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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1560-01-530-2176 Item Description: Stiffener Aircraft | 1560 | 015302176 | 0 | P | A | |
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | A | 0 | |||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
69-6122-2 | 5 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-3621 FED SPEC SINGLE MATERIAL RESPONSE |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | STIFFENER-BALANCE PANEL, OUTBOARD AILERSON |
ABMK | OVERALL WIDTH | 4.800 INCHES NOMINAL |
ABHP | OVERALL LENGTH | 15.000 INCHES NOMINAL |
MATT | MATERIAL | ALUMINUM ALLOY 2024 |
SR-5 | MANUFACTURERS CODE | 81205 |
CZDJ | AIRCRAFT LOCATION | OUTBOARD AILERON |
SR-5 | THE MANUFACTURERS DATA | |
CZEK | AIRCRAFT MISSION DESIGN SERIES | KC-135 ACFT |
ABPX | MATERIAL THICKNESS | 0.032 INCHES NOMINAL |
AGAV | III END ITEM IDENTIFICATION | KC-135 ACFT |
FEAT | SPECIAL FEATURES | HEAT TREAT T4; OPPOSITE -2 (EXCEPT AS SHOWN); USED ON DWG 5-96130 |
SR-5 | DESIGN CONTROL REFERENCE | 69-6122-2 |
69-0001-00 | 69-00007-02 | 69-00015-001 | 69-00065-001 |
69-00006-001 | 69-00006-001 | 69-00047-001 | 69-0-50HM |
69-00047-001 | 69-0001-00 | 69-0000 | 69-0-5T0600 0HM |
69.0 X 3.0 | 69-0000 | 69-00007-002 | 69-00047-001 |
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