9663M23G11 — SHROUD SEGMENT,TURBINE,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9663M23G11: SHROUD SEGMENT,TURBINE,AIRCRAFT.

SHROUD SEGMENT,TURBINE,AIRCRAFT. Key specifications include diameter: 48.660 INCHES NOMINAL48.660 INCHES NOMINAL IN, material: STEEL OUTER CASE, overall_length: 2.720 INCHES MINIMUM AND 2.720 INCHES MINIMUM AND 2.740 INCHES MAXIMUM2.740 INCHES MAXIMUM IN, end_item_identification: ACFT ENG TF39ACFT ENG TF39, engine_section_location: TURBINETURBINE, criticality_code_justification: AGAVAGAV. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-122-1881, 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

9663M23G11

NSN: 2840-01-122-1881
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

diameter	48.660 INCHES NOMINAL48.660 INCHES NOMINAL IN
material	STEEL OUTER CASE
overall_length	2.720 INCHES MINIMUM AND 2.720 INCHES MINIMUM AND 2.740 INCHES MAXIMUM2.740 INCHES MAXIMUM IN
end_item_identification	ACFT ENG TF39ACFT ENG TF39
engine_section_location	TURBINETURBINE
criticality_code_justification	AGAVAGAV
material_document_and_classification	B50TF25CL-A MFR REF SINGLE MATERIAL RESPONSE OUTER CASEB50TF25CL-A MFR REF SINGLE MATERIAL RESPONSE OUTER CASE
NSN	2840-01-122-1881

COMPONENT DIAGRAM

KEY FEATURES

•

CRITICALITY CODE JUSTIFICATION: AGAVAGAV

•

MATERIAL DOCUMENT AND CLASSIFICATION: B50TF25CL-A MFR REF SINGLE MATERIAL RESPONSE OUTER CASEB50TF25CL-A MFR REF SINGLE MATERIAL RESPONSE OUTER CASE

•

DIAMETER: 48.660 INCHES NOMINAL48.660 INCHES NOMINAL IN

•

ENGINE SECTION LOCATION: TURBINETURBINE

•

MATERIAL: STEEL OUTER CASE

TECHNICAL CHARACTERISTICS

CRITICALITY CODE JUSTIFICATION	AGAVAGAV
MATERIAL DOCUMENT AND CLASSIFICATION	B50TF25CL-A MFR REF SINGLE MATERIAL RESPONSE OUTER CASEB50TF25CL-A MFR REF SINGLE MATERIAL RESPONSE OUTER CASE
DIAMETER	48.660 INCHES NOMINAL48.660 INCHES NOMINAL IN
OVERALL LENGTH	2.720 INCHES MINIMUM AND 2.720 INCHES MINIMUM AND 2.740 INCHES MAXIMUM2.740 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	TURBINETURBINE
END ITEM IDENTIFICATION	ACFT ENG TF39ACFT ENG TF39
MATERIAL	STEEL 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

No substitute or cross-reference records for this part.

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 9663M23G11?

9663M23G11 is a SHROUD SEGMENT,TURBINE,AIRCRAFT.

What is the NSN for 9663M23G11?

9663M23G11 is cataloged in the U.S. Government catalog under NSN 2840-01-122-1881. This indicates validated use in U.S. government and defense supply chains.

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9663M23G11 — SHROUD SEGMENT,TURBINE,AIRCRAFT

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