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1364M25P01 — SUPPORT,TURBINE COMPONENT,AIRCRA

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

1364M25P01: SUPPORT,TURBINE COMPONENT,AIRCRA.

SUPPORT,TURBINE COMPONENT,AIRCRA. Key specifications include material: NICKEL ALLOY, overall_length: 2.150 INCHES MINIMUM AND 2.190 INCHES MAXIMUM IN, inside_diameter: 15.580 INCHES MINIMUM AND 15.620 INCHES MAXIMUM IN, outside_diameter: 19.140 INCHES MINIMUM AND 19.200 INCHES MAXIMUM IN, mounting_hole_diameter: 0.210 INCHES MINIMUM AND 0.218 INCHES MAXIMUM IN, mounting_hole_quantity: 19. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-368-6236, 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
1364M25P01
NSN: 2840-01-368-6236
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)
SPECIFICATIONS
materialNICKEL ALLOY
overall_length2.150 INCHES MINIMUM AND 2.190 INCHES MAXIMUM IN
inside_diameter15.580 INCHES MINIMUM AND 15.620 INCHES MAXIMUM IN
outside_diameter19.140 INCHES MINIMUM AND 19.200 INCHES MAXIMUM IN
mounting_hole_diameter0.210 INCHES MINIMUM AND 0.218 INCHES MAXIMUM IN
mounting_hole_quantity19
end_item_identificationF110-GE-129 AIRCRAFT ENGINE
criticality_code_justificationAGAV
NSN2840-01-368-6236
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available SUPPORT,TURBINE COMPONENT,AIRCRA TITLE COMPONENT PN 1364M25P01 MFR SUPPORT,TURBINE COMPON
KEY FEATURES
•
MOUNTING HOLE QUANTITY: 19
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
MOUNTING HOLE DIAMETER: 0.210 INCHES MINIMUM AND 0.218 INCHES MAXIMUM IN
•
OUTSIDE DIAMETER: 19.140 INCHES MINIMUM AND 19.200 INCHES MAXIMUM IN
•
INSIDE DIAMETER: 15.580 INCHES MINIMUM AND 15.620 INCHES MAXIMUM IN
•
MATERIAL: NICKEL ALLOY
TECHNICAL CHARACTERISTICS
MOUNTING HOLE QUANTITY19
CRITICALITY CODE JUSTIFICATIONAGAV
MOUNTING HOLE DIAMETER0.210 INCHES MINIMUM AND 0.218 INCHES MAXIMUM IN
OVERALL LENGTH2.150 INCHES MINIMUM AND 2.190 INCHES MAXIMUM IN
OUTSIDE DIAMETER19.140 INCHES MINIMUM AND 19.200 INCHES MAXIMUM IN
INSIDE DIAMETER15.580 INCHES MINIMUM AND 15.620 INCHES MAXIMUM IN
END ITEM IDENTIFICATIONF110-GE-129 AIRCRAFT ENGINE
MATERIALNICKEL ALLOY
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

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 — mutilation
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FREQUENTLY ASKED QUESTIONS
What is 1364M25P01?
1364M25P01 is a SUPPORT,TURBINE COMPONENT,AIRCRA.
What is the NSN for 1364M25P01?
1364M25P01 is cataloged in the U.S. Government catalog under NSN 2840-01-368-6236. 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.