4081633-01 — ROTOR,COMPRESSOR,AIRCRAFT GAS TU

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

4081633-01: ROTOR,COMPRESSOR,AIRCRAFT GAS TU.

ROTOR,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include diameter: 18.783 INCHES NOMINAL IN, material: TITANIUM ALLOY OVERALL, overall_length: 15.500 INCHES NOMINAL IN, end_item_identification: F100PW229 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: COMPRESSOR, material_document_and_classification: PWA 1215 MFR REF SINGLE MATERIAL RESPONSE OVERALL. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-430-2158, 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

4081633-01

NSN: 2840-01-430-2158
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	18.783 INCHES NOMINAL IN
material	TITANIUM ALLOY OVERALL
stage_number	3
overall_length	15.500 INCHES NOMINAL IN
end_item_identification	F100PW229 AIRCRAFT GAS TURBINE ENGINE
engine_section_location	COMPRESSOR
material_document_and_classification	PWA 1215 MFR REF SINGLE MATERIAL RESPONSE OVERALL
NSN	2840-01-430-2158

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 3

•

MATERIAL DOCUMENT AND CLASSIFICATION: PWA 1215 MFR REF SINGLE MATERIAL RESPONSE OVERALL

•

DIAMETER: 18.783 INCHES NOMINAL IN

•

ENGINE SECTION LOCATION: COMPRESSOR

•

MATERIAL: TITANIUM ALLOY OVERALL

TECHNICAL CHARACTERISTICS

STAGE NUMBER	3
MATERIAL DOCUMENT AND CLASSIFICATION	PWA 1215 MFR REF SINGLE MATERIAL RESPONSE OVERALL
DIAMETER	18.783 INCHES NOMINAL IN
OVERALL LENGTH	15.500 INCHES NOMINAL IN
ENGINE SECTION LOCATION	COMPRESSOR
SPECIAL FEATURES	ROTOR CONSISTS OF 3 STGS; DISK & HUB; 1STG O/A DIA ON/C 14.590; O/A LENGTH 9.000; 2ND STG O/A DIA ON/C 16.188; O/A LENGTH 7.970; INVOLUTE SPLINE DATA: NO OF TEETH 79; SPLINE PITCH 20/40; PRESSURE ANGLE 30 DEG.; PITCH DIA. 3.9500; 3RD STG O/A LENGTH 4.000; ALL STAGES RECIEVE DOVETAIL BLADES
END ITEM IDENTIFICATION	F100PW229 AIRCRAFT GAS TURBINE ENGINE
MATERIAL	TITANIUM ALLOY OVERALL

SUBSTITUTES & CROSS-REFERENCES 3

4071223-01Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

4086294-01Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

4086295-01Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

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 4081633-01?

4081633-01 is a ROTOR,COMPRESSOR,AIRCRAFT GAS TU.

What parts can replace 4081633-01?

There are 3 known substitutes for 4081633-01: 4071223-01, 4086294-01, 4086295-01. Substitute compatibility should be verified for your specific system.

What is the NSN for 4081633-01?

4081633-01 is cataloged in the U.S. Government catalog under NSN 2840-01-430-2158. This indicates validated use in U.S. government and defense supply chains.

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4081633-01 — ROTOR,COMPRESSOR,AIRCRAFT GAS TU

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