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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 |