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625512 — BLADE,COMPRESSOR,AIRCRAFT GAS TU

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

625512: BLADE,COMPRESSOR,AIRCRAFT GAS TU.

BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: STEEL BLADE, design_type: COMPRESSOR, overall_width: 1.160 INCHES MINIMUM AND 1.170 INCHES MAXIMUM IN, overall_length: 2.782 INCHES MINIMUM AND 2.791 INCHES MAXIMUM IN, hardness_rating: 32.0 ROCKWELL C MINIMUM AND 38.0 ROCKWELL C MAXIMUM BLADE, special_features: TOLARANCE, FIT. This part is cataloged in the U.S.

Government catalog under NSN 2840-00-166-2356, 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
625512
NSN: 2840-00-166-2356
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 77445 — RTX CORPORATION DBA PRATT & WHITNEY DIV PRATT &WHITNEY (USA)
SPECIFICATIONS
materialSTEEL BLADE
design_typeCOMPRESSOR
overall_width1.160 INCHES MINIMUM AND 1.170 INCHES MAXIMUM IN
overall_length2.782 INCHES MINIMUM AND 2.791 INCHES MAXIMUM IN
hardness_rating32.0 ROCKWELL C MINIMUM AND 38.0 ROCKWELL C MAXIMUM BLADE
special_featuresTOLARANCE, FIT
material_thickness0.493 INCHES MINIMUM AND 0.499 INCHES MAXIMUM IN
end_item_identificationENGINE MODEL TF33
engine_section_locationCOMPRESSOR
criticality_code_justificationFEAT
material_document_and_classificationAMS5616 ASSN STD SINGLE MATERIAL RESPONSE BLADE
NSN2840-00-166-2356
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available BLADE,COMPRESSOR,AIRCRAFT GAS TU TITLE COMPONENT PN 625512 MFR BLADE,COMPRESSOR,AIRCR
KEY FEATURES
•
DESIGN TYPE: COMPRESSOR
•
HARDNESS RATING: 32.0 ROCKWELL C MINIMUM AND 38.0 ROCKWELL C MAXIMUM BLADE
•
CRITICALITY CODE JUSTIFICATION: FEAT
•
MATERIAL DOCUMENT AND CLASSIFICATION: AMS5616 ASSN STD SINGLE MATERIAL RESPONSE BLADE
•
ENGINE SECTION LOCATION: COMPRESSOR
•
MATERIAL THICKNESS: 0.493 INCHES MINIMUM AND 0.499 INCHES MAXIMUM IN
TECHNICAL CHARACTERISTICS
DESIGN TYPECOMPRESSOR
HARDNESS RATING32.0 ROCKWELL C MINIMUM AND 38.0 ROCKWELL C MAXIMUM BLADE
CRITICALITY CODE JUSTIFICATIONFEAT
MATERIAL DOCUMENT AND CLASSIFICATIONAMS5616 ASSN STD SINGLE MATERIAL RESPONSE BLADE
OVERALL LENGTH2.782 INCHES MINIMUM AND 2.791 INCHES MAXIMUM IN
OVERALL WIDTH1.160 INCHES MINIMUM AND 1.170 INCHES MAXIMUM IN
ENGINE SECTION LOCATIONCOMPRESSOR
MATERIAL THICKNESS0.493 INCHES MINIMUM AND 0.499 INCHES MAXIMUM IN
SPECIAL FEATURESTOLARANCE, FIT
END ITEM IDENTIFICATIONENGINE MODEL TF33
SUBSTITUTES & CROSS-REFERENCES 1
726712Same NSN cross-reference
Same NSN cross-reference
Also cataloged under this NSN
LIFECYCLE
NSN statusActive· U.S. Government catalog
Demilitarization required — critical (Q)
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FREQUENTLY ASKED QUESTIONS
What is 625512?
625512 is a BLADE,COMPRESSOR,AIRCRAFT GAS TU.
What parts can replace 625512?
There is 1 known substitute for 625512: 726712. Substitute compatibility should be verified for your specific system.
What is the NSN for 625512?
625512 is cataloged in the U.S. Government catalog under NSN 2840-00-166-2356. 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.