If you are in search of part numbers like SS40-7A252000, SS40C7A252000, and others that fall under the NSN 4720-00-782-1422, we have you covered with the catalog and procurement resources provided on this page. At the top of the page, you will be able to review a number of details and data that pertain to this particular NSN, while available offerings are listed out below. If any items on our NSN 4720-00-782-1422 catalog interest you, be sure to request a quote from our staff at your earliest convenience. You can do this by submitting a Request for Quote (RFQ) form through our website or by getting in touch with our team via phone or email.
As an ASAP Semiconductor platform operating with quality as a focus, all NSN 4720-00-782-1422 parts we stock come from trusted manufacturers and undergo any necessary inspections or testing prior to shipment. Additionally, every purchase you make will come delivered with all applicable qualifying certifications or manufacturing trace documentation. Aside from such commitments, we also strive to provide customers procurement solutions that equally balance competitive pricing and timely fulfillment. With so much to offer, choose ASAP MilSTD for NSN 4720-00-782-1422 supplies and more.
Item Name | Hose Assembly Nonmetallic |
Federal Supply Group (FSG) | Pipe Tubing Hose and Fittings |
Federal Supply Class (FSC) | 4720 Hose and Tubing Flexible |
National Item Identification Number (NIIN) | 00-782-1422 (007821422) |
NCB Code | USA (00) |
Manufacturer | Sikorsky Aircraft Corporation |
Part Number | Manufacturer | Item Name | Cage Code | RFQ |
---|---|---|---|---|
SS40-7A252000 | sikorsky aircraft corporation | hose assembly nonmetallic | 78286 | RFQ |
SS40C7A252000 | sikorsky aircraft corporation | hose assembly nonmetallic | 78286 | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AAJD | Thread Class | 3B 2ND END |
CQRB | Seat Angle | 37.0 DEGREES 2ND END |
CQRB | Seat Angle | 37.0 DEGREES 1ST END |
CRWL | Inside Surface Condition | SMOOTH |
AAJF | Thread Direction | RIGHT-HAND 2ND END |
AWLS | Connection Type | THREADED INTERNAL TUBE 2ND END |
CRDW | Hydrostatic Test Pressure | 3000.0 POUNDS PER SQUARE INCH |
CQGM | Maximum Operating Pressure | 1500.0 POUNDS PER SQUARE INCH |
AAJF | Thread Direction | RIGHT-HAND 1ST END |
AKUU | End Connection Design | ELBOW 1ST END |
AAJD | Thread Class | 3B 1ST END |
AKUU | End Connection Design | STRAIGHT 2ND END |
CRFY | Flow Angle | 90.0 DEGREES 1ST END |
THSD | Thread Series Designator | UNF 2ND END |
CRXX | Measuring Method And Length | 25.200 INCHES NOMINAL WORKING |
THSD | Thread Series Designator | UNF 1ST END |
ABKV | Outside Diameter | 0.312 INCHES NOMINAL |
CQBD | Burst Test Pressure | 12000.0 POUNDS PER SQUARE INCH |
CQJX | Nominal Thread Size | 0.438 INCHES 1ST END |
MRC | Decoded Requirement | Clear Text Reply |
AARX | Inside Diameter | 0.187 INCHES NOMINAL |
AAGR | Cross-Sectional Shape Style | ROUND |
CQJX | Nominal Thread Size | 0.438 INCHES 2ND END |
AWLS | Connection Type | THREADED INTERNAL TUBE 1ST END |
AHNC | Connection Style | SWIVEL NUT FLARE 2ND END |
CMLP | Thread Quantity Per Inch | 20 1ST END |
CMLP | Thread Quantity Per Inch | 20 2ND END |
CQCS | Layer Composition And Location | OUTER LAYER BRAIDED CORROSION RESISTANT STEEL WIRE |
AHNC | Connection Style | SWIVEL NUT FLARE 1ST END |
ABJH | Temp Rating | -65.0 DEG FAHRENHEIT SINGLE RESPONSE AND 450.0 DEG FAHRENHEIT SINGLE RESPONSE |
Relevant Components for NSN - 4720-00-782-1422, 4720007821422 | ||||
4710-01-441-8899 (4710014418899) | 4710-01-498-7114 (4710014987114) | 4730-01-220-9884 (4730012209884) | 4730-01-501-3937 (4730015013937) | |
4730-01-420-1964 (4730014201964) | 4710-01-577-3240 (4710015773240) | 4730-01-666-8794 (4730016668794) | 4730-00-764-6544 (4730007646544) | |
4710-00-921-8621 (4710009218621) | 4720-01-314-0923 (4720013140923) | 4710-01-587-0220 (4710015870220) | 4710-12-176-9032 (4710121769032) | |
If You’re Ever Looking for NSN parts Or Have an Aircraft On Ground Situation, Don’t forget That We offer Competitive Pricing and Guaranteed On-Time Delivery.
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