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4084743CLR — NOZZLE ASSEMBLY,TURBINE,AIRCRAFT

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

4084743CLR: NOZZLE ASSEMBLY,TURBINE,AIRCRAFT.

NOZZLE ASSEMBLY,TURBINE,AIRCRAFT. Key specifications include material: NICKEL ALLOY VANE, design_type: AXIAL COMPRESSOR, overall_length: 4.689 INCHES MINIMUM AND 4.714 INCHES MAXIMUM IN, special_features: DRAWING NAME VANE,TURBINE STATOR,3 STAGE,ASSY OF; OVERALL LENGTH IS FLOW AREA OF NOZZLE, blade_attachment_method: SLOT, end_item_identification: ACFT ENG F100PW100. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-445-3716, 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
4084743CLR
NSN: 2840-01-445-3716
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 VANE
design_typeAXIAL COMPRESSOR
stage_number3
overall_length4.689 INCHES MINIMUM AND 4.714 INCHES MAXIMUM IN
special_featuresDRAWING NAME VANE,TURBINE STATOR,3 STAGE,ASSY OF; OVERALL LENGTH IS FLOW AREA OF NOZZLE
blade_attachment_methodSLOT
end_item_identificationACFT ENG F100PW100
engine_section_locationLOW PRESSURE COMPRESSOR
criticality_code_justificationAGAV
NSN2840-01-445-3716
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available NOZZLE ASSEMBLY,TURBINE,AIRCRAFT TITLE COMPONENT PN 4084743CLR MFR NOZZLE ASSEMBLY,TURBIN
KEY FEATURES
•
STAGE NUMBER: 3
•
DESIGN TYPE: AXIAL COMPRESSOR
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
BLADE ATTACHMENT METHOD: SLOT
•
ENGINE SECTION LOCATION: LOW PRESSURE COMPRESSOR
TECHNICAL CHARACTERISTICS
STAGE NUMBER3
DESIGN TYPEAXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATIONAGAV
BLADE ATTACHMENT METHODSLOT
OVERALL LENGTH4.689 INCHES MINIMUM AND 4.714 INCHES MAXIMUM IN
ENGINE SECTION LOCATIONLOW PRESSURE COMPRESSOR
SPECIAL FEATURESDRAWING NAME VANE,TURBINE STATOR,3 STAGE,ASSY OF; OVERALL LENGTH IS FLOW AREA OF NOZZLE
END ITEM IDENTIFICATIONACFT ENG F100PW100
MATERIALNICKEL ALLOY VANE
SUBSTITUTES & CROSS-REFERENCES 1
4084743Reference document
Same NSN cross-reference
Reference document — Drawing number reference only
LIFECYCLE
NSN statusActive· U.S. Government catalog
Demilitarization required — mutilation + specific procedure
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FREQUENTLY ASKED QUESTIONS
What is 4084743CLR?
4084743CLR is a NOZZLE ASSEMBLY,TURBINE,AIRCRAFT.
What parts can replace 4084743CLR?
There is 1 known substitute for 4084743CLR: 4084743. Substitute compatibility should be verified for your specific system.
What is the NSN for 4084743CLR?
4084743CLR is cataloged in the U.S. Government catalog under NSN 2840-01-445-3716. 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.