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804351CL22 — NOZZLE,TURBINE,AIRCRAFT GAS TURB

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

804351CL22: NOZZLE,TURBINE,AIRCRAFT GAS TURB.

NOZZLE,TURBINE,AIRCRAFT GAS TURB. Key specifications include material: COBALT ALLOY VANE, overall_width: 2.045 INCHES NOMINAL IN, overall_height: 4.153 INCHES NOMINAL IN, overall_length: 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM IN, special_features: FLOW AREA 1.464 - 1.489.PITCH IS 34DEG 38MIN 28SEC, blade_attachment_method: SLOT. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-394-7115, 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
804351CL22
NSN: 2840-01-394-7115
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 77445 — RTX CORPORATION DBA PRATT & WHITNEY DIV PRATT &WHITNEY (USA)
SPECIFICATIONS
materialCOBALT ALLOY VANE
stage_number1
overall_width2.045 INCHES NOMINAL IN
overall_height4.153 INCHES NOMINAL IN
overall_length1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM IN
special_featuresFLOW AREA 1.464 - 1.489.PITCH IS 34DEG 38MIN 28SEC
blade_attachment_methodSLOT
end_item_identificationTF-33
engine_section_locationHIGH PRESSURE TURBINE
reference_data_and_literatureT.O. 2J-TF33-4 FIG 31, IND 50
criticality_code_justificationABMK
part_name_assigned_by_controlling_agencyVANE,HPT, 1 STG
NSN2840-01-394-7115
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available NOZZLE,TURBINE,AIRCRAFT GAS TURB TITLE COMPONENT PN 804351CL22 MFR NOZZLE,TURBINE,AIRCRAF
KEY FEATURES
•
STAGE NUMBER: 1
•
CRITICALITY CODE JUSTIFICATION: ABMK
•
REFERENCE DATA AND LITERATURE: T.O. 2J-TF33-4 FIG 31, IND 50
•
BLADE ATTACHMENT METHOD: SLOT
•
ENGINE SECTION LOCATION: HIGH PRESSURE TURBINE
TECHNICAL CHARACTERISTICS
OVERALL HEIGHT4.153 INCHES NOMINAL IN
STAGE NUMBER1
CRITICALITY CODE JUSTIFICATIONABMK
REFERENCE DATA AND LITERATURET.O. 2J-TF33-4 FIG 31, IND 50
BLADE ATTACHMENT METHODSLOT
OVERALL LENGTH1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM IN
OVERALL WIDTH2.045 INCHES NOMINAL IN
ENGINE SECTION LOCATIONHIGH PRESSURE TURBINE
SPECIAL FEATURESFLOW AREA 1.464 - 1.489.PITCH IS 34DEG 38MIN 28SEC
PART NAME ASSIGNED BY CONTROLLING AGENCYVANE,HPT, 1 STG
SUBSTITUTES & CROSS-REFERENCES 1
804351Reference document
Same NSN cross-reference
Reference document — Drawing number reference only
LIFECYCLE
NSN statusActive· U.S. Government catalog
Demilitarization required — mutilation + specific procedure
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FREQUENTLY ASKED QUESTIONS
What is 804351CL22?
804351CL22 is a NOZZLE,TURBINE,AIRCRAFT GAS TURB.
What parts can replace 804351CL22?
There is 1 known substitute for 804351CL22: 804351. Substitute compatibility should be verified for your specific system.
What is the NSN for 804351CL22?
804351CL22 is cataloged in the U.S. Government catalog under NSN 2840-01-394-7115. 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.