Mfg Part Number: D000004SS0318
NSN : 4720-01-544-7282
NIIN : 015447282
CAGE Code : 2T577
Manufacturer: Titeflex Corp
Item Name : Hose Assembly Nonme
Here at Internet For Aviation, we have D000004SS0318 Hose Assembly Nonme from Titeflex Corp, as well as a variety of other parts from reliable manufacturers. As the only independent distributor with a No China Sourcing policy, we go to great lengths to ensure that we source responsibly when it comes to certified standard items. If you’re in need of a specific D000004SS0318 to aid you in your aircraft repair capabilities, simply search by NSN part number, NSN or Cage Code on our parts directory. Submit an instant RFQ and a representative will get back to you in as little as 15 minutes.
Note : We Will Not Share Your Information To Any Third Parties.
We pride ourselves in our abilities to deliver quality superior grade aviation parts in a timely schedule. Thanks to the various supply chain locations that we have across the United States. We can execute fast shipping times that outpace our competitors. Unlike other competitors, we can promise same day shipping and delivery right to the very place you need. We’re leaders in our industry thanks to our parts streamlining process which includes quick stock and acquisition of the certified product and fast shipping. For whatever needs you have, be they Hose Assembly Nonme and D000004SS0318 parts, we can procure and deliver in a schedule that fits with you! Contact us today for an immediate quote!
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 4720-01-544-7282 Item Description: Hose Assembly Nonme | 4720 | 015447282 | 0 | N | A | |
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | A | 0 | |||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| D000004SS0318 | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ACKH | MINIMUM INSIDE BENDING RADIUS | 2.000 INCHES |
| CQBB | (NON-CORE DATA) SECOND END RELATIONSHIP WITH FIRST END | IDENTICAL |
| FEAT | SPECIAL FEATURES | LOCATION OF HOSE ASSY: SUCTION GAUGE TO PUMP INLET; STAINLESS STEEL F JIC FITTINGS PER MIL-DTL-27267 ON EACH END |
| ADJM | (NON-CORE DATA) INNER CONVEYING TUBE MATERIAL | PLASTIC, POLYTETRAFLUOROETHYLENE |
| AAJD | THREAD CLASS | 2B 1ST END |
| CQGH | (NON-CORE DATA) FIRST END FITTING/COMPONENT AND MATERIAL | COMPLETE FITTING STEEL, CORROSION RESISTING |
| CQBD | BURST TEST PRESSURE | 6500.0 POUNDS PER SQUARE INCH |
| CQRB | SEAT ANGLE | 37.0 DEGREES 1ST END |
| ABKV | OUTSIDE DIAMETER | 0.375 INCHES NOMINAL |
| AAJP | (NON-CORE DATA) OUTSIDE SURFACE TREATMENT | PASSIVATED |
| AHNC | CONNECTION STYLE | FLARE 1ST END |
| CQBG | (NON-CORE DATA) FIRST END SWIVEL ACTION CAPABILITY | NOT INCLUDED |
| AARX | INSIDE DIAMETER | 0.250 INCHES NOMINAL |
| AKUU | END CONNECTION DESIGN | STRAIGHT 1ST END |
| CRXX | MEASURING METHOD AND LENGTH | 31.500 INCHES NOMINAL OVERALL |
| CQCS | LAYER COMPOSITION AND LOCATION | OUTER LAYER BRAIDED CORROSION RESISTANT STEEL WIRE |
| AAGR | CROSS-SECTIONAL SHAPE STYLE | ROUND |
| CQJX | NOMINAL THREAD SIZE | 0.500 INCHES 1ST END |
| AWLS | CONNECTION TYPE | THREADED INTERNAL TUBE 1ST END |
| AAJF | THREAD DIRECTION | RIGHT-HAND 1ST END |
| CQGM | MAXIMUM OPERATING PRESSURE | 1500.0 POUNDS PER SQUARE INCH |
| CRWL | INSIDE SURFACE CONDITION | SMOOTH |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ASSEMBLY, HOSE FUEL PIPING (STATIC DISSIPATING) |
| AGAV | END ITEM IDENTIFICATION | FORCE SYSTEM, REFUELER |
| ABJH | TEMP RATING | -65.0 DEG FAHRENHEIT SINGLE RESPONSE AND 450.0 DEG FAHRENHEIT SINGLE RESPONSE |
| THSD | THREAD SERIES DESIGNATOR | UNF 1ST END |
Semiconductor's Certifications and Memberships
 |
“We Proudly Support Intrepid Fallen Heroes Fund that serves United States Military Personal experiencing the Invisible Wounds of War : Traumatic Brain Injury (TBI) and Post Traumatic Stress (PTS). Please visit website (www.fallenheroesfund.org) and help in their valiant effort”. |
We Hope that You'll Choose Buy Aviation Parts as Your Quick and Convenient Parts Distributor In the Future.
Request for Quote
