t2b
Kartei Details
| Karten | 168 |
|---|---|
| Sprache | Deutsch |
| Kategorie | Mathematik |
| Stufe | Andere |
| Erstellt / Aktualisiert | 21.06.2015 / 30.06.2023 |
| Weblink |
https://card2brain.ch/box/instrumentation_2
|
| Einbinden |
<iframe src="https://card2brain.ch/box/instrumentation_2/embed" width="780" height="150" scrolling="no" frameborder="0"></iframe>
|
The repsonse time of a VSI detector may be improved by adding a:
WHat happens when the static pressure supply, to a VSI, becomes blocked during a descent?
WHich statemnt is correct to the VSI?
The vertical speed inicator reads:
A blocked pitot head with a clear static source causes the airspeed indicator to:
The TAS is equal to EAS only if:
The reason for having a square-law compensation in the airspeed indicator mechaism is:
VFE is the may. speed:
What is the significance if the yellow arc in an airspeed indicator?
Hysteresis error?
Hysteresis error os caused by internal friction in the instrument mechanism
On the airspeed indicator of a twin-engie aeroplane , teh blue radial line corresponds to the:
To be as accurate as possible, an airspeed indicator must be calibrated according to the followig formula:
What crrections must be applied to indicated airspeed to produce TAS
IAS zu TAS ?
temperature and altitude => 2% for each 1000 ft
The airspeed indicator measures:
The airspeed indicator of an aircraft is provided with a moving red and white hatched pointer. This pointer indicates the:
An airspeed indicator includes a capsule; inside this capsule is:
VMO wie berechnet und in CAS TAS IAS EAS angeben ?
Velocity Maximum Operating expressed in CAS and calculate in EAS ==> Den Piloten in the form of IAS or CAS
The max. operating speed VMO is expressed in
The compressibility error must be taken into account inly for aerolane with:
In the air-tight instrument case of the airspeed indicaor we will find:
VMO is calculated from?
In case of static blockage the airspeed indicator ?
VNO is defined as:
Considering an airspeed indicator, a second, striped needle, if installed, indicates ?
The output data from teh ADC (Air data computer) are used by:
1) EFIS
2) Transponder
3) Automatic Flight control System
The output data calculated by the ADC (Air Data Computer) are:
1) Attitude
2) Pressure altitude
3) TAT
4) TAS
5) CAS
For TAS calculations, the ADC uses the following inputs
1) SAT
2) TAT
3) static pressure
4) total pressure
T/D is how calculated?
The FMC calculated top-of-descent ==> is green on den ND
PFD of an EFIS equipped aircraft displays the following parameters:
1) auto throttle modes
2) attitude
3) Vertical speed
4) flight director command bars
For an aurcraft EFIS equipped:
1) ND displays fligtj director command bars
2) PFD displays teh altimeter setting
3) ND displays teh attitude of teh aircraft
4) Fligt mode annunciator is part of teh ND
The PFD of an EFIS equipped transport category aircraft can typically display the following parameters
1)attitude
2) max. airspeed
3) selected heading
4) wind direction and speed
5) GS
On which of the following modes can weather information be displayed ?
Difference Expand and Full display
Expand +/- 45 degrees ==> Full= 360 Anzeige
The PFD of an EFIS equipped aircraft displays the following parameters
The DH warning light comes on when an aircraft:
The ND modes can be:
1) ARC or MAP covering 45 on either side of the instantaneous track
2) Rose or MAP CENTERED rose with current heading up
3) PLAN, map orientated to truth north
An EFIS includes the following components:
Plan mode ?
no possibility to overlay such as WX radar or TCAS => referenced to the True North => No moving map background
If only a single A/P is used to climb, cruise and approach; following a failure of an inner loop component:
