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2840-00-188-2211
Aircraft Gas Turbine Engine Airflow Baffle
2840001882211 001882211 106C3314G2
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. View more Aircraft Gas Turbine Engine Airflow Baffle
January 2023
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Restrictions 2840-00-188-2211
2840-00-188-2211 is a Aircraft Gas Turbine Engine Airflow Baffle that does not have a nuclear hardened feature, but does have another critical feature or features such as tolerance, fit restriction or application. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 2840-00-188-2211
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-00-188-2211
- Italy (ZR01)
- Effective Date:
- 1 Dec 2007
- Greece (ZU01)
- Effective Date:
- 1 Apr 1991
Approved Sources 2840-00-188-2211
- Part Number
- Manufacturer
- Status
- 106C3314G2
- Manufacturer
- 07482 - General Electric Company (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-00-188-2211
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- End Item Identification [AGAV]
- Acft Eng
- Criticality Code Justification [CRTL]
- Agav
- Engine Section Location [CZBJ]
- Turbine
- Material Thickness [ABPX]
- 0.040 Inches Minimum And 0.050 Inches Maximum
- Material [MATT]
- Steel Overall
- Overall Length [ABHP]
- 0.190 Inches Nominal
- Special Features [FEAT]
- 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
- Stage Number [CZCJ]
- 2
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Freight Information 2840-00-188-2211
2840-00-188-2211 has freight characteristics.. 2840-00-188-2211 has a variance between NMFC and UFC when transported by rail and the description should be consulted.