2835-01-266-0346

Nonaircraft Gas Turbine Engine email this page
ITAR Registered

Model or part number: 6046T10G01

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About this product
Type/model desingation f404-ge-400; reference data and literature ge ecp g404-c-42, page 11

pdf NSN 2835-01-266-0346 Datasheet

MRC:
Indicates the type of mount utilized to support the item.AAXX
Mounting Type:
Aircraft
MRC:
The power output for which the item is designed.AXKD
Power Output For Which Designed:
Shaft
MRC:
--
NIIN:
012660346
MRC:
--
NATO Stock Number:
2835-01-266-0346
MRC:
--
Shelf Life:
N/A
MRC:
--
UOM:
--
MRC:
--
DEMIL:
FIIG:
--
FIIG:
A526A0
MRC:
--
INC:
50489
MRC:
--
IMM:
CX
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Factory New, New Material, New Surplus, Overhauled, Serviceable, Repairable, and AS Removed / Used material will be accompanied by a Certificate of Conformance, and any other documents/trace when applicable. We have a 7 year record retention.

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We are committed to quality and follow an AS9120 quality management system. AeroBase Group is HAZMAT certified and registered with DDTC, ITAR, and Aviation Suppliers Association (ASA). All products are 100% inspected.

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Delivery of IN-STOCK orders ship same-day when order is placed before 2:00 PM EST.

Delivery dates for NON-STOCK items are estimates based on current backlog and are subject to confirmation at the time of order.

Parts and Components for Nonaircraft Gas Turbine Engine NSN 2835-01-266-0346 Parts and components for this end application.

NSN Component Description
NSN 2840-01-266-0344 Tur Centrifugal Compressor Rotor
NSN 6620-01-434-1011 Engine Computer
NSN 6620-01-434-1012 Engine Computer
NSN 2915-01-462-5226 Fuel Injector Assembly
NSN 5220-01-474-8267 Fixed Snap Gage
NSN 5210-01-474-8268 Conical Shaft Gage
NSN 5210-01-474-8269 Drive Shaft Bore Gage
NSN 2840-01-501-2775 Flameholder Gutter Ring
NSN 2840-01-521-3165 Damper Bracket Kit

Formal Definition

Government issue definition of NSN 2835-01-266-0346

A continuous combustion type engine. consists primarily of a compressor, nonaircraft gas turbine engine; chamber, combustion, nonaircraft gas turbine engine and a turbine assembly, nonaircraft gas turbine engine. it may have a fan section. air is compressed and heated by a combustible fuel and expanded through the turbine. it is designed to furnish a source of rotary shaft and/or pneumatic power. the pneumatic power is obtained by a bleedoff of the engine compressor. for a complete operating power unit, mounted on a base, see power unit, gas turbine engine.

Manufacturers

This NSN is registered to the following cage codes.
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