9540-01-479-0438 ( HS1004AA04B0100 )
NSN Information
NSN | FSC | NIIN | Item Name | INC |
---|---|---|---|---|
9540-01-479-0438 | 9540 | 014790438 | ANGLE,STRUCTURAL | 3701 |
NSN Features
MRC | Parameter | Characteristics |
---|---|---|
AJGP | BASE FLANGE THICKNESS | 0.062 INCHES NOMINAL |
ADXL | LEFT SIDE FLANGE THICKNESS | 0.062 INCHES NOMINAL |
AARN | FABRICATION METHOD | EXTRUDED |
HEAT | HEAT TREATMENT | T-6 SOLUTION HEAT TREATED OR T-6511 SOLUTION HEAT TREATED |
AGAV | END ITEM IDENTIFICATION | APACHE HELICOPTER |
ABRY | LENGTH | 1.000 INCHES NOMINAL |
AJGL | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.062 INCHES NOMINAL |
CQHP | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
ABKW | OVERALL HEIGHT | 0.750 INCHES NOMINAL |
ABMK | OVERALL WIDTH | 1.000 INCHES NOMINAL |
CMZY | FIRST TIP STYLE | SQUARE END |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-200/11 |
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 |
---|---|---|---|---|---|---|---|
HS1004AA04B0100 | 8V613 | A | 2 | 3 | 2 | 9Z |
Manufacturers
Part SKU | Cage | Manufacturer | Type | Status |
---|---|---|---|---|
HS1004AA04B0100 | 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 | A | 1 | 10/06/2 | A | N | 3701 |
FLIS Management
MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
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Demilitarization Codes & Management
DML | PMI | HMIC | ADP | CC | ESDC |
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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 |
---|---|---|---|---|---|---|---|---|---|---|---|---|