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9524M58P01 — HUB,TURBINE,AIRCRAFT GAS TURBINE

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

9524M58P01: HUB,TURBINE,AIRCRAFT GAS TURBINE.

HUB,TURBINE,AIRCRAFT GAS TURBINE. Key specifications include diameter: 13.430 INCHES MINIMUM AND 13.441 INCHES MAXIMUM IN, design_type: AXIAL COMPRESSOR, end_item_identification: ACFT ENG F101-GE-100 AND F110-GE-100, engine_section_location: TURBINE, reference_data_and_literature: T.O. 2J-F101-4, FIG 56, IND 22, part_name_assigned_by_controlling_agency: ORIGINAL NAME SHAFT,TURBINE,AIRCRAFT GAS TURBINE ENGINE.

This part is cataloged in the U.S. Government catalog under NSN 2840-01-146-9475, 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
9524M58P01
NSN: 2840-01-146-9475
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)
SPECIFICATIONS
diameter13.430 INCHES MINIMUM AND 13.441 INCHES MAXIMUM IN
design_typeAXIAL COMPRESSOR
end_item_identificationACFT ENG F101-GE-100 AND F110-GE-100
engine_section_locationTURBINE
reference_data_and_literatureT.O. 2J-F101-4, FIG 56, IND 22
part_name_assigned_by_controlling_agencyORIGINAL NAME SHAFT,TURBINE,AIRCRAFT GAS TURBINE ENGINE
NSN2840-01-146-9475
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available HUB,TURBINE,AIRCRAFT GAS TURBINE TITLE COMPONENT PN 9524M58P01 MFR HUB,TURBINE,AIRCRAFT G
KEY FEATURES
•
DESIGN TYPE: AXIAL COMPRESSOR
•
REFERENCE DATA AND LITERATURE: T.O. 2J-F101-4, FIG 56, IND 22
•
DIAMETER: 13.430 INCHES MINIMUM AND 13.441 INCHES MAXIMUM IN
•
ENGINE SECTION LOCATION: TURBINE
TECHNICAL CHARACTERISTICS
DESIGN TYPEAXIAL COMPRESSOR
REFERENCE DATA AND LITERATURET.O. 2J-F101-4, FIG 56, IND 22
DIAMETER13.430 INCHES MINIMUM AND 13.441 INCHES MAXIMUM IN
ENGINE SECTION LOCATIONTURBINE
PART NAME ASSIGNED BY CONTROLLING AGENCYORIGINAL NAME SHAFT,TURBINE,AIRCRAFT GAS TURBINE ENGINE
END ITEM IDENTIFICATIONACFT ENG F101-GE-100 AND F110-GE-100
SUBSTITUTES & CROSS-REFERENCES 1
9524M58Reference document
Same NSN cross-reference
Reference document — Drawing number reference only
LIFECYCLE
NSN statusActive· U.S. Government catalog
Acquisition advice: Terminal item — no further procurement; issued until stock is exhaustedDemilitarization required — mutilation + specific procedure
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FREQUENTLY ASKED QUESTIONS
What is 9524M58P01?
9524M58P01 is a HUB,TURBINE,AIRCRAFT GAS TURBINE.
What parts can replace 9524M58P01?
There is 1 known substitute for 9524M58P01: 9524M58. Substitute compatibility should be verified for your specific system.
What is the NSN for 9524M58P01?
9524M58P01 is cataloged in the U.S. Government catalog under NSN 2840-01-146-9475. This indicates validated use in U.S. government and defense supply chains.
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