747059R1 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

747059R1: SEAL,AIR,AIRCRAFT GAS TURBINE EN.

SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 20.585 INCHES MINIMUM AND 20.595 INCHES MAXIMUM IN, material: STEEL CORROSION RESISTING OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 0.775 INCHES MINIMUM AND 0.805 INCHES MAXIMUM IN, special_features: T.O. 2J-TF33-4, FIG 16, IND 15; UUSED ON THE INTERMEDIATE COMPRESSOR; NO.

2, 2 1/2 & 3 BEARINGS, end_item_identification: TF-33 AIRCRAFT GAS TURBINE ENGINE. This part is cataloged in the U.S. Government catalog under NSN 2840-01-161-0474, 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

747059R1

NSN: 2840-01-161-0474
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	20.585 INCHES MINIMUM AND 20.595 INCHES MAXIMUM IN
material	STEEL CORROSION RESISTING OVERALL
design_type	AXIAL COMPRESSOR
stage_number	9
overall_length	0.775 INCHES MINIMUM AND 0.805 INCHES MAXIMUM IN
special_features	T.O. 2J-TF33-4, FIG 16, IND 15; UUSED ON THE INTERMEDIATE COMPRESSOR; NO. 2, 2 1/2 & 3 BEARINGS
end_item_identification	TF-33 AIRCRAFT GAS TURBINE ENGINE
engine_section_location	COMPRESSOR
criticality_code_justification	ABHP AND ABMZ AND CZBJ AND FEAT
material_document_and_classification	AMS5613 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
part_name_assigned_by_controlling_agency	ORIGINAL NAME RING,AIRSEAL,COMPRESSOR
NSN	2840-01-161-0474

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 9

•

DESIGN TYPE: AXIAL COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: ABHP AND ABMZ AND CZBJ AND FEAT

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS5613 ASSN STD SINGLE MATERIAL RESPONSE OVERALL

•

DIAMETER: 20.585 INCHES MINIMUM AND 20.595 INCHES MAXIMUM IN

•

ENGINE SECTION LOCATION: COMPRESSOR

TECHNICAL CHARACTERISTICS

STAGE NUMBER	9
DESIGN TYPE	AXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATION	ABHP AND ABMZ AND CZBJ AND FEAT
MATERIAL DOCUMENT AND CLASSIFICATION	AMS5613 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
DIAMETER	20.585 INCHES MINIMUM AND 20.595 INCHES MAXIMUM IN
OVERALL LENGTH	0.775 INCHES MINIMUM AND 0.805 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	COMPRESSOR
SPECIAL FEATURES	T.O. 2J-TF33-4, FIG 16, IND 15; UUSED ON THE INTERMEDIATE COMPRESSOR; NO. 2, 2 1/2 & 3 BEARINGS
PART NAME ASSIGNED BY CONTROLLING AGENCY	ORIGINAL NAME RING,AIRSEAL,COMPRESSOR
END ITEM IDENTIFICATION	TF-33 AIRCRAFT GAS TURBINE ENGINE

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: Insurance item — stocked against contingency demandDemilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 747059R1?

747059R1 is a SEAL,AIR,AIRCRAFT GAS TURBINE EN.

What is the NSN for 747059R1?

747059R1 is cataloged in the U.S. Government catalog under NSN 2840-01-161-0474. This indicates validated use in U.S. government and defense supply chains.

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747059R1 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

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