4080380-01 — SHROUD SEGMENT,TURBINE,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

4080380-01: SHROUD SEGMENT,TURBINE,AIRCRAFT.

SHROUD SEGMENT,TURBINE,AIRCRAFT. Key specifications include diameter: 17.431 INCHES MINIMUM AND 17.436 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, design_type: COMPRESSOR, stage_number: 10, overall_length: 0.846 INCHES MINIMUM AND 0.850 INCHES MAXIMUM IN, end_item_identification: F100PW0229 AIRCRAFT ENGINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-356-3536, 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

4080380-01

NSN: 2840-01-356-3536
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	17.431 INCHES MINIMUM AND 17.436 INCHES MAXIMUM IN
material	NICKEL ALLOY OVERALL
design_type	COMPRESSOR
stage_number	10
overall_length	0.846 INCHES MINIMUM AND 0.850 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	2840-01-356-3536

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 10

•

DESIGN TYPE: COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

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

•

DIAMETER: 17.431 INCHES MINIMUM AND 17.436 INCHES MAXIMUM IN

•

ENGINE SECTION LOCATION: COMPRESSOR

TECHNICAL CHARACTERISTICS

STAGE NUMBER	10
DESIGN TYPE	COMPRESSOR
CRITICALITY CODE JUSTIFICATION	AGAV
MATERIAL DOCUMENT AND CLASSIFICATION	AMS5666 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
DIAMETER	17.431 INCHES MINIMUM AND 17.436 INCHES MAXIMUM IN
OVERALL LENGTH	0.846 INCHES MINIMUM AND 0.850 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

2840PL0697035Reference 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 4080380-01?

4080380-01 is a SHROUD SEGMENT,TURBINE,AIRCRAFT.

What parts can replace 4080380-01?

There is 1 known substitute for 4080380-01: 2840PL0697035. Substitute compatibility should be verified for your specific system.

What is the NSN for 4080380-01?

4080380-01 is cataloged in the U.S. Government catalog under NSN 2840-01-356-3536. This indicates validated use in U.S. government and defense supply chains.

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4080380-01 — SHROUD SEGMENT,TURBINE,AIRCRAFT

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