1560-01-488-1713 ( 5HF42546-121 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 1560-01-488-1713 | 1560 | 014881713 | PANEL,STRUCTURAL,AIRCRAFT | 3598 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | PANEL ASSEMBLY |
| AGAV | END ITEM IDENTIFICATION | F-22 RAPTOR |
| CZDJ | AIRCRAFT LOCATION | PAN, ANTENNA-L BAND |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | F-22A |
| FEAT | SPECIAL FEATURES | FRACTURE/DURABILITY CRITICAL ITEM; C/O: 123 CAP, -125 & -126 STIFFENER, AND -127 & -129 FLOOR; M/F: TITANIUM, 6AL-4V ANN |
| MATT | MATERIAL | TITANIUM |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS4911 FED SPEC SINGLE MATERIAL RESPONSE |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| 5HF42546-121 | 81755 | A | 2 | 3 | C | ZZ |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| 5HF42546-121 | 81755 | LOCKHEED MARTIN CORPORATION | A | A |
FLIS Identification
| PMIC | ADPE Code | CRITL Code | DEMIL Code | DEMIL INTG | NIIN Asgt | ESD | HMIC | ENAC | Schedule-B | INC |
|---|---|---|---|---|---|---|---|---|---|---|
| A | 0 | X | D | 1 | 08/23/2 | A | P | 8803909060 | 3598 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DF | N | --SFR-E | F | ||
| DF | ------- | I |
Demilitarization Codes & Management
| DML | PMI | HMIC | ADP | CC | ESDC |
|---|---|---|---|---|---|
| D | A | P | 0 | X | A |
Miscellaneous Management
| MOE (S_A) | SOS | AAC | QUP | UI | SLC | CIIC | RC | MCC | SVC |
|---|---|---|---|---|---|---|---|---|---|
| DF | F01 | D | 1 | EA | 0 | 7 | --SFR-E | D | |
| DF | F01 | D | 1 | EA | 0 | 7 | ------- | 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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|