5120-01-294-3541 ( 7-367310005-603 , 7-367310005-603 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 5120-01-294-3541 | 5120 | 012943541 | JACK,LEVELING-SUPPORT | 3660 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| BSSY | BASE DESIGN | RIGID |
| AXGY | MOUNTING METHOD | BALL SOCKET |
| FEAT | SPECIAL FEATURES | PROOF LOAD TO WITHSTAND 4450 LBS,APPLICATION AH-64 AIRCRAFT,STA 450 |
| APHE | OPERATION METHOD | PLAIN SCREW |
| BSSZ | PIN HOLE ADJUSTMENT FEATURE | INCLUDED |
| ABKW | OVERALL HEIGHT | 21.000 INCHES NOMINAL |
| AWET | BASE TYPE | SHOE |
| BSST | OPERATING MECHANISM LOCATION | MOUNTING END |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| 7-367310005-603 | 02731 | R | 9 | 5 | 1 | CT | |
| 7-367310005-603 | 8V613 | A | 2 | 3 | 1 | ZZ |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| 7-367310005-603 | 02731 | MCDONNELL DOUGLAS HELICOPTER CO | A | R |
| 7-367310005-603 | 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 | N | A | 02/15/1 | A | N | 8425490000 | 3660 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DA | D | H21BZX- | L |
Demilitarization Codes & Management
| DML | PMI | HMIC | ADP | CC | ESDC |
|---|---|---|---|---|---|
| A | A | N | 0 | N | A |
Miscellaneous Management
| MOE (S_A) | SOS | AAC | QUP | UI | SLC | CIIC | RC | MCC | SVC |
|---|---|---|---|---|---|---|---|---|---|
| DA | B17 | X | 1 | EA | 0 | U | D | H21BZX- | L |
Management Control Army
| MATCAT 1 | MATCAT 2 | MATCAT 3 | MATCAT 4 5 | ARC |
|---|---|---|---|---|
| H | 2 | 1 | BZ | X |
Freight
| NMFC | NMFC SUB | UFC | HMC | LTL | LCL | WCC | TCC | SHC | ADC | ACC | ASH | NMF DESC |
|---|---|---|---|---|---|---|---|---|---|---|---|---|