1441M31P06 — LOCK,TURBINE ROTOR BLADE,AIRCRAF

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

1441M31P06: LOCK,TURBINE ROTOR BLADE,AIRCRAF.

LOCK,TURBINE ROTOR BLADE,AIRCRAF. Key specifications include material: TITANIUM, overall_width: 0.658 INCHES NOMINAL IN, overall_length: 0.666 INCHES MINIMUM AND 0.676 INCHES MAXIMUM IN, special_features: USED ON THE REAR HIGH PRESSURE TURBINE, material_thickness: 0.074 INCHES MINIMUM AND 0.083 INCHES MAXIMUM IN, end_item_identification: F110GE129 ACFT ENGINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-307-6361, 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

1441M31P06

NSN: 2840-01-307-6361
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

material	TITANIUM
overall_width	0.658 INCHES NOMINAL IN
overall_length	0.666 INCHES MINIMUM AND 0.676 INCHES MAXIMUM IN
special_features	USED ON THE REAR HIGH PRESSURE TURBINE
material_thickness	0.074 INCHES MINIMUM AND 0.083 INCHES MAXIMUM IN
end_item_identification	F110GE129 ACFT ENGINE
material_document_and_classification	C50TF70,CL-A MFR REF SINGLE MATERIAL RESPONSE
NSN	2840-01-307-6361

COMPONENT DIAGRAM

KEY FEATURES

•

MATERIAL DOCUMENT AND CLASSIFICATION: C50TF70,CL-A MFR REF SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.074 INCHES MINIMUM AND 0.083 INCHES MAXIMUM IN

•

MATERIAL: TITANIUM

TECHNICAL CHARACTERISTICS

MATERIAL DOCUMENT AND CLASSIFICATION	C50TF70,CL-A MFR REF SINGLE MATERIAL RESPONSE
OVERALL LENGTH	0.666 INCHES MINIMUM AND 0.676 INCHES MAXIMUM IN
OVERALL WIDTH	0.658 INCHES NOMINAL IN
MATERIAL THICKNESS	0.074 INCHES MINIMUM AND 0.083 INCHES MAXIMUM IN
SPECIAL FEATURES	USED ON THE REAR HIGH PRESSURE TURBINE
END ITEM IDENTIFICATION	F110GE129 ACFT ENGINE
MATERIAL	TITANIUM

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 1

KDS 2840-4003Reference document

Same NSN cross-reference

Reference document — Secondary reference

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Normally procured from the manufacturer (OEM)Demilitarization required — mutilation

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FREQUENTLY ASKED QUESTIONS

What is 1441M31P06?

1441M31P06 is a LOCK,TURBINE ROTOR BLADE,AIRCRAF.

What parts can replace 1441M31P06?

There is 1 known substitute for 1441M31P06: KDS 2840-4003. Substitute compatibility should be verified for your specific system.

What is the NSN for 1441M31P06?

1441M31P06 is cataloged in the U.S. Government catalog under NSN 2840-01-307-6361. This indicates validated use in U.S. government and defense supply chains.

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1441M31P06 — LOCK,TURBINE ROTOR BLADE,AIRCRAF

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