4076722 — PLATE,COMPONENT MOUNTING,AIRCRAF

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

4076722: PLATE,COMPONENT MOUNTING,AIRCRAF.

PLATE,COMPONENT MOUNTING,AIRCRAF. Key specifications include material: NICKEL ALLOY OVERALL, overall_width: 1.000 INCHES NOMINAL IN, overall_length: 4.330 INCHES NOMINAL IN, hardness_rating: 34.0 ROCKWELL C MINIMUM AND 44.0 ROCKWELL C MAXIMUM OVERALL, special_features: 8 MTG HOLES 0.078-0.109; ACTS AS A BRACE ON THE COMBUSTION CHAMBER, end_item_identification: F100PW0229 AIRCRAFT ENGINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-323-4308, 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

4076722

NSN: 2840-01-323-4308
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	1.000 INCHES NOMINAL IN
overall_length	4.330 INCHES NOMINAL IN
hardness_rating	34.0 ROCKWELL C MINIMUM AND 44.0 ROCKWELL C MAXIMUM OVERALL
special_features	8 MTG HOLES 0.078-0.109; ACTS AS A BRACE ON THE COMBUSTION CHAMBER
end_item_identification	F100PW0229 AIRCRAFT ENGINE
engine_section_location	COMBUSTION CHAMBER
criticality_code_justification	AGAV
material_document_and_classification	AMS5540 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
NSN	2840-01-323-4308

COMPONENT DIAGRAM

KEY FEATURES

•

HARDNESS RATING: 34.0 ROCKWELL C MINIMUM AND 44.0 ROCKWELL C MAXIMUM OVERALL

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS5540 ASSN STD SINGLE MATERIAL RESPONSE OVERALL

•

ENGINE SECTION LOCATION: COMBUSTION CHAMBER

TECHNICAL CHARACTERISTICS

HARDNESS RATING	34.0 ROCKWELL C MINIMUM AND 44.0 ROCKWELL C MAXIMUM OVERALL
CRITICALITY CODE JUSTIFICATION	AGAV
MATERIAL DOCUMENT AND CLASSIFICATION	AMS5540 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
OVERALL LENGTH	4.330 INCHES NOMINAL IN
OVERALL WIDTH	1.000 INCHES NOMINAL IN
ENGINE SECTION LOCATION	COMBUSTION CHAMBER
SPECIAL FEATURES	8 MTG HOLES 0.078-0.109; ACTS AS A BRACE ON THE COMBUSTION CHAMBER
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

No substitute or cross-reference records for this part.

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Normally procured from the manufacturer (OEM)Demilitarization required — critical (Q)

Ready to buy 4076722?

Compare prices from verified sellers on eBay

Buy on eBay →

As an eBay Partner, PartsTable may earn a commission. Your price is not affected.

FREQUENTLY ASKED QUESTIONS

What is 4076722?

4076722 is a PLATE,COMPONENT MOUNTING,AIRCRAF.

What is the NSN for 4076722?

4076722 is cataloged in the U.S. Government catalog under NSN 2840-01-323-4308. This indicates validated use in U.S. government and defense supply chains.

Community Feedback

4076722 — PLATE,COMPONENT MOUNTING,AIRCRAF

Request a Quote — 4076722