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618208 — BLADE,COMPRESSOR,AIRCRAFT GAS TU

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

618208: BLADE,COMPRESSOR,AIRCRAFT GAS TU.

BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: TITANIUM ALLOY BLADE, design_type: COMPRESSOR, overall_width: 1.198 INCHES NOMINAL IN, overall_length: 3.091 INCHES NOMINAL IN, special_features: ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE, material_thickness: 0.293 INCHES NOMINAL IN. This part is cataloged in the U.S.

Government catalog under NSN 2840-00-922-4372, 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
618208
NSN: 2840-00-922-4372
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 77445 — RTX CORPORATION DBA PRATT & WHITNEY DIV PRATT &WHITNEY (USA)
SPECIFICATIONS
materialTITANIUM ALLOY BLADE
design_typeCOMPRESSOR
overall_width1.198 INCHES NOMINAL IN
overall_length3.091 INCHES NOMINAL IN
special_featuresORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE
material_thickness0.293 INCHES NOMINAL IN
end_item_identificationTF30 ACFT ENGINE
engine_section_locationCOMPRESSOR
criticality_code_justificationAGAV
material_document_and_classificationPWA1202 ASSN STD SINGLE MATERIAL RESPONSE BLADE
NSN2840-00-922-4372
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available BLADE,COMPRESSOR,AIRCRAFT GAS TU TITLE COMPONENT PN 618208 MFR BLADE,COMPRESSOR,AIRCR
KEY FEATURES
•
DESIGN TYPE: COMPRESSOR
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
MATERIAL DOCUMENT AND CLASSIFICATION: PWA1202 ASSN STD SINGLE MATERIAL RESPONSE BLADE
•
ENGINE SECTION LOCATION: COMPRESSOR
•
MATERIAL THICKNESS: 0.293 INCHES NOMINAL IN
TECHNICAL CHARACTERISTICS
DESIGN TYPECOMPRESSOR
CRITICALITY CODE JUSTIFICATIONAGAV
MATERIAL DOCUMENT AND CLASSIFICATIONPWA1202 ASSN STD SINGLE MATERIAL RESPONSE BLADE
OVERALL LENGTH3.091 INCHES NOMINAL IN
OVERALL WIDTH1.198 INCHES NOMINAL IN
ENGINE SECTION LOCATIONCOMPRESSOR
MATERIAL THICKNESS0.293 INCHES NOMINAL IN
SPECIAL FEATURESORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE
END ITEM IDENTIFICATIONTF30 ACFT ENGINE
MATERIALTITANIUM ALLOY BLADE
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.
2840-00-000-0048 2840-00-000-0049 2840-00-001-1741 2840-00-001-1743 2840-00-001-2117 2840-00-001-2284 2840-00-001-3922 2840-00-001-4903
SUBSTITUTES & CROSS-REFERENCES

No substitute or cross-reference records for this part.

LIFECYCLE
NSN statusActive· U.S. Government catalog
Acquisition advice: Normally procured from the manufacturer (OEM)Demilitarization required — mutilation
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FREQUENTLY ASKED QUESTIONS
What is 618208?
618208 is a BLADE,COMPRESSOR,AIRCRAFT GAS TU.
What is the NSN for 618208?
618208 is cataloged in the U.S. Government catalog under NSN 2840-00-922-4372. 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.