703173 — CASE,COMPRESSOR,AIRCRAFT GAS TUR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

703173: CASE,COMPRESSOR,AIRCRAFT GAS TUR.

CASE,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include diameter: 58.200 INCHES NOMINAL IN, material: STEEL CORROSION RESISTING OVERALL, design_type: AXIAL COMPRESSOR, special_features: HARDNESS RATE ROCKWELL C25-33 OR EQUIV., end_item_identification: TF33-PW-102 TURBINE FAN JET ENGINE,KC-135 AIRCRAFT, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-160-7250, 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

703173

NSN: 2840-01-160-7250
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 77445 — RTX CORPORATION DBA PRATT & WHITNEY DIV PRATT &WHITNEY (USA)

SPECIFICATIONS

diameter	58.200 INCHES NOMINAL IN
material	STEEL CORROSION RESISTING OVERALL
design_type	AXIAL COMPRESSOR
special_features	HARDNESS RATE ROCKWELL C25-33 OR EQUIV.
end_item_identification	TF33-PW-102 TURBINE FAN JET ENGINE,KC-135 AIRCRAFT
engine_section_location	COMPRESSOR
reference_data_and_literature	T.O.2J-TF33-34 FIG 14, IND 1
criticality_code_justification	AGAV
part_name_assigned_by_controlling_agency	CASE REAR COMPRESSOR,INNER
NSN	2840-01-160-7250

COMPONENT DIAGRAM

KEY FEATURES

•

DESIGN TYPE: AXIAL COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

REFERENCE DATA AND LITERATURE: T.O.2J-TF33-34 FIG 14, IND 1

•

DIAMETER: 58.200 INCHES NOMINAL IN

•

ENGINE SECTION LOCATION: COMPRESSOR

TECHNICAL CHARACTERISTICS

DESIGN TYPE	AXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATION	AGAV
REFERENCE DATA AND LITERATURE	T.O.2J-TF33-34 FIG 14, IND 1
DIAMETER	58.200 INCHES NOMINAL IN
ENGINE SECTION LOCATION	COMPRESSOR
SPECIAL FEATURES	HARDNESS RATE ROCKWELL C25-33 OR EQUIV.
PART NAME ASSIGNED BY CONTROLLING AGENCY	CASE REAR COMPRESSOR,INNER
END ITEM IDENTIFICATION	TF33-PW-102 TURBINE FAN JET ENGINE,KC-135 AIRCRAFT
MATERIAL	STEEL CORROSION RESISTING OVERALL

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

Demilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 703173?

703173 is a CASE,COMPRESSOR,AIRCRAFT GAS TUR.

What is the NSN for 703173?

703173 is cataloged in the U.S. Government catalog under NSN 2840-01-160-7250. This indicates validated use in U.S. government and defense supply chains.

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703173 — CASE,COMPRESSOR,AIRCRAFT GAS TUR

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