9084M40P01 — HUB,COMPRESSOR,AIRCRAFT GAS TURB

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9084M40P01: HUB,COMPRESSOR,AIRCRAFT GAS TURB.

HUB,COMPRESSOR,AIRCRAFT GAS TURB. Key specifications include material: STEEL HUB, design_type: COMPRESSOR, overall_width: 0.860 INCHES MINIMUM AND 0.920 INCHES MAXIMUM IN, overall_length: 1.100 INCHES MINIMUM AND 1.140 INCHES MAXIMUM IN, special_features: ORIG NAME HUB,COMPRESSOR FRAME, material_thickness: 0.185 INCHES NOMINAL IN. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-144-2473, 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

9084M40P01

NSN: 2840-01-144-2473
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

material	STEEL HUB
design_type	COMPRESSOR
overall_width	0.860 INCHES MINIMUM AND 0.920 INCHES MAXIMUM IN
overall_length	1.100 INCHES MINIMUM AND 1.140 INCHES MAXIMUM IN
special_features	ORIG NAME HUB,COMPRESSOR FRAME
material_thickness	0.185 INCHES NOMINAL IN
end_item_identification	ACFT ENG TF-39
engine_section_location	COMPRESSOR
criticality_code_justification	APGF AND CZBJ AND ABHP AND ABMK AND ABPX
material_document_and_classification	B50TF14,CL-A MFR REF 1ST MATERIAL RESPONSE HUB
NSN	2840-01-144-2473

COMPONENT DIAGRAM

KEY FEATURES

•

DESIGN TYPE: COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: APGF AND CZBJ AND ABHP AND ABMK AND ABPX

•

MATERIAL DOCUMENT AND CLASSIFICATION: B50TF14,CL-A MFR REF 1ST MATERIAL RESPONSE HUB

•

ENGINE SECTION LOCATION: COMPRESSOR

•

MATERIAL THICKNESS: 0.185 INCHES NOMINAL IN

TECHNICAL CHARACTERISTICS

DESIGN TYPE	COMPRESSOR
CRITICALITY CODE JUSTIFICATION	APGF AND CZBJ AND ABHP AND ABMK AND ABPX
MATERIAL DOCUMENT AND CLASSIFICATION	B50TF14,CL-A MFR REF 1ST MATERIAL RESPONSE HUB
OVERALL LENGTH	1.100 INCHES MINIMUM AND 1.140 INCHES MAXIMUM IN
OVERALL WIDTH	0.860 INCHES MINIMUM AND 0.920 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	COMPRESSOR
MATERIAL THICKNESS	0.185 INCHES NOMINAL IN
SPECIAL FEATURES	ORIG NAME HUB,COMPRESSOR FRAME
END ITEM IDENTIFICATION	ACFT ENG TF-39
MATERIAL	STEEL HUB

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: Normally procured from the manufacturer (OEM)Demilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 9084M40P01?

9084M40P01 is a HUB,COMPRESSOR,AIRCRAFT GAS TURB.

What is the NSN for 9084M40P01?

9084M40P01 is cataloged in the U.S. Government catalog under NSN 2840-01-144-2473. This indicates validated use in U.S. government and defense supply chains.

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9084M40P01 — HUB,COMPRESSOR,AIRCRAFT GAS TURB

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