715049 — LOCK,TURBINE ROTOR BLADE,AIRCRAF

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

715049: LOCK,TURBINE ROTOR BLADE,AIRCRAF.

LOCK,TURBINE ROTOR BLADE,AIRCRAF. Key specifications include material: STEEL CORROSION RESISTING, overall_width: 0.264 INCHES MINIMUM AND 0.294 INCHES MAXIMUM IN, overall_length: 1.315 INCHES MINIMUM AND 1.365 INCHES MAXIMUM IN, hardness_rating: 63.0 ROCKWELL A MINIMUM AND 68.0 ROCKWELL A MAXIMUM, special_features: GOES ON THE COMPRESSOR ROTOR-FRONT, end_item_identification: TF-33 AIRCRAFT ENGINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-00-883-5965, 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

715049

NSN: 2840-00-883-5965
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	STEEL CORROSION RESISTING
stage_number	8
overall_width	0.264 INCHES MINIMUM AND 0.294 INCHES MAXIMUM IN
overall_length	1.315 INCHES MINIMUM AND 1.365 INCHES MAXIMUM IN
hardness_rating	63.0 ROCKWELL A MINIMUM AND 68.0 ROCKWELL A MAXIMUM
special_features	GOES ON THE COMPRESSOR ROTOR-FRONT
end_item_identification	TF-33 AIRCRAFT ENGINE
reference_data_and_literature	2J-TF33-4
material_document_and_classification	AMS5517 ASSN STD SINGLE MATERIAL RESPONSE
NSN	2840-00-883-5965

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 8

•

HARDNESS RATING: 63.0 ROCKWELL A MINIMUM AND 68.0 ROCKWELL A MAXIMUM

•

REFERENCE DATA AND LITERATURE: 2J-TF33-4

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS5517 ASSN STD SINGLE MATERIAL RESPONSE

TECHNICAL CHARACTERISTICS

STAGE NUMBER	8
HARDNESS RATING	63.0 ROCKWELL A MINIMUM AND 68.0 ROCKWELL A MAXIMUM
REFERENCE DATA AND LITERATURE	2J-TF33-4
MATERIAL DOCUMENT AND CLASSIFICATION	AMS5517 ASSN STD SINGLE MATERIAL RESPONSE
OVERALL LENGTH	1.315 INCHES MINIMUM AND 1.365 INCHES MAXIMUM IN
OVERALL WIDTH	0.264 INCHES MINIMUM AND 0.294 INCHES MAXIMUM IN
SPECIAL FEATURES	GOES ON THE COMPRESSOR ROTOR-FRONT
END ITEM IDENTIFICATION	TF-33 AIRCRAFT ENGINE
MATERIAL	STEEL CORROSION RESISTING

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

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FREQUENTLY ASKED QUESTIONS

What is 715049?

715049 is a LOCK,TURBINE ROTOR BLADE,AIRCRAF.

What is the NSN for 715049?

715049 is cataloged in the U.S. Government catalog under NSN 2840-00-883-5965. This indicates validated use in U.S. government and defense supply chains.

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715049 — LOCK,TURBINE ROTOR BLADE,AIRCRAF

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