4920-01-183-9878 ( 14B22000-001 , R-TBD-924 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 4920-01-183-9878 | 4920 | 011839878 | ADAPTER SET,ASYMMETRICAL BRAKE S | 7777 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | B-1B ACFT AGE. |
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | C/O ADAPTER PLATE 1,SPLINE ADAPTER 1;5.000 IN. O/A DIA;FIVE 0.344 IN. DIA HOLES;FOUR 0.125 IN. DIA HOLES |
| FTLD | FUNCTIONAL DESCRIPTION | INTERFACES FLAP AND SLAT BRAKE OF ASYMMETRICAL BRAKE SYSTEM TO MOTOR DRIVE OF HYDRAULIC COMPONENTS TEST STAND DURING FAULT ISOLATION AND VERIFICATION TESTING AT DEPOT MAINTENANCE LEVEL |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| 14B22000-001 | 43999 | A | 2 | 3 | 4 | SB | |
| R-TBD-924 | 43999 | A | 9 | 5 | 5 | SB |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| 14B22000-001 | 43999 | BOEING COMPANY THE | A | A |
| R-TBD-924 | 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 | X | A | 07/12/1 | N | 7777 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DF | N | SF9TG-E | F | ||
| DS | N | I |
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 |
|---|---|---|---|---|---|---|---|---|---|
| DF | SMS | V | 1 | EA | 0 | U | SF9TG-E | F | |
| DS | SMS | Y | 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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|