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7D0181D0200A by Boeing Company The - Receive a Competitive Quote

Part Number: 7D0181D0200A Manufacturer: Boeing Company The NSN : 4720-01-449-2729 Item Name : Hose Assembly Nonme CAGE Code: 88277 FSC : 4720 Hose and Tubing Flexible

We’re excited to announce that 7D0181D0200A NSN part is now available and ready for immediate shipping. Part number 7D0181D0200A is a Hose Assembly Nonme manufactured by Boeing Company The with NSN 4720014492729. Are you interested in a quick and competitive quote for this part?

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NSN Information for Part Number 7D0181D0200A with NSN 4720-01-449-2729, 4720014492729

NSNFSCNIINCLSHazmatDEMILCancelled NSN
4720-01-449-2729

Item PartTypeName:

HOSE ASSEMBLY,NONMETALLIC

47200144927290N
CIICHCCESDPMICCriticalityENAC
UA
Part NumberISCRNVCRNCCHCCMSDSSADC
7D0181D0200A225

Characteristics Data of NSN 4720-01-449-2729, 4720014492729

MRCCriteriaCharacteristic
THSDThread Series DesignatorUNJF 1ST END
ABKVOutside Diameter0.640 INCHES NOMINAL
CQRBSeat Angle12.0 DEGREES 1ST END
CQCSLayer Composition And LocationOUTER LAYER MOLDED POLYTETRAFLUOROETHYLENE
CQGMMaximum Operating Pressure4000.0 POUNDS PER SQUARE INCH
AAJFThread DirectionRIGHT-HAND 1ST END
ADKXAngle Between Rigid Elbow Fittings In Deg0
ABJHTemp Rating-65.0 DEG FAHRENHEIT SINGLE RESPONSE AND 275.0 DEG FAHRENHEIT SINGLE RESPONSE
AAJDThread Class3B 1ST END
AKUUEnd Connection DesignSTRAIGHT 1ST END
CRDWHydrostatic Test Pressure8000.0 POUNDS PER SQUARE INCH
CRXXMeasuring Method And Length20.000 INCHES NOMINAL WORKING
MRCDecoded RequirementClear Text Reply
ACKHMinimum Inside Bending Radius2.500 INCHES
CQBDBurst Test Pressure16000.0 POUNDS PER SQUARE INCH
AARXInside Diameter0.333 INCHES NOMINAL
CQJXNominal Thread Size0.375 INCHES 1ST END
CRWLInside Surface ConditionSMOOTH
AAGRCross-Sectional Shape StyleROUND
AWLSConnection TypeTHREADED INTERNAL TUBE 1ST END
AGAVEnd Item IdentificationC-17A ACTF CAGE 88277, W/S CODE DT AIRCRAFT, AIRLIFTER C-17A
AHNCConnection StyleSWIVEL NUT, FLARELESS 1ST END
MEDAMedia For Which DesignedHYDRAULIC FLUID SINGLE RESPONSE