Aerospace Engineering Solutions is proud to offer immediate purchasing options on Lockheed Martin Corporation part number 376596-1, a Panel Indicating Li product we carry that is listed with the NSN 6220-00-650-4216 for ease of identification. If you would like to learn more about this item, be sure to complete the Request for Quote (RFQ) form provided on this page. By including essential details like your target price, desired quantity, and expected fulfillment timeline, you are ensured a fully customized quote from our team.
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For your reference, this product is traceable to Lockheed Martin Corporation through the CAGE Code 98897, as well as categorized under FSC 6220 Electric Vehicular lights and Fixtures based on the first four digits of the NSN 6220-00-650-4216. Using such information, you can easily narrow down exact items of need for an ease of procurement. With our quotation service in mind, be sure to submit a completed form when you are ready to begin. Should you wish to speak with one of our representatives to discuss services, you can also give us a call or email at your convenience. With all that we offer, choose Aerospace Engineering Solutions for part number 376596-1 and other NSN items of need.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 6220-00-650-4216 Item PartTypeName: PANEL,INDICATING,LIGHT TRANSMITT | 6220 | 006504216 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 376596-1 | 2 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ACYN | AC VOLTAGE RATING | 115.0 VOLTS NOMINAL |
| ACZB | FREQUENCY RATING | 400.0 HERTZ NOMINAL |
| ADUM | OVERALL THICKNESS | 0.240 INCHES NOMINAL |
| ANJG | PANEL MATERIAL | PLASTIC |
| FEAT | SPECIAL FEATURES | THE LIGHT SOURCE MAY BE INCANDESCENT,LED OR EL. THE INCANDESCENT LAMPS SHALL MEET THE REQUIREMENTS OF MIL-DTL-6363 (INCLUDING VIBRATION) AND ONE OF THE FOLLOWING DRAWINGS: MS90451 OR MS90452 |
| FTLD | FUNCTIONAL DESCRIPTION | AIRCRAFT INSTRUMENT PANEL,ILLUMINATED |
| SPCL | SPECIAL TEST FEATURES | THE PANELS SHALL BE SUBJECTED TO THE ALTITUDE TEST OF 30 MINUTES AT AN ALTITUDE OF 100,000 FEET,CORRESPONDING TO 0.32 OF MERCURY |
| SUPP | SUPPLEMENTARY FEATURES | PANELS SHALL BE CAPABLE OF WITHSTANDING 5 CYCLES OF TEMPERATURE SHOCK WHERE EACH CYCLE CONSISTS OF 1HR SOAK TIME AT-65C,A MAXIMUM 3 MINUTE TRANSITION BETWEEN-65C AND 85C AND A 1HR SOAK TIME AT 85C |
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