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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1560-01-506-8630 Item Description: Tip Aircraft | 1560 | 015068630 | 0 | P | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
7 | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
L2100204-015 | 6 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
CZDJ | AIRCRAFT LOCATION | TIP, HORIZONTAL STABILIZER |
FEAT | SPECIAL FEATURES | U/0 B-1B; DIMS ARE STOCK MATERIAL; MATERIAL IS AL CLAD SHEET, HEAT TREATR TO T-62 PER ST0111LA0009, FINISH 09 PRIOR TO BONDING |
ABMK | OVERALL WIDTH | 2.000 INCHES NOMINAL |
ABHP | OVERALL LENGTH | 84.000 INCHES NOMINAL |
ABPX | MATERIAL THICKNESS | 0.020 INCHES NOMINAL |
SR-5 | DESIGN CONTROL REFERENCE | L2100204-015 |
CZEK | AIRCRAFT MISSION DESIGN SERIES | B-1B |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | LEADING EDGE FACE SHEET |
MATT | MATERIAL | ALUMINUM ALLOY 2024 |
SR-5 | MANUFACTURERS CODE | 43999 |
SR-5 | THE MANUFACTURERS DATA | |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5, T-62 FED SPEC SINGLE MATERIAL RESPONSE |
L21-58-8 | L21-10-5PN-20-103 | L21-30C | L21-20-1 |
L21-179 | L21-30C | L21-232 | L21-30C |
L21 20PT1 | L21-179 | L21-4F2H-1F 2 | L21 396 |
L21-20R | L21-30C | L21-58-6 | L21-4F2H-1F 2 |
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