710208 — DISK,COMPRESSOR,AIRCRAFT GAS TUR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

710208: DISK,COMPRESSOR,AIRCRAFT GAS TUR.

DISK,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include diameter: 14.015 INCHES MINIMUM AND 14.025 INCHES MAXIMUM IN, material: TITANIUM ALLOY DISK, design_type: AXIAL COMPRESSOR, overall_length: 1.193 INCHES MINIMUM AND 1.203 INCHES MAXIMUM IN, special_features: WAS DISK,AXIAL COMPRESSOR,TURBINEENGINE, end_item_identification: TF-30 AIRCRAFT ENGINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-00-488-7518, 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

710208

NSN: 2840-00-488-7518
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	14.015 INCHES MINIMUM AND 14.025 INCHES MAXIMUM IN
material	TITANIUM ALLOY DISK
design_type	AXIAL COMPRESSOR
overall_length	1.193 INCHES MINIMUM AND 1.203 INCHES MAXIMUM IN
special_features	WAS DISK,AXIAL COMPRESSOR,TURBINEENGINE
end_item_identification	TF-30 AIRCRAFT ENGINE
engine_section_location	COMPRESSOR
criticality_code_justification	AGAV
material_document_and_classification	PWA1202 ASSN STD SINGLE MATERIAL RESPONSE DISK
NSN	2840-00-488-7518

COMPONENT DIAGRAM

KEY FEATURES

•

DESIGN TYPE: AXIAL COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

MATERIAL DOCUMENT AND CLASSIFICATION: PWA1202 ASSN STD SINGLE MATERIAL RESPONSE DISK

•

DIAMETER: 14.015 INCHES MINIMUM AND 14.025 INCHES MAXIMUM IN

•

ENGINE SECTION LOCATION: COMPRESSOR

TECHNICAL CHARACTERISTICS

DESIGN TYPE	AXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATION	AGAV
MATERIAL DOCUMENT AND CLASSIFICATION	PWA1202 ASSN STD SINGLE MATERIAL RESPONSE DISK
DIAMETER	14.015 INCHES MINIMUM AND 14.025 INCHES MAXIMUM IN
OVERALL LENGTH	1.193 INCHES MINIMUM AND 1.203 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	COMPRESSOR
SPECIAL FEATURES	WAS DISK,AXIAL COMPRESSOR,TURBINEENGINE
END ITEM IDENTIFICATION	TF-30 AIRCRAFT ENGINE
MATERIAL	TITANIUM ALLOY DISK

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

No substitute or cross-reference records for this part.

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Normally procured from the manufacturer (OEM)Demilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 710208?

710208 is a DISK,COMPRESSOR,AIRCRAFT GAS TUR.

What is the NSN for 710208?

710208 is cataloged in the U.S. Government catalog under NSN 2840-00-488-7518. This indicates validated use in U.S. government and defense supply chains.

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710208 — DISK,COMPRESSOR,AIRCRAFT GAS TUR

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