727611 — BLADE,COMPRESSOR,AIRCRAFT GAS TU

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

727611: BLADE,COMPRESSOR,AIRCRAFT GAS TU.

BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: STEEL BLADE, design_type: COMPRESSOR, overall_width: 1.212 INCHES MINIMUM AND 1.222 INCHES MAXIMUM IN, overall_length: 3.103 INCHES NOMINAL IN, hardness_rating: 32.0 ROCKWELL C MINIMUM AND 38.0 ROCKWELL C MAXIMUM BLADE, special_features: ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-00-222-4164, 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

727611

NSN: 2840-00-222-4164
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 BLADE
design_type	COMPRESSOR
overall_width	1.212 INCHES MINIMUM AND 1.222 INCHES MAXIMUM IN
overall_length	3.103 INCHES NOMINAL IN
hardness_rating	32.0 ROCKWELL C MINIMUM AND 38.0 ROCKWELL C MAXIMUM BLADE
special_features	ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE
material_thickness	0.493 INCHES MINIMUM AND 0.499 INCHES MAXIMUM IN
end_item_identification	ENGINE MODEL TF33
engine_section_location	COMPRESSOR
criticality_code_justification	AGAVG
material_document_and_classification	AMS5616 ASSN STD SINGLE MATERIAL RESPONSE BLADE
NSN	2840-00-222-4164

COMPONENT DIAGRAM

KEY FEATURES

•

DESIGN TYPE: COMPRESSOR

•

HARDNESS RATING: 32.0 ROCKWELL C MINIMUM AND 38.0 ROCKWELL C MAXIMUM BLADE

•

CRITICALITY CODE JUSTIFICATION: AGAVG

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS5616 ASSN STD SINGLE MATERIAL RESPONSE BLADE

•

ENGINE SECTION LOCATION: COMPRESSOR

•

MATERIAL THICKNESS: 0.493 INCHES MINIMUM AND 0.499 INCHES MAXIMUM IN

TECHNICAL CHARACTERISTICS

DESIGN TYPE	COMPRESSOR
HARDNESS RATING	32.0 ROCKWELL C MINIMUM AND 38.0 ROCKWELL C MAXIMUM BLADE
CRITICALITY CODE JUSTIFICATION	AGAVG
MATERIAL DOCUMENT AND CLASSIFICATION	AMS5616 ASSN STD SINGLE MATERIAL RESPONSE BLADE
OVERALL LENGTH	3.103 INCHES NOMINAL IN
OVERALL WIDTH	1.212 INCHES MINIMUM AND 1.222 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	COMPRESSOR
MATERIAL THICKNESS	0.493 INCHES MINIMUM AND 0.499 INCHES MAXIMUM IN
SPECIAL FEATURES	ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE
END ITEM IDENTIFICATION	ENGINE MODEL TF33

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 1

716111Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 727611?

727611 is a BLADE,COMPRESSOR,AIRCRAFT GAS TU.

What parts can replace 727611?

There is 1 known substitute for 727611: 716111. Substitute compatibility should be verified for your specific system.

What is the NSN for 727611?

727611 is cataloged in the U.S. Government catalog under NSN 2840-00-222-4164. This indicates validated use in U.S. government and defense supply chains.

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727611 — BLADE,COMPRESSOR,AIRCRAFT GAS TU

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