1560-01-548-1907 ( 5HL88220-104 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 1560-01-548-1907 | 1560 | 015481907 | SUPPORT,STRUCTURAL COMPONENT,AIR | 3224 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | F-22 RAPTOR |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-T-9046 ASSN STD SINGLE MATERIAL RESPONSE |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | F-22A |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | SUPPORT ASSEMBLY |
| MATT | MATERIAL | TITANIUM ALLOY |
| CZDJ | AIRCRAFT LOCATION | OUTBOARD MLG DOOR |
| FEAT | SPECIAL FEATURES | OPP -103; C/O: -114 HINGE FITTING, BUSINGS (NAS77A6-013 & NAS774B-013); M/F: 6AL-4V (AB-1) ANN, TITANIUM PLATE, L:4.000 X W:4.000 |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| 5HL88220-104 | 81205 | A | 2 | 3 | C | ZZ |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| 5HL88220-104 | 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 | B | 3 | 02/12/2 | P | 8803909060 | 3224 |
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 |
|---|---|---|---|---|---|
| B | A | P | 0 | X |
Miscellaneous Management
| MOE (S_A) | SOS | AAC | QUP | UI | SLC | CIIC | RC | MCC | SVC |
|---|---|---|---|---|---|---|---|---|---|
| DF | F01 | D | 1 | EA | 0 | U | --SFR-E | D | |
| DF | F01 | D | 1 | EA | 0 | U | ------- | 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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|