9530M95P13 — BLADE,TURBINE ROTOR,AIRCRAFT GAS

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9530M95P13: BLADE,TURBINE ROTOR,AIRCRAFT GAS.

BLADE,TURBINE ROTOR,AIRCRAFT GAS. Key specifications include diameter: 28.604 INCHES MINIMUM AND 28.644 INCHES MAXIMUM IN, design_type: AXIAL COMPRESSOR, overall_length: 2.767 INCHES MINIMUM AND 2.777 INCHES MAXIMUM IN, special_features: BLADE ATTACHMENT METHOD IS DOVETAIL, end_item_identification: ACFT ENG F110, engine_section_location: HIGH PRESSURE TURBINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-192-0856, 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

9530M95P13

NSN: 2840-01-192-0856
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

diameter	28.604 INCHES MINIMUM AND 28.644 INCHES MAXIMUM IN
design_type	AXIAL COMPRESSOR
overall_length	2.767 INCHES MINIMUM AND 2.777 INCHES MAXIMUM IN
special_features	BLADE ATTACHMENT METHOD IS DOVETAIL
end_item_identification	ACFT ENG F110
engine_section_location	HIGH PRESSURE TURBINE
criticality_code_justification	APGF AND CZBJ AND ABHP AND ABMZ
NSN	2840-01-192-0856

COMPONENT DIAGRAM

KEY FEATURES

•

DESIGN TYPE: AXIAL COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: APGF AND CZBJ AND ABHP AND ABMZ

•

DIAMETER: 28.604 INCHES MINIMUM AND 28.644 INCHES MAXIMUM IN

•

ENGINE SECTION LOCATION: HIGH PRESSURE TURBINE

TECHNICAL CHARACTERISTICS

DESIGN TYPE	AXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATION	APGF AND CZBJ AND ABHP AND ABMZ
DIAMETER	28.604 INCHES MINIMUM AND 28.644 INCHES MAXIMUM IN
OVERALL LENGTH	2.767 INCHES MINIMUM AND 2.777 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	HIGH PRESSURE TURBINE
SPECIAL FEATURES	BLADE ATTACHMENT METHOD IS DOVETAIL
END ITEM IDENTIFICATION	ACFT ENG F110

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 1

9530M95P09Reference document

Same NSN cross-reference

Reference document — Secondary reference

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 9530M95P13?

9530M95P13 is a BLADE,TURBINE ROTOR,AIRCRAFT GAS.

What parts can replace 9530M95P13?

There is 1 known substitute for 9530M95P13: 9530M95P09. Substitute compatibility should be verified for your specific system.

What is the NSN for 9530M95P13?

9530M95P13 is cataloged in the U.S. Government catalog under NSN 2840-01-192-0856. This indicates validated use in U.S. government and defense supply chains.

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9530M95P13 — BLADE,TURBINE ROTOR,AIRCRAFT GAS

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