9993M67G02 — SUPPORT,TURBINE NOZZLE,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9993M67G02: SUPPORT,TURBINE NOZZLE,AIRCRAFT.

SUPPORT,TURBINE NOZZLE,AIRCRAFT. Key specifications include material: NICKEL ALLOY, overall_length: 1.897 INCHES NOMINAL IN, inside_diameter: 20.586 INCHES NOMINAL IN, outside_diameter: 24.860 INCHES NOMINAL IN, special_features: MATERIAL INCOLOY 903, mounting_hole_diameter: 0.481 INCHES MINIMUM AND 0.490 INCHES MAXIMUM IN. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-187-8178, 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

9993M67G02

NSN: 2840-01-187-8178
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

material	NICKEL ALLOY
overall_length	1.897 INCHES NOMINAL IN
inside_diameter	20.586 INCHES NOMINAL IN
outside_diameter	24.860 INCHES NOMINAL IN
special_features	MATERIAL INCOLOY 903
mounting_hole_diameter	0.481 INCHES MINIMUM AND 0.490 INCHES MAXIMUM IN
mounting_hole_quantity	23
end_item_identification	ACFT ENG F108
reference_data_and_literature	T.O. 2J-F108-14, FIG. 72-41-00-1, IND. 30
criticality_code_justification	AGAV
part_name_assigned_by_controlling_agency	SUPPORT-SEAL OUTER HPT STTR.
NSN	2840-01-187-8178

COMPONENT DIAGRAM

KEY FEATURES

•

MOUNTING HOLE QUANTITY: 23

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

REFERENCE DATA AND LITERATURE: T.O. 2J-F108-14, FIG. 72-41-00-1, IND. 30

•

MOUNTING HOLE DIAMETER: 0.481 INCHES MINIMUM AND 0.490 INCHES MAXIMUM IN

•

OUTSIDE DIAMETER: 24.860 INCHES NOMINAL IN

•

INSIDE DIAMETER: 20.586 INCHES NOMINAL IN

TECHNICAL CHARACTERISTICS

MOUNTING HOLE QUANTITY	23
CRITICALITY CODE JUSTIFICATION	AGAV
REFERENCE DATA AND LITERATURE	T.O. 2J-F108-14, FIG. 72-41-00-1, IND. 30
MOUNTING HOLE DIAMETER	0.481 INCHES MINIMUM AND 0.490 INCHES MAXIMUM IN
OVERALL LENGTH	1.897 INCHES NOMINAL IN
OUTSIDE DIAMETER	24.860 INCHES NOMINAL IN
INSIDE DIAMETER	20.586 INCHES NOMINAL IN
SPECIAL FEATURES	MATERIAL INCOLOY 903
PART NAME ASSIGNED BY CONTROLLING AGENCY	SUPPORT-SEAL OUTER HPT STTR.
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 1

1285M66G02Reference 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 exhaustedDemilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 9993M67G02?

9993M67G02 is a SUPPORT,TURBINE NOZZLE,AIRCRAFT.

What parts can replace 9993M67G02?

There is 1 known substitute for 9993M67G02: 1285M66G02. Substitute compatibility should be verified for your specific system.

What is the NSN for 9993M67G02?

9993M67G02 is cataloged in the U.S. Government catalog under NSN 2840-01-187-8178. This indicates validated use in U.S. government and defense supply chains.

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9993M67G02 — SUPPORT,TURBINE NOZZLE,AIRCRAFT

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