220571Y2 — LOCK,COMPRESSOR BLADE,AIRCRAFT G

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

220571Y2: LOCK,COMPRESSOR BLADE,AIRCRAFT G.

LOCK,COMPRESSOR BLADE,AIRCRAFT G. Key specifications include material: STEEL, overall_width: 0.112 INCHES MINIMUM AND 0.116 INCHES MAXIMUM IN, overall_length: 0.548 INCHES MINIMUM AND 0.552 INCHES MAXIMUM IN, hardness_rating: 19.0 ROCKWELL C MINIMUM AND 26.0 ROCKWELL C MAXIMUM, special_features: GOES ON CENTER MAIN BEARING SUPPORT; COMPRESSOR STATOR; FRONT EXIT STAGE BLADE, material_thickness: 0.010 INCHES NOMINAL IN. This part is cataloged in the U.S.

Government catalog under NSN 2840-00-326-1011, 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

220571Y2

NSN: 2840-00-326-1011
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 0AHP5 — CURTISS-WRIGHT CONTROLS, INC. DIV ACTUATION DIVISION (USA)

SPECIFICATIONS

material	STEEL
stage_number	1
overall_width	0.112 INCHES MINIMUM AND 0.116 INCHES MAXIMUM IN
overall_length	0.548 INCHES MINIMUM AND 0.552 INCHES MAXIMUM IN
hardness_rating	19.0 ROCKWELL C MINIMUM AND 26.0 ROCKWELL C MAXIMUM
special_features	GOES ON CENTER MAIN BEARING SUPPORT; COMPRESSOR STATOR; FRONT EXIT STAGE BLADE
material_thickness	0.010 INCHES NOMINAL IN
end_item_identification	J-65 AIRCRAFT ENGINE
reference_data_and_literature	2J-J65-4
criticality_code_justification	AGAV
material_document_and_classification	AMS5613 ASSN STD SINGLE MATERIAL RESPONSE
NSN	2840-00-326-1011

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 1

•

HARDNESS RATING: 19.0 ROCKWELL C MINIMUM AND 26.0 ROCKWELL C MAXIMUM

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

REFERENCE DATA AND LITERATURE: 2J-J65-4

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS5613 ASSN STD SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.010 INCHES NOMINAL IN

TECHNICAL CHARACTERISTICS

STAGE NUMBER	1
HARDNESS RATING	19.0 ROCKWELL C MINIMUM AND 26.0 ROCKWELL C MAXIMUM
CRITICALITY CODE JUSTIFICATION	AGAV
REFERENCE DATA AND LITERATURE	2J-J65-4
MATERIAL DOCUMENT AND CLASSIFICATION	AMS5613 ASSN STD SINGLE MATERIAL RESPONSE
OVERALL LENGTH	0.548 INCHES MINIMUM AND 0.552 INCHES MAXIMUM IN
OVERALL WIDTH	0.112 INCHES MINIMUM AND 0.116 INCHES MAXIMUM IN
MATERIAL THICKNESS	0.010 INCHES NOMINAL IN
SPECIAL FEATURES	GOES ON CENTER MAIN BEARING SUPPORT; COMPRESSOR STATOR; FRONT EXIT STAGE BLADE
END ITEM IDENTIFICATION	J-65 AIRCRAFT 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.

2840-00-004-4242 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)No demilitarization required

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FREQUENTLY ASKED QUESTIONS

What is 220571Y2?

220571Y2 is a LOCK,COMPRESSOR BLADE,AIRCRAFT G.

What is the NSN for 220571Y2?

220571Y2 is cataloged in the U.S. Government catalog under NSN 2840-00-326-1011. This indicates validated use in U.S. government and defense supply chains.

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220571Y2 — LOCK,COMPRESSOR BLADE,AIRCRAFT G

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