PartsTable
Technical Data Sheet
Download PDF

1559M63G04 — DISK AND HUB,COMPRESSOR,AIRCRAFT

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

1559M63G04: DISK AND HUB,COMPRESSOR,AIRCRAFT.

DISK AND HUB,COMPRESSOR,AIRCRAFT. Key specifications include diameter: 17.225 INCHES MINIMUM AND 17.229 INCHES MAXIMUM IN, material: TITANIUM ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 6.425 INCHES MINIMUM AND 6.455 INCHES MAXIMUM IN, end_item_identification: F110-GE-129 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-447-2868, 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
1559M63G04
NSN: 2840-01-447-2868
NIINs: 014472868, 014610351
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)
SPECIFICATIONS
diameter17.225 INCHES MINIMUM AND 17.229 INCHES MAXIMUM IN
materialTITANIUM ALLOY OVERALL
design_typeAXIAL COMPRESSOR
overall_length6.425 INCHES MINIMUM AND 6.455 INCHES MAXIMUM IN
special_featuresT.O 2J-F110-14, FIG 67, IND 5; REPL P/N 1559M63G02; HPCR STG 1-2 SPOOL OIL DRAIN HOLES ARE ENLARGED 1.48 LARGER THAN THE CURRENT ELLIPTICAL HOLES TO ALLOW BETTER DRAINAGE
end_item_identificationF110-GE-129 AIRCRAFT GAS TURBINE ENGINE
engine_section_locationCOMPRESSOR
criticality_code_justificationABHP AND ABMZ AND FEAT
part_name_assigned_by_controlling_agencyORIGINAL NAME SPOOL, COMPRESSOR ROTOR
NSN2840-01-447-2868
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available DISK AND HUB,COMPRESSOR,AIRCRAFT TITLE COMPONENT PN 1559M63G04 MFR DISK AND HUB,COMPRESSO
KEY FEATURES
•
DESIGN TYPE: AXIAL COMPRESSOR
•
CRITICALITY CODE JUSTIFICATION: ABHP AND ABMZ AND FEAT
•
DIAMETER: 17.225 INCHES MINIMUM AND 17.229 INCHES MAXIMUM IN
•
ENGINE SECTION LOCATION: COMPRESSOR
TECHNICAL CHARACTERISTICS
DESIGN TYPEAXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATIONABHP AND ABMZ AND FEAT
DIAMETER17.225 INCHES MINIMUM AND 17.229 INCHES MAXIMUM IN
OVERALL LENGTH6.425 INCHES MINIMUM AND 6.455 INCHES MAXIMUM IN
ENGINE SECTION LOCATIONCOMPRESSOR
SPECIAL FEATUREST.O 2J-F110-14, FIG 67, IND 5; REPL P/N 1559M63G02; HPCR STG 1-2 SPOOL OIL DRAIN HOLES ARE ENLARGED 1.48 LARGER THAN THE CURRENT ELLIPTICAL HOLES TO ALLOW BETTER DRAINAGE
PART NAME ASSIGNED BY CONTROLLING AGENCYORIGINAL NAME SPOOL, COMPRESSOR ROTOR
END ITEM IDENTIFICATIONF110-GE-129 AIRCRAFT GAS TURBINE ENGINE
MATERIALTITANIUM ALLOY OVERALL
SUBSTITUTES & CROSS-REFERENCES

No substitute or cross-reference records for this part.

LIFECYCLE
NSN statusActive· U.S. Government catalog
Demilitarization required — mutilation + specific procedure
Ready to buy 1559M63G04?
Compare prices from verified sellers on eBay
Buy on eBay →
As an eBay Partner, PartsTable may earn a commission. Your price is not affected.
FREQUENTLY ASKED QUESTIONS
What is 1559M63G04?
1559M63G04 is a DISK AND HUB,COMPRESSOR,AIRCRAFT.
What is the NSN for 1559M63G04?
1559M63G04 is cataloged in the U.S. Government catalog under NSN 2840-01-447-2868. This indicates validated use in U.S. government and defense supply chains.
Community Feedback
Leave a Comment
Comments are reviewed before appearing. You will receive an email to verify before your comment appears.

Request a Quote — 1559M63G04

✓ PartsTable — the parts reference. Every fact cited to its source.
PartsTable Design LLC · partstable.com
U.S. Government catalog: edition PUBLOGDVD v12.0.0 (OCT 2026), edition date 2026-10-01, retrieved 2026-10-18.
PartsTable commercial catalog: edition Unified commercial catalog snapshot through 2026-09-28, edition date not on file, retrieved 2026-09-28.