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1359M24P02-118 — DISK,TURBINE,AIRCRAFT GAS TURBIN

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

1359M24P02-118: DISK,TURBINE,AIRCRAFT GAS TURBIN.

DISK,TURBINE,AIRCRAFT GAS TURBIN. Key specifications include material: STEEL DISK, design_type: AXIAL COMPRESSOR, overall_length: 18.995 INCHES MINIMUM AND 19.005 INCHES MAXIMUM IN, special_features: TRACKING PURPOSES ONLY F118 USED, end_item_identification: ACFT ENG F118GE100, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-449-6573, 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
1359M24P02-118
NSN: 2840-01-449-6573
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)
SPECIFICATIONS
materialSTEEL DISK
design_typeAXIAL COMPRESSOR
overall_length18.995 INCHES MINIMUM AND 19.005 INCHES MAXIMUM IN
special_featuresTRACKING PURPOSES ONLY F118 USED
end_item_identificationACFT ENG F118GE100
engine_section_locationCOMPRESSOR
criticality_code_justificationAGAV
NSN2840-01-449-6573
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available DISK,TURBINE,AIRCRAFT GAS TURBIN TITLE COMPONENT PN 1359M24P02-118 MFR DISK,TURBINE,AIRCRAFT
KEY FEATURES
•
DESIGN TYPE: AXIAL COMPRESSOR
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
ENGINE SECTION LOCATION: COMPRESSOR
•
MATERIAL: STEEL DISK
TECHNICAL CHARACTERISTICS
DESIGN TYPEAXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATIONAGAV
OVERALL LENGTH18.995 INCHES MINIMUM AND 19.005 INCHES MAXIMUM IN
ENGINE SECTION LOCATIONCOMPRESSOR
SPECIAL FEATURESTRACKING PURPOSES ONLY F118 USED
END ITEM IDENTIFICATIONACFT ENG F118GE100
MATERIALSTEEL DISK
SUBSTITUTES & CROSS-REFERENCES 4
1275M14Reference document
Same NSN cross-reference
Reference document — Drawing number reference only
1275M14P02-118Reference document
Same NSN cross-reference
Reference document — Secondary reference
1359M24P01-118Same NSN cross-reference
Same NSN cross-reference
Also cataloged under this NSN
1359M24Reference document
Same NSN cross-reference
Reference document — Drawing number reference only
LIFECYCLE
NSN statusActive· U.S. Government catalog
Demilitarization required — mutilation + specific procedure
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FREQUENTLY ASKED QUESTIONS
What is 1359M24P02-118?
1359M24P02-118 is a DISK,TURBINE,AIRCRAFT GAS TURBIN.
What parts can replace 1359M24P02-118?
There are 4 known substitutes for 1359M24P02-118: 1275M14, 1275M14P02-118, 1359M24P01-118 and 1 more. Substitute compatibility should be verified for your specific system.
What is the NSN for 1359M24P02-118?
1359M24P02-118 is cataloged in the U.S. Government catalog under NSN 2840-01-449-6573. This indicates validated use in U.S. government and defense supply chains.
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