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022 Instrumentation
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An inner loop control (stabilisation) is...
When the autothrust part of the flight guidance system is in SPEED mode, the thrust is...
In an autopilot system, the guidance modes are:
1 - Pitch angle hold
2 - IAS and Mach number hold
3 - Altitude hold
4 - Glide slope intercept and track
The combination that regroups all of the correct statements is..
During a climb with the autopilot engaged in the V/S mode (holding of vertical speed), the auto-throttle:
How can you distinguish between an "armed" and an "engaged" mode on the Flight Mode Annunciator (FMA)? The caption:
A pilot is flying a GNSS non-precision approach using the autopilot. The pilot intends to disconnect the autopilot on final approach after having obtained sufficient visual references to complete a manual landing. When disconnecting the autopilot using the instinctive or quick disengagement
Which statements below that applies best to an ADIRU?
The positions of the mode selector of an inertial navigation unit are: OFF - STBY - ALIGN NAV - ATT:
1 - in "STBY", the unit aligns on the local geographic co-ordinate system
2 - the "ATT" position is used during autom: landing (LAND mode)
3 - in "NAV" the co-ordinates of the start position can be entered
4 - the platform is levelled before azimuth alignment
5 - in cruise, the unit can only be used in "NAV" mode.
The combination that regroups all of the correct statements is:
The alignment time, at mid-latitudes, for an Inertial Reference System using laser ring gyros is approximately:
"Contingency Fuel" is the amount of fuel that should account for (1) — to the (2) _ aerodrome.