6615-01-561-8892 ( 114H4307-1 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 6615-01-561-8892 | 6615 | 015618892 | PISTON,LOCK ELA | 7777 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | (INAVY)PISTON, LOCK - EXTENSIBLE LINK, ACTUATING CYLINDER |
| ABHP | OVERALL LENGTH | 2.625 INCHES NOMINAL |
| FEAT | SPECIAL FEATURES | MFG STANDARDS PER VERTOL VS60904; HEAT TREAT TO ROCKWELL RC50-55 (245,000 - 285,000 PSI); ELECTOLIZE ALL OVER EXTERIOR SURFACES ONLY |
| SFTT | SURFACE TREATMENT | ANODIZE |
| MATT | MATERIAL | STEEL CORROSION RESISTING |
| AGAV | END ITEM IDENTIFICATION | CYLINDER ASSEMBLY, AIRCRAFT |
| ADAV | OVERALL DIAMETER | 1.730 INCHES MINIMUM AND 1.731 INCHES MAXIMUM |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| 114H4307-1 | 77272 | A | 2 | 3 | A | ZZ |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| 114H4307-1 | 77272 | THE BOEING COMPANY | A | 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 | 03/20/2 | N | 7777 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DS | I | ||||
| DN | 9B----- | N |
Demilitarization Codes & Management
| DML | PMI | HMIC | ADP | CC | ESDC |
|---|---|---|---|---|---|
| A | A | N | 0 | X |
Miscellaneous Management
| MOE (S_A) | SOS | AAC | QUP | UI | SLC | CIIC | RC | MCC | SVC |
|---|---|---|---|---|---|---|---|---|---|
| DS | SMS | H | 1 | EA | 0 | U | D | ||
| DN | SMS | H | 1 | EA | 0 | U | 9B----- | N |
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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|