4082212-03 — BLADE,COMPRESSOR,AIRCRAFT GAS TU

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

4082212-03: BLADE,COMPRESSOR,AIRCRAFT GAS TU.

BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: NICKEL ALLOY OVERALL, design_type: COMPRESSOR, stage_number: 12, overall_width: 0.758 INCHES MINIMUM AND 0.766 INCHES MAXIMUM IN, overall_length: 1.468 INCHES NOMINAL IN, special_features: USE ONLY ON 4079287-01,4080405-01,4080720-01,4080812-01 AND 4080884-01 FOR SPARES REPL USE 4077512-04. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-373-6449, 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

4082212-03

NSN: 2840-01-373-6449
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	NICKEL ALLOY OVERALL
design_type	COMPRESSOR
stage_number	12
overall_width	0.758 INCHES MINIMUM AND 0.766 INCHES MAXIMUM IN
overall_length	1.468 INCHES NOMINAL IN
special_features	USE ONLY ON 4079287-01,4080405-01,4080720-01,4080812-01 AND 4080884-01 FOR SPARES REPL USE 4077512-04
end_item_identification	F100PW0229 AIRCRAFT ENGINE CORE
engine_section_location	COMPRESSOR
criticality_code_justification	AGAV
NSN	2840-01-373-6449

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 12

•

DESIGN TYPE: COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

ENGINE SECTION LOCATION: COMPRESSOR

TECHNICAL CHARACTERISTICS

STAGE NUMBER	12
DESIGN TYPE	COMPRESSOR
CRITICALITY CODE JUSTIFICATION	AGAV
OVERALL LENGTH	1.468 INCHES NOMINAL IN
OVERALL WIDTH	0.758 INCHES MINIMUM AND 0.766 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	COMPRESSOR
SPECIAL FEATURES	USE ONLY ON 4079287-01,4080405-01,4080720-01,4080812-01 AND 4080884-01 FOR SPARES REPL USE 4077512-04
END ITEM IDENTIFICATION	F100PW0229 AIRCRAFT ENGINE CORE
MATERIAL	NICKEL ALLOY OVERALL

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 2

4079412-03Reference document

Same NSN cross-reference

Reference document — Secondary reference

2840PL0711224Reference document

Same NSN cross-reference

Reference document — Informative reference only

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 4082212-03?

4082212-03 is a BLADE,COMPRESSOR,AIRCRAFT GAS TU.

What parts can replace 4082212-03?

There are 2 known substitutes for 4082212-03: 4079412-03, 2840PL0711224. Substitute compatibility should be verified for your specific system.

What is the NSN for 4082212-03?

4082212-03 is cataloged in the U.S. Government catalog under NSN 2840-01-373-6449. This indicates validated use in U.S. government and defense supply chains.

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4082212-03 — BLADE,COMPRESSOR,AIRCRAFT GAS TU

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