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4080381-01 — SHROUD SEGMENT,TURBINE,AIRCRAFT

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

4080381-01: SHROUD SEGMENT,TURBINE,AIRCRAFT.

SHROUD SEGMENT,TURBINE,AIRCRAFT. Key specifications include diameter: 17.065 INCHES NOMINAL IN, material: NICKEL ALLOY OVERALL, design_type: COMPRESSOR, stage_number: 11, overall_length: 0.837 INCHES MINIMUM AND 0.841 INCHES MAXIMUM IN, end_item_identification: F100PW0229 AIRCRAFT ENGINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-357-5078, 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
4080381-01
NSN: 2840-01-357-5078
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 77445 — RTX CORPORATION DBA PRATT & WHITNEY DIV PRATT &WHITNEY (USA)
SPECIFICATIONS
diameter17.065 INCHES NOMINAL IN
materialNICKEL ALLOY OVERALL
design_typeCOMPRESSOR
stage_number11
overall_length0.837 INCHES MINIMUM AND 0.841 INCHES MAXIMUM IN
end_item_identificationF100PW0229 AIRCRAFT ENGINE
engine_section_locationCOMPRESSOR
criticality_code_justificationAGAV
material_document_and_classificationAMS5666 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
NSN2840-01-357-5078
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available SHROUD SEGMENT,TURBINE,AIRCRAFT TITLE COMPONENT PN 4080381-01 MFR SHROUD SEGMENT,TURBINE
KEY FEATURES
•
STAGE NUMBER: 11
•
DESIGN TYPE: COMPRESSOR
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
MATERIAL DOCUMENT AND CLASSIFICATION: AMS5666 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
•
DIAMETER: 17.065 INCHES NOMINAL IN
•
ENGINE SECTION LOCATION: COMPRESSOR
TECHNICAL CHARACTERISTICS
STAGE NUMBER11
DESIGN TYPECOMPRESSOR
CRITICALITY CODE JUSTIFICATIONAGAV
MATERIAL DOCUMENT AND CLASSIFICATIONAMS5666 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
DIAMETER17.065 INCHES NOMINAL IN
OVERALL LENGTH0.837 INCHES MINIMUM AND 0.841 INCHES MAXIMUM IN
ENGINE SECTION LOCATIONCOMPRESSOR
END ITEM IDENTIFICATIONF100PW0229 AIRCRAFT ENGINE
MATERIALNICKEL 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
2840PL0697078Reference 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 4080381-01?
4080381-01 is a SHROUD SEGMENT,TURBINE,AIRCRAFT.
What parts can replace 4080381-01?
There is 1 known substitute for 4080381-01: 2840PL0697078. Substitute compatibility should be verified for your specific system.
What is the NSN for 4080381-01?
4080381-01 is cataloged in the U.S. Government catalog under NSN 2840-01-357-5078. This indicates validated use in U.S. government and defense supply chains.
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