4062773 — PLATE,COMPONENT MOUNTING,AIRCRAF

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

4062773: PLATE,COMPONENT MOUNTING,AIRCRAF.

PLATE,COMPONENT MOUNTING,AIRCRAF. Key specifications include material: NICKEL ALLOY OVERALL, overall_width: 0.240 INCHES MINIMUM AND 0.260 INCHES MAXIMUM IN, overall_height: 0.285 INCHES MINIMUM AND 0.325 INCHES MAXIMUM IN, overall_length: 0.690 INCHES MINIMUM AND 0.710 INCHES MAXIMUM IN, special_features: MATL IS COBALT; T.O. 2J-F100-54, end_item_identification: F100PW0229 AIRCRAFT ENGINE.

This part is cataloged in the U.S. Government catalog under NSN 2840-01-323-9770, 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

4062773

NSN: 2840-01-323-9770
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 77445 — RTX CORPORATION DBA PRATT & WHITNEY DIV PRATT &WHITNEY (USA)

SPECIFICATIONS

material	NICKEL ALLOY OVERALL
overall_width	0.240 INCHES MINIMUM AND 0.260 INCHES MAXIMUM IN
overall_height	0.285 INCHES MINIMUM AND 0.325 INCHES MAXIMUM IN
overall_length	0.690 INCHES MINIMUM AND 0.710 INCHES MAXIMUM IN
special_features	MATL IS COBALT; T.O. 2J-F100-54
end_item_identification	F100PW0229 AIRCRAFT ENGINE
engine_section_location	COMBUSTION CHAMBER
criticality_code_justification	AGAV
material_document_and_classification	AMS5772 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
NSN	2840-01-323-9770

COMPONENT DIAGRAM

KEY FEATURES

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS5772 ASSN STD SINGLE MATERIAL RESPONSE OVERALL

•

ENGINE SECTION LOCATION: COMBUSTION CHAMBER

TECHNICAL CHARACTERISTICS

OVERALL HEIGHT	0.285 INCHES MINIMUM AND 0.325 INCHES MAXIMUM IN
CRITICALITY CODE JUSTIFICATION	AGAV
MATERIAL DOCUMENT AND CLASSIFICATION	AMS5772 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
OVERALL LENGTH	0.690 INCHES MINIMUM AND 0.710 INCHES MAXIMUM IN
OVERALL WIDTH	0.240 INCHES MINIMUM AND 0.260 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	COMBUSTION CHAMBER
SPECIAL FEATURES	MATL IS COBALT; T.O. 2J-F100-54
END ITEM IDENTIFICATION	F100PW0229 AIRCRAFT ENGINE
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 1

4062773CReference document

Same NSN cross-reference

Reference document — Drawing number reference only

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 4062773?

4062773 is a PLATE,COMPONENT MOUNTING,AIRCRAF.

What parts can replace 4062773?

There is 1 known substitute for 4062773: 4062773C. Substitute compatibility should be verified for your specific system.

What is the NSN for 4062773?

4062773 is cataloged in the U.S. Government catalog under NSN 2840-01-323-9770. This indicates validated use in U.S. government and defense supply chains.

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4062773 — PLATE,COMPONENT MOUNTING,AIRCRAF

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