4084243CLM — NOZZLE ASSEMBLY,TURBINE,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

4084243CLM: NOZZLE ASSEMBLY,TURBINE,AIRCRAFT.

NOZZLE ASSEMBLY,TURBINE,AIRCRAFT. 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: 2.820 INCHES NOMINAL IN, special_features: T.O. 2J-F100-24, FIG 109; FLOW AREA 4.615-4.639 SQUARE INCH AREA.

This part is cataloged in the U.S. Government catalog under NSN 2840-01-447-4909, 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

4084243CLM

NSN: 2840-01-447-4909
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	2.820 INCHES NOMINAL IN
special_features	T.O. 2J-F100-24, FIG 109; FLOW AREA 4.615-4.639 SQUARE INCH AREA
blade_attachment_method	SLOT
end_item_identification	F100-PW-100/200/220E AIRCRAFT GAS TURBINE ENGINE
engine_section_location	LOW PRESSURE TURBINE
criticality_code_justification	MATT AND ABKW AND ABMK AND ABHP AND FEAT
part_name_assigned_by_controlling_agency	ORIGINAL NAME VANE,TURBINE STATOR
NSN	2840-01-447-4909

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 3

•

DESIGN TYPE: AXIAL COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: MATT AND ABKW AND ABMK AND ABHP AND FEAT

•

BLADE ATTACHMENT METHOD: SLOT

•

ENGINE SECTION LOCATION: LOW PRESSURE 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	MATT AND ABKW AND ABMK AND ABHP AND FEAT
BLADE ATTACHMENT METHOD	SLOT
OVERALL LENGTH	2.820 INCHES NOMINAL IN
OVERALL WIDTH	2.036 INCHES MINIMUM AND 2.084 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	LOW PRESSURE TURBINE
SPECIAL FEATURES	T.O. 2J-F100-24, FIG 109; FLOW AREA 4.615-4.639 SQUARE INCH AREA
PART NAME ASSIGNED BY CONTROLLING AGENCY	ORIGINAL NAME VANE,TURBINE STATOR

SUBSTITUTES & CROSS-REFERENCES 1

4084243Reference 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 4084243CLM?

4084243CLM is a NOZZLE ASSEMBLY,TURBINE,AIRCRAFT.

What parts can replace 4084243CLM?

There is 1 known substitute for 4084243CLM: 4084243. Substitute compatibility should be verified for your specific system.

What is the NSN for 4084243CLM?

4084243CLM is cataloged in the U.S. Government catalog under NSN 2840-01-447-4909. This indicates validated use in U.S. government and defense supply chains.

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4084243CLM — NOZZLE ASSEMBLY,TURBINE,AIRCRAFT

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