Model: 106C3314G2

Aircraft Gas Turb Airflow Baffle

Special Features:

Radius 12.25 in. Min and 12.29 in. Max; 5 mounting holes, 1 at 0.251-0.254 in. Diameter and 4 at 0.281 in. Dia

Properties:

Overall Length
0.190 inches
Material Thickness
Between 0.040 inches and 0.050 inches
End Application
Aircraft eng
Criticality Code Justification
Agav
Engine Section Location
Turbine
Stage Number
2
Material
Steel
NSN
2840-00-188-2211
Part Number
106C3314G2
Description
Baffle,airflow,aircraft Gas Turb
CAGE
07482

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 106C3314G2 NSN 2840-00-188-2211

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50529
FIIG:
A10700
Concept No.:
App. Key:
A
Cond. Code:
1
Status:
A

Material Classification

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators
HMIC
PMIC
ESD/EMI
ENAC
MMAC
CRITL
HMIC:
N
PMIC:
A
ESD:
ESD:
MMAC:
CRITL:
Y

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Schedule B and Export
  • Schedule B: 8411997050
  • SITC: 71499
  • End Use: Engines and turbines for military aircraft
  • NAICS: 336412
  • USDA: 1

Freight Class: Parts of gas turbine aircraft engines, other than for use in civil aircraft

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