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1317M81G01 — SHROUD,FAN,AIRCRAFT GAS TURBINE

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

1317M81G01: SHROUD,FAN,AIRCRAFT GAS TURBINE.

SHROUD,FAN,AIRCRAFT GAS TURBINE. Key specifications include diameter: 11.267 INCHES NOMINAL IN, material: ALUMINUM ALLOY OUTER CASE, overall_length: 2.405 INCHES MINIMUM AND 2.415 INCHES MAXIMUM IN, end_item_identification: F110-GE-129 TURBO-FAN ENGINE, engine_section_location: TURBINE, criticality_code_justification: AGAV. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-199-7453, 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
1317M81G01
NSN: 2840-01-199-7453
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)
SPECIFICATIONS
diameter11.267 INCHES NOMINAL IN
materialALUMINUM ALLOY OUTER CASE
overall_length2.405 INCHES MINIMUM AND 2.415 INCHES MAXIMUM IN
end_item_identificationF110-GE-129 TURBO-FAN ENGINE
engine_section_locationTURBINE
criticality_code_justificationAGAV
material_document_and_classificationAMS4132 ASSN STD SINGLE MATERIAL RESPONSE OUTER CASE
NSN2840-01-199-7453
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available SHROUD,FAN,AIRCRAFT GAS TURBINE TITLE COMPONENT PN 1317M81G01 MFR SHROUD,FAN,AIRCRAFT GA
KEY FEATURES
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
MATERIAL DOCUMENT AND CLASSIFICATION: AMS4132 ASSN STD SINGLE MATERIAL RESPONSE OUTER CASE
•
DIAMETER: 11.267 INCHES NOMINAL IN
•
ENGINE SECTION LOCATION: TURBINE
•
MATERIAL: ALUMINUM ALLOY OUTER CASE
TYPICAL APPLICATIONS
  • Server thermal management and cooling
  • Hot-swap fan replacement in production environments
  • Redundant cooling for high-availability systems
TECHNICAL CHARACTERISTICS
CRITICALITY CODE JUSTIFICATIONAGAV
MATERIAL DOCUMENT AND CLASSIFICATIONAMS4132 ASSN STD SINGLE MATERIAL RESPONSE OUTER CASE
DIAMETER11.267 INCHES NOMINAL IN
OVERALL LENGTH2.405 INCHES MINIMUM AND 2.415 INCHES MAXIMUM IN
ENGINE SECTION LOCATIONTURBINE
END ITEM IDENTIFICATIONF110-GE-129 TURBO-FAN ENGINE
MATERIALALUMINUM ALLOY OUTER CASE
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
Acquisition advice: Insurance item — stocked against contingency demandDemilitarization required — critical (Q)
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FREQUENTLY ASKED QUESTIONS
What is 1317M81G01?
1317M81G01 is a SHROUD,FAN,AIRCRAFT GAS TURBINE.
What is the NSN for 1317M81G01?
1317M81G01 is cataloged in the U.S. Government catalog under NSN 2840-01-199-7453. 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.