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8186
The purpose of a bleed valve, located in the beginning stages of the compressor, in an aircraft gas turbine engine is to
| | A) Vent high ram air pressure overboard to prevent a compressor stall. |
| | B) Control excessively high RPM to prevent a compressor stall. |
| | C) vent some of the air overboard to prevent a compressor stall. |
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