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1359M81P04 — BLADE,FAN,AIRCRAFT GAS TURBINE E

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

1359M81P04: BLADE,FAN,AIRCRAFT GAS TURBINE E.

BLADE,FAN,AIRCRAFT GAS TURBINE E. Key specifications include material: TITANIUM ALLOY BLADE, overall_width: 6.600 INCHES NOMINAL IN, overall_length: 12.700 INCHES NOMINAL IN, material_thickness: 2.700 INCHES NOMINAL IN, blade_attachment_method: DOVETAIL, end_item_identification: F118-100 ENGINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-474-2341, 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
1359M81P04
NSN: 2840-01-474-2341
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)
SPECIFICATIONS
materialTITANIUM ALLOY BLADE
stage_number1
overall_width6.600 INCHES NOMINAL IN
overall_length12.700 INCHES NOMINAL IN
material_thickness2.700 INCHES NOMINAL IN
blade_attachment_methodDOVETAIL
end_item_identificationF118-100 ENGINE
engine_section_locationFAN
reference_data_and_literature2J-F118-4, FIG 17, IND 5
criticality_code_justificationAGAV
NSN2840-01-474-2341
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available BLADE,FAN,AIRCRAFT GAS TURBINE E TITLE COMPONENT PN 1359M81P04 MFR BLADE,FAN,AIRCRAFT GAS
KEY FEATURES
•
STAGE NUMBER: 1
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
REFERENCE DATA AND LITERATURE: 2J-F118-4, FIG 17, IND 5
•
BLADE ATTACHMENT METHOD: DOVETAIL
•
ENGINE SECTION LOCATION: FAN
•
MATERIAL THICKNESS: 2.700 INCHES NOMINAL IN
TYPICAL APPLICATIONS
  • Server thermal management and cooling
  • Hot-swap fan replacement in production environments
  • Redundant cooling for high-availability systems
TECHNICAL CHARACTERISTICS
STAGE NUMBER1
CRITICALITY CODE JUSTIFICATIONAGAV
REFERENCE DATA AND LITERATURE2J-F118-4, FIG 17, IND 5
BLADE ATTACHMENT METHODDOVETAIL
OVERALL LENGTH12.700 INCHES NOMINAL IN
OVERALL WIDTH6.600 INCHES NOMINAL IN
ENGINE SECTION LOCATIONFAN
MATERIAL THICKNESS2.700 INCHES NOMINAL IN
END ITEM IDENTIFICATIONF118-100 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
1359M81P05Reference document
Same NSN cross-reference
Reference document — Secondary reference
LIFECYCLE
NSN statusActive· U.S. Government catalog
Demilitarization required — mutilation + specific procedure
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FREQUENTLY ASKED QUESTIONS
What is 1359M81P04?
1359M81P04 is a BLADE,FAN,AIRCRAFT GAS TURBINE E.
What parts can replace 1359M81P04?
There is 1 known substitute for 1359M81P04: 1359M81P05. Substitute compatibility should be verified for your specific system.
What is the NSN for 1359M81P04?
1359M81P04 is cataloged in the U.S. Government catalog under NSN 2840-01-474-2341. 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.