1680-01-478-9873 ( A55F9004-15 , 43088-015 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 1680-01-478-9873 | 1680 | 014789873 | CONTROL ASSEMBLY,QUADRANT | 3994 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| CZEK | AIRCRAFT MISSION DESIGN SERIES | F14 |
| AGAV | END ITEM IDENTIFICATION | F-14 AIRCRAFT |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | QUADRANT ASSEMBLY, THROTTLE CONTROL |
| FEAT | SPECIAL FEATURES | CONTROL ENGINE POWER,FLAP SETTINGS AND WING SWEEP |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| A55F9004-15 | 26512 | A | 2 | 3 | 1 | ZZ | |
| 43088-015 | 86831 | A | 1 | 5 | 5 | KE |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| A55F9004-15 | 26512 | NORTHROP GRUMMAN SYSTEMS CORPORA | A | A |
| 43088-015 | 86831 | ROCKWELL COLLINS ELECTROMECHANIC | F | A |
FLIS Identification
| PMIC | ADPE Code | CRITL Code | DEMIL Code | DEMIL INTG | NIIN Asgt | ESD | HMIC | ENAC | Schedule-B | INC |
|---|---|---|---|---|---|---|---|---|---|---|
| A | 0 | Y | D | 2 | 10/05/2 | N | 8803300060 | 3994 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DN | H | 7RPFAR9 | L | R | REFER TO NET PRICE 29529.00 |
Demilitarization Codes & Management
| DML | PMI | HMIC | ADP | CC | ESDC |
|---|---|---|---|---|---|
| D | A | N | 0 | Y |
Miscellaneous Management
| MOE (S_A) | SOS | AAC | QUP | UI | SLC | CIIC | RC | MCC | SVC |
|---|---|---|---|---|---|---|---|---|---|
| DN | NRP | V | 1 | EA | 0 | 7 | 7RPFAR9 | 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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 133300 | Z | 74240 | W | W | 671 | 3 | 9 | A | A | Z | MACHINERY/MACHINES NOI |