1285M66G01 — SUPPORT,TURBINE NOZZLE,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

1285M66G01: 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 2840-01-240-3435, 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

1285M66G01

NSN: 2840-01-240-3435
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. 30J
criticality_code_justification	AGAV
part_name_assigned_by_controlling_agency	SUPPORT-SEAL OUTER HPT STTR
NSN	2840-01-240-3435

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. 30J

•

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. 30J
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 7

1808M66G04Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

1285M66G03Reference document

Same NSN cross-reference

Reference document — Secondary reference

1285M66G05Reference document

Same NSN cross-reference

Reference document — Secondary reference

1498M95G02Reference document

Same NSN cross-reference

Reference document — Secondary reference

1495M95G02Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

1498M95G04Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 1285M66G01?

1285M66G01 is a SUPPORT,TURBINE NOZZLE,AIRCRAFT.

What parts can replace 1285M66G01?

There are 7 known substitutes for 1285M66G01: 1808M66G04, 1285M66G03, 1285M66G05 and 4 more. Substitute compatibility should be verified for your specific system.

What is the NSN for 1285M66G01?

1285M66G01 is cataloged in the U.S. Government catalog under NSN 2840-01-240-3435. This indicates validated use in U.S. government and defense supply chains.

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1285M66G01 — SUPPORT,TURBINE NOZZLE,AIRCRAFT

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