPTER CABLE - ENGINE/APU FIRE BOTTLE SQUIB (REFER TO USAGE TABLE IN THE A26001 TOOL DRAWING FOR REQUIRED CABLES) | 5 | |
| A26001-24 | ADAPTER CABLE - ENGINE/APU FIRE BOTTLE SQUIB (REFER TO USAGE TABLE IN THE A26001 TOOL DRAWING FOR REQUIRED CABLES) | 4 | |
| A26001-4 | ADAPTER CABLE - ENGINE/APU FIRE BOTTLE SQUIB (REFER TO USAGE TABLE IN THE A26001 TOOL DRAWING FOR REQUIRED CABLES) | 1 | |
| A26001-5 | ADAPTER CABLE - ENGINE FIRE BOTTLE SQUIB (REFER TO USAGE TABLE IN THE A26001 TOOL DRAWING FOR REQUIRED CABLES) | 2 | |
| AFNDT-2160/19MM | Custom ASME ultrasonic phased array PAUT Calibration Block per customer supplied drawing. 270mm x 150mm x 19mm. Material: 1018 Carbon Steel. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2160/38MM | Custom ASME ultrasonic phased array PAUT Calibration Block per customer supplied drawing. 330mm x 150mm x 38mm. Material: 1018 Carbon Steel. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3019S | CUSTOM AIR FORCE EDDY CURRENT BOLT HOLE STANDARD PER CUSTOMER SUPPLIED DRAWING, 1/4" 8630 STEEL PLATE (4130 EQUIVALENT ALTERNATIVE). EDM: 0.030 x 0.030 CORNER NOTCH. HOLE DIAMETER= 0.437Ø. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3059 | Custom Eddy Current 2 Hole Calibration Standard per Customer Supplied Drawing. Material: 7050-T7451. Hole Sizes: .516"Ø and .812"Ø with a total of 4 EDM Notches 0.021" x 0.021" x .004" Wide Max. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3060 | Custom Eddy Current 2 Hole Calibration Standard per Customer Supplied Drawing. Material: 7050-T7451. Hole Sizes: .252"Ø and .516"Ø with a total of 4 EDM Notches 0.021" x 0.021" x .004" Wide Max. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3071 | Custom designed eddy current multi-layer aircraft aluminum skin test specimen, drawing 2, sheets 1-4. reference standard for Central Piedmont Community College. Material: 2024-T3 Aluminum. Includes Certification Report Traceable to NIST. | 1 | |
| AFNDT-3072 | Custom designed eddy current aircraft calibration standard, Drawing 3, Sheets 1-3, for Central Piedmont Community College. Material: 2024-T3 Aluminum. Includes Certification Report Traceable to NIST. | 1 | |
| AFNDT-3290AL | Custom ST Aerospace Engineering Multi-Hole Standard 2 Plate Assembly, Manufactured to the Customer Supplied Drawing Specifications . Material: 7075-T6 Aluminum. 6 Total Hole Sizes to be determined. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-PR-T-2521/22 | CUSTOM EDDY CURRENT SURFACE CALIBRATION BLOCK. PER CUSTOMER SUPPLIED DRAWING. MATERIAL: 7075-T6 Aluminum. EDM Notch size 1mm (.040') , .76mm(.030"), .2mm(.008") deep x .1mm(.004") wide +/- .002". Includes Test Report and Certificate of Conformance. | 1 | |
| AMS2630C Custom | Custom Reference Standard Per SAE AMS2630C. material: Titanium Alloy, Ti6Al4V per AMS-4928R Annealed. Includes 2 EDM Flaws per customer supplied Drawing. Includes Test Report Traceable to NIST and Certificate of Conformance. | 1 | |
| B27067-1 | Check Drawing | 7 | |
| B28005-2 | CHECK DRAWINGS | 2 | |
| B71001-271 | CHECK DRAWING | 2 | |
| B71001-313 | CHECK DRAWING | 4 | |
| B71040-10 | ROPE ASSY AS PER DRAWING | 1 | |
| C-130 FIXTURE | Custom C-130 Blade Inside Bushing Probe Fixture per Drawing No. 201757983. Material: ABS Plastic machined not 3D Printed. | 1 | |
| C27001-24 | CHECK DRAWING | 4 | |
| C27001-25 | Check Drawing | 2 | |
| C32037-1 | Check Drawing | 10 | |
| C652-103SP | RIVET SET, CUSTOM DRAWING | 1 | |
| DHC-29444 | Q400 Reference Standard, De Havilland Drawing No DHC29444-01 | 1 | |
| DHC-29444-001 | Q400 Reference Standard, De Havilland Drawing No DHC29444-001 | 1 | |
| F70063 | KIT -0 PLUG SHIELD AND COVER KIT DRAWING LISTING | 1 | |
| F72978 | COPY OF DRAWING | 1 | |
| G601R274001-101 | DRAWING - HORIZONTAL-STABILIZER LIFTING FIXTURE | 2 | |
| G601R551000-1 | DRAWING - HORIZONTAL-STABILIZER LIFT | 1 | |
| G601R551000???1 | DRAWING HORIZONTAL STABILIZER LIFTING FIXTURE | 1 | |
| G601R551000−1 | DRAWING − HORIZONTAL−STABILIZER LIFTING FIXTURE | 1 | |
| G601R551000−1 | Drawing − Horizontal−Stabilizer Lifting Fixture | 1 | |
| GSB2712002 | TOOL-AILERON RIGGING (DRAWING AND MYLAR TEMPLATE) | 1 | |
| GSB2712003 | TOOL-AILERON TRIM TAB RIGGING (DRAWING AND MYLAR TEMPLATE) | 1 | |
| GSB2712004 | TOOL-TAB RIGGING (DRAWING AND MYLAR TEMPLATE) | 3 | |
| GSB2712005 | TOOL-TRIM TAB RIGGING (DRAWING AND MYLAR TEMPLATE) | 1 | |
| GSB2712005| | TOOL-TRIM TAB RIGGING (DRAWING AND MYLAR TEMPLATE) | 1 | |
| GSB2712006 | TOOL-L/H GEAR TAB RIGGING (DRAWING AND MYLAR TEMPLATE) | 1 | |
| GSB2712007 | TOOL-R/H GEAR TAB RIGGING (DRAWING AND MYLAR TEMPLATE) | 1 | |
| GSB2715001 | TOOL-LEFT GEAR TAB RIGGING (DRAWING AND MYLAR TEMPLATE) | 3 | |
| GSB2715002 | TOOL-RIGHT GEAR TAB RIGGING (DRAWING AND MYLAR TEMPLATE) | 2 | |
| GSB2715003 | TOOL-LEFT ELEVATOR RIGGING (DRAWING AND MYLAR TEMPLATE) | 2 | |
| GSB2715004 | TOOL-RIGHT ELEVATOR RIGGING (DRAWING AND MYLAR TEMPLATE) | 1 | |
| GSB2715005 | TOOL-AILERON RIGGING (DRAWING AND MYLAR TEMPLATE) | 4 | |
| H150E-1000-20-DOC | DOCUMENT/DRAWING PACKAGE | 1 | |
| HP-6000-50-DOC | DOCUMENT/DRAWING PACKAGE | 1 | |
| HP-6000-60-DOC | DOCUMENT/DRAWING PACKAGE | 1 | |
| HUOK 2012 -1/4 ASP | FASTENER DRAWING TOOL | 1 | |
| J26004-49 | Cable - Fire Extinguishing System (Cargo/LLAR): Refer To The Tool Drawing, Usage Table, To Determine The Required Cables. | 7 | |
| K1025S | ENVELOPE DRAWING POSITIONER | 4 | |
| M47382-200 | New drawing- Guide cone- Brakes | 1 | |
| MITSM112T5435-2 | TOOL DRAWING(COPY) | 1 | |
| MITSM112T5435-3 | TOOL DRAWING(COPY) | 1 | |
| MITSM112T5435-4 | TOOL DRAWING(COPY) | 1 | |
| MITSM112T5435-5 | TOOL DRAWING(COPY) | 1 | |
| NDT1087-R&D V4 | 3 plates per customer drawing | 1 | |
| NDT1088-036X2/050-B | Boeing Reference Standard, Bare, Drawing Provided | 1 | |
| NDT1088-036X2/050-C | Boeing Reference Standard, Drawing Provided | 1 | |
| NDT1088-250/250 | Boeing Standard, Drawing Provided, Figure 2 | 1 | |
| NDT1099G-P1 | BEOING REFERENCE STANDARD 757 Part 4 53-30-04 Page 15-17 Figure 3. Material: Delrin. *** SEE FINALIZED DRAWING*** | 1 | |
| NDT251 | Boeing Standard, 727 PT6 57-30-27:PG30 FIG3 SHEET6, engrave per drawing | 1 | |
| NDT262 | Boeing Standard, 727 PART6 53-10-27, Drawing No. Fig 11 Sheet 8 | 1 | |
| NDT263 | Boeing Standard, 727 PART6 53-10-27, Drawing No. Fig6, Page 29 | 1 | |
| NDT3038P1 | Reference Standard, 737 PART4 57-50-02 **SEE NEW DRAWING** (DM) | 3 | |
| NDT650 | Boeing Standard, 767 PART6 57-04-01, Drawing No. FIG 2 | 2 | |
| NDT688 | Boeing Standard, 767 PT4 57-50-03:PG8 FIG2 **** USE NEW DRAWING**** | 3 | |
| P/N: 171 865 | QTY, 1 EA NUTADAPTOR;OEM P/N: BL171865D18570.0703OEM: SPXL/SPIETHOEM P/N: 171 865OEM: BRAN LUEBBE;DRAWING: SA-JER-AR141-ARBX-270013 (H3-OA3)POS: NO.40;MATERIAL: CARBON STEELMATERIAL GRADE: 5.8;THREAD DIAMETER: M16THREAD PITCH: 1.5 MMTHREAD SERIES: METRI | 1 | |
| PDL 1034 | Calibration Standard, C130 SMP 515-C-NDI 20-40-00:FIG18 PG26, engrave per drawing Standard | 1 | |
| PDL 1034/1040 | Calibration Standard, C130 SMP 515-C-NDI 20-40-00:FIG18 PG26, engrave per drawing Standard + Guide | 1 | |
| PDL 1034J | Calibration Standard, C130 SMP 515-C-NDI 20-40-00:FIG18 PG26, engrave per drawing Standard | 1 | |
| PDL 1034J/1040J | Calibration Standard, C130 SMP 515-C-NDI 20-40-00:FIG18 PG26 & PG27, engrave per drawing, Standard + Guide | 2 | |
| PM81458 | BOX COMPLETE WITH WOODEN BLOCKS AS PER DRAWING | 1 | |
| PRE65B94003 | PLUG - FAN REVERSER EXIT NOZZLE, CF6-50 ENGINE (SPECIFICATION DRAWING) | 1 | |
| PWA107103 | KIT,DRAWINGS-ALL 4 MOUNT SUPPORTS | 1 | |
| PWA23985 | DRAWING WRENCH_[PWA23985] | 1 | |
| PWC31217 | ICD,DRAWING ONLY | 1 | |
| PWC90034 | RIVETER SOURCE CONTROL DRAWING | 3 | |
| RH-4-37 | 4-37 Reference Standard, 7075-T6 Aluminum, per drawing | 1 | |
| S41-E1A | BOEING CUSTOM REFERENCE STANDARD MCU ESM S41-E1A NDI REF STD PER DRAWING SK667-00011. | 1 | |
| S41-E1C | BOEING CUSTOM REFERENCE STANDARD MCU ESM S41-E1C NDI REF STD PER DRAWING SK667-00012. | 1 | |
| S41-F1B | BOEING CUSTOM REFERENCE STANDARD MCU ESM S41-F1B NDI REF STD PER DRAWING SK667-00010. | 1 | |
| SB 146/53-167/2 | BAe 146 Series/ AVRO 146-RJ Series PG 23-24 Drawing 15 & 16 | 1 | |
| SLS-123456-SS304 | 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. | 1 | |
| SN11570000 | MD-11 Access Door Cutout, DRAWING SN11570000:SHEET9 FIG2 | 1 | |
| SO111-7 | 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. | 1 | |
| ST2580-267 | Wrench - Spanner, Adapter For BACN10RF Nuts. (See ST2580-267 Drawing For Correct Dash Number) | 13 | |
| ST2580-267-XX-X-X | SPANNER WRENCH ADAPTER FOR BACN10RF NUTS. (ST2580-267 DRAWING) | 1 | |
| STANDARD-A1 | .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) | 1 | |
| STANDARD-A2 | .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) | 1 | |
| STANDARD-A3 | .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) | 1 | |
| STANDARD-B | 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 | 1 | |
| STD-1--AL | 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. | 1 | |
| STD-1-TI | 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. | 1 | |
| TE65B00112 | PRESSURE TEST SEAL PLUG INSTALLATION DRAWING WING SECTION 12 | 1 | |
| TOILET TEST BOX | TOILET CUBICLE TEST BOX AND DRAWINGS | 1 | |
| TRS-6-12A | Custom 6 Step Wedge .020", .040", .080", .150" ,0.300", 0.600" +/-.001", Per Drawing Specification TXX003503. Material: 2219-T81 Aluminum. Includes Teflon Base. | 1 | |
| TRS-6-12I | Custom 6 Step Wedge .040", .050", .060", .075" ,0.090", 0.110" +/-.001", Per Drawing Specification TXX003461. Material: 718 Inconel. Includes Teflon Base. | 1 |
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