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2840PL2128152 — SHROUD SEGMENT,TURBINE,AIRCRAFT

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

2840PL2128152: SHROUD SEGMENT,TURBINE,AIRCRAFT.

SHROUD SEGMENT,TURBINE,AIRCRAFT. Key specifications include diameter: 20.480 INCHES MINIMUM AND 20.500 INCHES MAXIMUM IN, material: TITANIUM ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_width: 3.825 INCHES NOMINAL IN, overall_length: 0.532 INCHES MINIMUM AND 0.542 INCHES MAXIMUM IN, special_features: T.O. 2J-F100-54; 35 HOLES EQ SP 0.520-0.540.

This part is cataloged in the U.S. Government catalog under NSN 2840-01-322-2051, 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
2840PL2128152
NSN: 2840-01-322-2051
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 9009H — JEDNOLITY INDEKS MATERIALOWY - UNIFORM MATERIAL INDEX (POL)
SPECIFICATIONS
diameter20.480 INCHES MINIMUM AND 20.500 INCHES MAXIMUM IN
materialTITANIUM ALLOY OVERALL
design_typeAXIAL COMPRESSOR
stage_number3
overall_width3.825 INCHES NOMINAL IN
overall_length0.532 INCHES MINIMUM AND 0.542 INCHES MAXIMUM IN
special_featuresT.O. 2J-F100-54; 35 HOLES EQ SP 0.520-0.540
material_thickness0.050 INCHES MINIMUM AND 0.060 INCHES MAXIMUM IN
end_item_identificationF100PW0229 AIRCRAFT ENGINE
engine_section_locationCOMPRESSOR
criticality_code_justificationAGAV
material_document_and_classificationAMS4928 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
NSN2840-01-322-2051
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available SHROUD SEGMENT,TURBINE,AIRCRAFT TITLE COMPONENT PN 2840PL2128152 MFR SHROUD SEGMENT,TURBINE
KEY FEATURES
•
STAGE NUMBER: 3
•
DESIGN TYPE: AXIAL COMPRESSOR
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
MATERIAL DOCUMENT AND CLASSIFICATION: AMS4928 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
•
DIAMETER: 20.480 INCHES MINIMUM AND 20.500 INCHES MAXIMUM IN
•
ENGINE SECTION LOCATION: COMPRESSOR
TECHNICAL CHARACTERISTICS
STAGE NUMBER3
DESIGN TYPEAXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATIONAGAV
MATERIAL DOCUMENT AND CLASSIFICATIONAMS4928 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
DIAMETER20.480 INCHES MINIMUM AND 20.500 INCHES MAXIMUM IN
OVERALL LENGTH0.532 INCHES MINIMUM AND 0.542 INCHES MAXIMUM IN
OVERALL WIDTH3.825 INCHES NOMINAL IN
ENGINE SECTION LOCATIONCOMPRESSOR
MATERIAL THICKNESS0.050 INCHES MINIMUM AND 0.060 INCHES MAXIMUM IN
SPECIAL FEATUREST.O. 2J-F100-54; 35 HOLES EQ SP 0.520-0.540
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.
2840-00-004-4242 2840-00-021-4702 2840-00-043-0981 2840-00-043-0982 2840-00-048-5261 2840-00-407-9165 2840-01-171-0875
SUBSTITUTES & CROSS-REFERENCES

No substitute or cross-reference records for this part.

LIFECYCLE
NSN statusActive· U.S. Government catalog
Demilitarization required — mutilation + specific procedure
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FREQUENTLY ASKED QUESTIONS
What is 2840PL2128152?
2840PL2128152 is a SHROUD SEGMENT,TURBINE,AIRCRAFT.
What is the NSN for 2840PL2128152?
2840PL2128152 is cataloged in the U.S. Government catalog under NSN 2840-01-322-2051. This indicates validated use in U.S. government and defense supply chains.
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