5360-01-538-1692 ( 17P2A3257-1 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 5360-01-538-1692 | 5360 | 015381692 | SPRING,HELICAL,TORSION | 0422 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| APCN | COIL QUANTITY | 3 |
| MATT | MATERIAL | STEEL CORROSION RESISTING OVERALL |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | ADPS9.07 FED SPEC 5TH TREATMENT RESPONSE OVERALL |
| FEAT | SPECIAL FEATURES | SPRING RATE 5.94IN-LB/TURN, COIL DIA. .662 +.009/-.009 DIAMETER OF ROD OVER WHICH SPRING IS TESTED .40 |
| AGAV | END ITEM IDENTIFICATION | C-17A AIRCRAFT |
| AXLH | COIL HELIX DIRECTION | RIGHT-HAND |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | SPRING, HELICAL TORSION, CAM FOLLOWER ASSY, TROOP DOOR |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| 17P2A3257-1 | 88277 | A | 2 | 3 | 3 | ZZ |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| 17P2A3257-1 | 88277 | 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 | 03/13/2 | A | N | 0422 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DF | N | --SBA-E | F | ||
| DF | ------- | I |
Demilitarization Codes & Management
| DML | PMI | HMIC | ADP | CC | ESDC |
|---|---|---|---|---|---|
| A | A | N | 0 | X | A |
Miscellaneous Management
| MOE (S_A) | SOS | AAC | QUP | UI | SLC | CIIC | RC | MCC | SVC |
|---|---|---|---|---|---|---|---|---|---|
| DF | F77 | D | 1 | EA | 0 | U | ------- | D | |
| DF | F77 | D | 1 | EA | 0 | U | --SBA-E | D |
Management Control Army
| MATCAT 1 | MATCAT 2 | MATCAT 3 | MATCAT 4 5 | ARC |
|---|
Freight
| NMFC | NMFC SUB | UFC | HMC | LTL | LCL | WCC | TCC | SHC | ADC | ACC | ASH | NMF DESC |
|---|---|---|---|---|---|---|---|---|---|---|---|---|