9940M55P13 — DISK,COMPRESSOR,AIRCRAFT GAS TUR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9940M55P13: DISK,COMPRESSOR,AIRCRAFT GAS TUR.

DISK,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include diameter: 17.000 INCHES NOMINAL IN, material: TITANIUM OVERALL, design_type: AXIAL COMPRESSOR, overall_width: 1.180 INCHES MINIMUM AND 1.190 INCHES MAXIMUM IN, special_features: ORIGINAL NAME DISK,TURBINE,TURBINE ENGINE, material_thickness: 1.5000 INCHES NOMINAL IN. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-187-3182, 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

9940M55P13

NSN: 2840-01-187-3182
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

diameter	17.000 INCHES NOMINAL IN
material	TITANIUM OVERALL
design_type	AXIAL COMPRESSOR
stage_number	3
overall_width	1.180 INCHES MINIMUM AND 1.190 INCHES MAXIMUM IN
special_features	ORIGINAL NAME DISK,TURBINE,TURBINE ENGINE
material_thickness	1.5000 INCHES NOMINAL IN
end_item_identification	ACFT ENG F108
engine_section_location	COMPRESSOR
reference_data_and_literature	2J-F108-14 FIG 72-31-00-1 IND 120D
part_name_assigned_by_controlling_agency	DISK,COMPRESSOR ROTOR - STAGE 3
NSN	2840-01-187-3182

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 3

•

DESIGN TYPE: AXIAL COMPRESSOR

•

REFERENCE DATA AND LITERATURE: 2J-F108-14 FIG 72-31-00-1 IND 120D

•

DIAMETER: 17.000 INCHES NOMINAL IN

•

ENGINE SECTION LOCATION: COMPRESSOR

•

MATERIAL THICKNESS: 1.5000 INCHES NOMINAL IN

TECHNICAL CHARACTERISTICS

STAGE NUMBER	3
DESIGN TYPE	AXIAL COMPRESSOR
REFERENCE DATA AND LITERATURE	2J-F108-14 FIG 72-31-00-1 IND 120D
DIAMETER	17.000 INCHES NOMINAL IN
OVERALL WIDTH	1.180 INCHES MINIMUM AND 1.190 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	COMPRESSOR
MATERIAL THICKNESS	1.5000 INCHES NOMINAL IN
SPECIAL FEATURES	ORIGINAL NAME DISK,TURBINE,TURBINE ENGINE
PART NAME ASSIGNED BY CONTROLLING AGENCY	DISK,COMPRESSOR ROTOR - STAGE 3
END ITEM IDENTIFICATION	ACFT ENG F108

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 3

1590M59P01Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

9940M55P08-108Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

9940M55P18Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 9940M55P13?

9940M55P13 is a DISK,COMPRESSOR,AIRCRAFT GAS TUR.

What parts can replace 9940M55P13?

There are 3 known substitutes for 9940M55P13: 1590M59P01, 9940M55P08-108, 9940M55P18. Substitute compatibility should be verified for your specific system.

What is the NSN for 9940M55P13?

9940M55P13 is cataloged in the U.S. Government catalog under NSN 2840-01-187-3182. This indicates validated use in U.S. government and defense supply chains.

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9940M55P13 — DISK,COMPRESSOR,AIRCRAFT GAS TUR

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