305-415-908-0 — BLADE,TURBINE ROTOR,AIRCRAFT GAS

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

305-415-908-0: BLADE,TURBINE ROTOR,AIRCRAFT GAS.

BLADE,TURBINE ROTOR,AIRCRAFT GAS. Key specifications include material: NICKEL ALLOY OVERALL, design_type: COMPRESSOR, overall_length: 5.500 INCHES NOMINAL IN, special_features: MATERIAL RENE 77, blade_attachment_method: LOCK, end_item_identification: F108 AIRCRAFT ENGINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-371-5783, 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

305-415-908-0

NSN: 2840-01-371-5783
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
design_type	COMPRESSOR
stage_number	2
overall_length	5.500 INCHES NOMINAL IN
special_features	MATERIAL RENE 77
blade_attachment_method	LOCK
end_item_identification	F108 AIRCRAFT ENGINE
engine_section_location	LOW PRESSURE TURBINE
reference_data_and_literature	T.O. 2J-F108-14, FIG 72-54-00-9A, IND 54A A
criticality_code_justification	AGAV
part_name_assigned_by_controlling_agency	BLADE ASSY-LPT RTR STG 2
NSN	2840-01-371-5783

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 2

•

DESIGN TYPE: COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

REFERENCE DATA AND LITERATURE: T.O. 2J-F108-14, FIG 72-54-00-9A, IND 54A A

•

BLADE ATTACHMENT METHOD: LOCK

•

ENGINE SECTION LOCATION: LOW PRESSURE TURBINE

TECHNICAL CHARACTERISTICS

STAGE NUMBER	2
DESIGN TYPE	COMPRESSOR
CRITICALITY CODE JUSTIFICATION	AGAV
REFERENCE DATA AND LITERATURE	T.O. 2J-F108-14, FIG 72-54-00-9A, IND 54A A
BLADE ATTACHMENT METHOD	LOCK
OVERALL LENGTH	5.500 INCHES NOMINAL IN
ENGINE SECTION LOCATION	LOW PRESSURE TURBINE
SPECIAL FEATURES	MATERIAL RENE 77
PART NAME ASSIGNED BY CONTROLLING AGENCY	BLADE ASSY-LPT RTR STG 2
END ITEM IDENTIFICATION	F108 AIRCRAFT ENGINE

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

305-415-907-0Reference 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 305-415-908-0?

305-415-908-0 is a BLADE,TURBINE ROTOR,AIRCRAFT GAS.

What parts can replace 305-415-908-0?

There is 1 known substitute for 305-415-908-0: 305-415-907-0. Substitute compatibility should be verified for your specific system.

What is the NSN for 305-415-908-0?

305-415-908-0 is cataloged in the U.S. Government catalog under NSN 2840-01-371-5783. This indicates validated use in U.S. government and defense supply chains.

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305-415-908-0 — BLADE,TURBINE ROTOR,AIRCRAFT GAS

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