4062762 — CASE,TURBINE,AIRCRAFT GAS TURBIN

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

4062762: CASE,TURBINE,AIRCRAFT GAS TURBIN.

CASE,TURBINE,AIRCRAFT GAS TURBIN. Key specifications include diameter: 16.841 INCHES MINIMUM AND 16.843 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, overall_length: 0.610 INCHES MINIMUM AND 0.620 INCHES MAXIMUM IN, special_features: WAS CASE,TURBINE ROTOR,TURBINE ENGINE; 12TH STAGE, end_item_identification: ACFT ENG F100-PW-100/200, engine_section_location: TURBINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-215-7607, 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

4062762

NSN: 2840-01-215-7607
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 77445 — RTX CORPORATION DBA PRATT & WHITNEY DIV PRATT &WHITNEY (USA)

SPECIFICATIONS

diameter	16.841 INCHES MINIMUM AND 16.843 INCHES MAXIMUM IN
material	NICKEL ALLOY OVERALL
overall_length	0.610 INCHES MINIMUM AND 0.620 INCHES MAXIMUM IN
special_features	WAS CASE,TURBINE ROTOR,TURBINE ENGINE; 12TH STAGE
end_item_identification	ACFT ENG F100-PW-100/200
engine_section_location	TURBINE
criticality_code_justification	AGAV
material_document_and_classification	AMS5706 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
NSN	2840-01-215-7607

COMPONENT DIAGRAM

KEY FEATURES

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS5706 ASSN STD SINGLE MATERIAL RESPONSE OVERALL

•

DIAMETER: 16.841 INCHES MINIMUM AND 16.843 INCHES MAXIMUM IN

•

ENGINE SECTION LOCATION: TURBINE

•

MATERIAL: NICKEL ALLOY OVERALL

TECHNICAL CHARACTERISTICS

CRITICALITY CODE JUSTIFICATION	AGAV
MATERIAL DOCUMENT AND CLASSIFICATION	AMS5706 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
DIAMETER	16.841 INCHES MINIMUM AND 16.843 INCHES MAXIMUM IN
OVERALL LENGTH	0.610 INCHES MINIMUM AND 0.620 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	TURBINE
SPECIAL FEATURES	WAS CASE,TURBINE ROTOR,TURBINE ENGINE; 12TH STAGE
END ITEM IDENTIFICATION	ACFT ENG F100-PW-100/200
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.

2840-00-000-0048 2840-00-000-0049 2840-00-001-1741 2840-00-001-1743 2840-00-001-2117 2840-00-001-2284 2840-00-001-3922 2840-00-001-4903

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)

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FREQUENTLY ASKED QUESTIONS

What is 4062762?

4062762 is a CASE,TURBINE,AIRCRAFT GAS TURBIN.

What is the NSN for 4062762?

4062762 is cataloged in the U.S. Government catalog under NSN 2840-01-215-7607. This indicates validated use in U.S. government and defense supply chains.

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4062762 — CASE,TURBINE,AIRCRAFT GAS TURBIN

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