Request a Quote on General Electric Company Part Number 9184M63G05 with the NSN 2840-01-434-7020 Today!

Part Number: 9184M63G05

Manufacturer: General Electric Company

NSN: 2840-01-434-7020

NIIN: 014347020

Item Name : Frame Turbine Aircraft Gas Turbine Engine

CAGE Code: 07482

FSC: 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components

FSG: 28 Engines Turbines and Components

Country: USA

NCB Code: 01

Thank you for taking an interest in the Frame Turbine Aircraft Gas Turbine Engine NSN parts that we carry here on Buy Military Ground Vehicle Parts. You have reached the RFQ page for part number 9184M63G05, an item that traces back to the manufacturer General Electric Company. Listed with NSN 2840014347020, this listing is available for purchase from our website at any time. If you are interested in part number 9184M63G05 and wish to learn more, be sure to fill out and submit the RFQ form found on this page. By presenting us information such as your target price and expected delivery date, we can best formulate and present a solution that closely caters to your unique needs and restrictions alike.

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To make the part searching process as simple as possible, we choose to list offerings with as much relevant information as we can. For example, while part number 9184M63G05 is manufactured by General Electric Company, it is specifically listed along with CAGE Code 07482. With this identifier, you can trace this item back to the exact facility it was sourced from. Additionally, with the NSN 2840-01-434-7020, this signifies that the product belongs to the Federal Supply Class 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Alongside our easy-to-navigate database, we also offer highly competitive pricing and rapid lead times for the benefit of our customers. Get in touch with an industry expert today and see why so many customers steadily depend on us for their operational needs.

Characteristics Data of NSN 2840-01-434-7020, 2840014347020

MRC	Criteria	Characteristic
FEAT	Special Features	6TURBINE MID FRAME ASSY; NEW FRAME TO REDUCE NUMBER OF LINER SADDLE AND BLIPPER CRACKS; G10 FRAME HAS NEW LINER, 1820M83G01, WHICH INCORPORATES A REDESIGNED BLIPPER, HIGHER IN STRENGTH/TEMPERATURE; INTERGAL WITH THE LINER FOWARD OUT RING INSTEAD OF BEING WELDED TO THE RING AS OF NOW; TURBINE MID FRAME NOT AFFECTED IN PHYSICAL INTERCHANGEABILITY; NEW LINER AND CURRENT LINER ARE PHYSICALLY INTERCHANGEABLE; FUNCTIONAL INTERCHANGEABILITY IS AFFECTED IN THAT THE NEW LINER HAS HIGHER STRENGTH/TEMPERATURE
RDAL	Reference Data And Literature	T.O. 2J-TF39-4, FIG 63 IND 1
ABHP	Overall Length	13.165 INCHES MINIMUM AND 13.205 INCHES MAXIMUM
CRTL	Criticality Code Justification	ABHP AND ABKV AND FEAT
AGAV	End Item Identification	TF-39 AIRCRAFT GAS TURBINE ENGINE
ABKV	Outside Diameter	16.160 INCHES MINIMUM AND 16.200 INCHES MAXIMUM
MATT	Material	NICKEL ALLOY
MRC	Decoded Requirement	Clear Text Reply