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9663M24G15 — CASE,TURBINE,AIRCRAFT GAS TURBIN

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

9663M24G15: CASE,TURBINE,AIRCRAFT GAS TURBIN.

CASE,TURBINE,AIRCRAFT GAS TURBIN. Key specifications include diameter: 48.720 INCHES NOMINAL IN, material: STEEL OUTER CASE, overall_length: 2.702 INCHES MINIMUM AND 2.722 INCHES MAXIMUM IN, special_features: 2ND STAGE; ORIGINIALLY CASE,TURBINE ROTOR,TURBINE ENGINE, end_item_identification: ACFT ENG TF39, engine_section_location: TURBINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-123-0016, 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
9663M24G15
NSN: 2840-01-123-0016
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)
SPECIFICATIONS
diameter48.720 INCHES NOMINAL IN
materialSTEEL OUTER CASE
overall_length2.702 INCHES MINIMUM AND 2.722 INCHES MAXIMUM IN
special_features2ND STAGE; ORIGINIALLY CASE,TURBINE ROTOR,TURBINE ENGINE
end_item_identificationACFT ENG TF39
engine_section_locationTURBINE
criticality_code_justificationAGAV
material_document_and_classificationB50TF25-CLA MFR REF SINGLE MATERIAL RESPONSE OUTER CASE
NSN2840-01-123-0016
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available CASE,TURBINE,AIRCRAFT GAS TURBIN TITLE COMPONENT PN 9663M24G15 MFR CASE,TURBINE,AIRCRAFT
KEY FEATURES
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
MATERIAL DOCUMENT AND CLASSIFICATION: B50TF25-CLA MFR REF SINGLE MATERIAL RESPONSE OUTER CASE
•
DIAMETER: 48.720 INCHES NOMINAL IN
•
ENGINE SECTION LOCATION: TURBINE
•
MATERIAL: STEEL OUTER CASE
TECHNICAL CHARACTERISTICS
CRITICALITY CODE JUSTIFICATIONAGAV
MATERIAL DOCUMENT AND CLASSIFICATIONB50TF25-CLA MFR REF SINGLE MATERIAL RESPONSE OUTER CASE
DIAMETER48.720 INCHES NOMINAL IN
OVERALL LENGTH2.702 INCHES MINIMUM AND 2.722 INCHES MAXIMUM IN
ENGINE SECTION LOCATIONTURBINE
SPECIAL FEATURES2ND STAGE; ORIGINIALLY CASE,TURBINE ROTOR,TURBINE ENGINE
END ITEM IDENTIFICATIONACFT ENG TF39
MATERIALSTEEL OUTER CASE
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
2840PL0786506Reference document
Same NSN cross-reference
Reference document — Informative reference only
LIFECYCLE
NSN statusActive· U.S. Government catalog
Demilitarization required — critical (Q)
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FREQUENTLY ASKED QUESTIONS
What is 9663M24G15?
9663M24G15 is a CASE,TURBINE,AIRCRAFT GAS TURBIN.
What parts can replace 9663M24G15?
There is 1 known substitute for 9663M24G15: 2840PL0786506. Substitute compatibility should be verified for your specific system.
What is the NSN for 9663M24G15?
9663M24G15 is cataloged in the U.S. Government catalog under NSN 2840-01-123-0016. 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.