1559M93P05 — DISK,FAN,AIRCRAFT GAS TURBINE EN

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

1559M93P05: DISK,FAN,AIRCRAFT GAS TURBINE EN.

DISK,FAN,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 23.255 INCHES MINIMUM AND 23.263 INCHES MAXIMUM IN, material: TITANIUM ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 3.687 INCHES MINIMUM AND 4.807 INCHES MAXIMUM IN, special_features: MATL IS TI17, end_item_identification: F110-GE-100,F110-GE-100B,F110-GE-129,F118-GE-100. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-484-0453, 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

1559M93P05

NSN: 2840-01-484-0453
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

diameter	23.255 INCHES MINIMUM AND 23.263 INCHES MAXIMUM IN
material	TITANIUM ALLOY OVERALL
design_type	AXIAL COMPRESSOR
stage_number	3
overall_length	3.687 INCHES MINIMUM AND 4.807 INCHES MAXIMUM IN
special_features	MATL IS TI17
end_item_identification	F110-GE-100,F110-GE-100B,F110-GE-129,F118-GE-100
engine_section_location	FAN
NSN	2840-01-484-0453

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 3

•

DESIGN TYPE: AXIAL COMPRESSOR

•

DIAMETER: 23.255 INCHES MINIMUM AND 23.263 INCHES MAXIMUM IN

•

ENGINE SECTION LOCATION: FAN

•

MATERIAL: TITANIUM ALLOY OVERALL

TYPICAL APPLICATIONS

Server thermal management and cooling
Hot-swap fan replacement in production environments
Redundant cooling for high-availability systems

TECHNICAL CHARACTERISTICS

STAGE NUMBER	3
DESIGN TYPE	AXIAL COMPRESSOR
DIAMETER	23.255 INCHES MINIMUM AND 23.263 INCHES MAXIMUM IN
OVERALL LENGTH	3.687 INCHES MINIMUM AND 4.807 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	FAN
SPECIAL FEATURES	MATL IS TI17
END ITEM IDENTIFICATION	F110-GE-100,F110-GE-100B,F110-GE-129,F118-GE-100
MATERIAL	TITANIUM ALLOY OVERALL

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

1559M93P04Reference document

Same NSN cross-reference

Reference document — Secondary reference

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 1559M93P05?

1559M93P05 is a DISK,FAN,AIRCRAFT GAS TURBINE EN.

What parts can replace 1559M93P05?

There is 1 known substitute for 1559M93P05: 1559M93P04. Substitute compatibility should be verified for your specific system.

What is the NSN for 1559M93P05?

1559M93P05 is cataloged in the U.S. Government catalog under NSN 2840-01-484-0453. This indicates validated use in U.S. government and defense supply chains.

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1559M93P05 — DISK,FAN,AIRCRAFT GAS TURBINE EN

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