4080012-01 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

4080012-01: SEAL,AIR,AIRCRAFT GAS TURBINE EN.

SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 19.764 INCHES MINIMUM AND 19.768 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, overall_length: 1.309 INCHES MINIMUM AND 1.329 INCHES MAXIMUM IN, material_thickness: 0.033 INCHES MINIMUM AND 0.037 INCHES MAXIMUM IN, end_item_identification: F100PW0229 AIRCRAFT ENGINE/CORE, engine_section_location: TURBINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-369-6006, 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

4080012-01

NSN: 2840-01-369-6006
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	19.764 INCHES MINIMUM AND 19.768 INCHES MAXIMUM IN
material	NICKEL ALLOY OVERALL
stage_number	1
overall_length	1.309 INCHES MINIMUM AND 1.329 INCHES MAXIMUM IN
material_thickness	0.033 INCHES MINIMUM AND 0.037 INCHES MAXIMUM IN
end_item_identification	F100PW0229 AIRCRAFT ENGINE/CORE
engine_section_location	TURBINE
criticality_code_justification	AGAV
material_document_and_classification	AMS5599 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
NSN	2840-01-369-6006

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 1

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS5599 ASSN STD SINGLE MATERIAL RESPONSE OVERALL

•

DIAMETER: 19.764 INCHES MINIMUM AND 19.768 INCHES MAXIMUM IN

•

ENGINE SECTION LOCATION: TURBINE

•

MATERIAL THICKNESS: 0.033 INCHES MINIMUM AND 0.037 INCHES MAXIMUM IN

TECHNICAL CHARACTERISTICS

STAGE NUMBER	1
CRITICALITY CODE JUSTIFICATION	AGAV
MATERIAL DOCUMENT AND CLASSIFICATION	AMS5599 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
DIAMETER	19.764 INCHES MINIMUM AND 19.768 INCHES MAXIMUM IN
OVERALL LENGTH	1.309 INCHES MINIMUM AND 1.329 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	TURBINE
MATERIAL THICKNESS	0.033 INCHES MINIMUM AND 0.037 INCHES MAXIMUM IN
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

No substitute or cross-reference records for this part.

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 4080012-01?

4080012-01 is a SEAL,AIR,AIRCRAFT GAS TURBINE EN.

What is the NSN for 4080012-01?

4080012-01 is cataloged in the U.S. Government catalog under NSN 2840-01-369-6006. This indicates validated use in U.S. government and defense supply chains.

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4080012-01 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

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