4084113-01 — DISK,TURBINE,AIRCRAFT GAS TURBIN

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

4084113-01: DISK,TURBINE,AIRCRAFT GAS TURBIN.

DISK,TURBINE,AIRCRAFT GAS TURBIN. Key specifications include diameter: 17.311 INCHES NOMINAL IN, material: NICKEL ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 3.156 INCHES MINIMUM AND 3.166 INCHES MAXIMUM IN, special_features: BLADE SLOTS ARE FIR TREE DESIGN, end_item_identification: F100-PW-100 AIRCRAFT GAS TURBINE ENGINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-443-4088, 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

4084113-01

NSN: 2840-01-443-4088
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 77445 — RTX CORPORATION DBA PRATT & WHITNEY DIV PRATT &WHITNEY (USA)

SPECIFICATIONS

diameter	17.311 INCHES NOMINAL IN
material	NICKEL ALLOY OVERALL
design_type	AXIAL COMPRESSOR
stage_number	3
overall_length	3.156 INCHES MINIMUM AND 3.166 INCHES MAXIMUM IN
special_features	BLADE SLOTS ARE FIR TREE DESIGN
end_item_identification	F100-PW-100 AIRCRAFT GAS TURBINE ENGINE
engine_section_location	TURBINE
criticality_code_justification	CZBJ AND CZCJ AND ABHP AND ABMZ AND FEAT
material_document_and_classification	PWA1106 MFR REF SINGLE MATERIAL RESPONSE OVERALL
NSN	2840-01-443-4088

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 3

•

DESIGN TYPE: AXIAL COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: CZBJ AND CZCJ AND ABHP AND ABMZ AND FEAT

•

MATERIAL DOCUMENT AND CLASSIFICATION: PWA1106 MFR REF SINGLE MATERIAL RESPONSE OVERALL

•

DIAMETER: 17.311 INCHES NOMINAL IN

•

ENGINE SECTION LOCATION: TURBINE

TECHNICAL CHARACTERISTICS

STAGE NUMBER	3
DESIGN TYPE	AXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATION	CZBJ AND CZCJ AND ABHP AND ABMZ AND FEAT
MATERIAL DOCUMENT AND CLASSIFICATION	PWA1106 MFR REF SINGLE MATERIAL RESPONSE OVERALL
DIAMETER	17.311 INCHES NOMINAL IN
OVERALL LENGTH	3.156 INCHES MINIMUM AND 3.166 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	TURBINE
SPECIAL FEATURES	BLADE SLOTS ARE FIR TREE DESIGN
END ITEM IDENTIFICATION	F100-PW-100 AIRCRAFT GAS TURBINE ENGINE
MATERIAL	NICKEL ALLOY OVERALL

OTHER ITEMS IN FSC 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components

Items in the same Federal Supply class. No interchangeability or substitution relationship is implied.

2840-00-004-4242 2840-00-021-4702 2840-00-043-0981 2840-00-043-0982 2840-00-048-5261 2840-00-407-9165 2840-01-171-0875

SUBSTITUTES & CROSS-REFERENCES

No substitute or cross-reference records for this part.

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 4084113-01?

4084113-01 is a DISK,TURBINE,AIRCRAFT GAS TURBIN.

What is the NSN for 4084113-01?

4084113-01 is cataloged in the U.S. Government catalog under NSN 2840-01-443-4088. This indicates validated use in U.S. government and defense supply chains.

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4084113-01 — DISK,TURBINE,AIRCRAFT GAS TURBIN

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