Part Number: 39 12994 1 | Manufacturer: The Boeing Company | NSN: 6220-00-790-5431 (6220007905431) | |
Item Name: panel indicating light transmitt | CAGE Code: 82918 | ||
Alternate P/N : 39129941 |
Please utilize the RFQ form below to submit an online quote request for NSN part number 39 12994 1 of Panel Indicating Light Transmitt by manufacturer The Boeing Company having CAGE Code 82918 with NSN number 6220-00-790-5431. Please also fill the requested quantity and need by date form fields for your required part 39 12994 1. This information will help us prioritize your request effectively.
“*” Symbols for mandatory fields
Aerospace Orbit is owned and operated by ASAP Semiconductor – an AS9120B, ISO 9001:2015, and FAA AC 00-56B distributor of The Boeing Company NSN parts. We stock difficult-to-find parts from more than 75,000 manufacturers. Request a quote for part number 39 12994 1 and an account manager will contact you shortly.
Our industry relationships allow us to assure competitive prices on all obsolete parts, and shorten the supply chain to deliver as soon as possible. You will receive a response within 15 minutes from a sales representative at Aerospace Orbit. Additionally, you can call us at +1-714-705-4780 or submit a Bill of Materials (BOM) to sales@aerospaceorbit.com to expedite the purchase process.
MRC | Criteria | Characteristic |
---|---|---|
ANJG | PANEL MATERIAL | PLASTIC, MIL-P-5425 |
CXCY | III PART NAME ASSIGNED BY CONTROLLING AGENCY | PANELS, INFORMATION, INTEGRALLY ILLUMINATED |
FTLD | III FUNCTIONAL DESCRIPTION | ALL LAMPS SHALL BE PROTECTED BY A MINIMUM OF 0.030 OF PLASTIC BETWEEN THE LAMPS AND THE FRONT FACE OF THE PANEL,ALL EMBEDDED LIGHT SOURCES AND ASSOCIATED CIRCUITRY SHALL BE RECESSED FROM THE REAR SURFACE OF THE PANEL AND COVERED WITH A MIN |
SUPP | III SUPPLEMENTARY FEATURES | THE PANELS SHALL BE CAPABLE OF WITHSTANDING FIVE CYCLES OF TEMPERATURE SHOCK WHERE EACH CYCLE CONSISTS OF A 1HR SOAK TIME AT -65C, A MAXIMUM 3 MINUTE TRANSITION BETWEEN-65C AND 85C, AND A 1HR SOAK TIME AT 85C |
ADUM | OVERALL THICKNESS | 0.240 INCHES NOMINAL |
FEAT | SPECIAL FEATURES | THE PANELS SHALL BE SUBJECTED TO THE ALTITUDE TEST OF METHOD 105 OF MIL-STD-202 FOR 30 MINUTES AT AN ALTITUDE OF 100,000 FEET |
Please Remember to Visit Us Again the Next Time You Need Parts.
Request for Quote