9992M69G40 — CASE,COMPRESSOR,AIRCRAFT GAS TUR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9992M69G40: CASE,COMPRESSOR,AIRCRAFT GAS TUR.

CASE,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include material: TITANIUM OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 22.000 INCHES NOMINAL IN, special_features: ORIGINAL NAME CASE AND NOZZLE,TURBINE,TURBINE ENGINE, end_item_identification: ACFT ENG F108, engine_section_location: TURBINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-189-2633, 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

9992M69G40

NSN: 2840-01-189-2633
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 58828 — CFM INTERNATIONAL INC DBA CFM INTERNATIONAL (USA)

SPECIFICATIONS

material	TITANIUM OVERALL
design_type	AXIAL COMPRESSOR
overall_length	22.000 INCHES NOMINAL IN
special_features	ORIGINAL NAME CASE AND NOZZLE,TURBINE,TURBINE ENGINE
end_item_identification	ACFT ENG F108
engine_section_location	TURBINE
reference_data_and_literature	T.O. 2J-F108-14 FIG 72-32-00-05 IND 400L
criticality_code_justification	AGAV
part_name_assigned_by_controlling_agency	CASE ASSY-FRONT & EXTENSION CPRSR STTR
NSN	2840-01-189-2633

COMPONENT DIAGRAM

KEY FEATURES

•

DESIGN TYPE: AXIAL COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

REFERENCE DATA AND LITERATURE: T.O. 2J-F108-14 FIG 72-32-00-05 IND 400L

•

ENGINE SECTION LOCATION: TURBINE

TECHNICAL CHARACTERISTICS

DESIGN TYPE	AXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATION	AGAV
REFERENCE DATA AND LITERATURE	T.O. 2J-F108-14 FIG 72-32-00-05 IND 400L
OVERALL LENGTH	22.000 INCHES NOMINAL IN
ENGINE SECTION LOCATION	TURBINE
SPECIAL FEATURES	ORIGINAL NAME CASE AND NOZZLE,TURBINE,TURBINE ENGINE
PART NAME ASSIGNED BY CONTROLLING AGENCY	CASE ASSY-FRONT & EXTENSION CPRSR STTR
END ITEM IDENTIFICATION	ACFT ENG F108
MATERIAL	TITANIUM 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 6

1276M13G08Reference document

Same NSN cross-reference

Reference document — Secondary reference

1276M13G11Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

1276M13G05Reference document

Same NSN cross-reference

Reference document — Secondary reference

1276M13G07Reference document

Same NSN cross-reference

Reference document — Secondary reference

1276M13G04Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

9513M64G02Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Terminal item — no further procurement; issued until stock is exhaustedDemilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 9992M69G40?

9992M69G40 is a CASE,COMPRESSOR,AIRCRAFT GAS TUR.

What parts can replace 9992M69G40?

There are 6 known substitutes for 9992M69G40: 1276M13G08, 1276M13G11, 1276M13G05 and 3 more. Substitute compatibility should be verified for your specific system.

What is the NSN for 9992M69G40?

9992M69G40 is cataloged in the U.S. Government catalog under NSN 2840-01-189-2633. This indicates validated use in U.S. government and defense supply chains.

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9992M69G40 — CASE,COMPRESSOR,AIRCRAFT GAS TUR

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