4940-01-376-1601 ( 884Y )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 4940-01-376-1601 | 4940 | 013761601 | ADAPTER,PRESSURE TEST | 7777 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| FEAT | SPECIAL FEATURES | PITOT OR PITOT/STATIC TUBE MODEL NUMBER 858DH,DH1,AJ |
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | FOR APPLYING REFERENCE PRESSURES TO AIRCRAFT'S PITOT,PITOT-STATIC OR PNEUMATIC FLOW ANGLE PROBES; OVERALL DIA IS 1.625IN.,OVERALL LENGTH IS 5.3IN.; INCLUDES A PRESSURE SLEEVE OF ACETAL PLASTIC,A STAINLESS STEEL COMPRESSION CLAMP,A STAINLESS STEEL PRESSURE FITTING WITH THREADS PER MS33656-4; FIVE NYLON FITTINGS WITH RUBBER GASKETS AND TWO PRESSURE SEALING RINGS |
| AGAV | END ITEM IDENTIFICATION | ACMI TEST SET; W/S CODE 51,AIRCRAFT MANUEVERING |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| 884Y | 59885 | A | 2 | 3 | A | AX |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| 884Y | 59885 | ROSEMOUNT AEROSPACE INC. | 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 | 05/27/1 | N | 7777 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DF | N | SF9SU-N | 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 |
|---|---|---|---|---|---|---|---|---|---|
| DS | SMS | J | 0 | EA | 0 | U | D | ||
| DF | SMS | J | 0 | EA | 0 | U | SF9SU-N | F |
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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|