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4064671 — CASE AND NOZZLE ASSEMBLY,TURBINE

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

4064671: CASE AND NOZZLE ASSEMBLY,TURBINE.

CASE AND NOZZLE ASSEMBLY,TURBINE. Key specifications include diameter: 34.105 INCHES MINIMUM AND 34.125 INCHES MAXIMUM IN, design_type: AXIAL COMPRESSOR, special_features: T.O. 2J-F100-14, FIG 141, IND 1, end_item_identification: F100-PW-100/200 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: TURBINE, criticality_code_justification: ABMZ AND FEAT AND CZBJ.

This part is cataloged in the U.S. Government catalog under NSN 2840-01-192-2386, 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
4064671
NSN: 2840-01-192-2386
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 77445 — RTX CORPORATION DBA PRATT & WHITNEY DIV PRATT &WHITNEY (USA)
SPECIFICATIONS
diameter34.105 INCHES MINIMUM AND 34.125 INCHES MAXIMUM IN
design_typeAXIAL COMPRESSOR
special_featuresT.O. 2J-F100-14, FIG 141, IND 1
end_item_identificationF100-PW-100/200 AIRCRAFT GAS TURBINE ENGINE
engine_section_locationTURBINE
criticality_code_justificationABMZ AND FEAT AND CZBJ
part_name_assigned_by_controlling_agencyORIGINAL NAME CASE AND NOZZLE,TURBINE,TURBINE ENGINE
NSN2840-01-192-2386
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available CASE AND NOZZLE ASSEMBLY,TURBINE TITLE COMPONENT PN 4064671 MFR CASE AND NOZZLE ASSEMB
KEY FEATURES
•
DESIGN TYPE: AXIAL COMPRESSOR
•
CRITICALITY CODE JUSTIFICATION: ABMZ AND FEAT AND CZBJ
•
DIAMETER: 34.105 INCHES MINIMUM AND 34.125 INCHES MAXIMUM IN
•
ENGINE SECTION LOCATION: TURBINE
TECHNICAL CHARACTERISTICS
DESIGN TYPEAXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATIONABMZ AND FEAT AND CZBJ
DIAMETER34.105 INCHES MINIMUM AND 34.125 INCHES MAXIMUM IN
ENGINE SECTION LOCATIONTURBINE
SPECIAL FEATUREST.O. 2J-F100-14, FIG 141, IND 1
PART NAME ASSIGNED BY CONTROLLING AGENCYORIGINAL NAME CASE AND NOZZLE,TURBINE,TURBINE ENGINE
END ITEM IDENTIFICATIONF100-PW-100/200 AIRCRAFT GAS TURBINE ENGINE
SUBSTITUTES & CROSS-REFERENCES 1
4076802Reference document
Same NSN cross-reference
Reference document — Secondary reference
LIFECYCLE
NSN statusActive· U.S. Government catalog
Acquisition advice: Terminal item — no further procurement; issued until stock is exhaustedDemilitarization required — critical (Q)
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FREQUENTLY ASKED QUESTIONS
What is 4064671?
4064671 is a CASE AND NOZZLE ASSEMBLY,TURBINE.
What parts can replace 4064671?
There is 1 known substitute for 4064671: 4076802. Substitute compatibility should be verified for your specific system.
What is the NSN for 4064671?
4064671 is cataloged in the U.S. Government catalog under NSN 2840-01-192-2386. 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.