1560-01-491-8621 ( 35-8220-45 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 1560-01-491-8621 | 1560 | 014918621 | PLATE,STRUCTURAL,AIRCRAFT | 3149 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| FEAT | SPECIAL FEATURES | OPTIONAL MATERIAL 6061-T4 SHEET PER QQ-A-827,T4 ; MACHINED TO BAC1511-161 DIM. |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | B-52 |
| ABHP | OVERALL LENGTH | 69.300 INCHES NOMINAL |
| CZDJ | AIRCRAFT LOCATION | FRAME-CANTED BODY COWL PANEL |
| BWJF | SIDE FOR WHICH DESIGNED | LEFT SIDE |
| MATT | MATERIAL | ALUMINUM ALLOY 6061 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-270,T4 FED SPEC SINGLE MATERIAL RESPONSE |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | RETAINER STRIP,SEAL |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| 35-8220-45 | 81205 | A | 2 | 3 | C | ZZ |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| 35-8220-45 | 81205 | THE BOEING COMPANY | F | A |
FLIS Identification
| PMIC | ADPE Code | CRITL Code | DEMIL Code | DEMIL INTG | NIIN Asgt | ESD | HMIC | ENAC | Schedule-B | INC |
|---|---|---|---|---|---|---|---|---|---|---|
| A | 0 | X | D | 7 | 11/02/2 | P | 8803909060 | 3149 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DF | N | SF8FG-E | F | ||
| DF | ------- | I |
Demilitarization Codes & Management
| DML | PMI | HMIC | ADP | CC | ESDC |
|---|---|---|---|---|---|
| D | A | P | 0 | X |
Miscellaneous Management
| MOE (S_A) | SOS | AAC | QUP | UI | SLC | CIIC | RC | MCC | SVC |
|---|---|---|---|---|---|---|---|---|---|
| DF | FHZ | J | 1 | EA | 0 | 7 | SF8FG-E | D | |
| DF | FHZ | J | 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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|