4087201 — DISK,TURBINE,AIRCRAFT GAS TURBIN

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

4087201: DISK,TURBINE,AIRCRAFT GAS TURBIN.

DISK,TURBINE,AIRCRAFT GAS TURBIN. Key specifications include diameter: 36.696 INCHES MINIMUM AND 36.736 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 1.809 INCHES MINIMUM AND 1.811 INCHES MAXIMUM IN, end_item_identification: F100-PW-229 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: TURBINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-448-7539, 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

4087201

NSN: 2840-01-448-7539
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	36.696 INCHES MINIMUM AND 36.736 INCHES MAXIMUM IN
material	NICKEL ALLOY OVERALL
design_type	AXIAL COMPRESSOR
stage_number	1
overall_length	1.809 INCHES MINIMUM AND 1.811 INCHES MAXIMUM IN
special_features	T.O. 2J-F100-54, FIG 99, IND 42; USE ONLY ON P/NS 4084517-700 AND 4083015-701; LOCATED NEAR THE REAR COMPRESSOR DRIVE TURBINE ROTOR AND STATOR ASSY
end_item_identification	F100-PW-229 AIRCRAFT GAS TURBINE ENGINE
engine_section_location	TURBINE
criticality_code_justification	APGF AND CZBJ AND ABMZ AND ABHP AND FEAT
material_document_and_classification	PWA1106 MFR REF SINGLE MATERIAL RESPONSE OVERALL
NSN	2840-01-448-7539

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 1

•

DESIGN TYPE: AXIAL COMPRESSOR

•

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

•

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

•

DIAMETER: 36.696 INCHES MINIMUM AND 36.736 INCHES MAXIMUM IN

•

ENGINE SECTION LOCATION: TURBINE

TECHNICAL CHARACTERISTICS

STAGE NUMBER	1
DESIGN TYPE	AXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATION	APGF AND CZBJ AND ABMZ AND ABHP AND FEAT
MATERIAL DOCUMENT AND CLASSIFICATION	PWA1106 MFR REF SINGLE MATERIAL RESPONSE OVERALL
DIAMETER	36.696 INCHES MINIMUM AND 36.736 INCHES MAXIMUM IN
OVERALL LENGTH	1.809 INCHES MINIMUM AND 1.811 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	TURBINE
SPECIAL FEATURES	T.O. 2J-F100-54, FIG 99, IND 42; USE ONLY ON P/NS 4084517-700 AND 4083015-701; LOCATED NEAR THE REAR COMPRESSOR DRIVE TURBINE ROTOR AND STATOR ASSY
END ITEM IDENTIFICATION	F100-PW-229 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 1

2840PL1775715Reference document

Same NSN cross-reference

Reference document — Informative reference only

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Terminal item — no further procurement; issued until stock is exhaustedDemilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 4087201?

4087201 is a DISK,TURBINE,AIRCRAFT GAS TURBIN.

What parts can replace 4087201?

There is 1 known substitute for 4087201: 2840PL1775715. Substitute compatibility should be verified for your specific system.

What is the NSN for 4087201?

4087201 is cataloged in the U.S. Government catalog under NSN 2840-01-448-7539. This indicates validated use in U.S. government and defense supply chains.

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4087201 — DISK,TURBINE,AIRCRAFT GAS TURBIN

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