4080382-01 — SHROUD SEGMENT,TURBINE,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

4080382-01: SHROUD SEGMENT,TURBINE,AIRCRAFT.

SHROUD SEGMENT,TURBINE,AIRCRAFT. Key specifications include diameter: 16.659 INCHES MINIMUM AND 16.667 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, design_type: COMPRESSOR, stage_number: 12, overall_length: 0.737 INCHES MINIMUM AND 0.747 INCHES MAXIMUM IN, end_item_identification: F100PW0229 AIRCRAFT ENGINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-357-5079, 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

4080382-01

NSN: 2840-01-357-5079
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	16.659 INCHES MINIMUM AND 16.667 INCHES MAXIMUM IN
material	NICKEL ALLOY OVERALL
design_type	COMPRESSOR
stage_number	12
overall_length	0.737 INCHES MINIMUM AND 0.747 INCHES MAXIMUM IN
end_item_identification	F100PW0229 AIRCRAFT ENGINE
engine_section_location	COMPRESSOR
criticality_code_justification	AGAV
material_document_and_classification	AMS5666 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
NSN	2840-01-357-5079

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 12

•

DESIGN TYPE: COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS5666 ASSN STD SINGLE MATERIAL RESPONSE OVERALL

•

DIAMETER: 16.659 INCHES MINIMUM AND 16.667 INCHES MAXIMUM IN

•

ENGINE SECTION LOCATION: COMPRESSOR

TECHNICAL CHARACTERISTICS

STAGE NUMBER	12
DESIGN TYPE	COMPRESSOR
CRITICALITY CODE JUSTIFICATION	AGAV
MATERIAL DOCUMENT AND CLASSIFICATION	AMS5666 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
DIAMETER	16.659 INCHES MINIMUM AND 16.667 INCHES MAXIMUM IN
OVERALL LENGTH	0.737 INCHES MINIMUM AND 0.747 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	COMPRESSOR
END ITEM IDENTIFICATION	F100PW0229 AIRCRAFT 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.

2840-00-000-0048 2840-00-000-0049 2840-00-001-1741 2840-00-001-1743 2840-00-001-2117 2840-00-001-2284 2840-00-001-3922 2840-00-001-4903

SUBSTITUTES & CROSS-REFERENCES 1

2840PL0697082Reference document

Same NSN cross-reference

Reference document — Informative reference only

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 4080382-01?

4080382-01 is a SHROUD SEGMENT,TURBINE,AIRCRAFT.

What parts can replace 4080382-01?

There is 1 known substitute for 4080382-01: 2840PL0697082. Substitute compatibility should be verified for your specific system.

What is the NSN for 4080382-01?

4080382-01 is cataloged in the U.S. Government catalog under NSN 2840-01-357-5079. This indicates validated use in U.S. government and defense supply chains.

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4080382-01 — SHROUD SEGMENT,TURBINE,AIRCRAFT

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