1560-01-484-1782 ( 160D610001-23 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 1560-01-484-1782 | 1560 | 014841782 | WING SECTION,CENTER | 6133 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| CZEK | AIRCRAFT MISSION DESIGN SERIES | A-10 AIRC. |
| BWJF | SIDE FOR WHICH DESIGNED | BOTH SIDES |
| MATT | MATERIAL | ALUMINUM ALLOY |
| FEAT | SPECIAL FEATURES | C/O SUPPORT ASSY; FAIRING INSTL.;SPLICE FAIRING INSTL.; FOAM INSTL.; EQPT & HARN.INSTL.; TE INSTL.; LE INSTL.;RIB INSTL.; REAR SPAR INSTL.; CTR. SPAR INSTL.;FRONT SPAR INSTL.; LWR. SKINAFT.; LWR SKIN FWD; WING SPLICE INSTL.; FLAP TRACK INSTL.; PYLON FTG. INSTL.; MISC. HARDWARE; SAME AS 160J611011-5,EXCEPT ALL NEW PARTS USED; MANUFACTURER SUGGESTED NAME IS WING, ASSY |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| 160D610001-23 | 26512 | A | 2 | 3 | 2 | ZZ |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| 160D610001-23 | 26512 | NORTHROP GRUMMAN SYSTEMS CORPORA | A | A |
FLIS Identification
| PMIC | ADPE Code | CRITL Code | DEMIL Code | DEMIL INTG | NIIN Asgt | ESD | HMIC | ENAC | Schedule-B | INC |
|---|---|---|---|---|---|---|---|---|---|---|
| A | 0 | X | C | 7 | 04/20/2 | P | 8803909060 | 6133 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DF | T | SF8FJ-N | L | F | WHEN EXHAUSTED USE 1560-01-492-6056 |
Demilitarization Codes & Management
| DML | PMI | HMIC | ADP | CC | ESDC |
|---|---|---|---|---|---|
| C | A | P | 0 | X |
Miscellaneous Management
| MOE (S_A) | SOS | AAC | QUP | UI | SLC | CIIC | RC | MCC | SVC |
|---|---|---|---|---|---|---|---|---|---|
| DF | FGZ | C | 1 | EA | 0 | 7 | SF8FJ-N | L |
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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|