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9526M12G01 — SUPPORT,TURBINE NOZZLE,AIRCRAFT

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

9526M12G01: SUPPORT,TURBINE NOZZLE,AIRCRAFT.

SUPPORT,TURBINE NOZZLE,AIRCRAFT. Key specifications include material: STEEL, overall_length: 2.174 INCHES MINIMUM AND 2.178 INCHES MAXIMUM IN, inside_diameter: 28.940 INCHES MINIMUM AND 28.944 INCHES MAXIMUM IN, outside_diameter: 32.212 INCHES MINIMUM AND 32.216 INCHES MAXIMUM IN, mounting_hole_diameter: 0.309 INCHES MINIMUM AND 0.318 INCHES MAXIMUM IN, mounting_hole_quantity: 79. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-171-2482, 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
9526M12G01
NSN: 2840-01-171-2482
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)
SPECIFICATIONS
materialSTEEL
overall_length2.174 INCHES MINIMUM AND 2.178 INCHES MAXIMUM IN
inside_diameter28.940 INCHES MINIMUM AND 28.944 INCHES MAXIMUM IN
outside_diameter32.212 INCHES MINIMUM AND 32.216 INCHES MAXIMUM IN
mounting_hole_diameter0.309 INCHES MINIMUM AND 0.318 INCHES MAXIMUM IN
mounting_hole_quantity79
end_item_identificationACFT ENG F110
criticality_code_justificationAGAV
NSN2840-01-171-2482
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available SUPPORT,TURBINE NOZZLE,AIRCRAFT TITLE COMPONENT PN 9526M12G01 MFR SUPPORT,TURBINE NOZZLE
KEY FEATURES
•
MOUNTING HOLE QUANTITY: 79
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
MOUNTING HOLE DIAMETER: 0.309 INCHES MINIMUM AND 0.318 INCHES MAXIMUM IN
•
OUTSIDE DIAMETER: 32.212 INCHES MINIMUM AND 32.216 INCHES MAXIMUM IN
•
INSIDE DIAMETER: 28.940 INCHES MINIMUM AND 28.944 INCHES MAXIMUM IN
•
MATERIAL: STEEL
TECHNICAL CHARACTERISTICS
MOUNTING HOLE QUANTITY79
CRITICALITY CODE JUSTIFICATIONAGAV
MOUNTING HOLE DIAMETER0.309 INCHES MINIMUM AND 0.318 INCHES MAXIMUM IN
OVERALL LENGTH2.174 INCHES MINIMUM AND 2.178 INCHES MAXIMUM IN
OUTSIDE DIAMETER32.212 INCHES MINIMUM AND 32.216 INCHES MAXIMUM IN
INSIDE DIAMETER28.940 INCHES MINIMUM AND 28.944 INCHES MAXIMUM IN
END ITEM IDENTIFICATIONACFT ENG F110
MATERIALSTEEL
SUBSTITUTES & CROSS-REFERENCES 1
9526M12Reference document
Same NSN cross-reference
Reference document — Drawing number reference only
LIFECYCLE
NSN statusActive· U.S. Government catalog
Demilitarization required — critical (Q)
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FREQUENTLY ASKED QUESTIONS
What is 9526M12G01?
9526M12G01 is a SUPPORT,TURBINE NOZZLE,AIRCRAFT.
What parts can replace 9526M12G01?
There is 1 known substitute for 9526M12G01: 9526M12. Substitute compatibility should be verified for your specific system.
What is the NSN for 9526M12G01?
9526M12G01 is cataloged in the U.S. Government catalog under NSN 2840-01-171-2482. 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.