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2840PL0711120 — COMPRESSOR,AIRCRAFT GAS TURBINE

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

2840PL0711120: COMPRESSOR,AIRCRAFT GAS TURBINE.

COMPRESSOR,AIRCRAFT GAS TURBINE. Key specifications include diameter: 21.935 INCHES MINIMUM AND 21.942 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 6.669 INCHES MINIMUM AND 6.679 INCHES MAXIMUM IN, end_item_identification: F100PW0229 AIRCRAFT ENGINE/CORE, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-369-6008, 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
2840PL0711120
NSN: 2840-01-369-6008
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 9009H — JEDNOLITY INDEKS MATERIALOWY - UNIFORM MATERIAL INDEX (POL)
SPECIFICATIONS
diameter21.935 INCHES MINIMUM AND 21.942 INCHES MAXIMUM IN
materialNICKEL ALLOY OVERALL
design_typeAXIAL COMPRESSOR
overall_length6.669 INCHES MINIMUM AND 6.679 INCHES MAXIMUM IN
end_item_identificationF100PW0229 AIRCRAFT ENGINE/CORE
engine_section_locationCOMPRESSOR
criticality_code_justificationAGAV
NSN2840-01-369-6008
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available COMPRESSOR,AIRCRAFT GAS TURBINE TITLE COMPONENT PN 2840PL0711120 MFR COMPRESSOR,AIRCRAFT GA
KEY FEATURES
•
DESIGN TYPE: AXIAL COMPRESSOR
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
DIAMETER: 21.935 INCHES MINIMUM AND 21.942 INCHES MAXIMUM IN
•
ENGINE SECTION LOCATION: COMPRESSOR
•
MATERIAL: NICKEL ALLOY OVERALL
TECHNICAL CHARACTERISTICS
DESIGN TYPEAXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATIONAGAV
DIAMETER21.935 INCHES MINIMUM AND 21.942 INCHES MAXIMUM IN
OVERALL LENGTH6.669 INCHES MINIMUM AND 6.679 INCHES MAXIMUM IN
ENGINE SECTION LOCATIONCOMPRESSOR
END ITEM IDENTIFICATIONF100PW0229 AIRCRAFT ENGINE/CORE
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.
2840-00-004-4242 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 2
4077880-01Same NSN cross-reference
Same NSN cross-reference
Also cataloged under this NSN
2840PL1602498Reference document
Same NSN cross-reference
Reference document — Informative reference only
LIFECYCLE
NSN statusActive· U.S. Government catalog
Acquisition advice: Terminal item — no further procurement; issued until stock is exhaustedDemilitarization required — mutilation + specific procedure
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FREQUENTLY ASKED QUESTIONS
What is 2840PL0711120?
2840PL0711120 is a COMPRESSOR,AIRCRAFT GAS TURBINE.
What parts can replace 2840PL0711120?
There are 2 known substitutes for 2840PL0711120: 4077880-01, 2840PL1602498. Substitute compatibility should be verified for your specific system.
What is the NSN for 2840PL0711120?
2840PL0711120 is cataloged in the U.S. Government catalog under NSN 2840-01-369-6008. This indicates validated use in U.S. government and defense supply chains.
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