4067357 — HUB,COMPRESSOR,AIRCRAFT GAS TURB

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

4067357: HUB,COMPRESSOR,AIRCRAFT GAS TURB.

HUB,COMPRESSOR,AIRCRAFT GAS TURB. Key specifications include diameter: 7.162 INCHES MINIMUM AND 7.166 INCHES MAXIMUM IN, material: NICKEL ALLOY HUB, design_type: COMPRESSOR, overall_length: 4.004 INCHES MINIMUM AND 4.014 INCHES MAXIMUM IN, end_item_identification: F100-PW-100 AIRCRAFT ENGINE, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-216-0526, 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

4067357

NSN: 2840-01-216-0526
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 77445 — RTX CORPORATION DBA PRATT & WHITNEY DIV PRATT &WHITNEY (USA)

SPECIFICATIONS

diameter	7.162 INCHES MINIMUM AND 7.166 INCHES MAXIMUM IN
material	NICKEL ALLOY HUB
design_type	COMPRESSOR
stage_number	2
overall_length	4.004 INCHES MINIMUM AND 4.014 INCHES MAXIMUM IN
special_features	INTL INVOLUTE SPLINE DATA: TEETH 140; PRESSURE ANGLE 30 DEG.; T.O. 2J-F100-4, FIGURE 115, INDEX 3; USED ON THE REAR COMPRESSOR DRIVE; REIDENTIFIED FROM P/N 4047224
end_item_identification	F100-PW-100 AIRCRAFT ENGINE
engine_section_location	COMPRESSOR
criticality_code_justification	APGF AND CZBJ AND CZCJ AND ABHP AND ABMZ
material_document_and_classification	PWA1022 MFR REF SINGLE MATERIAL RESPONSE HUB
part_name_assigned_by_controlling_agency	ORIG NAME NUT,DRIVE SHAFT
NSN	2840-01-216-0526

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 2

•

DESIGN TYPE: COMPRESSOR

•

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

•

MATERIAL DOCUMENT AND CLASSIFICATION: PWA1022 MFR REF SINGLE MATERIAL RESPONSE HUB

•

DIAMETER: 7.162 INCHES MINIMUM AND 7.166 INCHES MAXIMUM IN

•

ENGINE SECTION LOCATION: COMPRESSOR

TECHNICAL CHARACTERISTICS

STAGE NUMBER	2
DESIGN TYPE	COMPRESSOR
CRITICALITY CODE JUSTIFICATION	APGF AND CZBJ AND CZCJ AND ABHP AND ABMZ
MATERIAL DOCUMENT AND CLASSIFICATION	PWA1022 MFR REF SINGLE MATERIAL RESPONSE HUB
DIAMETER	7.162 INCHES MINIMUM AND 7.166 INCHES MAXIMUM IN
OVERALL LENGTH	4.004 INCHES MINIMUM AND 4.014 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	COMPRESSOR
SPECIAL FEATURES	INTL INVOLUTE SPLINE DATA: TEETH 140; PRESSURE ANGLE 30 DEG.; T.O. 2J-F100-4, FIGURE 115, INDEX 3; USED ON THE REAR COMPRESSOR DRIVE; REIDENTIFIED FROM P/N 4047224
PART NAME ASSIGNED BY CONTROLLING AGENCY	ORIG NAME NUT,DRIVE SHAFT
END ITEM IDENTIFICATION	F100-PW-100 AIRCRAFT 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 + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 4067357?

4067357 is a HUB,COMPRESSOR,AIRCRAFT GAS TURB.

What is the NSN for 4067357?

4067357 is cataloged in the U.S. Government catalog under NSN 2840-01-216-0526. This indicates validated use in U.S. government and defense supply chains.

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4067357 — HUB,COMPRESSOR,AIRCRAFT GAS TURB

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