804351CL18 — NOZZLE,TURBINE,AIRCRAFT GAS TURB

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

804351CL18: NOZZLE,TURBINE,AIRCRAFT GAS TURB.

NOZZLE,TURBINE,AIRCRAFT GAS TURB. Key specifications include material: COBALT ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_width: 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM IN, overall_height: 4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM IN, overall_length: 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM IN, special_features: FLOW AREA 1.427-1.436; PITCH 34 DEG. 2 MIN.

28 SEC.; 2ND END WIDTH 0.760-0.780. This part is cataloged in the U.S. Government catalog under NSN 2840-01-394-5231, 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

804351CL18

NSN: 2840-01-394-5231
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 77445 — RTX CORPORATION DBA PRATT & WHITNEY DIV PRATT &WHITNEY (USA)

SPECIFICATIONS

material	COBALT ALLOY OVERALL
design_type	AXIAL COMPRESSOR
stage_number	1
overall_width	1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM IN
overall_height	4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM IN
overall_length	2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM IN
special_features	FLOW AREA 1.427-1.436; PITCH 34 DEG. 2 MIN. 28 SEC.; 2ND END WIDTH 0.760-0.780
blade_attachment_method	SLOT
end_item_identification	TF-33 AIRCRAFT ENGINE
engine_section_location	HIGH PRESSURE TURBINE
reference_data_and_literature	T.O. 2J-TF33-4 FIG31 IND50
criticality_code_justification	APGF AND CZBJ AND CZCJ AND BGLW AND FEAT
NSN	2840-01-394-5231

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 1

•

DESIGN TYPE: AXIAL COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: APGF AND CZBJ AND CZCJ AND BGLW AND FEAT

•

REFERENCE DATA AND LITERATURE: T.O. 2J-TF33-4 FIG31 IND50

•

BLADE ATTACHMENT METHOD: SLOT

•

MATERIAL DOCUMENT AND CLASSIFICATION: PWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL

TECHNICAL CHARACTERISTICS

OVERALL HEIGHT	4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM IN
STAGE NUMBER	1
DESIGN TYPE	AXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATION	APGF AND CZBJ AND CZCJ AND BGLW AND FEAT
REFERENCE DATA AND LITERATURE	T.O. 2J-TF33-4 FIG31 IND50
BLADE ATTACHMENT METHOD	SLOT
MATERIAL DOCUMENT AND CLASSIFICATION	PWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
OVERALL LENGTH	2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM IN
OVERALL WIDTH	1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	HIGH PRESSURE TURBINE

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 804351CL18?

804351CL18 is a NOZZLE,TURBINE,AIRCRAFT GAS TURB.

What parts can replace 804351CL18?

There is 1 known substitute for 804351CL18: 804351. Substitute compatibility should be verified for your specific system.

What is the NSN for 804351CL18?

804351CL18 is cataloged in the U.S. Government catalog under NSN 2840-01-394-5231. This indicates validated use in U.S. government and defense supply chains.

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804351CL18 — NOZZLE,TURBINE,AIRCRAFT GAS TURB

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