23031176 — DISK,TURBINE,AIRCRAFT GAS TURBIN

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

23031176: DISK,TURBINE,AIRCRAFT GAS TURBIN.

DISK,TURBINE,AIRCRAFT GAS TURBIN. Key specifications include material: STEEL CORROSION RESISTING OVERALL, overall_length: 11.445 INCHES NOMINAL IN, hardness_rating: 38.0 ROCKWELL C MINIMUM AND 43.0 ROCKWELL C MAXIMUM OVERALL, fsc_application_data: TURBINE COMPRESSOR ROTOR, engine_section_location: COMPRESSOR, part_name_assigned_by_controlling_agency: DISK,GAS TURBINE ENGINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-343-3768, 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

23031176

NSN: 2840-01-343-3768
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 63005 — ROLLS-ROYCE CORPORATION (USA)

SPECIFICATIONS

material	STEEL CORROSION RESISTING OVERALL
stage_number	6
overall_length	11.445 INCHES NOMINAL IN
hardness_rating	38.0 ROCKWELL C MINIMUM AND 43.0 ROCKWELL C MAXIMUM OVERALL
fsc_application_data	TURBINE COMPRESSOR ROTOR
engine_section_location	COMPRESSOR
part_name_assigned_by_controlling_agency	DISK,GAS TURBINE ENGINE
NSN	2840-01-343-3768

COMPONENT DIAGRAM

KEY FEATURES

•

FSC APPLICATION DATA: TURBINE COMPRESSOR ROTOR

•

STAGE NUMBER: 6

•

HARDNESS RATING: 38.0 ROCKWELL C MINIMUM AND 43.0 ROCKWELL C MAXIMUM OVERALL

•

ENGINE SECTION LOCATION: COMPRESSOR

•

MATERIAL: STEEL CORROSION RESISTING OVERALL

TECHNICAL CHARACTERISTICS

FSC APPLICATION DATA	TURBINE COMPRESSOR ROTOR
STAGE NUMBER	6
HARDNESS RATING	38.0 ROCKWELL C MINIMUM AND 43.0 ROCKWELL C MAXIMUM OVERALL
OVERALL LENGTH	11.445 INCHES NOMINAL IN
ENGINE SECTION LOCATION	COMPRESSOR
SPECIAL FEATURES	INTERNAL INVOLUTE SPLINE DATA; NO. OF TEETH 364,PITCH 32/64,PRESSURE ANGLE 30 DEGREES,BASE CIRCLE DIA. 9.851 IN.,MINOR DIA. 11.344/11.347 IN.,PITCH DIA. 11.375 IN. BASIC,FORM DIA. 11.412 IN.,MAJOR DIA. 11.433 IN. MAX.,SPLINES IN ACCORDANCE WITH ANSI B92.1,DIMENSION BTWN TWO 0.054 DIA. PINS = 11.2945/11.2980 IN.,EXTERNAL INVOLUTE SPLINE DATA; NO. OF TEETH 374,PITCH 32/64,PRESSURE ANGLE 30 DEGREES,BASE CIRCLE DIA. 10.121 IN.,MINOR DIA.11.636 IN. MIN.,PITCH DIA. 11.6875 IN. BASIC,FORM DIA. 11.652 IN.,MAJOR DIA. 11.716/11.719 IN.,SPLINES IN ACCORDANCE WITH ANSI B92.1,DIMENSION OVER TWO 0.0540 DIA. PINS = 11.7696/11.7730 IN. IN
PART NAME ASSIGNED BY CONTROLLING AGENCY	DISK,GAS TURBINE ENGINE
MATERIAL	STEEL CORROSION RESISTING 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.

2840-00-000-0048 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

Demilitarization required — mutilation

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FREQUENTLY ASKED QUESTIONS

What is 23031176?

23031176 is a DISK,TURBINE,AIRCRAFT GAS TURBIN.

What is the NSN for 23031176?

23031176 is cataloged in the U.S. Government catalog under NSN 2840-01-343-3768. This indicates validated use in U.S. government and defense supply chains.

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23031176 — DISK,TURBINE,AIRCRAFT GAS TURBIN

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