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565854CL9 — NOZZLE,TURBINE,AIRCRAFT GAS TURB

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

565854CL9: NOZZLE,TURBINE,AIRCRAFT GAS TURB.

NOZZLE,TURBINE,AIRCRAFT GAS TURB. Key specifications include material: NICKEL ALLOY VANE, overall_width: 2.390 INCHES NOMINAL IN, overall_length: 8.740 INCHES NOMINAL IN, special_features: ORIGINAL NAME VANE,TURBINE NOZZLE,TURBINE ENGINE, material_thickness: 1.245 INCHES NOMINAL IN, end_item_identification: ACFT ENG TF-33. This part is cataloged in the U.S.

Government catalog under NSN 2840-00-962-1266, 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
565854CL9
NSN: 2840-00-962-1266
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 77445 — RTX CORPORATION DBA PRATT & WHITNEY DIV PRATT &WHITNEY (USA)
SPECIFICATIONS
materialNICKEL ALLOY VANE
overall_width2.390 INCHES NOMINAL IN
overall_length8.740 INCHES NOMINAL IN
special_featuresORIGINAL NAME VANE,TURBINE NOZZLE,TURBINE ENGINE
material_thickness1.245 INCHES NOMINAL IN
end_item_identificationACFT ENG TF-33
engine_section_locationTURBINE
criticality_code_justificationAGAV
material_document_and_classificationAMS 5388 ASSN STD SINGLE MATERIAL RESPONSE VANE
NSN2840-00-962-1266
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available NOZZLE,TURBINE,AIRCRAFT GAS TURB TITLE COMPONENT PN 565854CL9 MFR NOZZLE,TURBINE,AIRCRAF
KEY FEATURES
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
MATERIAL DOCUMENT AND CLASSIFICATION: AMS 5388 ASSN STD SINGLE MATERIAL RESPONSE VANE
•
ENGINE SECTION LOCATION: TURBINE
•
MATERIAL THICKNESS: 1.245 INCHES NOMINAL IN
TECHNICAL CHARACTERISTICS
CRITICALITY CODE JUSTIFICATIONAGAV
MATERIAL DOCUMENT AND CLASSIFICATIONAMS 5388 ASSN STD SINGLE MATERIAL RESPONSE VANE
OVERALL LENGTH8.740 INCHES NOMINAL IN
OVERALL WIDTH2.390 INCHES NOMINAL IN
ENGINE SECTION LOCATIONTURBINE
MATERIAL THICKNESS1.245 INCHES NOMINAL IN
SPECIAL FEATURESORIGINAL NAME VANE,TURBINE NOZZLE,TURBINE ENGINE
END ITEM IDENTIFICATIONACFT ENG TF-33
MATERIALNICKEL ALLOY VANE
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
495254CL9Same NSN cross-reference
Same NSN cross-reference
Also cataloged under this NSN
LIFECYCLE
NSN statusActive· U.S. Government catalog
Demilitarization required — mutilation + specific procedure
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FREQUENTLY ASKED QUESTIONS
What is 565854CL9?
565854CL9 is a NOZZLE,TURBINE,AIRCRAFT GAS TURB.
What parts can replace 565854CL9?
There is 1 known substitute for 565854CL9: 495254CL9. Substitute compatibility should be verified for your specific system.
What is the NSN for 565854CL9?
565854CL9 is cataloged in the U.S. Government catalog under NSN 2840-00-962-1266. 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.