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9524M31G02 — CASE,TURBINE,AIRCRAFT GAS TURBIN

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

9524M31G02: CASE,TURBINE,AIRCRAFT GAS TURBIN.

CASE,TURBINE,AIRCRAFT GAS TURBIN. Key specifications include diameter: 21.634 INCHES NOMINAL IN, material: ALUMINUM ALLOY OVERALL, overall_length: 2.717 INCHES MINIMUM AND 2.727 INCHES MAXIMUM IN, special_features: WAS CASE,TURBINE ROTOR,TURBINE ENGINE, end_item_identification: ACFT ENG F101, engine_section_location: TURBINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-173-7430, 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
9524M31G02
NSN: 2840-01-173-7430
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)
SPECIFICATIONS
diameter21.634 INCHES NOMINAL IN
materialALUMINUM ALLOY OVERALL
overall_length2.717 INCHES MINIMUM AND 2.727 INCHES MAXIMUM IN
special_featuresWAS CASE,TURBINE ROTOR,TURBINE ENGINE
end_item_identificationACFT ENG F101
engine_section_locationTURBINE
criticality_code_justificationAGAV
material_document_and_classificationAMS4132 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
NSN2840-01-173-7430
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available CASE,TURBINE,AIRCRAFT GAS TURBIN TITLE COMPONENT PN 9524M31G02 MFR CASE,TURBINE,AIRCRAFT
KEY FEATURES
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
MATERIAL DOCUMENT AND CLASSIFICATION: AMS4132 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
•
DIAMETER: 21.634 INCHES NOMINAL IN
•
ENGINE SECTION LOCATION: TURBINE
•
MATERIAL: ALUMINUM ALLOY OVERALL
TECHNICAL CHARACTERISTICS
CRITICALITY CODE JUSTIFICATIONAGAV
MATERIAL DOCUMENT AND CLASSIFICATIONAMS4132 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
DIAMETER21.634 INCHES NOMINAL IN
OVERALL LENGTH2.717 INCHES MINIMUM AND 2.727 INCHES MAXIMUM IN
ENGINE SECTION LOCATIONTURBINE
SPECIAL FEATURESWAS CASE,TURBINE ROTOR,TURBINE ENGINE
END ITEM IDENTIFICATIONACFT ENG F101
MATERIALALUMINUM 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 1
9524M31G03Reference document
Same NSN cross-reference
Reference document — Secondary reference
LIFECYCLE
NSN statusActive· U.S. Government catalog
Acquisition advice: Insurance item — stocked against contingency demandDemilitarization required — mutilation + specific procedure
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FREQUENTLY ASKED QUESTIONS
What is 9524M31G02?
9524M31G02 is a CASE,TURBINE,AIRCRAFT GAS TURBIN.
What parts can replace 9524M31G02?
There is 1 known substitute for 9524M31G02: 9524M31G03. Substitute compatibility should be verified for your specific system.
What is the NSN for 9524M31G02?
9524M31G02 is cataloged in the U.S. Government catalog under NSN 2840-01-173-7430. This indicates validated use in U.S. government and defense supply chains.
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✓ PartsTable — the parts reference. Every fact cited to its source.
PartsTable Design LLC · partstable.com
U.S. Government catalog: edition PUBLOGDVD v12.0.0 (OCT 2026), edition date 2026-10-01, retrieved 2026-10-18.
PartsTable commercial catalog: edition Unified commercial catalog snapshot through 2026-09-28, edition date not on file, retrieved 2026-09-28.