9523M21P01 — SHROUD SEGMENT,TURBINE,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9523M21P01: SHROUD SEGMENT,TURBINE,AIRCRAFT.

SHROUD SEGMENT,TURBINE,AIRCRAFT. Key specifications include material: NICKEL ALLOY OUTER CASE, design_type: COMPRESSOR, overall_length: 0.254 INCHES MINIMUM AND 0.375 INCHES MAXIMUM IN, special_features: T.O. 2J-F108-4; HIGH PRESSURE TURBINE SHROUD AND 1ST STAGE L.P.

TURBINE NOZZLE; U-SHAPED CLIPS, material_thickness: 0.077 INCHES MINIMUM AND 0.085 INCHES MAXIMUM IN, end_item_identification: B1B ACFT/F108 ACFT ENGINE. This part is cataloged in the U.S. Government catalog under NSN 2840-01-175-3023, 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

9523M21P01

NSN: 2840-01-175-3023
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

material	NICKEL ALLOY OUTER CASE
design_type	COMPRESSOR
stage_number	1
overall_length	0.254 INCHES MINIMUM AND 0.375 INCHES MAXIMUM IN
special_features	T.O. 2J-F108-4; HIGH PRESSURE TURBINE SHROUD AND 1ST STAGE L.P. TURBINE NOZZLE; U-SHAPED CLIPS
material_thickness	0.077 INCHES MINIMUM AND 0.085 INCHES MAXIMUM IN
end_item_identification	B1B ACFT/F108 ACFT ENGINE
engine_section_location	HIGH PRESSURE TURBINE
NSN	2840-01-175-3023

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 1

•

DESIGN TYPE: COMPRESSOR

•

ENGINE SECTION LOCATION: HIGH PRESSURE TURBINE

•

MATERIAL THICKNESS: 0.077 INCHES MINIMUM AND 0.085 INCHES MAXIMUM IN

•

MATERIAL: NICKEL ALLOY OUTER CASE

TECHNICAL CHARACTERISTICS

STAGE NUMBER	1
DESIGN TYPE	COMPRESSOR
OVERALL LENGTH	0.254 INCHES MINIMUM AND 0.375 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	HIGH PRESSURE TURBINE
MATERIAL THICKNESS	0.077 INCHES MINIMUM AND 0.085 INCHES MAXIMUM IN
SPECIAL FEATURES	T.O. 2J-F108-4; HIGH PRESSURE TURBINE SHROUD AND 1ST STAGE L.P. TURBINE NOZZLE; U-SHAPED CLIPS
END ITEM IDENTIFICATION	B1B ACFT/F108 ACFT ENGINE
MATERIAL	NICKEL ALLOY OUTER CASE

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 1

9532M21P01Reference document

Same NSN cross-reference

Reference document — Secondary reference

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 9523M21P01?

9523M21P01 is a SHROUD SEGMENT,TURBINE,AIRCRAFT.

What parts can replace 9523M21P01?

There is 1 known substitute for 9523M21P01: 9532M21P01. Substitute compatibility should be verified for your specific system.

What is the NSN for 9523M21P01?

9523M21P01 is cataloged in the U.S. Government catalog under NSN 2840-01-175-3023. This indicates validated use in U.S. government and defense supply chains.

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9523M21P01 — SHROUD SEGMENT,TURBINE,AIRCRAFT

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