6004T50G01 — SHROUD SEGMENT,TURBINE,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

6004T50G01: SHROUD SEGMENT,TURBINE,AIRCRAFT.

SHROUD SEGMENT,TURBINE,AIRCRAFT. Key specifications include diameter: 7.628 INCHES NOMINAL IN, material: ALUMINUM ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 1.027 INCHES MINIMUM AND 1.031 INCHES MAXIMUM IN, special_features: T.O. 2J-J85-94; 125.0 MICROINCH FINISH ALL SURFACES, end_item_identification: J-85 AIRCRAFT ENGINE.

This part is cataloged in the U.S. Government catalog under NSN 2840-00-488-4947, indicating validated use in U.S. government and defense logistics supply chains.

Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels. Verify compatibility with your specific system configuration before ordering.

WHERE IT FITS

6004T50G01

NSN: 2840-00-488-4947
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 99207 — GENERAL ELECTRIC COMPANY DBA GE AEROSPACE (USA)

SPECIFICATIONS

diameter	7.628 INCHES NOMINAL IN
material	ALUMINUM ALLOY OVERALL
design_type	AXIAL COMPRESSOR
stage_number	1
overall_length	1.027 INCHES MINIMUM AND 1.031 INCHES MAXIMUM IN
special_features	T.O. 2J-J85-94; 125.0 MICROINCH FINISH ALL SURFACES
end_item_identification	J-85 AIRCRAFT ENGINE
engine_section_location	COMPRESSOR
criticality_code_justification	AGAV
material_document_and_classification	AMS4027 ASSN STD 1ST MATERIAL RESPONSE OR AMS4117 ASSN STD 2ND MATERIAL RESPONSE OR AMS4150 ASSN STD 2ND MATERIAL RESPONSE OVERALL
NSN	2840-00-488-4947

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 1

•

DESIGN TYPE: AXIAL COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS4027 ASSN STD 1ST MATERIAL RESPONSE OR AMS4117 ASSN STD 2ND MATERIAL RESPONSE OR AMS4150 ASSN STD 2ND MATERIAL RESPONSE OVERALL

•

DIAMETER: 7.628 INCHES NOMINAL IN

•

ENGINE SECTION LOCATION: COMPRESSOR

TECHNICAL CHARACTERISTICS

STAGE NUMBER	1
DESIGN TYPE	AXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATION	AGAV
MATERIAL DOCUMENT AND CLASSIFICATION	AMS4027 ASSN STD 1ST MATERIAL RESPONSE OR AMS4117 ASSN STD 2ND MATERIAL RESPONSE OR AMS4150 ASSN STD 2ND MATERIAL RESPONSE OVERALL
DIAMETER	7.628 INCHES NOMINAL IN
OVERALL LENGTH	1.027 INCHES MINIMUM AND 1.031 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	COMPRESSOR
SPECIAL FEATURES	T.O. 2J-J85-94; 125.0 MICROINCH FINISH ALL SURFACES
END ITEM IDENTIFICATION	J-85 AIRCRAFT ENGINE
MATERIAL	ALUMINUM ALLOY OVERALL

OTHER ITEMS IN FSC 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components

Items in the same Federal Supply class. No interchangeability or substitution relationship is implied.

2840-00-004-4242 2840-00-021-4702 2840-00-043-0981 2840-00-043-0982 2840-00-048-5261 2840-00-407-9165 2840-01-171-0875

SUBSTITUTES & CROSS-REFERENCES

No substitute or cross-reference records for this part.

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Insurance item — stocked against contingency demandDemilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 6004T50G01?

6004T50G01 is a SHROUD SEGMENT,TURBINE,AIRCRAFT.

What is the NSN for 6004T50G01?

6004T50G01 is cataloged in the U.S. Government catalog under NSN 2840-00-488-4947. This indicates validated use in U.S. government and defense supply chains.

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6004T50G01 — SHROUD SEGMENT,TURBINE,AIRCRAFT

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