Book 3 - Engine Controls Flashcards
control _____ is the movement of controls due to engine/airframe vibration
it is prevented by adjustable friction devices (_______) fitted in the control quadrant, or by passing the control mechanism through a ______ operated auto throttle system
control CREEP is the movement of controls due to engine/airframe vibration
it is prevented by adjustable friction devices (DAMPERS) fitted in the control quadrant, or by passing the control mechanism through a CLUTCH operated auto throttle system
the auto throttle has two main purposes:
- maintain constant ________ during the localiser and glide path phases of an automatic landing
- to close ________ at constant rate during flare
the auto throttle has two main purposes:
- maintain constant AIRSPEED during the localiser and glide path phases of an automatic landing
- to close THROTTLE at constant rate during flare
whenever a control run is rigged, it must be remembered that:
- the primary stop is always the maximum fuel flow stop on the engine fuel control unit. the pilot must always have the confidence that the ______ is causing the throttle lever to stop moving forward and NOT the stop on the _____ ____
- if there is more than one engine that the _______ of the throttle levers at any given thrust/power setting must be within the limits described in the manual
- the _____ required to move the throttle levers must always be within laid down limits
whenever a control run is rigged, it must be remembered that:
- the primary stop is always the maximum fuel flow stop on the engine fuel control unit. the pilot must always have the confidence that the ENGINE is causing the throttle lever to stop moving forward and NOT the stop on the FLIGHT DECK
- if there is more than one engine that the STAGGER of the throttle levers at any given thrust/power setting must be within the limits described in the manual
- the EFFORT required to move the throttle levers must always be within laid down limits
adjustment to MAX RPM at the engine can affect ______ in the cockpit
adjustment to MAX RPM at the engine can affect BOUNCE in the cockpit
when all work on the controls has been completed, the work should be subject to _________ inspections
when all work on the controls has been completed, the work should be subject to DUPLICATE inspections
in order to achieve the correct _____ of throttle movement, it must be remembered that:
- changing the radius of an adjustment will alter the ______ of range
- changing the length of a rod will change the _________ of the range
- stagger angle is corrected by changing the ______ of the adjusting rods
in order to achieve the correct RANGE of throttle movement, it must be remembered that:
- changing the radius of an adjustment will alter the AMOUNT of range
- changing the length of a rod will change the LOCATION of the range
- stagger angle is corrected by changing the LENGTH of the adjusting rods
one of the primary considerations of a duplicate inspection on the engine control system will be to ensure there is ______ at the maximum throttle position
this is to ensure that the full signal from the ___________ in the throttle control unit has been achieved in the same way that the mechanical fuel flow stop has been reached on a mechanical system
one of the primary considerations of a duplicate inspection on the engine control system will be to ensure there is BOUNCE at the maximum throttle position
this is to ensure that the full signal from the POTENTIOMETERS in the throttle control unit has been achieved in the same way that the mechanical fuel flow stop has been reached on a mechanical system
effort required to move the throttle levers is accomplished through a _____-out or ____-off check
the effort needed is usually between .-_._lbf
FADEC engines with a high degree of supervisory control require ____ effort because the mechanical control linkage is considerably ______ and/or much of the work is done by throttle servo motors
effort required to move the throttle levers is accomplished through a BREAK-out or PULL-off check
the effort needed is usually between 1.5-4.5lbf
FADEC engines with a high degree of supervisory control require LESS effort because the mechanical control linkage is considerably SHORTER and/or much of the work is done by throttle servo motors
throttle lever bearing checks on aircraft with three or four engines should be carried out twice on the ______ levers, pushing towards each of the adjacent levers in turn
throttle lever bearing checks on aircraft with three or four engines should be carried out twice on the CENTRE levers, pushing towards each of the adjacent levers in turn