1559M93P03 — DISK,FAN,AIRCRAFT GAS TURBINE EN

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

1559M93P03: 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: NICKEL ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 3.687 INCHES MINIMUM AND 4.807 INCHES MAXIMUM IN, end_item_identification: F110-GE-129 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: FAN. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-442-3557, 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

1559M93P03

NSN: 2840-01-442-3557
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	NICKEL ALLOY OVERALL
design_type	AXIAL COMPRESSOR
stage_number	3
overall_length	3.687 INCHES MINIMUM AND 4.807 INCHES MAXIMUM IN
end_item_identification	F110-GE-129 AIRCRAFT GAS TURBINE ENGINE
engine_section_location	FAN
NSN	2840-01-442-3557

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: NICKEL 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	CID A197875INTRODUCES LPTR DISKS W/MODIFIED CUSP AND MISMATCH DEFINITIONS FOR THE DOVETAIL SLOT; NEW DOVETAIL SLOTS IMPROVE AND CLARIFY VARIATION ALLOWANCE DEFINITION OF ALLOWABLE SURFACE CONDITIONS; THESE DISK IMPROVEMENTS ALLOW MISMATCH SIZE AND LOCATION THATIMPROVE CONTROL OF THE SLOT FEATURE LIVES; REWORKED FROM P/N 1559M93P02
END ITEM IDENTIFICATION	F110-GE-129 AIRCRAFT GAS TURBINE ENGINE
MATERIAL	NICKEL 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.

2840-00-004-4242 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

No substitute or cross-reference records for this part.

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Terminal item — no further procurement; issued until stock is exhaustedDemilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 1559M93P03?

1559M93P03 is a DISK,FAN,AIRCRAFT GAS TURBINE EN.

What is the NSN for 1559M93P03?

1559M93P03 is cataloged in the U.S. Government catalog under NSN 2840-01-442-3557. This indicates validated use in U.S. government and defense supply chains.

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1559M93P03 — DISK,FAN,AIRCRAFT GAS TURBINE EN

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