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2840PL0711409 — BLADE,COMPRESSOR,AIRCRAFT GAS TU

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

2840PL0711409: BLADE,COMPRESSOR,AIRCRAFT GAS TU.

BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: TITANIUM ALLOY BLADE, design_type: AXIAL COMPRESSOR, overall_width: 0.674 INCHES NOMINAL IN, overall_length: 2.936 INCHES NOMINAL IN, end_item_identification: F100-PW-229 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-418-9485, 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
2840PL0711409
NSN: 2840-01-418-9485
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 9009H — JEDNOLITY INDEKS MATERIALOWY - UNIFORM MATERIAL INDEX (POL)
SPECIFICATIONS
materialTITANIUM ALLOY BLADE
design_typeAXIAL COMPRESSOR
stage_number7
overall_width0.674 INCHES NOMINAL IN
overall_length2.936 INCHES NOMINAL IN
end_item_identificationF100-PW-229 AIRCRAFT GAS TURBINE ENGINE
engine_section_locationCOMPRESSOR
criticality_code_justificationCZBJ AND ABHP AND ABMK
material_document_and_classificationPWA1209 MFR REF SINGLE MATERIAL RESPONSE BLADE
NSN2840-01-418-9485
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available BLADE,COMPRESSOR,AIRCRAFT GAS TU TITLE COMPONENT PN 2840PL0711409 MFR BLADE,COMPRESSOR,AIRCR
KEY FEATURES
•
STAGE NUMBER: 7
•
DESIGN TYPE: AXIAL COMPRESSOR
•
CRITICALITY CODE JUSTIFICATION: CZBJ AND ABHP AND ABMK
•
MATERIAL DOCUMENT AND CLASSIFICATION: PWA1209 MFR REF SINGLE MATERIAL RESPONSE BLADE
•
ENGINE SECTION LOCATION: COMPRESSOR
TECHNICAL CHARACTERISTICS
STAGE NUMBER7
DESIGN TYPEAXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATIONCZBJ AND ABHP AND ABMK
MATERIAL DOCUMENT AND CLASSIFICATIONPWA1209 MFR REF SINGLE MATERIAL RESPONSE BLADE
OVERALL LENGTH2.936 INCHES NOMINAL IN
OVERALL WIDTH0.674 INCHES NOMINAL IN
ENGINE SECTION LOCATIONCOMPRESSOR
END ITEM IDENTIFICATIONF100-PW-229 AIRCRAFT GAS TURBINE ENGINE
MATERIALTITANIUM ALLOY BLADE
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
4081507Same NSN cross-reference
Same NSN cross-reference
Also cataloged under this NSN
LIFECYCLE
NSN statusActive· U.S. Government catalog
Demilitarization required — critical (Q)
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FREQUENTLY ASKED QUESTIONS
What is 2840PL0711409?
2840PL0711409 is a BLADE,COMPRESSOR,AIRCRAFT GAS TU.
What parts can replace 2840PL0711409?
There is 1 known substitute for 2840PL0711409: 4081507. Substitute compatibility should be verified for your specific system.
What is the NSN for 2840PL0711409?
2840PL0711409 is cataloged in the U.S. Government catalog under NSN 2840-01-418-9485. This indicates validated use in U.S. government and defense supply chains.
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