9995M21G01 — CASE AND NOZZLE ASSEMBLY,TURBINE

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9995M21G01: CASE AND NOZZLE ASSEMBLY,TURBINE.

CASE AND NOZZLE ASSEMBLY,TURBINE. Key specifications include material: NICKEL ALLOY OVERALL, overall_width: 6.000 INCHES NOMINAL IN, overall_length: 36.000 INCHES NOMINAL IN, special_features: ORIGINAL NAME CASE,TURBINE ROTOR,TURBINE ENGINE, end_item_identification: ACFT ENG F108-CF-100,KC135 ACFT, engine_section_location: TURBINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-139-2420, 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

9995M21G01

NSN: 2840-01-139-2420
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
overall_width	6.000 INCHES NOMINAL IN
overall_length	36.000 INCHES NOMINAL IN
special_features	ORIGINAL NAME CASE,TURBINE ROTOR,TURBINE ENGINE
end_item_identification	ACFT ENG F108-CF-100,KC135 ACFT
engine_section_location	TURBINE
reference_data_and_literature	T.O. 2J-F108-14 FIG 72-00-02 IND 10C
part_name_assigned_by_controlling_agency	SHROUD ASSY-HPT/LPT NOZZLE
NSN	2840-01-139-2420

COMPONENT DIAGRAM

KEY FEATURES

•

REFERENCE DATA AND LITERATURE: T.O. 2J-F108-14 FIG 72-00-02 IND 10C

•

ENGINE SECTION LOCATION: TURBINE

•

MATERIAL: NICKEL ALLOY OVERALL

TECHNICAL CHARACTERISTICS

REFERENCE DATA AND LITERATURE	T.O. 2J-F108-14 FIG 72-00-02 IND 10C
OVERALL LENGTH	36.000 INCHES NOMINAL IN
OVERALL WIDTH	6.000 INCHES NOMINAL IN
ENGINE SECTION LOCATION	TURBINE
SPECIAL FEATURES	ORIGINAL NAME CASE,TURBINE ROTOR,TURBINE ENGINE
PART NAME ASSIGNED BY CONTROLLING AGENCY	SHROUD ASSY-HPT/LPT NOZZLE
END ITEM IDENTIFICATION	ACFT ENG F108-CF-100,KC135 ACFT
MATERIAL	NICKEL ALLOY 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.

2840-00-004-4242 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 2

9995M27G01Reference document

Same NSN cross-reference

Reference document — Secondary reference

9995M27G03Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 9995M21G01?

9995M21G01 is a CASE AND NOZZLE ASSEMBLY,TURBINE.

What parts can replace 9995M21G01?

There are 2 known substitutes for 9995M21G01: 9995M27G01, 9995M27G03. Substitute compatibility should be verified for your specific system.

What is the NSN for 9995M21G01?

9995M21G01 is cataloged in the U.S. Government catalog under NSN 2840-01-139-2420. This indicates validated use in U.S. government and defense supply chains.

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9995M21G01 — CASE AND NOZZLE ASSEMBLY,TURBINE

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