2840PL0696883 — PLATE,COMPONENT MOUNTING,AIRCRAF

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

2840PL0696883: PLATE,COMPONENT MOUNTING,AIRCRAF.

PLATE,COMPONENT MOUNTING,AIRCRAF. Key specifications include diameter: 2.882 INCHES NOMINAL IN, material: TITANIUM ALLOY OVERALL, overall_width: 0.194 INCHES MINIMUM AND 0.240 INCHES MAXIMUM IN, overall_length: 3.370 INCHES MINIMUM AND 3.390 INCHES MAXIMUM IN, special_features: GOES ON FAN DUCT; 3 MTG HOLES 0.276-0.286; BORE HOLE DIA. 1.590-1.610, end_item_identification: F100PW0229 ACFT ENGINE.

This part is cataloged in the U.S. Government catalog under NSN 2840-01-320-5349, 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

2840PL0696883

NSN: 2840-01-320-5349
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 9009H — JEDNOLITY INDEKS MATERIALOWY - UNIFORM MATERIAL INDEX (POL)

SPECIFICATIONS

diameter	2.882 INCHES NOMINAL IN
material	TITANIUM ALLOY OVERALL
overall_width	0.194 INCHES MINIMUM AND 0.240 INCHES MAXIMUM IN
overall_length	3.370 INCHES MINIMUM AND 3.390 INCHES MAXIMUM IN
special_features	GOES ON FAN DUCT; 3 MTG HOLES 0.276-0.286; BORE HOLE DIA. 1.590-1.610
end_item_identification	F100PW0229 ACFT ENGINE
engine_section_location	TURBINE
criticality_code_justification	AGAV
material_document_and_classification	AMS4911 ASSN STD 1ST MATERIAL RESPONSE OR AMS4928 ASSN STD 2ND MATERIAL RESPONSE OVERALL
NSN	2840-01-320-5349

COMPONENT DIAGRAM

KEY FEATURES

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS4911 ASSN STD 1ST MATERIAL RESPONSE OR AMS4928 ASSN STD 2ND MATERIAL RESPONSE OVERALL

•

DIAMETER: 2.882 INCHES NOMINAL IN

•

ENGINE SECTION LOCATION: TURBINE

TECHNICAL CHARACTERISTICS

CRITICALITY CODE JUSTIFICATION	AGAV
MATERIAL DOCUMENT AND CLASSIFICATION	AMS4911 ASSN STD 1ST MATERIAL RESPONSE OR AMS4928 ASSN STD 2ND MATERIAL RESPONSE OVERALL
DIAMETER	2.882 INCHES NOMINAL IN
OVERALL LENGTH	3.370 INCHES MINIMUM AND 3.390 INCHES MAXIMUM IN
OVERALL WIDTH	0.194 INCHES MINIMUM AND 0.240 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	TURBINE
SPECIAL FEATURES	GOES ON FAN DUCT; 3 MTG HOLES 0.276-0.286; BORE HOLE DIA. 1.590-1.610
END ITEM IDENTIFICATION	F100PW0229 ACFT ENGINE
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

4069559Same 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 2840PL0696883?

2840PL0696883 is a PLATE,COMPONENT MOUNTING,AIRCRAF.

What parts can replace 2840PL0696883?

There is 1 known substitute for 2840PL0696883: 4069559. Substitute compatibility should be verified for your specific system.

What is the NSN for 2840PL0696883?

2840PL0696883 is cataloged in the U.S. Government catalog under NSN 2840-01-320-5349. This indicates validated use in U.S. government and defense supply chains.

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2840PL0696883 — PLATE,COMPONENT MOUNTING,AIRCRAF

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