1441M54P02 — BLADE,TURBINE ROTOR,AIRCRAFT GAS

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

1441M54P02: BLADE,TURBINE ROTOR,AIRCRAFT GAS.

BLADE,TURBINE ROTOR,AIRCRAFT GAS. Key specifications include material: STEEL BLADE, design_type: AXIAL COMPRESSOR, overall_width: 1.556 INCHES NOMINAL IN, overall_length: 2.825 INCHES NOMINAL IN, special_features: BLADE ATTACHMENT IS DOVETAIL, end_item_identification: ACFT ENG F110. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-192-0857, 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

1441M54P02

NSN: 2840-01-192-0857
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

material	STEEL BLADE
design_type	AXIAL COMPRESSOR
overall_width	1.556 INCHES NOMINAL IN
overall_length	2.825 INCHES NOMINAL IN
special_features	BLADE ATTACHMENT IS DOVETAIL
end_item_identification	ACFT ENG F110
engine_section_location	HIGH PRESSURE TURBINE
criticality_code_justification	APGF AND CZBJ AND ABHP AND ABMK
NSN	2840-01-192-0857

COMPONENT DIAGRAM

KEY FEATURES

•

DESIGN TYPE: AXIAL COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: APGF AND CZBJ AND ABHP AND ABMK

•

ENGINE SECTION LOCATION: HIGH PRESSURE TURBINE

•

MATERIAL: STEEL BLADE

TECHNICAL CHARACTERISTICS

DESIGN TYPE	AXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATION	APGF AND CZBJ AND ABHP AND ABMK
OVERALL LENGTH	2.825 INCHES NOMINAL IN
OVERALL WIDTH	1.556 INCHES NOMINAL IN
ENGINE SECTION LOCATION	HIGH PRESSURE TURBINE
SPECIAL FEATURES	BLADE ATTACHMENT IS DOVETAIL
END ITEM IDENTIFICATION	ACFT ENG F110
MATERIAL	STEEL BLADE

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 2

9530M95P10Reference document

Same NSN cross-reference

Reference document — Secondary reference

9530M95P14Reference document

Same NSN cross-reference

Reference document — Secondary reference

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 1441M54P02?

1441M54P02 is a BLADE,TURBINE ROTOR,AIRCRAFT GAS.

What parts can replace 1441M54P02?

There are 2 known substitutes for 1441M54P02: 9530M95P10, 9530M95P14. Substitute compatibility should be verified for your specific system.

What is the NSN for 1441M54P02?

1441M54P02 is cataloged in the U.S. Government catalog under NSN 2840-01-192-0857. This indicates validated use in U.S. government and defense supply chains.

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1441M54P02 — BLADE,TURBINE ROTOR,AIRCRAFT GAS

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