4084743CLL — NOZZLE,TURBINE,AIRCRAFT GAS TURB

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

4084743CLL: 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 4.590-4.615.

This part is cataloged in the U.S. Government catalog under NSN 2840-01-445-4015, 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

4084743CLL

NSN: 2840-01-445-4015
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 77445 — RTX CORPORATION DBA PRATT & WHITNEY DIV PRATT &WHITNEY (USA)

SPECIFICATIONS

material	NICKEL ALLOY OVERALL
design_type	AXIAL COMPRESSOR
stage_number	3
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 4.590-4.615
end_item_identification	F100-PW-100 AIRCRAFT GAS TURBINE ENGINE
engine_section_location	TURBINE
criticality_code_justification	ABMK AND ABHP AND ABKW AND FEAT AND CZCJ
NSN	2840-01-445-4015

COMPONENT DIAGRAM

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 HEIGHT	4.717 INCHES MINIMUM AND 4.737 INCHES MAXIMUM IN
STAGE NUMBER	3
DESIGN TYPE	AXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATION	ABMK AND ABHP AND ABKW AND FEAT AND CZCJ
OVERALL LENGTH	2.246 INCHES MINIMUM AND 2.254 INCHES MAXIMUM IN
OVERALL WIDTH	2.036 INCHES MINIMUM AND 2.084 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	TURBINE
SPECIAL FEATURES	T.O. 2J-F100-14, FIG 132, FLOW AREA 4.590-4.615
END ITEM IDENTIFICATION	F100-PW-100 AIRCRAFT GAS TURBINE ENGINE
MATERIAL	NICKEL ALLOY OVERALL

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

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FREQUENTLY ASKED QUESTIONS

What is 4084743CLL?

4084743CLL is a NOZZLE,TURBINE,AIRCRAFT GAS TURB.

What parts can replace 4084743CLL?

There is 1 known substitute for 4084743CLL: 4084743. Substitute compatibility should be verified for your specific system.

What is the NSN for 4084743CLL?

4084743CLL is cataloged in the U.S. Government catalog under NSN 2840-01-445-4015. This indicates validated use in U.S. government and defense supply chains.

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4084743CLL — NOZZLE,TURBINE,AIRCRAFT GAS TURB

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