Product Details | AIRCRAFT GAS TURBINE ENGINE AIRFLOW BAFFLE

2840-00-188-2211 A generally metallic item of various shapes designed to provide an optimum diversion of cooling air around and through an air-cooled ENGINE, GAS TURBINE, AIRCRAFT. Excludes DEFLECTOR, AIR FLOW.

Part Alternates: 106C3314G2, 2840-00-188-2211, 00-188-2211, 2840001882211, 001882211

Engines, Turbines, and Components | Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components

Supply Group (FSG) NSN Assign. NIIN
28 01 SEP 1972 00-188-2211

Cross Reference | NSN 2840-00-188-2211

Part Number Cage Code Manufacturer
106C3314G2 07482 GENERAL ELECTRIC COMPANY DBA GE

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Technical Data | NSN 2840-00-188-2211

Characteristic Specifications
MATERIAL STEEL OVERALL
ENGINE SECTION LOCATION TURBINE
STAGE NUMBER 2
OVERALL LENGTH 0.190 INCHES NOMINAL
MATERIAL THICKNESS 0.040 INCHES MINIMUM AND 0.050 INCHES MAXIMUM
SPECIAL FEATURES RADIUS 12.25 IN. MIN AND 12.29 IN. MAX; 5 MOUNTING HOLES, 1 AT 0.251-0.254 IN. DIA AND 4 AT 0.281 IN. DIA
CRITICALITY CODE JUSTIFICATION AGAV
III END ITEM IDENTIFICATION ACFT ENG

Restrictions/Controls & Freight Information | NSN 2840-00-188-2211

Category Code Description
Hazardous Material Indicator CodeNThere is no data in the HMIS and the NSN is in an FSC not generally suspected of containing hazardous materials
Demilitarization Code:ANon-Munitions List Item/ Non-Strategic List Item - Demilitarization not required.
Precious Metals Indicator Code:AItem does not contain precious metal
Criticality Code:YThe item does not have a nuclear hardened feature but does have other critical feature(s) such as tolerance, fit restriction or application.
Category Code Description
No Freight Information