1560-01-564-4307 ( 69-11622-10 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 1560-01-564-4307 | 1560 | 015644307 | PANEL,STRUCTURAL,AIRCRAFT | 3598 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| CZEJ | AIRCRAFT STATION NUMBER | RS93.26 TO RS102.18 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/13 FED SPEC SINGLE MATERIAL RESPONSE |
| AGAV | END ITEM IDENTIFICATION | KC-135 ACFT |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | KC-135 AIRCRAFT |
| FEAT | SPECIAL FEATURES | C/O SKIN PANEL-BONDED ASSY, STIFFENER-ANGLE; U/O 65-3495; FINISH SRF-2.10 |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | SKIN PANEL, BONDED |
| MATT | MATERIAL | ALUMINUM ALLOY 7075 |
| CZDJ | AIRCRAFT LOCATION | RUDDER |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| 69-11622-10 | 82918 | A | 2 | 3 | C | ZZ |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| 69-11622-10 | 82918 | THE BOEING COMPANY | A | A |
FLIS Identification
| PMIC | ADPE Code | CRITL Code | DEMIL Code | DEMIL INTG | NIIN Asgt | ESD | HMIC | ENAC | Schedule-B | INC |
|---|---|---|---|---|---|---|---|---|---|---|
| A | 0 | X | B | 3 | 06/17/2 | A | P | 8803909060 | 3598 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DF | N | SF9---N | F | ||
| DS | N | I |
Demilitarization Codes & Management
| DML | PMI | HMIC | ADP | CC | ESDC |
|---|---|---|---|---|---|
| B | A | P | 0 | X | A |
Miscellaneous Management
| MOE (S_A) | SOS | AAC | QUP | UI | SLC | CIIC | RC | MCC | SVC |
|---|---|---|---|---|---|---|---|---|---|
| DF | SMS | D | 1 | EA | 0 | U | SF9---N | F | |
| DS | SMS | D | 1 | EA | 0 | U | 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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|