2840PL0696921 — PLATE,COMPONENT MOUNTING,AIRCRAF

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

2840PL0696921: PLATE,COMPONENT MOUNTING,AIRCRAF.

PLATE,COMPONENT MOUNTING,AIRCRAF. Key specifications include diameter: 3.855 INCHES NOMINAL IN, material: TITANIUM ALLOY OVERALL, overall_width: 0.168 INCHES MINIMUM AND 0.198 INCHES MAXIMUM IN, overall_length: 3.850 INCHES MINIMUM AND 3.860 INCHES MAXIMUM IN, end_item_identification: F100-PW-100/-200/-220 AIRCRAFT ENGINES, engine_section_location: COMBUSTION CHAMBER. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-324-0274, 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

2840PL0696921

NSN: 2840-01-324-0274
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 9009H — JEDNOLITY INDEKS MATERIALOWY - UNIFORM MATERIAL INDEX (POL)

SPECIFICATIONS

diameter	3.855 INCHES NOMINAL IN
material	TITANIUM ALLOY OVERALL
overall_width	0.168 INCHES MINIMUM AND 0.198 INCHES MAXIMUM IN
overall_length	3.850 INCHES MINIMUM AND 3.860 INCHES MAXIMUM IN
end_item_identification	F100-PW-100/-200/-220 AIRCRAFT ENGINES
engine_section_location	COMBUSTION CHAMBER
criticality_code_justification	AGAV
material_document_and_classification	AMS4928 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
NSN	2840-01-324-0274

COMPONENT DIAGRAM

KEY FEATURES

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS4928 ASSN STD SINGLE MATERIAL RESPONSE OVERALL

•

DIAMETER: 3.855 INCHES NOMINAL IN

•

ENGINE SECTION LOCATION: COMBUSTION CHAMBER

•

MATERIAL: TITANIUM ALLOY OVERALL

TECHNICAL CHARACTERISTICS

CRITICALITY CODE JUSTIFICATION	AGAV
MATERIAL DOCUMENT AND CLASSIFICATION	AMS4928 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
DIAMETER	3.855 INCHES NOMINAL IN
OVERALL LENGTH	3.850 INCHES MINIMUM AND 3.860 INCHES MAXIMUM IN
OVERALL WIDTH	0.168 INCHES MINIMUM AND 0.198 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	COMBUSTION CHAMBER
END ITEM IDENTIFICATION	F100-PW-100/-200/-220 AIRCRAFT ENGINES
MATERIAL	TITANIUM 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 1

4076047Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

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 2840PL0696921?

2840PL0696921 is a PLATE,COMPONENT MOUNTING,AIRCRAF.

What parts can replace 2840PL0696921?

There is 1 known substitute for 2840PL0696921: 4076047. Substitute compatibility should be verified for your specific system.

What is the NSN for 2840PL0696921?

2840PL0696921 is cataloged in the U.S. Government catalog under NSN 2840-01-324-0274. This indicates validated use in U.S. government and defense supply chains.

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2840PL0696921 — PLATE,COMPONENT MOUNTING,AIRCRAF

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