4081007 — SHIELD,HEAT,AIRCRAFT GAS TURBINE

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

4081007: SHIELD,HEAT,AIRCRAFT GAS TURBINE.

SHIELD,HEAT,AIRCRAFT GAS TURBINE. Key specifications include diameter: 25.760 INCHES NOMINAL IN, material: COBALT ALLOY SHIELD, overall_width: 0.245 INCHES MINIMUM AND 0.255 INCHES MAXIMUM IN, overall_length: 2.023 INCHES MINIMUM AND 2.133 INCHES MAXIMUM IN, special_features: USED ON THE AUGMENTOR SPRAY MANIFOLD, end_item_identification: F100-PW-100/200 AIRCRAFT ENGINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-390-2377, 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

4081007

NSN: 2840-01-390-2377
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 65065 — WOODWARD FST, INC (USA)

SPECIFICATIONS

diameter	25.760 INCHES NOMINAL IN
material	COBALT ALLOY SHIELD
overall_width	0.245 INCHES MINIMUM AND 0.255 INCHES MAXIMUM IN
overall_length	2.023 INCHES MINIMUM AND 2.133 INCHES MAXIMUM IN
special_features	USED ON THE AUGMENTOR SPRAY MANIFOLD
end_item_identification	F100-PW-100/200 AIRCRAFT ENGINE
engine_section_location	AFTERBURNER
criticality_code_justification	ABHP AND ABMZ AND CZBJ AND ABMK AND FEAT
material_document_and_classification	PWA1042 MFR REF SINGLE MATERIAL RESPONSE SHIELD
NSN	2840-01-390-2377

COMPONENT DIAGRAM

KEY FEATURES

•

CRITICALITY CODE JUSTIFICATION: ABHP AND ABMZ AND CZBJ AND ABMK AND FEAT

•

MATERIAL DOCUMENT AND CLASSIFICATION: PWA1042 MFR REF SINGLE MATERIAL RESPONSE SHIELD

•

DIAMETER: 25.760 INCHES NOMINAL IN

•

ENGINE SECTION LOCATION: AFTERBURNER

TECHNICAL CHARACTERISTICS

CRITICALITY CODE JUSTIFICATION	ABHP AND ABMZ AND CZBJ AND ABMK AND FEAT
MATERIAL DOCUMENT AND CLASSIFICATION	PWA1042 MFR REF SINGLE MATERIAL RESPONSE SHIELD
DIAMETER	25.760 INCHES NOMINAL IN
OVERALL LENGTH	2.023 INCHES MINIMUM AND 2.133 INCHES MAXIMUM IN
OVERALL WIDTH	0.245 INCHES MINIMUM AND 0.255 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	AFTERBURNER
SPECIAL FEATURES	USED ON THE AUGMENTOR SPRAY MANIFOLD
END ITEM IDENTIFICATION	F100-PW-100/200 AIRCRAFT ENGINE
MATERIAL	COBALT ALLOY SHIELD

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: Insurance item — stocked against contingency demandDemilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 4081007?

4081007 is a SHIELD,HEAT,AIRCRAFT GAS TURBINE.

What is the NSN for 4081007?

4081007 is cataloged in the U.S. Government catalog under NSN 2840-01-390-2377. This indicates validated use in U.S. government and defense supply chains.

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4081007 — SHIELD,HEAT,AIRCRAFT GAS TURBINE

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