| Item Name | Shielding Gasket Electronic |
| Federal Supply Group (FSG) | Electrical and Electronic Equipment Components |
| Federal Supply Class (FSC) | 5999 Miscellaneous Electrical and Electronic Components |
| National Item Identification Number (NIIN) | 01-466-6149 (014666149) |
| NCB Code | USA (01) |
| Manufacturer | Spira Manufacturing Corporation, Boeing Company The |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| 1-1062-001 | spira manufacturing corporation | shielding gasket electronic | 60050 | RFQ |
| 483-0360 | boeing company the | shielding gasket electronic | 94756 | RFQ |
| 483-0360-001 | boeing company the | shielding gasket electronic | 94756 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAGR | CROSS-SECTIONAL SHAPE STYLE | METAL AND SYNTHETIC RUBBER" |
| ABJH | TEMP RATING | -55.0 DEG CELSIUS AND 125.0 DEG CELSIUS" |
| ABKV | OUTSIDE DIAMETER | 4.761 INCHES MAXIMUM" |
| ABVL | APERTURE DIAMETER | 4.473 INCHES NOMINAL" |
| ADVM | CROSS-SECTIONAL THICKNESS | 4.761 INCHES MAXIMUM" |
| AGAV | END ITEM IDENTIFICATION | T-38 AIRCRAFT" |
| FEAT | SPECIAL FEATURES | OUTER SHIELD DIAMETER SHALL COMPRESS 25 PERCENT AT COMPRESSION FORCE OF 1 TO 4 POUNDS PER LINEAR INCH; INNER CORE SHALL BE SOLID WITH A BONDED BUTT JOINT; OUTER SHIELD SHALL BE OVERLAPPED 1 - 2 TURNS WITH THE END OF THE OUTSIDE HELIX LAP-JO" |
| MATT | MATERIAL | COPPER ALLOY 172 EMI/RFI CONDUCTOR" |
| MATT | MATERIAL | RUBBER CORE AND SILICONE CORE" |
| SFTT | SURFACE TREATMENT | TIN ALLOY OVERALL AND LEAD OVERALL" |
| STYL | STYLE DESIGNATOR | CIRCULAR" |
| AAGR | CROSS-SECTIONAL SHAPE STYLE | METAL AND SYNTHETIC RUBBER" |
| ABJH | TEMP RATING | -55.0 DEG CELSIUS AND 125.0 DEG CELSIUS" |
| ABKV | OUTSIDE DIAMETER | 4.761 INCHES MAXIMUM" |
| ABVL | APERTURE DIAMETER | 4.473 INCHES NOMINAL" |
| ADVM | CROSS-SECTIONAL THICKNESS | 4.761 INCHES MAXIMUM" |
| AGAV | END ITEM IDENTIFICATION | T-38 AIRCRAFT" |
| FEAT | SPECIAL FEATURES | OUTER SHIELD DIAMETER SHALL COMPRESS 25 PERCENT AT COMPRESSION FORCE OF 1 TO 4 POUNDS PER LINEAR INCH; INNER CORE SHALL BE SOLID WITH A BONDED BUTT JOINT; OUTER SHIELD SHALL BE OVERLAPPED 1 - 2 TURNS WITH THE END OF THE OUTSIDE HELIX LAP-JO" |
| MATT | MATERIAL | COPPER ALLOY 172 EMI/RFI CONDUCTOR" |
| MATT | MATERIAL | RUBBER CORE AND SILICONE CORE" |
| SFTT | SURFACE TREATMENT | TIN ALLOY OVERALL AND LEAD OVERALL" |
| STYL | STYLE DESIGNATOR | CIRCULAR" |
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