1560-01-558-5366 ( 5HL71022-101 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 1560-01-558-5366 | 1560 | 015585366 | FITTING,STRUCTURAL COMPONENT,AIR | 4101 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| ABHP | OVERALL LENGTH | 2.000 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | F-22 RAPTOR AIRCRAFT |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-T-9047 MIL SPEC SINGLE MATERIAL RESPONSE |
| CZDJ | AIRCRAFT LOCATION | UPLOCK STRUT,ARRESTING GEAR |
| FEAT | SPECIAL FEATURES | ANN TITANIUM ROD;DIM.ARE STOCKSIZE MATL |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | F-22 RAPTOR ACFT |
| MATT | MATERIAL | TITANIUM ALLOY |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | CYLINDER |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| 5HL71022-101 | 81205 | A | 2 | 3 | C | ZZ |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| 5HL71022-101 | 81205 | THE BOEING COMPANY | F | A |
FLIS Identification
| PMIC | ADPE Code | CRITL Code | DEMIL Code | DEMIL INTG | NIIN Asgt | ESD | HMIC | ENAC | Schedule-B | INC |
|---|---|---|---|---|---|---|---|---|---|---|
| A | 0 | X | D | 1 | 11/13/2 | P | 8803909060 | 4101 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DF | ------- | I | |||
| DF | N | --SFR-E | F |
Demilitarization Codes & Management
| DML | PMI | HMIC | ADP | CC | ESDC |
|---|---|---|---|---|---|
| D | A | P | 0 | X |
Miscellaneous Management
| MOE (S_A) | SOS | AAC | QUP | UI | SLC | CIIC | RC | MCC | SVC |
|---|---|---|---|---|---|---|---|---|---|
| DF | F01 | D | 1 | EA | 0 | 7 | --SFR-E | D | |
| DF | F01 | D | 1 | EA | 0 | 7 | ------- | 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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|