9662M43G02 — SHROUD SEGMENT,TURBINE,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9662M43G02: SHROUD SEGMENT,TURBINE,AIRCRAFT.

SHROUD SEGMENT,TURBINE,AIRCRAFT. Key specifications include diameter: 16.724 INCHES MINIMUM AND 16.736 INCHES MAXIMUM IN, material: ALUMINUM ALLOY OVERALL, design_type: COMPRESSOR, overall_length: 1.493 INCHES MINIMUM AND 1.506 INCHES MAXIMUM IN, special_features: WAS SHROUD,COMPRESSOR, end_item_identification: ACFT ENG TF-39. This part is cataloged in the U.S.

Government catalog under NSN 2840-00-110-8927, 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

9662M43G02

NSN: 2840-00-110-8927
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

diameter	16.724 INCHES MINIMUM AND 16.736 INCHES MAXIMUM IN
material	ALUMINUM ALLOY OVERALL
design_type	COMPRESSOR
stage_number	2
overall_length	1.493 INCHES MINIMUM AND 1.506 INCHES MAXIMUM IN
special_features	WAS SHROUD,COMPRESSOR
end_item_identification	ACFT ENG TF-39
engine_section_location	COMPRESSOR
criticality_code_justification	AGAV
material_document_and_classification	AMS4127 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
NSN	2840-00-110-8927

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 2

•

DESIGN TYPE: COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS4127 ASSN STD SINGLE MATERIAL RESPONSE OVERALL

•

DIAMETER: 16.724 INCHES MINIMUM AND 16.736 INCHES MAXIMUM IN

•

ENGINE SECTION LOCATION: COMPRESSOR

TECHNICAL CHARACTERISTICS

STAGE NUMBER	2
DESIGN TYPE	COMPRESSOR
CRITICALITY CODE JUSTIFICATION	AGAV
MATERIAL DOCUMENT AND CLASSIFICATION	AMS4127 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
DIAMETER	16.724 INCHES MINIMUM AND 16.736 INCHES MAXIMUM IN
OVERALL LENGTH	1.493 INCHES MINIMUM AND 1.506 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	COMPRESSOR
SPECIAL FEATURES	WAS SHROUD,COMPRESSOR
END ITEM IDENTIFICATION	ACFT ENG TF-39
MATERIAL	ALUMINUM 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 2

9662M43G03Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

2840PL0832735Reference document

Same NSN cross-reference

Reference document — Informative reference only

LIFECYCLE

NSN statusActive· U.S. Government catalog

No demilitarization required

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FREQUENTLY ASKED QUESTIONS

What is 9662M43G02?

9662M43G02 is a SHROUD SEGMENT,TURBINE,AIRCRAFT.

What parts can replace 9662M43G02?

There are 2 known substitutes for 9662M43G02: 9662M43G03, 2840PL0832735. Substitute compatibility should be verified for your specific system.

What is the NSN for 9662M43G02?

9662M43G02 is cataloged in the U.S. Government catalog under NSN 2840-00-110-8927. This indicates validated use in U.S. government and defense supply chains.

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9662M43G02 — SHROUD SEGMENT,TURBINE,AIRCRAFT

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