9540-01-478-9729 ( HS1004DD48-0210 )
NSN Information
NSN | FSC | NIIN | Item Name | INC |
---|---|---|---|---|
9540-01-478-9729 | 9540 | 014789729 | ANGLE,STRUCTURAL | 3701 |
NSN Features
MRC | Parameter | Characteristics |
---|---|---|
ABRY | LENGTH | 2.312 INCHES NOMINAL |
AARN | FABRICATION METHOD | EXTRUDED |
AJGP | BASE FLANGE THICKNESS | 0.125 INCHES NOMINAL |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-200/3 |
AGAV | END ITEM IDENTIFICATION | APACHE HELICOPTER |
ABKW | OVERALL HEIGHT | 1.000 INCHES NOMINAL |
ADXL | LEFT SIDE FLANGE THICKNESS | 0.125 INCHES NOMINAL |
HEAT | HEAT TREATMENT | T-4 SOLUTION HEAT TREATED OR T-3511 SOLUTION HEAT TREATED |
CQHP | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
AJGL | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
CMZY | FIRST TIP STYLE | SQUARE END |
ABMK | OVERALL WIDTH | 1.750 INCHES NOMINAL |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | EXTRUDED ANGLE - UNEQUAL LEG, ALUMINUM ALLOY |
AGTA | BASIC SHAPE STYLE | ANGLE |
Manufacturing Part Numbers (SKUs)
Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
---|---|---|---|---|---|---|---|
HS1004DD48-0210 | 8V613 | A | 2 | 3 | 2 | 9Z |
Manufacturers
Part SKU | Cage | Manufacturer | Type | Status |
---|---|---|---|---|
HS1004DD48-0210 | 8V613 | BOEING COMPANY THE | F | A |
FLIS Identification
PMIC | ADPE Code | CRITL Code | DEMIL Code | DEMIL INTG | NIIN Asgt | ESD | HMIC | ENAC | Schedule-B | INC |
---|---|---|---|---|---|---|---|---|---|---|
A | 0 | X | B | 3 | 10/04/2 | A | N | 3701 |
FLIS Management
MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
---|
Demilitarization Codes & Management
DML | PMI | HMIC | ADP | CC | ESDC |
---|
Miscellaneous Management
MOE (S_A) | SOS | AAC | QUP | UI | SLC | CIIC | RC | MCC | SVC |
---|
Management Control Army
MATCAT 1 | MATCAT 2 | MATCAT 3 | MATCAT 4 5 | ARC |
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Freight
NMFC | NMFC SUB | UFC | HMC | LTL | LCL | WCC | TCC | SHC | ADC | ACC | ASH | NMF DESC |
---|---|---|---|---|---|---|---|---|---|---|---|---|