1560-01-491-9154 ( 17P2A6020-3 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 1560-01-491-9154 | 1560 | 014919154 | PANEL,STRUCTURAL,AIRCRAFT | 3598 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| CZDJ | AIRCRAFT LOCATION | FUSELAGE,UPPER,AFT |
| BWJF | SIDE FOR WHICH DESIGNED | BOTH SIDES |
| AARN | FABRICATION METHOD | LAMINATED |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-P-23377 MIL SPEC 1ST TREATMENT RESPONSE AND MIL-F-18264 MIL SPEC 2ND TREATMENT RESPONSE |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | C-17 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | DMS2288 MFR REF 1ST MATERIAL RESPONSE AND DMS1974 MFR REF 2ND MATERIAL RESPONSE |
| SFTT | SURFACE TREATMENT | PRIMER EPOXY |
| MATT | MATERIAL | PLASTIC ARAMID AND PLASTIC POLYAMIDE |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| 17P2A6020-3 | 88277 | A | 2 | 3 | C | ZZ |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| 17P2A6020-3 | 88277 | BOEING COMPANY THE | F | 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 | 11/05/2 | A | P | 8803909060 | 3598 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DF | T | --SBA-P | L |
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 | F77 | C | 1 | EA | 0 | U | --SBA-P | L |
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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|