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6841213 — DISK,COMPRESSOR,AIRCRAFT GAS TUR

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

6841213: DISK,COMPRESSOR,AIRCRAFT GAS TUR.

DISK,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include diameter: 9.736 INCHES MINIMUM AND 9.746 INCHES MAXIMUM IN, material: STEEL DISK, design_type: AXIAL COMPRESSOR, overall_length: 2.514 INCHES MINIMUM AND 2.518 INCHES MAXIMUM IN, hardness_rating: 32.0 ROCKWELL C MINIMUM AND 38.0 ROCKWELL C MAXIMUM DISK, special_features: T.O. 2J-T56-14; COMPRESSOR ROTOR ASSEMBLY.

This part is cataloged in the U.S. Government catalog under NSN 2840-00-011-0677, 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
6841213
NSN: 2840-00-011-0677
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 63005 — ROLLS-ROYCE CORPORATION (USA)
SPECIFICATIONS
diameter9.736 INCHES MINIMUM AND 9.746 INCHES MAXIMUM IN
materialSTEEL DISK
design_typeAXIAL COMPRESSOR
stage_number3
overall_length2.514 INCHES MINIMUM AND 2.518 INCHES MAXIMUM IN
hardness_rating32.0 ROCKWELL C MINIMUM AND 38.0 ROCKWELL C MAXIMUM DISK
special_featuresT.O. 2J-T56-14; COMPRESSOR ROTOR ASSEMBLY
end_item_identificationT56 ENG
engine_section_locationCOMPRESSOR
criticality_code_justificationCZCJ
material_document_and_classificationAMS5613 ASSN STD SINGLE MATERIAL RESPONSE DISK
NSN2840-00-011-0677
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available DISK,COMPRESSOR,AIRCRAFT GAS TUR TITLE COMPONENT PN 6841213 MFR DISK,COMPRESSOR,AIRCRA
KEY FEATURES
•
STAGE NUMBER: 3
•
DESIGN TYPE: AXIAL COMPRESSOR
•
HARDNESS RATING: 32.0 ROCKWELL C MINIMUM AND 38.0 ROCKWELL C MAXIMUM DISK
•
CRITICALITY CODE JUSTIFICATION: CZCJ
•
MATERIAL DOCUMENT AND CLASSIFICATION: AMS5613 ASSN STD SINGLE MATERIAL RESPONSE DISK
•
DIAMETER: 9.736 INCHES MINIMUM AND 9.746 INCHES MAXIMUM IN
•
ENGINE SECTION LOCATION: COMPRESSOR
TECHNICAL CHARACTERISTICS
STAGE NUMBER3
DESIGN TYPEAXIAL COMPRESSOR
HARDNESS RATING32.0 ROCKWELL C MINIMUM AND 38.0 ROCKWELL C MAXIMUM DISK
CRITICALITY CODE JUSTIFICATIONCZCJ
MATERIAL DOCUMENT AND CLASSIFICATIONAMS5613 ASSN STD SINGLE MATERIAL RESPONSE DISK
DIAMETER9.736 INCHES MINIMUM AND 9.746 INCHES MAXIMUM IN
OVERALL LENGTH2.514 INCHES MINIMUM AND 2.518 INCHES MAXIMUM IN
ENGINE SECTION LOCATIONCOMPRESSOR
SPECIAL FEATUREST.O. 2J-T56-14; COMPRESSOR ROTOR ASSEMBLY
END ITEM IDENTIFICATIONT56 ENG
SUBSTITUTES & CROSS-REFERENCES 1
6841203Reference document
Same NSN cross-reference
Reference document — Secondary reference
LIFECYCLE
NSN statusCancelled· U.S. Government catalog
Demilitarization required — mutilation
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FREQUENTLY ASKED QUESTIONS
What is 6841213?
6841213 is a DISK,COMPRESSOR,AIRCRAFT GAS TUR.
What parts can replace 6841213?
There is 1 known substitute for 6841213: 6841203. Substitute compatibility should be verified for your specific system.
What is the NSN for 6841213?
6841213 is cataloged in the U.S. Government catalog under NSN 2840-00-011-0677. 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.