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4081609-02 — BLADE,COMPRESSOR,AIRCRAFT GAS TU

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

4081609-02: BLADE,COMPRESSOR,AIRCRAFT GAS TU.

BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: NICKEL ALLOY BLADE, design_type: AXIAL COMPRESSOR, overall_width: 0.935 INCHES MINIMUM AND 0.943 INCHES MAXIMUM IN, overall_length: 1.905 INCHES NOMINAL IN, special_features: T.O. 2J-F100-54, blade_attachment_method: SLOT.

This part is cataloged in the U.S. Government catalog under NSN 2840-01-370-9804, 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
4081609-02
NSN: 2840-01-370-9804
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 77445 — RTX CORPORATION DBA PRATT & WHITNEY DIV PRATT &WHITNEY (USA)
SPECIFICATIONS
materialNICKEL ALLOY BLADE
design_typeAXIAL COMPRESSOR
stage_number9
overall_width0.935 INCHES MINIMUM AND 0.943 INCHES MAXIMUM IN
overall_length1.905 INCHES NOMINAL IN
special_featuresT.O. 2J-F100-54
blade_attachment_methodSLOT
end_item_identificationF100PW0229 AIRCRAFT ENGINE/CORE
engine_section_locationCOMPRESSOR
criticality_code_justificationAGAV
NSN2840-01-370-9804
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available BLADE,COMPRESSOR,AIRCRAFT GAS TU TITLE COMPONENT PN 4081609-02 MFR BLADE,COMPRESSOR,AIRCR
KEY FEATURES
•
STAGE NUMBER: 9
•
DESIGN TYPE: AXIAL COMPRESSOR
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
BLADE ATTACHMENT METHOD: SLOT
•
ENGINE SECTION LOCATION: COMPRESSOR
TECHNICAL CHARACTERISTICS
STAGE NUMBER9
DESIGN TYPEAXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATIONAGAV
BLADE ATTACHMENT METHODSLOT
OVERALL LENGTH1.905 INCHES NOMINAL IN
OVERALL WIDTH0.935 INCHES MINIMUM AND 0.943 INCHES MAXIMUM IN
ENGINE SECTION LOCATIONCOMPRESSOR
SPECIAL FEATUREST.O. 2J-F100-54
END ITEM IDENTIFICATIONF100PW0229 AIRCRAFT ENGINE/CORE
MATERIALNICKEL 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.
2840-00-004-4242 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
2840PL0711157Reference document
Same NSN cross-reference
Reference document — Informative reference only
4079309-02Reference document
Same NSN cross-reference
Reference document — Secondary reference
LIFECYCLE
NSN statusActive· U.S. Government catalog
Demilitarization required — critical (Q)
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FREQUENTLY ASKED QUESTIONS
What is 4081609-02?
4081609-02 is a BLADE,COMPRESSOR,AIRCRAFT GAS TU.
What parts can replace 4081609-02?
There are 2 known substitutes for 4081609-02: 2840PL0711157, 4079309-02. Substitute compatibility should be verified for your specific system.
What is the NSN for 4081609-02?
4081609-02 is cataloged in the U.S. Government catalog under NSN 2840-01-370-9804. This indicates validated use in U.S. government and defense supply chains.
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