Part Number: L3223760-067 | Manufacturer: Boeing Company The |
NSN : 1560-01-592-9411 (1560015929411) | Item Name : frame aircraft |
CAGE Code: 43999 | FSC : 1560 Airframe Structural Components |
Alternate P/N : L3223760067 | INC Code: 41024 |
NIIN : 01-592-9411 (015929411) | FSG : 15 Aircraft and Airframe Structural Components |
Country: USA | NCB Code: 01 |
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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1560-01-592-9411 Item Description: Frame Aircraft | 1560 | 015929411 | 0 | P | A | |
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
7 | A | A | 0 | |||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
L3223760-067 | 5 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 3.300 INCHES NOMINAL |
ABMK | OVERALL WIDTH | 2.800 INCHES NOMINAL |
ABPX | MATERIAL THICKNESS | 0.032 INCHES NOMINAL |
CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | GUSSET |
CZDJ | AIRCRAFT LOCATION | UNDERWING FAIRING |
CZEK | AIRCRAFT MISSION DESIGN SERIES | B-1B |
FEAT | SPECIAL FEATURES | HARDNESS CRITICAL ITEM;HEAT TREAT T81 |
MATT | III MATERIAL | ALUMINUM ALLOY 2024 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED STD SINGLE MATERIAL RESPONSE |
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