305-390-706-0 — NOZZLE SEGMENT,TURBINE,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

305-390-706-0: NOZZLE SEGMENT,TURBINE,AIRCRAFT.

NOZZLE SEGMENT,TURBINE,AIRCRAFT. Key specifications include material: NICKEL ALLOY OVERALL, overall_width: 5.200 INCHES NOMINAL IN, overall_height: 1.300 INCHES NOMINAL IN, overall_length: 5.200 INCHES NOMINAL IN, special_features: MFG. MATERIAL DESCRIPTION RENE 77, end_item_identification: F108 AIRCRAFT ENGINE.

This part is cataloged in the U.S. Government catalog under NSN 2840-01-341-0050, 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

305-390-706-0

NSN: 2840-01-341-0050
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	5.200 INCHES NOMINAL IN
overall_height	1.300 INCHES NOMINAL IN
overall_length	5.200 INCHES NOMINAL IN
special_features	MFG. MATERIAL DESCRIPTION RENE 77
end_item_identification	F108 AIRCRAFT ENGINE
engine_section_location	LOW PRESSURE TURBINE
criticality_code_justification	AGAV
NSN	2840-01-341-0050

COMPONENT DIAGRAM

KEY FEATURES

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

ENGINE SECTION LOCATION: LOW PRESSURE TURBINE

•

MATERIAL: NICKEL ALLOY OVERALL

TECHNICAL CHARACTERISTICS

OVERALL HEIGHT	1.300 INCHES NOMINAL IN
CRITICALITY CODE JUSTIFICATION	AGAV
OVERALL LENGTH	5.200 INCHES NOMINAL IN
OVERALL WIDTH	5.200 INCHES NOMINAL IN
ENGINE SECTION LOCATION	LOW PRESSURE TURBINE
SPECIAL FEATURES	MFG. MATERIAL DESCRIPTION RENE 77
END ITEM IDENTIFICATION	F108 AIRCRAFT ENGINE
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.

2840-00-000-0048 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 1

305-390-705-0Reference 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 305-390-706-0?

305-390-706-0 is a NOZZLE SEGMENT,TURBINE,AIRCRAFT.

What parts can replace 305-390-706-0?

There is 1 known substitute for 305-390-706-0: 305-390-705-0. Substitute compatibility should be verified for your specific system.

What is the NSN for 305-390-706-0?

305-390-706-0 is cataloged in the U.S. Government catalog under NSN 2840-01-341-0050. This indicates validated use in U.S. government and defense supply chains.

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305-390-706-0 — NOZZLE SEGMENT,TURBINE,AIRCRAFT

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