NSN 4720-01-452-2263, (4720014522263) Hose Assembly Nonmetallic Parts

The NSN 4720-01-452-2263 part numbers AS208, AS208K1116CP, 113552G1116C, 7D0195G1116C manufactured by Eaton Corporation, Smiths Tubular Systemslaconia I, Boeing Company is available in our inventory. As an ASAP Semiconductor owned and operated website, ASAP Aviation Unlimited has access to over three billion parts, paired with easy-to-use search engines that enable our customers to browse through our NSN 4720-01-452-2263 inventory quickly and efficiently. Our focus on quality control has earned us our FAA AC 0056B accreditation and AS9120B, ISO 9001:2015 certification, and we are the only independent distributor with a No China Sourcing pledge. If you are ready to get started, you can send an Instant RFQ form from this page for NSN 4720-01-452-2263 parts of Hose Assembly Nonmetallic, and one of our account managers will respond to it within fifteen minutes or less.


Alternative NSN: 4720-01-452-2263
Item Name: Hose Assembly Nonmetallic
FSG: 47 Pipe Tubing Hose and Fittings
Federal Supply Class (FSC): 4720 Hose and Flexible Tubing
NIIN: 014522263
NCB Code: USA (01)

Part Number's List for NSN 4720-01-452-2263, 4720014522263

Part No Manufacturer Item Name QTY RFQ
AS208 eaton corporation hose assembly nonmetallic Avl RFQ
AS208K1116CP eaton corporation hose assembly nonmetallic Avl RFQ
113552G1116C smiths tubular systemslaconia i hose assembly nonmetallic Avl RFQ
7D0195G1116C boeing company hose assembly nonmetallic Avl RFQ

Technical Characteristics of NSN 4720014522263

MRCCriteriaCharacteristic
CQBDBURST TEST PRESSURE16000.0 POUNDS PER SQUARE INCH
AAJDTHREAD CLASS3B 1ST END
ACKHMINIMUM INSIDE BENDING RADIUS7.750 INCHES
AWLSCONNECTION TYPETHREADED INTERNAL TUBE 1ST END
CRZY(NON-CORE DATA) SECOND END SWIVEL ACTION CAPABILITYNOT INCLUDED
CRWLINSIDE SURFACE CONDITIONSMOOTH
ADJM(NON-CORE DATA) INNER CONVEYING TUBE MATERIALPLASTIC, POLYTETRAFLUOROETHYLENE
ABJHTEMP RATING-65.0 DEG FAHRENHEIT AND 400.0 DEG FAHRENHEIT SINGLE RESPONSE
CQBB(NON-CORE DATA) SECOND END RELATIONSHIP WITH FIRST ENDNOT IDENTICAL
CQGH(NON-CORE DATA) FIRST END FITTING/COMPONENT AND MATERIALCOMPLETE FITTING TITANIUM
CQJXNOMINAL THREAD SIZE1.062 INCHES 1ST END 1.062 INCHES 2ND END
CQGMMAXIMUM OPERATING PRESSURE4000.0 POUNDS PER SQUARE INCH
CQRBSEAT ANGLE37.0 DEGREES 1ST END 37.0 DEGREES 2ND END
CQBG(NON-CORE DATA) FIRST END SWIVEL ACTION CAPABILITYNOT INCLUDED
CRDWHYDROSTATIC TEST PRESSURE8000.0 POUNDS PER SQUARE INCH
THSDTHREAD SERIES DESIGNATORUNJ 1ST END UNJ 2ND END
CRXXMEASURING METHOD AND LENGTH111.750 INCHES NOMINAL WORKING
AARXINSIDE DIAMETER0.690 INCHES NOMINAL
CRBL(NON-CORE DATA) SECOND END FITTING/COMPONENT AND MATERIALCOMPLETE FITTING TITANIUM
AKUUEND CONNECTION DESIGNSTRAIGHT 1ST END ELBOW 2ND END
ABKVOUTSIDE DIAMETER1.050 INCHES NOMINAL
CQCSLAYER COMPOSITION AND LOCATIONOUTER LAYER BRAIDED CORROSION RESISTANT STEEL WIRE
AHNCCONNECTION STYLESWIVEL NUT FLARE 1ST END SWIVEL NUT FLARE 2ND END
CMLPTHREAD QUANTITY PER INCH12 1ST END 12 2ND END
AAGRCROSS-SECTIONAL SHAPE STYLEROUND
AAJFTHREAD DIRECTIONRIGHT-HAND 1ST END
AGAVEND ITEM IDENTIFICATIONW/S CODE, AIRCRAFT, AIRLIFTER C-17A
CRFYFLOW ANGLE90.0 DEGREES 2ND END

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