1441M68G09 — SUPPORT,TURBINE NOZZLE,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

1441M68G09: SUPPORT,TURBINE NOZZLE,AIRCRAFT.

SUPPORT,TURBINE NOZZLE,AIRCRAFT. Key specifications include material: STEEL, overall_length: 7.464 INCHES NOMINAL IN, inside_diameter: 13.648 INCHES MINIMUM AND 13.652 INCHES MAXIMUM IN, outside_diameter: 22.590 INCHES MINIMUM AND 22.610 INCHES MAXIMUM IN, mounting_hole_diameter: 0.419 INCHES MINIMUM AND 0.430 INCHES MAXIMUM IN, mounting_hole_quantity: 62. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-308-7038, 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

1441M68G09

NSN: 2840-01-308-7038
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

material	STEEL
overall_length	7.464 INCHES NOMINAL IN
inside_diameter	13.648 INCHES MINIMUM AND 13.652 INCHES MAXIMUM IN
outside_diameter	22.590 INCHES MINIMUM AND 22.610 INCHES MAXIMUM IN
mounting_hole_diameter	0.419 INCHES MINIMUM AND 0.430 INCHES MAXIMUM IN
mounting_hole_quantity	62
end_item_identification	ACFT ENG F110GE129
criticality_code_justification	AGAV
NSN	2840-01-308-7038

COMPONENT DIAGRAM

KEY FEATURES

•

MOUNTING HOLE QUANTITY: 62

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

MOUNTING HOLE DIAMETER: 0.419 INCHES MINIMUM AND 0.430 INCHES MAXIMUM IN

•

OUTSIDE DIAMETER: 22.590 INCHES MINIMUM AND 22.610 INCHES MAXIMUM IN

•

INSIDE DIAMETER: 13.648 INCHES MINIMUM AND 13.652 INCHES MAXIMUM IN

•

MATERIAL: STEEL

TECHNICAL CHARACTERISTICS

MOUNTING HOLE QUANTITY	62
CRITICALITY CODE JUSTIFICATION	AGAV
MOUNTING HOLE DIAMETER	0.419 INCHES MINIMUM AND 0.430 INCHES MAXIMUM IN
OVERALL LENGTH	7.464 INCHES NOMINAL IN
OUTSIDE DIAMETER	22.590 INCHES MINIMUM AND 22.610 INCHES MAXIMUM IN
INSIDE DIAMETER	13.648 INCHES MINIMUM AND 13.652 INCHES MAXIMUM IN
END ITEM IDENTIFICATION	ACFT ENG F110GE129
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.

2840-00-000-0048 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 4

1441M68G13RReference document

Same NSN cross-reference

Reference document — Secondary reference

1441M68G11Reference document

Same NSN cross-reference

Reference document — Secondary reference

KDS 2840-4003Reference document

Same NSN cross-reference

Reference document — Secondary reference

1441M68G12Reference document

Same NSN cross-reference

Reference document — Secondary reference

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Terminal item — no further procurement; issued until stock is exhaustedDemilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 1441M68G09?

1441M68G09 is a SUPPORT,TURBINE NOZZLE,AIRCRAFT.

What parts can replace 1441M68G09?

There are 4 known substitutes for 1441M68G09: 1441M68G13R, 1441M68G11, KDS 2840-4003 and 1 more. Substitute compatibility should be verified for your specific system.

What is the NSN for 1441M68G09?

1441M68G09 is cataloged in the U.S. Government catalog under NSN 2840-01-308-7038. This indicates validated use in U.S. government and defense supply chains.

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1441M68G09 — SUPPORT,TURBINE NOZZLE,AIRCRAFT

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