9512M40P22 — SEAL,METALLIC,AIRCRAFT GAS TURBI

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9512M40P22: SEAL,METALLIC,AIRCRAFT GAS TURBI.

SEAL,METALLIC,AIRCRAFT GAS TURBI. Key specifications include diameter: 21.480 INCHES MINIMUM AND 21.500 INCHES MAXIMUM IN, material: CHROMIUM ALLOY AND COBALT ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 0.280 INCHES MINIMUM AND 0.290 INCHES MAXIMUM IN, special_features: HONEYCOMB; STATIONARY INNER AND OUTER, material_thickness: 0.340 INCHES MINIMUM AND 0.360 INCHES MAXIMUM IN. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-382-3653, 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

9512M40P22

NSN: 2840-01-382-3653
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 58828 — CFM INTERNATIONAL INC DBA CFM INTERNATIONAL (USA)

SPECIFICATIONS

diameter	21.480 INCHES MINIMUM AND 21.500 INCHES MAXIMUM IN
material	CHROMIUM ALLOY AND COBALT ALLOY OVERALL
design_type	AXIAL COMPRESSOR
overall_length	0.280 INCHES MINIMUM AND 0.290 INCHES MAXIMUM IN
special_features	HONEYCOMB; STATIONARY INNER AND OUTER
material_thickness	0.340 INCHES MINIMUM AND 0.360 INCHES MAXIMUM IN
end_item_identification	F110-GE-100 AIRCRAFT ENG
engine_section_location	HIGH PRESSURE TURBINE
criticality_code_justification	ABMZ AND ABHP AND ABPX AND APGF AND CZBJ
material_document_and_classification	AMS5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
NSN	2840-01-382-3653

COMPONENT DIAGRAM

KEY FEATURES

•

DESIGN TYPE: AXIAL COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: ABMZ AND ABHP AND ABPX AND APGF AND CZBJ

•

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

•

DIAMETER: 21.480 INCHES MINIMUM AND 21.500 INCHES MAXIMUM IN

•

ENGINE SECTION LOCATION: HIGH PRESSURE TURBINE

•

MATERIAL THICKNESS: 0.340 INCHES MINIMUM AND 0.360 INCHES MAXIMUM IN

TECHNICAL CHARACTERISTICS

DESIGN TYPE	AXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATION	ABMZ AND ABHP AND ABPX AND APGF AND CZBJ
MATERIAL DOCUMENT AND CLASSIFICATION	AMS5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
DIAMETER	21.480 INCHES MINIMUM AND 21.500 INCHES MAXIMUM IN
OVERALL LENGTH	0.280 INCHES MINIMUM AND 0.290 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	HIGH PRESSURE TURBINE
MATERIAL THICKNESS	0.340 INCHES MINIMUM AND 0.360 INCHES MAXIMUM IN
SPECIAL FEATURES	HONEYCOMB; STATIONARY INNER AND OUTER
END ITEM IDENTIFICATION	F110-GE-100 AIRCRAFT ENG
MATERIAL	CHROMIUM ALLOY AND COBALT ALLOY OVERALL

SUBSTITUTES & CROSS-REFERENCES 2

9512M40Reference document

Same NSN cross-reference

Reference document — Drawing number reference only

9512M40P28Reference document

Same NSN cross-reference

Reference document — Secondary reference

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Terminal item — no further procurement; issued until stock is exhaustedNo demilitarization required

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FREQUENTLY ASKED QUESTIONS

What is 9512M40P22?

9512M40P22 is a SEAL,METALLIC,AIRCRAFT GAS TURBI.

What parts can replace 9512M40P22?

There are 2 known substitutes for 9512M40P22: 9512M40, 9512M40P28. Substitute compatibility should be verified for your specific system.

What is the NSN for 9512M40P22?

9512M40P22 is cataloged in the U.S. Government catalog under NSN 2840-01-382-3653. This indicates validated use in U.S. government and defense supply chains.

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9512M40P22 — SEAL,METALLIC,AIRCRAFT GAS TURBI

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