Mfg Part Number: 204-076-437-003
Alternate P/N: 204076437003
NSN : 4820-00-923-0625
NIIN : 009230625
CAGE Code : 97499
Manufacturer: Bell Helicopter Textron Inc
Item Name : Valve Check
Here at Internet For Aviation, we have 204-076-437-003 Valve Check from Bell Helicopter Textron Inc, 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 204-076-437-003 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.
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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
4820-00-923-0625 Item Description: Valve Check | 4820 | 009230625 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | U | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
204-076-437-003 | 2 | 2 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
AAJD | THREAD CLASS | 3A 2ND END |
ADQU | FLOW CONTROL DEVICE | POPPET |
AHNC | CONNECTION STYLE | FLARED (TUBE) 1ST END |
AQLR | VALVE OPERATION METHOD | AUTOMATIC |
AWLS | CONNECTION TYPE | THREADED EXTERNAL TUBE 1ST END |
CQGM | MAXIMUM OPERATING PRESSURE | 1500.0 POUNDS PER SQUARE INCH SINGLE RESPONSE |
CQRB | SEAT ANGLE | 37.0 DEGREES 1ST END |
MEDA | MEDIA FOR WHICH DESIGNED | FUEL/OIL, HYDROCARBON SINGLE RESPONSE |
STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-A-8625,TY 2 MIL SPEC SINGLE TREATMENT RESPONSE |
AAJF | THREAD DIRECTION | RIGHT-HAND 1ST END |
ADSU | DISK LOADING METHOD | SPRING |
CMLP | THREAD QUANTITY PER INCH | 18 1ST END |
CQJX | NOMINAL THREAD SIZE | 0.5625 INCHES 2ND END |
CWFD | NOMINAL OUTSIDE DIAMETER TUBE ACCOMMODATED | 0.375 INCHES 2ND END |
SFTT | SURFACE TREATMENT | ANODIZE |
STYL | STYLE DESIGNATOR | STRAIGHT THRU |
THSD | THREAD SERIES DESIGNATOR | UNF 2ND END |
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