If you need to request a quote for the Boeing Company The's L2100148-123 Panel Structural Aircraft, with corresponding NSN 1560015754117, we have got you covered. Simply provide us with the desired quantity for the part number L2100148-123 available with CAGE Code 43999 and FSC 1560 Airframe Structural Components, targeted price, and order-fulfillment date, and our dedicated account manager will be in touch with you within 15 minutes.
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NSN Information for Part Number L2100148-123 with NSN 1560-01-575-4117, 1560015754117
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1560-01-575-4117 Item Description: Panel Structural Aircraft | 1560 | 015754117 | 0 | P | A | |
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | A | 0 | |||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| L2100148-123 | 5 | 2 | 3 |
Characteristics Data of NSN 1560-01-575-4117, 1560015754117
| MRC | Criteria | Characteristic |
|---|---|---|
| CZDJ | AIRCRAFT LOCATION | PANEL, LE - OUTBD, HORIZ STAB |
| ABHP | OVERALL LENGTH | 8.500 INCHES NOMINAL |
| MATT | MATERIAL | PLASTIC |
| ABMK | OVERALL WIDTH | 140.000 INCHES NOMINAL |
| AARN | FABRICATION METHOD | HONEYCOMB |
| FEAT | SPECIAL FEATURES | CORE, LB0130-136,HTF-3/16-4.0 CORE, USED ON L2100148-111 |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | PRE SHAPED CORE |
| ABNM | THICKNESS | 3.000 INCHES NOMINAL |
| SR-5 | DESIGN CONTROL REFERENCE | L2100148-123 |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | B-1B ACFT |
| AGAV | END ITEM IDENTIFICATION | B-1B |
| SR-5 | THE MANUFACTURERS DATA | |
| SR-5 | MANUFACTURERS CODE | 43999 |
