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9663M32G44 — CASE AND NOZZLE ASSEMBLY,TURBINE

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

9663M32G44: CASE AND NOZZLE ASSEMBLY,TURBINE.

CASE AND NOZZLE ASSEMBLY,TURBINE. Key specifications include design_type: AXIAL COMPRESSOR, special_features: ORIGINAL NAME CASE AND NOZZLE,TURBINE,TURBINE ENGINE, end_item_identification: ENGINE,AIRCRAFT,TURBOFAN,MODEL TF39GE100, engine_section_location: TURBINE, reference_data_and_literature: T.O.2J-TF39-4 FIGURE 63, INDEX 101 AND FIGURE 68 BREAKOUT, criticality_code_justification: AGAV. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-003-1162, 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
9663M32G44
NSN: 2840-01-003-1162
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)
SPECIFICATIONS
design_typeAXIAL COMPRESSOR
special_featuresORIGINAL NAME CASE AND NOZZLE,TURBINE,TURBINE ENGINE
end_item_identificationENGINE,AIRCRAFT,TURBOFAN,MODEL TF39GE100
engine_section_locationTURBINE
reference_data_and_literatureT.O.2J-TF39-4 FIGURE 63, INDEX 101 AND FIGURE 68 BREAKOUT
criticality_code_justificationAGAV
NSN2840-01-003-1162
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available CASE AND NOZZLE ASSEMBLY,TURBINE TITLE COMPONENT PN 9663M32G44 MFR CASE AND NOZZLE ASSEMB
KEY FEATURES
•
DESIGN TYPE: AXIAL COMPRESSOR
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
REFERENCE DATA AND LITERATURE: T.O.2J-TF39-4 FIGURE 63, INDEX 101 AND FIGURE 68 BREAKOUT
•
ENGINE SECTION LOCATION: TURBINE
TECHNICAL CHARACTERISTICS
DESIGN TYPEAXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATIONAGAV
REFERENCE DATA AND LITERATURET.O.2J-TF39-4 FIGURE 63, INDEX 101 AND FIGURE 68 BREAKOUT
ENGINE SECTION LOCATIONTURBINE
SPECIAL FEATURESORIGINAL NAME CASE AND NOZZLE,TURBINE,TURBINE ENGINE
END ITEM IDENTIFICATIONENGINE,AIRCRAFT,TURBOFAN,MODEL TF39GE100
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 3
9663M32G41Same NSN cross-reference
Same NSN cross-reference
Also cataloged under this NSN
9663M32G42Same NSN cross-reference
Same NSN cross-reference
Also cataloged under this NSN
9663M32G40Same NSN cross-reference
Same NSN cross-reference
Also cataloged under this NSN
LIFECYCLE
NSN statusActive· U.S. Government catalog
Demilitarization required — mutilation + specific procedure
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FREQUENTLY ASKED QUESTIONS
What is 9663M32G44?
9663M32G44 is a CASE AND NOZZLE ASSEMBLY,TURBINE.
What parts can replace 9663M32G44?
There are 3 known substitutes for 9663M32G44: 9663M32G41, 9663M32G42, 9663M32G40. Substitute compatibility should be verified for your specific system.
What is the NSN for 9663M32G44?
9663M32G44 is cataloged in the U.S. Government catalog under NSN 2840-01-003-1162. This indicates validated use in U.S. government and defense supply chains.
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