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4083112-01 — DUCT,EXHAUST,AIRCRAFT GAS TURBIN

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

4083112-01: DUCT,EXHAUST,AIRCRAFT GAS TURBIN.

DUCT,EXHAUST,AIRCRAFT GAS TURBIN. Key specifications include diameter: 15.670 INCHES MINIMUM AND 15.690 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, overall_length: 2.565 INCHES MINIMUM AND 2.625 INCHES MAXIMUM IN, special_features: DUCT ASSY CONSISTS OF DUCT/4083112-02; STIFFENER/4083112-03; STIFFENER/4083112-04; FLANGE/4083112-01, end_item_identification: F100-229 AIRCRAFT GAS TURBINE ENGINES, engine_section_location: EXHAUST. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-420-2437, 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
4083112-01
NSN: 2840-01-420-2437
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 77445 — RTX CORPORATION DBA PRATT & WHITNEY DIV PRATT &WHITNEY (USA)
SPECIFICATIONS
diameter15.670 INCHES MINIMUM AND 15.690 INCHES MAXIMUM IN
materialNICKEL ALLOY OVERALL
overall_length2.565 INCHES MINIMUM AND 2.625 INCHES MAXIMUM IN
special_featuresDUCT ASSY CONSISTS OF DUCT/4083112-02; STIFFENER/4083112-03; STIFFENER/4083112-04; FLANGE/4083112-01
end_item_identificationF100-229 AIRCRAFT GAS TURBINE ENGINES
engine_section_locationEXHAUST
criticality_code_justificationCZBJ AND ABHP AND ABMZ AND FEAT
material_document_and_classificationAMS5599 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
NSN2840-01-420-2437
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available DUCT,EXHAUST,AIRCRAFT GAS TURBIN TITLE COMPONENT PN 4083112-01 MFR DUCT,EXHAUST,AIRCRAFT
KEY FEATURES
•
CRITICALITY CODE JUSTIFICATION: CZBJ AND ABHP AND ABMZ AND FEAT
•
MATERIAL DOCUMENT AND CLASSIFICATION: AMS5599 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
•
DIAMETER: 15.670 INCHES MINIMUM AND 15.690 INCHES MAXIMUM IN
•
ENGINE SECTION LOCATION: EXHAUST
•
MATERIAL: NICKEL ALLOY OVERALL
TECHNICAL CHARACTERISTICS
CRITICALITY CODE JUSTIFICATIONCZBJ AND ABHP AND ABMZ AND FEAT
MATERIAL DOCUMENT AND CLASSIFICATIONAMS5599 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
DIAMETER15.670 INCHES MINIMUM AND 15.690 INCHES MAXIMUM IN
OVERALL LENGTH2.565 INCHES MINIMUM AND 2.625 INCHES MAXIMUM IN
ENGINE SECTION LOCATIONEXHAUST
SPECIAL FEATURESDUCT ASSY CONSISTS OF DUCT/4083112-02; STIFFENER/4083112-03; STIFFENER/4083112-04; FLANGE/4083112-01
END ITEM IDENTIFICATIONF100-229 AIRCRAFT GAS TURBINE ENGINES
MATERIALNICKEL 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.
2840-00-000-0048 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 2
4084485-01Same NSN cross-reference
Same NSN cross-reference
Also cataloged under this NSN
KDS 2840-1150Reference document
Same NSN cross-reference
Reference document — Secondary reference
LIFECYCLE
NSN statusActive· U.S. Government catalog
Demilitarization required — critical (Q)
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FREQUENTLY ASKED QUESTIONS
What is 4083112-01?
4083112-01 is a DUCT,EXHAUST,AIRCRAFT GAS TURBIN.
What parts can replace 4083112-01?
There are 2 known substitutes for 4083112-01: 4084485-01, KDS 2840-1150. Substitute compatibility should be verified for your specific system.
What is the NSN for 4083112-01?
4083112-01 is cataloged in the U.S. Government catalog under NSN 2840-01-420-2437. This indicates validated use in U.S. government and defense supply chains.
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