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9526M12G02 — SUPPORT,TURBINE NOZZLE,AIRCRAFT

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

9526M12G02: SUPPORT,TURBINE NOZZLE,AIRCRAFT.

SUPPORT,TURBINE NOZZLE,AIRCRAFT. Key specifications include material: NICKEL ALLOY, overall_length: 2.282 INCHES NOMINAL IN, inside_diameter: 28.940 INCHES MINIMUM AND 28.948 INCHES MAXIMUM IN, outside_diameter: 30.565 INCHES NOMINAL IN, mounting_hole_diameter: 0.309 INCHES MINIMUM AND 0.318 INCHES MAXIMUM IN, mounting_hole_quantity: 80. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-313-3364, 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
9526M12G02
NSN: 2840-01-313-3364
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)
SPECIFICATIONS
materialNICKEL ALLOY
overall_length2.282 INCHES NOMINAL IN
inside_diameter28.940 INCHES MINIMUM AND 28.948 INCHES MAXIMUM IN
outside_diameter30.565 INCHES NOMINAL IN
mounting_hole_diameter0.309 INCHES MINIMUM AND 0.318 INCHES MAXIMUM IN
mounting_hole_quantity80
end_item_identificationF110GE 100 ENGINE
criticality_code_justificationAGAV
NSN2840-01-313-3364
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available SUPPORT,TURBINE NOZZLE,AIRCRAFT TITLE COMPONENT PN 9526M12G02 MFR SUPPORT,TURBINE NOZZLE
KEY FEATURES
•
MOUNTING HOLE QUANTITY: 80
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
MOUNTING HOLE DIAMETER: 0.309 INCHES MINIMUM AND 0.318 INCHES MAXIMUM IN
•
OUTSIDE DIAMETER: 30.565 INCHES NOMINAL IN
•
INSIDE DIAMETER: 28.940 INCHES MINIMUM AND 28.948 INCHES MAXIMUM IN
•
MATERIAL: NICKEL ALLOY
TECHNICAL CHARACTERISTICS
MOUNTING HOLE QUANTITY80
CRITICALITY CODE JUSTIFICATIONAGAV
MOUNTING HOLE DIAMETER0.309 INCHES MINIMUM AND 0.318 INCHES MAXIMUM IN
OVERALL LENGTH2.282 INCHES NOMINAL IN
OUTSIDE DIAMETER30.565 INCHES NOMINAL IN
INSIDE DIAMETER28.940 INCHES MINIMUM AND 28.948 INCHES MAXIMUM IN
END ITEM IDENTIFICATIONF110GE 100 ENGINE
MATERIALNICKEL ALLOY
SUBSTITUTES & CROSS-REFERENCES 2
1386M15Reference document
Same NSN cross-reference
Reference document — Drawing number reference only
9526M12Reference document
Same NSN cross-reference
Reference document — Drawing number reference only
LIFECYCLE
NSN statusActive· U.S. Government catalog
Acquisition advice: Terminal item — no further procurement; issued until stock is exhaustedDemilitarization required — critical (Q)
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FREQUENTLY ASKED QUESTIONS
What is 9526M12G02?
9526M12G02 is a SUPPORT,TURBINE NOZZLE,AIRCRAFT.
What parts can replace 9526M12G02?
There are 2 known substitutes for 9526M12G02: 1386M15, 9526M12. Substitute compatibility should be verified for your specific system.
What is the NSN for 9526M12G02?
9526M12G02 is cataloged in the U.S. Government catalog under NSN 2840-01-313-3364. 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.