1620-01-456-6820 ( 17P1C2006-61 , 17P1C2006 , 17P1C2007 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 1620-01-456-6820 | 1620 | 014566820 | CYLINDER,STRUT | 7777 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | NOSE LANDING GEAR SHOCK STRUT CYLINDER |
| AGAV | END ITEM IDENTIFICATION | WEAPONS CODE DTF, AIRCRAFT, AIRLIFTER C-17A |
| MATT | MATERIAL | STEEL |
| ABMK | OVERALL WIDTH | 24.944 INCHES MINIMUM AND 24.966 INCHES MAXIMUM |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | CYLINDER |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| 17P1C2006-61 | 88277 | A | 2 | 3 | E | ZZ | |
| 17P1C2006 | 88277 | A | 9 | D | A | ZZ | |
| 17P1C2007 | 88277 | A | 9 | D | A | ZZ |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| 17P1C2006-61 | 88277 | BOEING COMPANY THE | F | A |
| 17P1C2006 | 88277 | BOEING COMPANY THE | F | A |
| 17P1C2007 | 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 | X | A | 06/23/1 | N | 8803200060 | 7777 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DF | ------- | I | |||
| DF | N | --SBA-N | F |
Demilitarization Codes & Management
| DML | PMI | HMIC | ADP | CC | ESDC |
|---|---|---|---|---|---|
| A | A | N | X |
Miscellaneous Management
| MOE (S_A) | SOS | AAC | QUP | UI | SLC | CIIC | RC | MCC | SVC |
|---|---|---|---|---|---|---|---|---|---|
| DF | F77 | D | 1 | EA | 0 | U | ------- | D | |
| DF | F77 | M | 1 | EA | 0 | U | --SBA-N | 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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|