4720-01-477-4063 ( BWT10-2240050G , 7-511A21569-37 , 7-511A21569 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 4720-01-477-4063 | 4720 | 014774063 | HOSE,AIR DUCT | 1111 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | 15200013558250 HELICOPTER ATTACH AH-64D |
| ACKH | MINIMUM INSIDE BENDING RADIUS | 1.500 INCHES |
| STYL | STYLE DESIGNATOR | HELICALLY WOUND CONTINOUS WIRE SUPPORTED |
| AWLS | CONNECTION TYPE | PREFORMED FIRST END |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| BWT10-2240050G | 53178 | A | 2 | 5 | 5 | ZZ | |
| 7-511A21569-37 | 8V613 | A | 2 | 3 | 2 | ZZ | |
| 7-511A21569 | 8V613 | A | 9 | D | 2 | ZZ |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| BWT10-2240050G | 53178 | BULL HN INFORMATION SYSTEMS INC | A | A |
| 7-511A21569-37 | 8V613 | BOEING COMPANY THE | F | A |
| 7-511A21569 | 8V613 | 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 | A | 1 | 08/08/2 | A | N | 1111 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DA | Z | J2200X- | A | ||
| DS | N | I |
Demilitarization Codes & Management
| DML | PMI | HMIC | ADP | CC | ESDC |
|---|---|---|---|---|---|
| A | A | N | 0 | X | A |
Miscellaneous Management
| MOE (S_A) | SOS | AAC | QUP | UI | SLC | CIIC | RC | MCC | SVC |
|---|---|---|---|---|---|---|---|---|---|
| DA | SMS | D | 1 | EA | 0 | U | Z | J2200X- | A |
| DS | SMS | D | 1 | EA | 0 | U | D |
Management Control Army
| MATCAT 1 | MATCAT 2 | MATCAT 3 | MATCAT 4 5 | ARC |
|---|---|---|---|---|
| J | 2 | 2 | 00 | X |
Freight
| NMFC | NMFC SUB | UFC | HMC | LTL | LCL | WCC | TCC | SHC | ADC | ACC | ASH | NMF DESC |
|---|---|---|---|---|---|---|---|---|---|---|---|---|