5104T40P01 by General Electric Company - Receive a Competitive Quote
Part Number: 5104T40P01 | Manufacturer: General Electric Company | NSN : 2835-01-518-4528 | Item Name : Plate Component Mou | CAGE Code: 99207 | FSC : 2835 Gas Turbines and Jet Engines Non-Aircraft Prime Mover Aircraft Non-Prime Mover and Components | ||
We’re excited to announce that 5104T40P01 NSN part is now available and ready for immediate shipping. Part number 5104T40P01 is a Plate Component Mou manufactured by General Electric Company with NSN 2835015184528. Are you interested in a quick and competitive quote for this part?
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NSN Information for Part Number 5104T40P01 with NSN 2835-01-518-4528, 2835015184528
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2835-01-518-4528 Item PartTypeName: PLATE,COMPONENT MOUNTING,NONAIRC | 2835 | 015184528 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
5104T40P01 | 5 | 2 | 3 |
Characteristics Data of NSN 2835-01-518-4528, 2835015184528
MRC | Criteria | Characteristic |
---|---|---|
FEAT | Special Features | HAVING ONE HOLE CENTERED ON PLATE WITH A 0.395 TO A 0.415 INCH DIAMETER; HAVING FOUR HOLES, ONE CENTERED ON EACH CORNER APPROXIMATELY 0.300 TO 0.310 INCHES FROM EDGES, EACH WITH A 0.143 TO A 0.146 INCH DIAMETER; HAVING TWO HOLES OFFSET FROM CENTER AT 29 DEGREES ACROSS LENGTH, 1.500 INCHES FROM CENTER, EACH WITH A 0.330 TO A 0.338 INCH DIAMTER |
ABPX | Material Thickness | 0.091 INCHES MINIMUM AND 0.109 INCHES MAXIMUM |
AGAV | End Item Identification | F/A18-E/F F414 GE-400 ENGINE |
CXCY | Part Name Assigned By Controlling Agency | PLATE,STIFFENING |
MATT | Material | TITANIUM ALLOY OVERALL |
ABHP | Overall Length | 4.300 INCHES MINIMUM AND 4.350 INCHES MAXIMUM |
MRC | Decoded Requirement | Clear Text Reply |
ABMK | Overall Width | 1.660 INCHES MINIMUM AND 1.700 INCHES MAXIMUM |
MDCL | Material Document And Classification | AMS 4911 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
CRTL | Criticality Code Justification | AGAV |