9524M27G04 — CASE,COMPRESSOR,AIRCRAFT GAS TUR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9524M27G04: CASE,COMPRESSOR,AIRCRAFT GAS TUR.

CASE,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include diameter: 42.390 INCHES MINIMUM AND 42.410 INCHES MAXIMUM IN, material: TITANIUM ALLOY OVERALL, design_type: AXIAL-CENTRIFUGAL, overall_length: 19.135 INCHES MINIMUM AND 19.145 INCHES MAXIMUM IN, end_item_identification: ACFT ENG F101, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-175-1284, 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

9524M27G04

NSN: 2840-01-175-1284
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

diameter	42.390 INCHES MINIMUM AND 42.410 INCHES MAXIMUM IN
material	TITANIUM ALLOY OVERALL
design_type	AXIAL-CENTRIFUGAL
overall_length	19.135 INCHES MINIMUM AND 19.145 INCHES MAXIMUM IN
end_item_identification	ACFT ENG F101
engine_section_location	COMPRESSOR
criticality_code_justification	AGAV
material_document_and_classification	AMS4928 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
NSN	2840-01-175-1284

COMPONENT DIAGRAM

KEY FEATURES

•

DESIGN TYPE: AXIAL-CENTRIFUGAL

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS4928 ASSN STD SINGLE MATERIAL RESPONSE OVERALL

•

DIAMETER: 42.390 INCHES MINIMUM AND 42.410 INCHES MAXIMUM IN

•

ENGINE SECTION LOCATION: COMPRESSOR

•

MATERIAL: TITANIUM ALLOY OVERALL

TECHNICAL CHARACTERISTICS

DESIGN TYPE	AXIAL-CENTRIFUGAL
CRITICALITY CODE JUSTIFICATION	AGAV
MATERIAL DOCUMENT AND CLASSIFICATION	AMS4928 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
DIAMETER	42.390 INCHES MINIMUM AND 42.410 INCHES MAXIMUM IN
OVERALL LENGTH	19.135 INCHES MINIMUM AND 19.145 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	COMPRESSOR
END ITEM IDENTIFICATION	ACFT ENG F101
MATERIAL	TITANIUM 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.

2840-00-000-0048 2840-00-000-0049 2840-00-001-1741 2840-00-001-1743 2840-00-001-2117 2840-00-001-2284 2840-00-001-3922 2840-00-001-4903

SUBSTITUTES & CROSS-REFERENCES 2

9524M27G03Reference document

Same NSN cross-reference

Reference document — Secondary reference

9524M27Reference document

Same NSN cross-reference

Reference document — Drawing number reference only

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 9524M27G04?

9524M27G04 is a CASE,COMPRESSOR,AIRCRAFT GAS TUR.

What parts can replace 9524M27G04?

There are 2 known substitutes for 9524M27G04: 9524M27G03, 9524M27. Substitute compatibility should be verified for your specific system.

What is the NSN for 9524M27G04?

9524M27G04 is cataloged in the U.S. Government catalog under NSN 2840-01-175-1284. This indicates validated use in U.S. government and defense supply chains.

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9524M27G04 — CASE,COMPRESSOR,AIRCRAFT GAS TUR

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