Mfg Part Number: 2621-166-01 PIECE 154
Alternate P/N: 262116601PIECE154
NSN : 4730-01-315-5611
NIIN : 013155611
CAGE Code : 8X098
Manufacturer: Triumph Mfg Co
Item Name : Elbow Flange To Pip
Here at Internet For Aviation, we have 2621-166-01 PIECE 154 Elbow Flange To Pip from Triumph Mfg Co, 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 2621-166-01 PIECE 154 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 |
---|---|---|---|---|---|---|
4730-01-315-5611 Item Description: Elbow Flange To Pip | 4730 | 013155611 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
2621-166-01 PIECE 154 | 5 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
AAAR | NOMINAL PIPE SIZE ACCOMMODATED | 4.000 INCHES 2ND END |
AHSJ | LEG LENGTH | 4.000 INCHES MINIMUM 2ND END AND 6.000 INCHES MAXIMUM 2ND END |
CQGM | MAXIMUM OPERATING PRESSURE | 700.0 POUNDS PER SQUARE INCH SINGLE RESPONSE |
CWCD | NOMINAL OUTSIDE DIAMETER | 8.688 INCHES 1ST END |
CWCQ | BOLT HOLE NOMINAL DIAMETER | 0.688 INCHES 1ST END |
MATT | MATERIAL | COPPER ALLOY OVERALL |
AECS | BOLT HOLE QUANTITY | 10 1ST END |
AHNC | CONNECTION STYLE | BEVELED (PIPE) 2ND END |
ARKN | FLANGE SHAPE | ROUND WITH HOLES 1ST END |
AWLS | CONNECTION TYPE | BUTT WELD PIPE 2ND END |
CRFY | FLOW ANGLE | 90.0 DEGREES |
CWCK | NOMINAL THICKNESS | 1.250 INCHES 1ST END |
CWCT | BOLT CIRCLE NOMINAL DIAMETER | 7.188 INCHES 1ST END |
CWDF | FLANGE FACE DESIGN | PLAIN WITH GASKET GROOVE 1ST END |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-C-20159,TY1 MIL SPEC SINGLE MATERIAL RESPONSE OVERALL |
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