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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1560-01-444-9026 Item Description: Frame Aircraft | 1560 | 014449026 | 0 | P | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
7 | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
L3010881-005 | 6 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
FEAT | SPECIAL FEATURES | P/O -011 FRAME ASY; U/O ACFT 1 & SUBQ; MATL: AL CLAD SH, ALY 2024-0; HEAT TREAT PER ST0111L0009 TO TEMP T62; FINISH 10AB02 |
ABMK | OVERALL WIDTH | 19.000 INCHES NOMINAL |
ABPX | MATERIAL THICKNESS | 0.080 INCHES NOMINAL |
CZDJ | AIRCRAFT LOCATION | LOWER OUTBOARD FUSELAGE |
BWJF | SIDE FOR WHICH DESIGNED | RIGHT SIDE |
CZEJ | AIRCRAFT STATION NUMBER | YF512.000 |
SR-5 | DESIGN CONTROL REFERENCE | L3010881-005 |
CZEK | AIRCRAFT MISSION DESIGN SERIES | B-1B |
MATT | MATERIAL | ALUMINUM ALLOY 2024 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE |
SR-5 | MANUFACTURERS CODE | 43999 |
ABHP | OVERALL LENGTH | 32.000 INCHES NOMINAL |
SR-5 | THE MANUFACTURERS DATA |
L30-2 | L30 115V | L30 17 E FT 180 120 S2 0 S | L30-08-000 |
L30-4 | L30-1 | L30-1F | L30-1F |
L30-1 | L30 0104 00 | L30-1F | L30-06-G00 |
L30-25-M-FF-180-S1-O-H | L30-18-14PN-20-8C9 | L30-18-14PN-20-8C9 | L30-06-000 |
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