1560-01-367-7466 ( DAA3121A325-009 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 1560-01-367-7466 | 1560 | 013677466 | BRACKET,STRUCTURAL COMPONENT,AIR | 4101 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| NHCF | NUCLEAR HARDNESS CRITICAL FEATURE | HARDENED |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE |
| FEAT | SPECIAL FEATURES | NUCLEAR HARDNESS CRITICAL ITEM,USED AS A UPLOCK ROLLER SUPPORT ASSY,MATL:AL ALLOY EXTRN,7075T3511,C/0 -007 SUPPORT & BUSHINGS |
| ABHP | OVERALL LENGTH | 9.035 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 7.650 INCHES NOMINAL |
| HGTH | HEIGHT | 3.718 INCHES NOMINAL |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | B-2 PACER SPECIAL |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| DAA3121A325-009 | 80378 | A | 2 | 3 | 2 | MF |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| DAA3121A325-009 | 80378 | TRIUMPH AEROSTRUCTURES, LLC | A | A |
FLIS Identification
| PMIC | ADPE Code | CRITL Code | DEMIL Code | DEMIL INTG | NIIN Asgt | ESD | HMIC | ENAC | Schedule-B | INC |
|---|---|---|---|---|---|---|---|---|---|---|
| A | 0 | H | B | 11/18/1 | P | 8803909060 | 4101 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DF | P | SF8FW-N | F | ||
| DF | ------- | I |
Demilitarization Codes & Management
| DML | PMI | HMIC | ADP | CC | ESDC |
|---|---|---|---|---|---|
| B | A | P | 0 | H |
Miscellaneous Management
| MOE (S_A) | SOS | AAC | QUP | UI | SLC | CIIC | RC | MCC | SVC |
|---|---|---|---|---|---|---|---|---|---|
| DF | FHZ | D | 1 | EA | 0 | U | SF8FW-N | F | |
| DF | FHZ | D | 1 | EA | 0 | U | ------- | F |
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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|