1650-01-510-0262 ( L5871400-072 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 1650-01-510-0262 | 1650 | 015100262 | SERVOCYLINDER | 3130 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| AMQZ | COMPRESSED LENGTH | 16.750 INCHES NOMINAL |
| NHCF | NUCLEAR HARDNESS CRITICAL FEATURE | HARDENED |
| ATEM | EXTENDED LENGTH | 20.250 INCHES NOMINAL |
| FEAT | SPECIAL FEATURES | P/N L5871400-072 REPLACES P/N L5871400-052, R. H. |
| CKSD | DESIGN CHARACTERISTICS | DOUBLE ACTING SINGLE CYLINDER |
| BGST | PRESSURE RATING | 4000.0 POUNDS PER SQUARE INCH NOMINAL |
| CKRM | INTEGRAL VALVE OPERATION METHOD | HYDRAULIC |
| AGAV | END ITEM IDENTIFICATION | B-1B AIRCRAFT;T.O.9H2-4-249-3 |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| L5871400-072 | 43999 | A | 2 | 3 | C | ZZ |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| L5871400-072 | 43999 | BOEING COMPANY THE | A | A |
FLIS Identification
| PMIC | ADPE Code | CRITL Code | DEMIL Code | DEMIL INTG | NIIN Asgt | ESD | HMIC | ENAC | Schedule-B | INC |
|---|---|---|---|---|---|---|---|---|---|---|
| A | 0 | H | B | 3 | 07/11/2 | N | 8803300060 | 3130 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DF | T | SF8---N | L | DOD I&S FAMILY MASTER NSN | |
| DF | T | SF8---N | L | G | USE UNTIL EXHAUSTED 1650-01-165-9346 |
Demilitarization Codes & Management
| DML | PMI | HMIC | ADP | CC | ESDC |
|---|---|---|---|---|---|
| B | A | N | 0 | H |
Miscellaneous Management
| MOE (S_A) | SOS | AAC | QUP | UI | SLC | CIIC | RC | MCC | SVC |
|---|---|---|---|---|---|---|---|---|---|
| DF | FHZ | C | 1 | EA | 0 | U | SF8---N | 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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|