Mfg Part Number: 6051T95G04
NSN : 2840-01-364-2281
NIIN : 013642281
CAGE Code : 99207
Manufacturer: General Electric Company
Item Name : Frame Rear Aircraft Gas Turbine
If you’re in need of NSN parts, Purchasing Synergy is the ultimate source. As an ASAP Semiconductor company, we have access to a vast and diverse inventory of parts and components like 6051T95G04 for the aerospace, civil aviation, defense, electronics, and industrial markets. This includes parts such as Frame Rear Aircraft Gas Turbine from General Electric Company with Cage Code 99207 as well as part numbers like 6051T95G04 and FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components with013642281. Purchasing Synergy has more than two billion new and obsolete parts readily available with short lead times and competitive prices and, as we are an AS9120B, ISO 9001:2015, and FAA AC 00-56B accredited business, and the only independent distributor with a No China Sourcing Pledge, each part we sell is fully traceable or comes directly from the manufacturer.
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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-364-2281 Item Description: Frame Rear Aircraft Gas Turbine | 2840 | 013642281 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
I | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
6051t95g04 | 1 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
AARX | INSIDE DIAMETER | 15.495 INCHES MINIMUM AND 15.535 INCHES MAXIMUM |
ABHP | OVERALL LENGTH | 4.517 INCHES MINIMUM AND 4.531 INCHES MAXIMUM |
ABKV | OUTSIDE DIAMETER | 16.995 INCHES MINIMUM AND 17.005 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | J85 AIRCRAFT ENGINE |
CRTL | CRITICALITY CODE JUSTIFICATION | ABHP AND ABKV AND AARX AND CZLB |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME FRAME ASSEMBLY,TURBINE |
CZLB | NUMBER OF VARIABLE GUIDE VANES | 6 |
FEAT | SPECIAL FEATURES | MAINFRAME COMPRESSOR SECTION; MUST CONFORM TO AS367 SAFETY WIRE, KEY WASHERS AND COTTER PIN |
MATT | MATERIAL | NICKEL ALLOY |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-J85-54, FIG 13, IND 1 |
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