Part Number | Description | Sources Available | Tool Request Qty |
---|---|---|---|
Z261750 | PLATE TEST | 1 |
Partial Match
Part Number | Description | Sources Available | Tool Request Qty |
---|---|---|---|
(CALIB) CB602-3 | NUTPLATE PUSHOFF TESTER (CALIBRATION) | 1 | |
0061R57524-3 | UNIVERSAL TEST PLATE | 1 | |
12-851154-3-101 | TEST PLATE | 1 | |
145-44131-001 | GENERAL EDDY CURRENT TEST - PLATE, ALUMINUM 7050-T7451 (NDT) | 6 | |
145-44131-003 | PLATE, NDI-GENERAL EDDY CURRENT TEST, STEEL | 3 | |
145-44131-005 | PLATE, NDI-GENERAL EDDY CURRENT TEST, TITANIUM | 3 | |
171T17969-401 | ULTRASONIC TEST PLATE | 3 | |
188090-7002 | SMART BREECH PLATE ADAPTER (SBPA) TESTER | 1 | |
1C8074 | BLANKOFF PLATES-ENG TEST | 1 | |
1C8074G02 | BLANKOFF PLATES-ENG TEST | 1 | |
2024233-1 | TEST ADAPTER PLATE | 1 | |
216692 | Pressure Test Plate | 2 | |
216692PM | PRESSURE TEST PLATE | 1 | |
216718 | PRESSURE TEST PLATE AND PLUG | 1 | |
216719 | PRESSURE TEST PLATE AND PLUG | 1 | |
216720 | PRESSURE TEST PLATE AND PLUG | 1 | |
216746 | PRESSURE TEST PLATE AND PLUG | 1 | |
2242694 | TEST TANK ADAPTOR PLATE | 1 | |
2242977 | ADAPTOR PLATE AND PRESSURE TEST BODY | 1 | |
23068589 | Plate – Oil Test No. 6 Seal | 1 | |
2TE65B98600 | PLATE BLANKING LEAKAGE TEST | 1 | |
332A94229001 | TESTER, MGB FLEXIBLE MOUNTING PLATE | 1 | |
367 | NDT TEST PLATE | 4 | |
4952361-T | TEST PLATE ADAPTER | 1 | |
506252 | NICKEL-CHROMIUM PLATED TEST PANELS | 3 | |
52391A0003-01 | TEST ADAPTOR PLATE | 1 | |
53023-T200 | TEST ADAPTER PLATE | 1 | |
717001 | PLATE, PRESSURE TEST CAPPING | 2 | |
89ED03545-1 | PRESS TEST PLATE_[89ED03545-1] | 1 | |
89ED03545-2 | PRESS TEST PLATE_[89ED03545-2] | 1 | |
89ED03549 | PRESS TEST PLATE_[89ED03549] | 1 | |
9-55674-2 | PLATEST, | 1 | |
905824-1-1 | ADAPTER PLATE TEST MOTOR SEAL LEAKAGE | 1 | |
9924095 | PLATE LINE TEST SET | 1 | |
99D57204197000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 57-29-11-PB6 PG.11. MATERIAL: ABM3-1031(7150-T6 AL), ABM3-1029(7050-T7 AL). Includes Test Report and Certificate of Conformance. Note: Repair Plate = .236" | 1 | |
99V57103002000 | Airbus Calibration Block A350-A-571100-AFAPE3-04J2E-A-001-01 Sheet 01 Page 1-2. Material: Ti-6Al-4V ANNEALED PLATE. Includes Test Report and Certificate of Conformance. | 1 | |
A521-11527-000W6700-01 | ADAPTER PLATE FOR PRESSURE TEST | 1 | |
AC21854000 | TEST PLATE | 1 | |
AC21856000 | TEST PLATES | 1 | |
AFC-550BCS | SINGLE ELEMENT FINGER TIP END MOUNT BNC CONTACT TRANSDUCER 5.0MHZ, .500"Ø ELEMENT WITH CERAMIC WEAR PLATE. Includes Test Report and Certificate of Conformance. | 1 | |
AFNDT-2068 | CUSTOM CORROSION TEST PLATE 7075-T6 ALUMINUM. , 5%, 10%, 20%. PLATE SIZE: 8.0" x 5.0" x .125". 1.0"Ø SPOTFACE 3 PLACES. Includes Test Report and Certificate of Conformance. | 1 | |
AFNDT-2110 | CUSTOM EDDY CURRENT TEMPLATE.2024-T3 ALUMINUM .063" THICK PLATE. (SELECTED RIVETS). Includes Test Report and Certificate of Conformance. | 1 | |
AFNDT-2110-.201 | CUSTOM EDDY CURRENT TEMPLATE.2024-T3 ALUMINUM .063" THICK PLATE. (.201" DIAMETER HOLE). Includes Test Report and Certificate of Conformance. | 1 | |
AFNDT-2110-.500D | CUSTOM EDDY CURRENT TEMPLATE.2024-T3 ALUMINUM .063" THICK PLATE. (.500" DIAMETER HOLE D SHAPE). Includes Test Report and Certificate of Conformance. | 1 | |
AFNDT-2110-.812 | CUSTOM EDDY CURRENT TEMPLATE.2024-T3 ALUMINUM .063" THICK PLATE. (.812" DIAMETER HOLE). Includes Test Report and Certificate of Conformance. | 1 | |
AFNDT-2110-.950 | CUSTOM EDDY CURRENT TEMPLATE.2024-T3 ALUMINUM .063" THICK PLATE. (.950" DIAMETER HOLE). Includes Test Report and Certificate of Conformance. | 1 | |
AFNDT-2110-1.06 | CUSTOM EDDY CURRENT TEMPLATE.2024-T3 ALUMINUM .063" THICK PLATE. (1.06" DIAMETER HOLE). 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-3112 | Custom Bolt hole Standard, Hole Sizes; 1/8", 5/32", 3/16", 1/4", inch diameter Holes. .020" Thru EDM notches .005" Wide(+/- .001"). Material: 2024-T3 Aluminum. Plate Size: 2.0" x 4.0" x 0.250". Includes Test Report and Certificate of Conformance. | 1 | |
AFNDT-3112/2014-T6 | Custom Bolt hole Standard, Hole Sizes; 1/8", 5/32", 3/16", 1/4", inch diameter Holes. .020" Thru EDM notches .005" Wide(+/- .001"). Material: 2014-T6 Aluminum. Plate Size: 2.0" x 5.0" x 0.250". Includes Test Report and Certificate of Conformance. | 1 | |
AFNDT-3112/2024-T6 | Custom Bolt hole Standard, Hole Sizes; 1/8", 5/32", 3/16", 1/4", inch diameter Holes. .020" Thru EDM notches .005" Wide(+/- .001"). Material: 2024-T6 Aluminum. Plate Size: 2.0" x 5.0" x 0.250". Includes Test Report and Certificate of Conformance. | 1 | |
AFNDT-3113 | Custom Bolt hole Standard, Hole Size; 5/8"Ø inch diameter Hole. .020" Thru EDM notch .005" Wide(+/- .001"). Material: 7075-T6 Aluminum. Plate Size: 2.0" x 2.0" x 0.250". Includes Test Report and Certificate of Conformance. | 1 | |
AFNDT-3166AL | CUSTOM 13 HOLE REFERENCE 3 PLATE STANDARD, 7075-T6 ALUMINUM. HOLE SIZES: 5/32, 3/16, 7/32, 1/4, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8, 3/4, 7/8, 1.0". Includes Test Report and Certificate of Conformance. | 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-3309AL | Custom Thin Plate Surface Standard. 7075-T76 Aluminum 10.0" x 10.0" x .050". 3 Surface EDM Notches ±.001" on Width. 1.) 0.010" x 0.200" x .004"W 2.) 0.015" x 0.200" x .004"W 3.) 0.020" x 0.200" x .004"W. Includes Test Report and Certificate of Conform | 1 | |
AFNDT-3348/4340 | 7 STEP METRIC WEDGE: Step Sizes: 1mm, 3mm, 5mm, 10mm, 15mm, 20mm, 25mm +/- .05mm . Pad Size: 20mm x 20mm. Supplied With Holding Block. Material- 4340 Steel (Nickle Plated for Corrosion Protection). Includes Test Report and Certificate of Conformance. Manu | 1 | |
AFNDT-3413 | Custom Boeing Eddy Current Hole Standard. Hole Sizes: .159 & .190"Ø. With one of each hole size plugged. Material: 2024-T3 Aluminum. Plugged holes contain a BACR15BA6A8C Rivet in the .056" plate. Apply BMS 545 sealant between each layer Includes Test Repo | 1 | |
AT1511/2 | TEST FITTING OIL INLET/OUTLET/BASEPLATE | 1 | |
B27028-8 | PLATE TEST EQP TORQUE LIMITER | 1 | |
BTR-57524-3 | UNIVERSAL TEST PLATE | 1 | |
CB602-3 | 3/16 NUTPLATE PUSH OFF TESTER | 1 | |
CB602-3-325 | NUT PLATE PUSH OFF TESTER | 2 | |
CD-14778 | TEST STAND MOUNTING PLATE | 1 | |
D1545-8673 | Plate-Pneumatic Test | 1 | |
DAH6026-32 | TEST PLATE | 1 | |
DAH602622 | DOOR SELECTOR TEST PLATE | 8 | |
E190-57-001 | TEST PLATE NDT | 1 | |
ECS-TE6013 | TEST PLATE ASSEMBLY, UNIVERSAL, 787 FANS | 1 | |
F65-0-3098-41 | Detail 41 (DLD Cover Plate), Nose Gear Steering Test Fixture | 1 | |
F70194-1 | VERTICAL GYRO TEST PLATE | 4 | |
F71213-48 | TEST PLATE ASSY | 1 | |
F71327 | PLATE ASSY -0 BOOST PUMP CAVITY LEAK TEST USED | 1 | |
F80258-2 | CLOSURE PLATE ASSY TEST EQUIP | 1 | |
Figure 4.E.-4 | Honeywell Positioning Plate and Spacers, 32-49-01 page 4.E.-5. Includes Test Report and Certificate of Conformance. | 1 | |
G28017-5 | TEST PLATE | 1 | |
G36047-1 | BLANKING PLATE - LEAK TEST, PRESSURE COMPENSATOR DUCT | 2 | |
GS13277 | PLATE ASSY IGV TEST | 1 | |
GS13798-1 | PLATE PRESSURE TEST | 2 | |
GS14204-1 | PLATE PRESSURE TEST | 1 | |
GS19660-1 | PLATE, PRESSURE TEST | 1 | |
GS19758-1 | PLATE, PRESSURE TEST | 1 | |
GS24014-2 | PLATE, PRESSURE TEST | 1 | |
HS7545 | MECHANICAL PULLER - TEST FLOW PLATE, PUMP HOUSING | 1 | |
HTET10321 | TEST PLATE | 1 | |
HTET7052-13 | TEST PLATE | 1 | |
IND81086 | PLATE-BASE,TEST | 1 | |
M46290 | ”ELECTRO SELECTOR” TEST PLATE | 1 | |
M82000228 | TEST PLATE | 1 | |
MIT65B90101 | BLANKING PLATE - LEAKAGE TEST, ENGINE PRECOOLER | 1 | |
MS33786-40-T | TEST PLATE (2 IT) | 1 | |
NDT1087-11 | BOEING REFERENCE STANDARD, 757 Part 6 53-00-11. Plate Thickness: Upper 1 - 0.140 / Lower 2 - 0.080. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
NDT1087-12 | BOEING REFERENCE STANDARD, 757 Part 6 53-00-11. Plate Thickness: Upper 1 - 0.120 / Lower 2 - 0.063. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
NDT1087-13 | BOEING REFERENCE STANDARD, 757 Part 6 53-00-11. Plate Thickness: Upper 1 - 0.140 / Lower 2 - 0.063. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
NDT1087-14 | BOEING REFERENCE STANDARD, 757 Part 6 53-00-11. Plate Thickness: Upper 1 - 0.160 / Lower 2 - 0.100. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
NDT3065 | NDT TEST PLATE | 3 | |
NDT3114 | Standard, Bonded Test Coupons, .032 thick coupons over .036 bottom plate | 1 | |
NDT3115 | Standard, Bonded Test Coupons, .080 thick coupons over .080 bottom plate | 1 | |
NDT4251 | BOEING REFERENCE STANDARD 747 Part 4 57-30-11 Page 11 Figure 2. Material: Aircraft Qualtiy Alimunim Plate, Any 2024 and 7075. Includes Test Report and Certificate of Conformance. | 1 | |
NDT6025-1 | BOEING REFERENCE STANDARD 767 PART 4 57-50-17 FIGURE 2 PAGE 6. MATERIAL MUST BE MANUFACTURE OUT OF 7075-T6 PLATE WITH GRAIN DIRECTION. Includes Test Report and Certificate of Conformance. | 1 | |
NDT6025-2 | BOEING REFERENCE STANDARD 767 PART 4 57-50-17 FIGURE 2 PAGE 6. MATERIAL MUST BE MANUFACTURE OUT OF 7075-T6 PLATE WITH GRAIN DIRECTION. Includes Test Report and Certificate of Conformance. | 1 | |
NDT6025-3 | BOEING REFERENCE STANDARD 767 PART 4 57-50-17 FIGURE 2 PAGE 6. MATERIAL MUST BE MANUFACTURE OUT OF 7075-T6 PLATE WITH GRAIN DIRECTION. Includes Test Report and Certificate of Conformance. | 1 | |
NDT6025-4 | BOEING REFERENCE STANDARD 767 PART 4 57-50-17 FIGURE 2 PAGE 6. MATERIAL MUST BE MANUFACTURE OUT OF 7075-T6 PLATE WITH GRAIN DIRECTION. Includes Test Report and Certificate of Conformance. | 1 | |
NDT6025-5 | BOEING REFERENCE STANDARD 767 PART 4 57-50-17 FIGURE 2 PAGE 6. MATERIAL MUST BE MANUFACTURE OUT OF 7075-T6 PLATE WITH GRAIN DIRECTION. Includes Test Report and Certificate of Conformance. | 2 | |
NDT6025-6 | BOEING REFERENCE STANDARD 767 PART 4 57-50-17 FIGURE 2 PAGE 6. MATERIAL MUST BE MANUFACTURE OUT OF 7075-T6 PLATE WITH GRAIN DIRECTION. Includes Test Report and Certificate of Conformance. | 2 | |
NS09IND01035 | OTC 6599 TEST PLATES | 1 | |
PT421-203M | Static Pre-Test Plate | 1 | |
PTS21025 | Static Pre-Test Plate | 1 | |
PTS3133R | Pre-Test Plate | 1 | |
PTS8175 | (Static Pre-Test Plate) | 1 | |
PWA 26120 | PLATESTG 2HPT TOOL | 2 | |
PWA 85287 | PLATE, AIRFLOW TEST | 1 | |
PWA 88206 | PLATE, AIRFLOW TEST | 1 | |
PWA26934 | PLATE - PRESS TEST IMC,FRONT_[PWA26934] | 2 | |
PWA28181C | PLATE - PRESSURE TEST IMC REAR_[PWA28181C] | 1 | |
PWA80821 | PLATE BLOCK OFF OIL SYSTEM LEAK TEST | 1 | |
PWC 54613-B | PLATE FUEL LEAK TEST | 1 | |
PWC30859 | press. test fixture plate | 4 | |
Q21911 | Q21911 COVER PLATE (FOR TESTING) | 2 | |
Q21912 | Q21912 COVER PLATE (FOR TESTING) | 2 | |
Q21966 | SERVO VALVE TEST PLATE | 1 | |
Q21966000 | TEST PLATE | 2 | |
Q21968 | ELECTRO DISTRIBUTOR TEST PLATE | 2 | |
R46218 | LEAKAGE TEST PLATE | 1 | |
SB10270203-5 | 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. | 1 | |
SBE1193 | LEAKAGE TEST PLATE | 1 | |
SKWR512 | 3/4IN R TEST PLATE | 1 | |
SKWR516 | 1IN R TEST PLATE | 1 | |
SKWR520 | 1 1/4IN R TEST PLATE | 1 | |
ST-483 | TEST PLATE | 1 | |
T335772 | TCAS ANTENNA TESTS TEMPLATES | 1 | |
T7052-13 | TEST PLATE | 1 | |
TE65B98600 | BLANKING PLATE - LEAKAGE TEST, APU BLEED AIR | 4 | |
UM6989030000000 | PICK-OFF PLUGS OR TEST PLATE | 1 | |
USD6146510 | ATR NDT TEST PLATE | 1 | |
UZ9605010000000 | PRESSURE TEST PLATE | 1 | |
XX27624 | TEST PLATE | 1 |
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