9526M77 — SHROUD SEGMENT,TURBINE,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9526M77: SHROUD SEGMENT,TURBINE,AIRCRAFT.

SHROUD SEGMENT,TURBINE,AIRCRAFT. Key specifications include diameter: 37.530 INCHES NOMINAL IN, material: CHROMIUM AND IRON AND COBALT ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 1.901 INCHES MINIMUM AND 1.911 INCHES MAXIMUM IN, special_features: MAT IS HASTALLOY X; HONEYCOMBED; ITEM IS PREGROUND; SUPERSEDED P/N 9526M77G02 PER CID 808396, end_item_identification: F101 AIRCRAFT GAS TURBINE ENGINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-430-2595, 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

9526M77

NSN: 2840-01-430-2595
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

diameter	37.530 INCHES NOMINAL IN
material	CHROMIUM AND IRON AND COBALT ALLOY OVERALL
design_type	AXIAL COMPRESSOR
stage_number	2
overall_length	1.901 INCHES MINIMUM AND 1.911 INCHES MAXIMUM IN
special_features	MAT IS HASTALLOY X; HONEYCOMBED; ITEM IS PREGROUND; SUPERSEDED P/N 9526M77G02 PER CID 808396
end_item_identification	F101 AIRCRAFT GAS TURBINE ENGINE
engine_section_location	TURBINE
reference_data_and_literature	T.O. 2J-F101-4, FIG 61, IND 12
criticality_code_justification	MATT AND CZBJ AND CZCJ AND ABHP AND ABMZ
material_document_and_classification	AMS5838 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
NSN	2840-01-430-2595

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 2

•

DESIGN TYPE: AXIAL COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: MATT AND CZBJ AND CZCJ AND ABHP AND ABMZ

•

REFERENCE DATA AND LITERATURE: T.O. 2J-F101-4, FIG 61, IND 12

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS5838 ASSN STD SINGLE MATERIAL RESPONSE OVERALL

•

DIAMETER: 37.530 INCHES NOMINAL IN

•

ENGINE SECTION LOCATION: TURBINE

TECHNICAL CHARACTERISTICS

STAGE NUMBER	2
DESIGN TYPE	AXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATION	MATT AND CZBJ AND CZCJ AND ABHP AND ABMZ
REFERENCE DATA AND LITERATURE	T.O. 2J-F101-4, FIG 61, IND 12
MATERIAL DOCUMENT AND CLASSIFICATION	AMS5838 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
DIAMETER	37.530 INCHES NOMINAL IN
OVERALL LENGTH	1.901 INCHES MINIMUM AND 1.911 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	TURBINE
SPECIAL FEATURES	MAT IS HASTALLOY X; HONEYCOMBED; ITEM IS PREGROUND; SUPERSEDED P/N 9526M77G02 PER CID 808396
END ITEM IDENTIFICATION	F101 AIRCRAFT GAS TURBINE ENGINE

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: Terminal item — no further procurement; issued until stock is exhaustedDemilitarization required — mutilation

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FREQUENTLY ASKED QUESTIONS

What is 9526M77?

9526M77 is a SHROUD SEGMENT,TURBINE,AIRCRAFT.

What is the NSN for 9526M77?

9526M77 is cataloged in the U.S. Government catalog under NSN 2840-01-430-2595. This indicates validated use in U.S. government and defense supply chains.

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9526M77 — SHROUD SEGMENT,TURBINE,AIRCRAFT

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