Quiz ATPL | Page 23 | AGK - Airframe, Systems,

In a compressor stage of a jet engine, the sequence is:	4 Answers
In the axial flow compressor of a turbo-jet engine, the flow duct is tapered. Its shape is calculated so as to:	4 Answers
In the stator of a turbine, the speed V and static pressure Ps vary as follows:	4 Answers
The purpose of a compressor bleed valve is to prevent surging:	4 Answers
A 'fan' stage of a ducted-fan turbine engine is driven by:	4 Answers
The diffuser in a centrifugal compressor is a device in which the:	4 Answers
The fan in a high by-pass ratio turbo-jet engine produces:	4 Answers
A reverse thrust door warning light on the flight deck instrument panel illuminates when:	4 Answers
In a single spool gas turbine engine, the compressor RPM is:	4 Answers
When the combustion gases pass through a turbine the:	4 Answers

ATPL - Airline Transport Pilot license - Aircraft General Knowledge - Airframe, Systems, Powerplant Page 23