1560-01-551-9278 ( 6-84177-1 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 1560-01-551-9278 | 1560 | 015519278 | BRACKET,STRUCTURAL COMPONENT,AIR | 4101 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| CZEK | AIRCRAFT MISSION DESIGN SERIES | KC-135 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-283 T6 FED SPEC SINGLE MATERIAL RESPONSE |
| FEAT | SPECIAL FEATURES | DIM. ARE STOCK MATERIAL |
| ABPX | MATERIAL THICKNESS | 0.091 INCHES NOMINAL |
| ABHP | OVERALL LENGTH | 6.800 INCHES NOMINAL |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ATTACH ANGLE |
| ABMK | OVERALL WIDTH | 2.700 INCHES NOMINAL |
| MATT | MATERIAL | ALUMINUM ALLOY 7075 |
| CZDJ | AIRCRAFT LOCATION | OUTBOARD ACTUATOR RIB,OUTBOARD FLAP |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| 6-84177-1 | 82918 | A | 2 | 3 | C | ZZ |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| 6-84177-1 | 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 | A | 1 | 05/31/2 | A | P | 8803909060 | 4101 |
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 |
|---|---|---|---|---|---|
| A | A | P | 0 | X | A |
Miscellaneous Management
| MOE (S_A) | SOS | AAC | QUP | UI | SLC | CIIC | RC | MCC | SVC |
|---|---|---|---|---|---|---|---|---|---|
| DF | SMS | H | 1 | EA | 0 | U | SF9---N | F | |
| DS | SMS | H | 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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|