Electrical and Electronic Properties Measuring and Testing Instruments: 16SW3-2-S, 16U174-3, 16U42554-3
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
16SW3-2-S 16SW32S | 6625-01-385-4221 | Keyboard, Data Entry | Overall Length: 4.500 inches nominal Overall Width: 3.620 inches nominal Overall Height: 2.610 inches maximum | Honeywell International Inc. (91929) | |
16SW3-2-S-H 16SW32SH | 6625-01-385-4221 | Keyboard, Data Entry | Overall Length: 4.500 inches nominal Overall Width: 3.620 inches nominal Overall Height: 2.610 inches maximum | Honeywell International Inc. (91929) | |
16TCVMP | 6625-01-484-6108 | Generator, Function, Electronic Te | Special Features: Generator, digital, video map End Item Identification: Video mapper (v-mapp) | GM Cope - LAU Joint Venture (051K3) | |
16U129-43 16U12943 | 6625-01-303-2105 | Test set Subassembly, Electrical | Lockheed Martin Corporation (81755) | ||
16U14519-1 16U145191 | 6625-01-041-5999 | Test set, Battery | Special Features: 115VAC 50/60HZ 1 phase required Overall Length: 17.000 inches nominal Overall Width: 14.500 inches nominal | BAE Systems Information And (94117) Lockheed Martin Corporation (81755) | |
16U14519-3 16U145193 | 6625-01-100-9344 | Test set, Battery | Special Features: 115VAC 50/60HZ 1 phase required Overall Length: 17.000 inches nominal Overall Width: 14.500 inches nominal | BAE Systems Information And (94117) Lockheed Martin Corporation (81755) | |
16U14519-5 16U145195 | 6625-01-131-6238 | Test set, Battery | Special Features: 115VAC 50/60HZ 1 phase required Overall Length: 17.000 inches nominal Overall Width: 14.500 inches nominal | BAE Systems Information And (94117) Lockheed Martin Corporation (81755) | |
16U14638L1-1 16U14638L11 | 6625-01-247-4296 | Adapter, cable Breakout | Test Item Connection Method: Cable | Lockheed Martin Corporation (81755) | |
16U174-1 16U1741 | 6625-01-070-0368 | Test set Subassembly, Electrical | End Item Identification: F-16 acft age. Major Components: Printed wiring board 1; microcircuit 20; support assembly 1; resistor 17; capacitor 19; switch 2; polarizing key 2; plug 1 Mounting Configuration: Mounted type | Lockheed Martin Corporation (81755) | |
16U174-3 16U1743 | 6625-01-070-0368 | Test set Subassembly, Electrical | End Item Identification: F-16 acft age. Major Components: Printed wiring board 1; microcircuit 20; support assembly 1; resistor 17; capacitor 19; switch 2; polarizing key 2; plug 1 Mounting Configuration: Mounted type | Lockheed Martin Corporation (81755) | |
16U174-5 16U1745 | 6625-01-070-0368 | Test set Subassembly, Electrical | End Item Identification: F-16 acft age. Major Components: Printed wiring board 1; microcircuit 20; support assembly 1; resistor 17; capacitor 19; switch 2; polarizing key 2; plug 1 Mounting Configuration: Mounted type | Lockheed Martin Corporation (81755) | |
16U174-801 16U174801 | 6625-01-070-0368 | Test set Subassembly, Electrical | End Item Identification: F-16 acft age. Major Components: Printed wiring board 1; microcircuit 20; support assembly 1; resistor 17; capacitor 19; switch 2; polarizing key 2; plug 1 Mounting Configuration: Mounted type | Lockheed Martin Corporation (81755) | |
16U214-1 16U2141 | 6625-01-079-4169 | Test set Subassembly, Electrical | End Item Identification: F-16 acft age. Major Components: Printed wiring board 1; microcircuit 2 Mounting Configuration: Mounted type | Lockheed Martin Corporation (81755) | |
16U42521-5 16U425215 | 6625-01-056-4384 | Adapter, Test | Test Item Connection Method: Cable and connector | Lockheed Martin Corporation (81755) | |
16U42545-1 16U425451 | 6625-01-065-6718 | Test set, Relay | Special Features: Consists of a chassis assembly mounted in the lower half of the test equipment instrument case and interconnect cables stowed in the lid half of the case; the front panel, which contains test receptacles, switches, indicators, test jacks and the power cable receptacle, is secured into the chassis by screws; case is portable and fitted with carring handles and locking fasteners; lid is detached by opening 180 degrees and removing from the case back hinge End Item Identification: F-16A/B aircraft age Test Type for Which Designed: Aircraft relays | BAE Systems Information And (94117) Lockheed Martin Corporation (81755) | |
16U42545-3 16U425453 | 6625-01-172-0130 | Test set, Relay | Width: 22.750 inches nominal Length: 23.750 inches nominal End Item Identification: F-16A/B aircraft age | BAE Systems Information And (94117) Lockheed Martin Corporation (81755) | |
16U42545L1-1 16U42545L11 | 6625-01-065-6718 | Test set, Relay | Special Features: Consists of a chassis assembly mounted in the lower half of the test equipment instrument case and interconnect cables stowed in the lid half of the case; the front panel, which contains test receptacles, switches, indicators, test jacks and the power cable receptacle, is secured into the chassis by screws; case is portable and fitted with carring handles and locking fasteners; lid is detached by opening 180 degrees and removing from the case back hinge End Item Identification: F-16A/B aircraft age Test Type for Which Designed: Aircraft relays | Lockheed Martin Corporation (81755) | |
16U42553L1-1 16U42553L11 | 6625-01-153-8500 | Adapter, Test | Overall Length: 8.375 inches nominal Overall Width: 6.875 inches nominal End Item Identification: F-16 acft | Lockheed Martin Corporation (81755) | |
16U42554-1 16U425541 | 6625-01-124-4726 | Test set, Electronic Systems | End Item Identification: F-16 a/b aircraft Electrical Power Source Relationship: Operating Test Type for Which Designed: Tests emergency power unit frequency | BAE Systems Information And (94117) Lockheed Martin Corporation (81755) | |
16U42554-3 16U425543 | 6625-01-581-4930 | Test set, Electronic Systems | Special Features: MIL-T-21200 combination case; output 1 at 28VDC with frequency from 1135 to 1265 +/-5HZ; output 2 at 28VDC when frequency exceeds 1320 +/-12HZ Frequency Rating: 50.0 hertz minimum and 60.0 hertz maximum Phase: Single | BAE Systems Information And (94117) |