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111R304P01 — BLADE,TURBINE ROTOR,AIRCRAFT GAS

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

111R304P01: BLADE,TURBINE ROTOR,AIRCRAFT GAS.

BLADE,TURBINE ROTOR,AIRCRAFT GAS. Key specifications include material: STEEL BLADE, overall_width: 1.530 INCHES MINIMUM AND 1.570 INCHES MAXIMUM IN, overall_length: 5.850 INCHES MINIMUM AND 5.868 INCHES MAXIMUM IN, material_thickness: 0.668 INCHES MINIMUM AND 0.683 INCHES MAXIMUM IN, end_item_identification: J79 ENGINE, engine_section_location: TURBINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-007-5442, 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
111R304P01
NSN: 2840-01-007-5442
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)
SPECIFICATIONS
materialSTEEL BLADE
overall_width1.530 INCHES MINIMUM AND 1.570 INCHES MAXIMUM IN
overall_length5.850 INCHES MINIMUM AND 5.868 INCHES MAXIMUM IN
material_thickness0.668 INCHES MINIMUM AND 0.683 INCHES MAXIMUM IN
end_item_identificationJ79 ENGINE
engine_section_locationTURBINE
criticality_code_justificationAGAV
NSN2840-01-007-5442
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available BLADE,TURBINE ROTOR,AIRCRAFT GAS TITLE COMPONENT PN 111R304P01 MFR BLADE,TURBINE ROTOR,AI
KEY FEATURES
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
ENGINE SECTION LOCATION: TURBINE
•
MATERIAL THICKNESS: 0.668 INCHES MINIMUM AND 0.683 INCHES MAXIMUM IN
•
MATERIAL: STEEL BLADE
TECHNICAL CHARACTERISTICS
CRITICALITY CODE JUSTIFICATIONAGAV
OVERALL LENGTH5.850 INCHES MINIMUM AND 5.868 INCHES MAXIMUM IN
OVERALL WIDTH1.530 INCHES MINIMUM AND 1.570 INCHES MAXIMUM IN
ENGINE SECTION LOCATIONTURBINE
MATERIAL THICKNESS0.668 INCHES MINIMUM AND 0.683 INCHES MAXIMUM IN
END ITEM IDENTIFICATIONJ79 ENGINE
MATERIALSTEEL 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

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 111R304P01?
111R304P01 is a BLADE,TURBINE ROTOR,AIRCRAFT GAS.
What is the NSN for 111R304P01?
111R304P01 is cataloged in the U.S. Government catalog under NSN 2840-01-007-5442. 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.