Showing 18421 - 18440 out of 18520

Page 922 out of 926

Part Number Description Equivalents Action
CUSTOM DOUGLAS DC-8 TAP TEST TOOL FIGURE 1 PER TASK G006. MATERIAL: 7075-T6 ALUMINUM.
EDDY CURRENT BLADE PROBE, STRAIGHT, .030" THICK, 50-500KHz, 6" LONG SUPPLIED WITH A TRIAX FISCHER CONNECTOR, REFERENCE: 737 PT 6 57-30-09. Includes Test report and Certificate of Conformance.....REFERENCE: 737 PT 6 57-30-09.
PTFE TEFLON TAPE ROLL 1.0" WIDE, .003" THICK, 36 YARD ROLL. Includes Certificate of Conformance.
PTFE TEFLON TAPE ROLL, 2.0" WIDE, .002"-.003" THICK, 36 YARD ROLL.
PTFE TEFLON TAPE ROLLl .500" WIDE, .003" THICK, 36 YARD ROLL. Includes Certificate of Conformance.
FORRESTER HIGH FREQUENCY EDDY CURRENT PROBE, 2-40 KHz, SHEILDED, ABSOLUTE REFLECTION, SUPPLIED WITH A TRIAX FISCHER CONNECTOR. Includes Test Report and Certificate of Conformance.
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". Includes certification Rep...
Titanium Block 110mm(3.937") x 18mm(7.09") x 15mm(.591") Block. Material: 6AL-4V. Includes Test Report and Certificate of Conformance.
BOMBARDIER GLOBAL 5000 / 604 REFERENECE STANDARD PART 6 71-20-004 PAGE 13 FIGURE 3, 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: ...
AIRBUS REFERENCE STANDARD A318-A321 51-63-07-PB1, PAGE 2 SHEET 01. MATERIAL: 7075-T6 ALUMINUM FASTENER (1/4-20 x 2 Socket Cap Screw x2). Includes Test Report and Certificate of Conformance.
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.
AIRBUS SPLIT CALIBRATION REFERENCE STANDARD A318-A321 51-63-07-991-002 PB1. MATERIAL: 6AL-4V TITANIUM. Includes Test Report and Certificate of Conformance.
CARBON SKIN:BMS 8-256, TYPE IV, CLASS 2, 3K-70-PW (350 °F CURE)..20 PLIES(4mm)..A:20mm×20mm,EIGTH PLY..B:f40mm,SIXTEENTH PLY
CARBON SKIN:BMS 8-256, TYPE IV, CLASS 2, 3K-70-PW (350 °F CURE)..30 PLIES(6mm)..A:20mm×30mm,EIGHTH PLY..B:f30mm, TWENTIETH PLY
CARBON SKIN:BMS 8-256, TYPE IV, CLASS 2, 3K-70-PW (350 °F CURE)..40 PLIES(6mm)..A:f20mm,TENTH PLY..B:f30mm,THIRTY-FIFTH PLY
CARBON SKIN:BMS 8-256, TYPE IV, CLASS 2, 3K-70-PW (350 °F CURE)..50 PLIES(6mm)..A:20X30mm, EIGTH PLY..B:f30mm, TWENTIETH PLY
4 0z Bottle (118 ml) UltraSoniX couplant. Conforms to ASTM F519. Includes Certificate of Conformance & Datasheet.
1 Gallon Jug (3.785 liters) UltraSoniX couplant. Conforms to ASTM F519. Includes Certificate of Conformance & Datasheet.
BOEING REFERENCE STANDARD, .120" X .120" X .008"± .003" CORNER EDM NOTCH. MATERIAL: 7075-T6 Aluminum. Includes CertificatIion Report.
AIR FORCE NDT STANDARD,..WING LOWER SKIN SPLICE AT WS 360,..STRINGER S-14 THROUGH FRONT SPAR. Includes Test Report and Certificate of Conformance.
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