Thank you for taking interest in Boeing Company The part number 17P6J4181-501, which is listed with the NSN 4710-01-460-6989 and a product description of “Tube Assembly Metal.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
4710-01-460-6989 Item PartTypeName: TUBE ASSEMBLY,METAL | 4710 | 014606989 | 0 | N | A | |
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | A | 0 | |||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
17P6J4181-501 | 5 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
MATT | Material | TITANIUM SINGLE END |
SUPP | Supplementary Features | TUBE IS WRAPPED TO PREVENT COIL TUBE FROM CHAFING ON ADJOINING STRUCTURE;THE SPIRAL WRAP HAS A STOCK SIZE OF .375 ODX 59.00, TOTAL LENGTH TO BE MEASURED IN RELAXED STATE PRIOR TO WRAPPING;THE WRAP IS GRAY, ANTI-CHAFE COAT, PRIME AND DN3635;IT IS CONTINUOUS WRAPPING IN LINEAR DIMENSIONS ALONG THE THREE COILS, WITH A GAP BETWEEN SPIRAL WRAP TO BE .06 MAX; TRIM TO NOTED DIMENSIONS AS REQUIRED; TUBE IS TAPED IN 2 PLACES, FROM STOCK SIZE OF 1.00 X 2.00, AND MADE FROM 7-TAPE-2045-5 |
CBBL | Features Provided | OUTER COVERING |
MRC | Decoded Requirement | Clear Text Reply |
ARJD | Design Form | PREBENT |
CXCY | Part Name Assigned By Controlling Agency | TUBE ASSEMBLY, METAL-COILED HYDRAULIC FLAP RETRACT PRESS, W4181 |
FEAT | Special Features | SURFACE TREAT TITANIUM PER MIL-S-5002;DIMENSIONAL TOLERANCES AND SYMBOLS PER ANSI Y14.5M-1982;FABRICATE PER DOUGLAS PROCESS STANDARD (DPS) 3.80-5;PREPARE TUBE END (S) PER S 5021205-78 |
AGAV | End Item Identification | C-17 AIRCRAFT |
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