2840PL0832736 — SHROUD SEGMENT,TURBINE,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

2840PL0832736: SHROUD SEGMENT,TURBINE,AIRCRAFT.

SHROUD SEGMENT,TURBINE,AIRCRAFT. Key specifications include diameter: 16.724 INCHES MINIMUM AND 16.724 INCHES MINIMUM AND 16.736 INCHES MAXIMUM16.736 INCHES MAXIMUM IN, material: ALUMINUM ALLOY OVERALL, design_type: COMPRESSORCOMPRESSOR, overall_length: 1.493 INCHES MINIMUM AND 1.493 INCHES MINIMUM AND 1.506 INCHES MAXIMUM1.506 INCHES MAXIMUM IN, special_features: WAS CASE,AXIAL COMPRESSOR,TURBINEENGINEWAS CASE,AXIAL COMPRESSOR,TURBINEENGINE, end_item_identification: ACFT ENG TF-39ACFT ENG TF-39. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-117-0323, 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

2840PL0832736

NSN: 2840-01-117-0323
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 9009H — JEDNOLITY INDEKS MATERIALOWY - UNIFORM MATERIAL INDEX (POL)

SPECIFICATIONS

diameter	16.724 INCHES MINIMUM AND 16.724 INCHES MINIMUM AND 16.736 INCHES MAXIMUM16.736 INCHES MAXIMUM IN
material	ALUMINUM ALLOY OVERALL
design_type	COMPRESSORCOMPRESSOR
overall_length	1.493 INCHES MINIMUM AND 1.493 INCHES MINIMUM AND 1.506 INCHES MAXIMUM1.506 INCHES MAXIMUM IN
special_features	WAS CASE,AXIAL COMPRESSOR,TURBINEENGINEWAS CASE,AXIAL COMPRESSOR,TURBINEENGINE
end_item_identification	ACFT ENG TF-39ACFT ENG TF-39
engine_section_location	COMPRESSORCOMPRESSOR
criticality_code_justification	AGAVAGAV
material_document_and_classification	AMS4127 ASSN STD SINGLE MATERIAL RESPONSE OVERALLAMS4127 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
NSN	2840-01-117-0323

COMPONENT DIAGRAM

KEY FEATURES

•

DESIGN TYPE: COMPRESSORCOMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: AGAVAGAV

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS4127 ASSN STD SINGLE MATERIAL RESPONSE OVERALLAMS4127 ASSN STD SINGLE MATERIAL RESPONSE OVERALL

•

DIAMETER: 16.724 INCHES MINIMUM AND 16.724 INCHES MINIMUM AND 16.736 INCHES MAXIMUM16.736 INCHES MAXIMUM IN

•

ENGINE SECTION LOCATION: COMPRESSORCOMPRESSOR

TECHNICAL CHARACTERISTICS

DESIGN TYPE	COMPRESSORCOMPRESSOR
CRITICALITY CODE JUSTIFICATION	AGAVAGAV
MATERIAL DOCUMENT AND CLASSIFICATION	AMS4127 ASSN STD SINGLE MATERIAL RESPONSE OVERALLAMS4127 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
DIAMETER	16.724 INCHES MINIMUM AND 16.724 INCHES MINIMUM AND 16.736 INCHES MAXIMUM16.736 INCHES MAXIMUM IN
OVERALL LENGTH	1.493 INCHES MINIMUM AND 1.493 INCHES MINIMUM AND 1.506 INCHES MAXIMUM1.506 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	COMPRESSORCOMPRESSOR
SPECIAL FEATURES	WAS CASE,AXIAL COMPRESSOR,TURBINEENGINEWAS CASE,AXIAL COMPRESSOR,TURBINEENGINE
END ITEM IDENTIFICATION	ACFT ENG TF-39ACFT ENG TF-39
MATERIAL	ALUMINUM 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

No substitute or cross-reference records for this part.

LIFECYCLE

NSN statusActive· U.S. Government catalog

No demilitarization required

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FREQUENTLY ASKED QUESTIONS

What is 2840PL0832736?

2840PL0832736 is a SHROUD SEGMENT,TURBINE,AIRCRAFT.

What is the NSN for 2840PL0832736?

2840PL0832736 is cataloged in the U.S. Government catalog under NSN 2840-01-117-0323. This indicates validated use in U.S. government and defense supply chains.

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2840PL0832736 — SHROUD SEGMENT,TURBINE,AIRCRAFT

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