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4084383CLS — NOZZLE,TURBINE,AIRCRAFT GAS TURB

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

4084383CLS: NOZZLE,TURBINE,AIRCRAFT GAS TURB.

NOZZLE,TURBINE,AIRCRAFT GAS TURB. Key specifications include material: NICKEL ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_width: 2.036 INCHES MINIMUM AND 2.084 INCHES MAXIMUM IN, overall_height: 4.717 INCHES MINIMUM AND 4.737 INCHES MAXIMUM IN, overall_length: 2.246 INCHES MINIMUM AND 2.254 INCHES MAXIMUM IN, special_features: T.O. 2J-F100-14, FIG 132, FLOW AREA 4.714-4.738.

This part is cataloged in the U.S. Government catalog under NSN 2840-01-445-5358, 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
4084383CLS
NSN: 2840-01-445-5358
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 77445 — RTX CORPORATION DBA PRATT & WHITNEY DIV PRATT &WHITNEY (USA)
SPECIFICATIONS
materialNICKEL ALLOY OVERALL
design_typeAXIAL COMPRESSOR
stage_number3
overall_width2.036 INCHES MINIMUM AND 2.084 INCHES MAXIMUM IN
overall_height4.717 INCHES MINIMUM AND 4.737 INCHES MAXIMUM IN
overall_length2.246 INCHES MINIMUM AND 2.254 INCHES MAXIMUM IN
special_featuresT.O. 2J-F100-14, FIG 132, FLOW AREA 4.714-4.738
end_item_identificationF100-PW-100 AIRCRAFT GAS TURBINE ENGINE
engine_section_locationTURBINE
criticality_code_justificationABMK AND ABHP AND ABKW AND FEAT AND CZCJ
NSN2840-01-445-5358
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available NOZZLE,TURBINE,AIRCRAFT GAS TURB TITLE COMPONENT PN 4084383CLS MFR NOZZLE,TURBINE,AIRCRAF
KEY FEATURES
•
STAGE NUMBER: 3
•
DESIGN TYPE: AXIAL COMPRESSOR
•
CRITICALITY CODE JUSTIFICATION: ABMK AND ABHP AND ABKW AND FEAT AND CZCJ
•
ENGINE SECTION LOCATION: TURBINE
TECHNICAL CHARACTERISTICS
OVERALL HEIGHT4.717 INCHES MINIMUM AND 4.737 INCHES MAXIMUM IN
STAGE NUMBER3
DESIGN TYPEAXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATIONABMK AND ABHP AND ABKW AND FEAT AND CZCJ
OVERALL LENGTH2.246 INCHES MINIMUM AND 2.254 INCHES MAXIMUM IN
OVERALL WIDTH2.036 INCHES MINIMUM AND 2.084 INCHES MAXIMUM IN
ENGINE SECTION LOCATIONTURBINE
SPECIAL FEATUREST.O. 2J-F100-14, FIG 132, FLOW AREA 4.714-4.738
END ITEM IDENTIFICATIONF100-PW-100 AIRCRAFT GAS TURBINE ENGINE
MATERIALNICKEL ALLOY OVERALL
SUBSTITUTES & CROSS-REFERENCES 1
4084383Reference document
Same NSN cross-reference
Reference document — Drawing number reference only
LIFECYCLE
NSN statusActive· U.S. Government catalog
Demilitarization required — mutilation
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FREQUENTLY ASKED QUESTIONS
What is 4084383CLS?
4084383CLS is a NOZZLE,TURBINE,AIRCRAFT GAS TURB.
What parts can replace 4084383CLS?
There is 1 known substitute for 4084383CLS: 4084383. Substitute compatibility should be verified for your specific system.
What is the NSN for 4084383CLS?
4084383CLS is cataloged in the U.S. Government catalog under NSN 2840-01-445-5358. 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.