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9547M14G08 — ROTOR,COMPRESSOR,AIRCRAFT GAS TU

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

9547M14G08: ROTOR,COMPRESSOR,AIRCRAFT GAS TU.

ROTOR,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include design_type: AXIAL COMPRESSOR, overall_length: 25.577 INCHES MINIMUM AND 25.597 INCHES MAXIMUM IN, end_item_identification: F110-129 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: COMPRESSOR, criticality_code_justification: FEAT AND CZBJ AND ABHP, part_name_assigned_by_controlling_agency: ORIGINAL NAME ROTOR ASSEMBLY,COMPRESSOR. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-447-2505, 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
9547M14G08
NSN: 2840-01-447-2505
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)
SPECIFICATIONS
design_typeAXIAL COMPRESSOR
overall_length25.577 INCHES MINIMUM AND 25.597 INCHES MAXIMUM IN
end_item_identificationF110-129 AIRCRAFT GAS TURBINE ENGINE
engine_section_locationCOMPRESSOR
criticality_code_justificationFEAT AND CZBJ AND ABHP
part_name_assigned_by_controlling_agencyORIGINAL NAME ROTOR ASSEMBLY,COMPRESSOR
NSN2840-01-447-2505
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available ROTOR,COMPRESSOR,AIRCRAFT GAS TU TITLE COMPONENT PN 9547M14G08 MFR ROTOR,COMPRESSOR,AIRCR
KEY FEATURES
•
DESIGN TYPE: AXIAL COMPRESSOR
•
CRITICALITY CODE JUSTIFICATION: FEAT AND CZBJ AND ABHP
•
ENGINE SECTION LOCATION: COMPRESSOR
TECHNICAL CHARACTERISTICS
DESIGN TYPEAXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATIONFEAT AND CZBJ AND ABHP
OVERALL LENGTH25.577 INCHES MINIMUM AND 25.597 INCHES MAXIMUM IN
ENGINE SECTION LOCATIONCOMPRESSOR
SPECIAL FEATURESINCLUDES STAGES 1-9; HPCR STG 1-2 HAS IMPROVED SPOOL OIL DRAIN HOLES (2) THAT ARE 1.48 TIME LARGER THAN THE CURRENT ELLIPTICAL HOLE; REPLACES P/N 9547M14G03 AND 9547M14G06; CHANGE OF HOLE IS A PHYSICAL CHANGE BUT NOT FUNCTIONALLY INTERCHANGEABLE
PART NAME ASSIGNED BY CONTROLLING AGENCYORIGINAL NAME ROTOR ASSEMBLY,COMPRESSOR
END ITEM IDENTIFICATIONF110-129 AIRCRAFT GAS TURBINE ENGINE
SUBSTITUTES & CROSS-REFERENCES 1
9547M14Reference 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 — critical (Q)
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FREQUENTLY ASKED QUESTIONS
What is 9547M14G08?
9547M14G08 is a ROTOR,COMPRESSOR,AIRCRAFT GAS TU.
What parts can replace 9547M14G08?
There is 1 known substitute for 9547M14G08: 9547M14. Substitute compatibility should be verified for your specific system.
What is the NSN for 9547M14G08?
9547M14G08 is cataloged in the U.S. Government catalog under NSN 2840-01-447-2505. This indicates validated use in U.S. government and defense supply chains.
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✓ 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.