9528M88G14 — SUPPORT,TURBINE COMPONENT,AIRCRA

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9528M88G14: SUPPORT,TURBINE COMPONENT,AIRCRA.

SUPPORT,TURBINE COMPONENT,AIRCRA. Key specifications include material: NICKEL ALLOY, overall_length: 2.000 INCHES NOMINAL IN, inside_diameter: 30.200 INCHES NOMINAL IN, outside_diameter: 31.819 INCHES NOMINAL IN, special_features: MATERIAL INCOLOY 718, mounting_hole_diameter: 0.260 INCHES NOMINAL IN. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-206-9819, 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

9528M88G14

NSN: 2840-01-206-9819
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 58828 — CFM INTERNATIONAL INC DBA CFM INTERNATIONAL (USA)

SPECIFICATIONS

material	NICKEL ALLOY
overall_length	2.000 INCHES NOMINAL IN
inside_diameter	30.200 INCHES NOMINAL IN
outside_diameter	31.819 INCHES NOMINAL IN
special_features	MATERIAL INCOLOY 718
mounting_hole_diameter	0.260 INCHES NOMINAL IN
mounting_hole_quantity	18
end_item_identification	ACFT ENG F108
reference_data_and_literature	T.O.2J-F108-14 FIG 72-53-00-1A, IND 70G A
criticality_code_justification	AGAV
part_name_assigned_by_controlling_agency	SUPPORT ASSY-SHOUD HPT NOZZLE
NSN	2840-01-206-9819

COMPONENT DIAGRAM

KEY FEATURES

•

MOUNTING HOLE QUANTITY: 18

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

REFERENCE DATA AND LITERATURE: T.O.2J-F108-14 FIG 72-53-00-1A, IND 70G A

•

MOUNTING HOLE DIAMETER: 0.260 INCHES NOMINAL IN

•

OUTSIDE DIAMETER: 31.819 INCHES NOMINAL IN

•

INSIDE DIAMETER: 30.200 INCHES NOMINAL IN

TECHNICAL CHARACTERISTICS

MOUNTING HOLE QUANTITY	18
CRITICALITY CODE JUSTIFICATION	AGAV
REFERENCE DATA AND LITERATURE	T.O.2J-F108-14 FIG 72-53-00-1A, IND 70G A
MOUNTING HOLE DIAMETER	0.260 INCHES NOMINAL IN
OVERALL LENGTH	2.000 INCHES NOMINAL IN
OUTSIDE DIAMETER	31.819 INCHES NOMINAL IN
INSIDE DIAMETER	30.200 INCHES NOMINAL IN
SPECIAL FEATURES	MATERIAL INCOLOY 718
PART NAME ASSIGNED BY CONTROLLING AGENCY	SUPPORT ASSY-SHOUD HPT NOZZLE
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.

2840-00-000-0048 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 2

9528M88G06Reference document

Same NSN cross-reference

Reference document — Secondary reference

9528M88G15Reference document

Same NSN cross-reference

Reference document — Secondary reference

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 9528M88G14?

9528M88G14 is a SUPPORT,TURBINE COMPONENT,AIRCRA.

What parts can replace 9528M88G14?

There are 2 known substitutes for 9528M88G14: 9528M88G06, 9528M88G15. Substitute compatibility should be verified for your specific system.

What is the NSN for 9528M88G14?

9528M88G14 is cataloged in the U.S. Government catalog under NSN 2840-01-206-9819. This indicates validated use in U.S. government and defense supply chains.

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9528M88G14 — SUPPORT,TURBINE COMPONENT,AIRCRA

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