1668M19P01 — NOZZLE,TURBINE,AIRCRAFT GAS TURB

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

1668M19P01: NOZZLE,TURBINE,AIRCRAFT GAS TURB.

NOZZLE,TURBINE,AIRCRAFT GAS TURB. Key specifications include material: NICKEL ALLOY OVERALL, overall_width: 0.166 INCHES MINIMUM AND 0.176 INCHES MAXIMUM IN, material_thickness: 0.0035 INCHES MINIMUM AND 0.0055 INCHES MAXIMUM IN, engine_section_location: TURBINE, material_document_and_classification: AMS5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL, part_name_assigned_by_controlling_agency: NOZZLE,TURBINE,TURBINE ENGINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-348-4984, 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

1668M19P01

NSN: 2840-01-348-4984
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

material	NICKEL ALLOY OVERALL
overall_width	0.166 INCHES MINIMUM AND 0.176 INCHES MAXIMUM IN
material_thickness	0.0035 INCHES MINIMUM AND 0.0055 INCHES MAXIMUM IN
engine_section_location	TURBINE
material_document_and_classification	AMS5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
part_name_assigned_by_controlling_agency	NOZZLE,TURBINE,TURBINE ENGINE
NSN	2840-01-348-4984

COMPONENT DIAGRAM

KEY FEATURES

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL

•

ENGINE SECTION LOCATION: TURBINE

•

MATERIAL THICKNESS: 0.0035 INCHES MINIMUM AND 0.0055 INCHES MAXIMUM IN

•

MATERIAL: NICKEL ALLOY OVERALL

TECHNICAL CHARACTERISTICS

MATERIAL DOCUMENT AND CLASSIFICATION	AMS5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
OVERALL WIDTH	0.166 INCHES MINIMUM AND 0.176 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	TURBINE
MATERIAL THICKNESS	0.0035 INCHES MINIMUM AND 0.0055 INCHES MAXIMUM IN
PART NAME ASSIGNED BY CONTROLLING AGENCY	NOZZLE,TURBINE,TURBINE 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.

2840-00-000-0048 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 — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 1668M19P01?

1668M19P01 is a NOZZLE,TURBINE,AIRCRAFT GAS TURB.

What is the NSN for 1668M19P01?

1668M19P01 is cataloged in the U.S. Government catalog under NSN 2840-01-348-4984. This indicates validated use in U.S. government and defense supply chains.

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1668M19P01 — NOZZLE,TURBINE,AIRCRAFT GAS TURB

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