Pt2240 exam part 5 of 5 - Study guides, Class notes & Summaries

PT2240 Exam Part 5 of 5 Questions & Answers trend monitoring - ANS->Performance monitoring of engines, commonly referred to as _______________, is a technique used by aviation maintenance organizations and engine manufacturers to improve engine service life and reduce operating costs. performance and mechanical. - ANS->Trend analysis information can be broken down into two broad categories; performance - ANS->trend monitoring: Typical _________________ parameters include infor...

PT2240 Exam PART 1 of 5 Questions & Answers 1. Hydromechanical 2. Hydromechanical/electronic 3. Full Authority Digital Engine (or Electronics) Control (FADEC) - ANS-Gas turbine engine fuel controls can be divided into three basic groups: 1. computing 2. metering - ANS-Fuel controls have two sections to provide the correct fuel flow for the engine: gas generator gear train - ANS-Hydromechanical fuel controls are generally driven by the _______________ of the engine to sense engine speed...

PT2240 Exam PART 2 of 5 Questions & Answers 500 horsepower - ANS-The more accessories an engine has, the greater the power needed to drive the accessory gearbox. - In fact, the accessory drive system on a large high by pass engine can require as much as ________________ from the engine . intermediate or transfer - ANS-Since turbine engines operate at a relatively high rpm, reduction gearing is necessary in the accessory drive system to provide appropriate drive speeds for the accessorie...

PT2240 Exam - Part 3 of 5 Questions & Answers Water injection - ANS-___________ augments thrust in a gas turbine engine. decreases - ANS-As the density of air passing through an engine decreases, thrust _______________. During flight, ambient air pressure can decrease and increased air temperature can reduce density. To counteract these conditions, water injection can be used to cool the airflow and increase air density in an engine. Vaporized water in the combustion chamber inlet increas...

PT2240 Exam PART 1 of 5 Questions And Answers New Review 2023/2024 1. Hydromechanical 2. Hydromechanical/electronic 3. Full Authority Digital Engine (or Electronics) Control (FADEC) Gas turbine engine fuel controls can be divided into three basic groups: 1. computing 2. metering Fuel controls have two sections to provide the correct fuel flow for the engine: gas generator gear train Hydromechanical fuel controls are generally driven by the _______________ of the engine to sense engine...

PT2240 Exam PART 1 of 5 Questions And Answers New Review 1. Hydromechanical 2. Hydromechanical/electronic 3. Full Authority Digital Engine (or Electronics) Control (FADEC) - ANS-Gas turbine engine fuel controls can be divided into three basic groups: 1. computing 2. metering - ANS-Fuel controls have two sections to provide the correct fuel flow for the engine: gas generator gear train - ANS-Hydromechanical fuel controls are generally driven by the _______________ of the engine to sens...

PT2240 Exam PART 1 of 5 Questions And Answers New Review 2023/2024 1. Hydromechanical 2. Hydromechanical/electronic 3. Full Authority Digital Engine (or Electronics) Control (FADEC) Gas turbine engine fuel controls can be divided into three basic groups: 1. computing 2. metering Fuel controls have two sections to provide the correct fuel flow for the engine: gas generator gear train Hydromechanical fuel controls are generally driven by the _______________ of the engine to sense engine...

PT2240 Exam PART 1 of 5 Questions And Answers New Review 2023/2024 1. Hydromechanical 2. Hydromechanical/electronic 3. Full Authority Digital Engine (or Electronics) Control (FADEC) Gas turbine engine fuel controls can be divided into three basic groups: 1. computing 2. metering Fuel controls have two sections to provide the correct fuel flow for the engine: gas generator gear train Hydromechanical fuel controls are generally driven by the _______________ of the engine to sense engine...

PT2240 Exam PART 1 of 5 Questions And Answers New Review 2023/2024 1. Hydromechanical 2. Hydromechanical/electronic 3. Full Authority Digital Engine (or Electronics) Control (FADEC) Gas turbine engine fuel controls can be divided into three basic groups: 1. computing 2. metering Fuel controls have two sections to provide the correct fuel flow for the engine: gas generator gear train Hydromechanical fuel controls are generally driven by the _______________ of the engine to sense engine...