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2840PL0854160 — BLADE,COMPRESSOR,AIRCRAFT GAS TU

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

2840PL0854160: BLADE,COMPRESSOR,AIRCRAFT GAS TU.

BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: STEEL BLADE, design_type: COMPRESSOR, overall_width: 1.696 INCHES NOMINAL IN, overall_length: 6.289 INCHES MINIMUM AND 6.309 INCHES MAXIMUM IN, special_features: ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE, blade_attachment_method: FIR TREE. This part is cataloged in the U.S.

Government catalog under NSN 2840-00-110-5977, 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
2840PL0854160
NSN: 2840-00-110-5977
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 9009H — JEDNOLITY INDEKS MATERIALOWY - UNIFORM MATERIAL INDEX (POL)
SPECIFICATIONS
materialSTEEL BLADE
design_typeCOMPRESSOR
stage_number3
overall_width1.696 INCHES NOMINAL IN
overall_length6.289 INCHES MINIMUM AND 6.309 INCHES MAXIMUM IN
special_featuresORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE
blade_attachment_methodFIR TREE
end_item_identificationTF-39
engine_section_locationCOMPRESSOR
criticality_code_justificationAGAV
NSN2840-00-110-5977
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available BLADE,COMPRESSOR,AIRCRAFT GAS TU TITLE COMPONENT PN 2840PL0854160 MFR BLADE,COMPRESSOR,AIRCR
KEY FEATURES
•
STAGE NUMBER: 3
•
DESIGN TYPE: COMPRESSOR
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
BLADE ATTACHMENT METHOD: FIR TREE
•
ENGINE SECTION LOCATION: COMPRESSOR
TECHNICAL CHARACTERISTICS
STAGE NUMBER3
DESIGN TYPECOMPRESSOR
CRITICALITY CODE JUSTIFICATIONAGAV
BLADE ATTACHMENT METHODFIR TREE
OVERALL LENGTH6.289 INCHES MINIMUM AND 6.309 INCHES MAXIMUM IN
OVERALL WIDTH1.696 INCHES NOMINAL IN
ENGINE SECTION LOCATIONCOMPRESSOR
SPECIAL FEATURESORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE
END ITEM IDENTIFICATIONTF-39
MATERIALSTEEL BLADE
SUBSTITUTES & CROSS-REFERENCES 3
9661M50P18Reference document
Same NSN cross-reference
Reference document — Secondary reference
9601M75P02Reference document
Same NSN cross-reference
Reference document — Secondary reference
K350P18Reference document
Same NSN cross-reference
Reference document — Secondary reference
LIFECYCLE
NSN statusActive· U.S. Government catalog
Acquisition advice: Insurance item — stocked against contingency demandDemilitarization required — critical (Q)
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FREQUENTLY ASKED QUESTIONS
What is 2840PL0854160?
2840PL0854160 is a BLADE,COMPRESSOR,AIRCRAFT GAS TU.
What parts can replace 2840PL0854160?
There are 3 known substitutes for 2840PL0854160: 9661M50P18, 9601M75P02, K350P18. Substitute compatibility should be verified for your specific system.
What is the NSN for 2840PL0854160?
2840PL0854160 is cataloged in the U.S. Government catalog under NSN 2840-00-110-5977. This indicates validated use in U.S. government and defense supply chains.
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✓ PartsTable — the parts reference. Every fact cited to its source.
PartsTable Design LLC · partstable.com
U.S. Government catalog: edition PUBLOGDVD v12.0.0 (OCT 2026), edition date 2026-10-01, retrieved 2026-10-18.
PartsTable commercial catalog: edition Unified commercial catalog snapshot through 2026-09-28, edition date not on file, retrieved 2026-09-28.