9526M80G01 — SUPPORT,TURBINE NOZZLE,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9526M80G01: SUPPORT,TURBINE NOZZLE,AIRCRAFT.

SUPPORT,TURBINE NOZZLE,AIRCRAFT. Key specifications include material: STEEL, overall_length: 1.897 INCHES NOMINAL IN, inside_diameter: 29.936 INCHES MINIMUM AND 29.940 INCHES MAXIMUM IN, outside_diameter: 33.320 INCHES MINIMUM AND 33.330 INCHES MAXIMUM IN, mounting_hole_diameter: 0.3118 INCHES MINIMUM AND 0.3123 INCHES MAXIMUM IN, end_item_identification: ACFT ENG F101. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-146-9371, 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

9526M80G01

NSN: 2840-01-146-9371
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 1U666 — DOVER TOOL OF CONNECTICUT, LLC DIV NA (USA)

SPECIFICATIONS

material	STEEL
overall_length	1.897 INCHES NOMINAL IN
inside_diameter	29.936 INCHES MINIMUM AND 29.940 INCHES MAXIMUM IN
outside_diameter	33.320 INCHES MINIMUM AND 33.330 INCHES MAXIMUM IN
mounting_hole_diameter	0.3118 INCHES MINIMUM AND 0.3123 INCHES MAXIMUM IN
mounting_hole_quantity	8
end_item_identification	ACFT ENG F101
criticality_code_justification	AGAV
NSN	2840-01-146-9371

COMPONENT DIAGRAM

KEY FEATURES

•

MOUNTING HOLE QUANTITY: 8

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

MOUNTING HOLE DIAMETER: 0.3118 INCHES MINIMUM AND 0.3123 INCHES MAXIMUM IN

•

OUTSIDE DIAMETER: 33.320 INCHES MINIMUM AND 33.330 INCHES MAXIMUM IN

•

INSIDE DIAMETER: 29.936 INCHES MINIMUM AND 29.940 INCHES MAXIMUM IN

•

MATERIAL: STEEL

TECHNICAL CHARACTERISTICS

MOUNTING HOLE QUANTITY	8
CRITICALITY CODE JUSTIFICATION	AGAV
MOUNTING HOLE DIAMETER	0.3118 INCHES MINIMUM AND 0.3123 INCHES MAXIMUM IN
OVERALL LENGTH	1.897 INCHES NOMINAL IN
OUTSIDE DIAMETER	33.320 INCHES MINIMUM AND 33.330 INCHES MAXIMUM IN
INSIDE DIAMETER	29.936 INCHES MINIMUM AND 29.940 INCHES MAXIMUM IN
END ITEM IDENTIFICATION	ACFT ENG F101
MATERIAL	STEEL

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 1

9526M80G02Reference document

Same NSN cross-reference

Reference document — Secondary reference

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Insurance item — stocked against contingency demandDemilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 9526M80G01?

9526M80G01 is a SUPPORT,TURBINE NOZZLE,AIRCRAFT.

What parts can replace 9526M80G01?

There is 1 known substitute for 9526M80G01: 9526M80G02. Substitute compatibility should be verified for your specific system.

What is the NSN for 9526M80G01?

9526M80G01 is cataloged in the U.S. Government catalog under NSN 2840-01-146-9371. This indicates validated use in U.S. government and defense supply chains.

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9526M80G01 — SUPPORT,TURBINE NOZZLE,AIRCRAFT

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