MCC - Systems

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L. W.

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L. W.

À propos de ce fichier

Diese Karteikarten bieten eine grundlegende Einführung in Flugzeugsysteme, insbesondere Turbo-Propeller-Systeme. Sie decken Themen wie Triebwerksleistung, Eis- und Regen-Schutz, Flügelflaps, Ruderboost, Landeklappen, Trimmeinstellungen, elektrische Systeme und Navigation ab. Piloten und Flugschüler profitieren davon, um die Funktionsweise und Wartung dieser Systeme zu verstehen, was für sichere und effiziente Flüge entscheidend ist.

Cartes-fiches

Utilisateurs

Langue

Allemand

Catégorie

Matières relative au métier

Niveau

École primaire

Créé / Mis à jour

28.06.2016 / 04.08.2016

Fichiers de cartes similaires

landing gear operates how?

actuated electrically => red light = a transit or unlocked situation

when comes the ldg gear warning horn?

1. flaps up or in APPR and either or both pwr levers below 80% N1

2. flaps beyond Approach situation

which navigation installed in B200?

1x GNS

2x VOR

2x ILS

2x DME

1x ADF

1x Transponder

1x Radio altimeter

left CRS knob can be used for?

right CRS knob can be used for?

left: VOR or ILS or GPS/OBS

right: Vor or ILS

what makes the 1-2 button ?

the onside (green) or offside (yellow) of ILS/VOR

DH knob is for what?

decision height displayed in the ADI

von wo nimmt das Pneumatic system den Druck?

bleed air from teh engines's fourth stage section (P3) and transit it to various other systems

system die pneumatic brauchen?

1. surface deice

2. rudder boost

3, brake de-ice

4. bleed air system

5. door seal

engines?

2x Pratt and whitney turbo propellr => has a compressor and a power turbine == Each 850 SHP

100% N1 ist wie viel rpm

37'500 rpm

propeller is connect via what to the power turbine?

propeller is connected via a reduction gearbox to the power turbine => the max speed of teh power turbine is 30'000 rpm ===> After reduction gearing the propeller rpm is ten 2000

3 levers ?

1. power levers => through a pneumatic fuel control system

2. propeller levers => through the primary governor

3. condition levers=> control the fuel cut-off and the idle speed of the engines (52% for low idle and 70% for high idle)

caution by revers?

power levers should not be moved into reversing position when the engines are not running because the reversing syste, will be damaged

when you must turn in the auto ignition?

critical phase of flight

when is the autofeathered armed?

switch switch armed and both power levers have to be advanced above 90% n1

what indicates the ITT?

the engine gas temperature between the compressor turbine and the power turbine => Max. ITT will be limiting power factor at high altittude

what makes the mgnetic chip?

the detector will alert the pilot of oil contamination or peding engine failure

how are the engine air inlet lips heated?

heatet by hot exhaust from the engine

wht allows electrically operated ice vanes?

electrically operated ice vanes allow the overboard deflection through a bypass door of moisture particles present in the ram air entering the engine air inlet

how is teh propeller deiced?

an electrically propeller de-ice system heating the propeller de-ice boots

differential Pressure by a normal working pressure differential of

Commandes clavier:

= tourner,

= avant/arrière,

= faire défiler

6.5 psi

how you can regulate the pressure system? with the

Commandes clavier:

= tourner,

= avant/arrière,

= faire défiler

Bleed air valve

basic modes A/P?

Commandes clavier:

= tourner,

= avant/arrière,

= faire défiler

pitch hold and wings level

when you use the UP/DN toggle switch => what you must do first, before you can leave an altitude?

Commandes clavier:

= tourner,

= avant/arrière,

= faire défiler

disengage the altitude hold mode before pressing toggle switch

ALT select panel allows target altitude => ARM button ==> was passiert wenn altitude kommt?

Commandes clavier:

= tourner,

= avant/arrière,

= faire défiler

ARM lights goes off and ALT HLD

How you can disengage g/o?

Commandes clavier:

= tourner,

= avant/arrière,

= faire défiler

depressing the pitch sync button

Why caution by disengage A/P button?

Commandes clavier:

= tourner,

= avant/arrière,

= faire défiler

2 Stufe: 1 stufe disengage A/P, 2 STufe disengage electrical trim

wo kann man Autopilot engagement sehen?

Commandes clavier:

= tourner,

= avant/arrière,

= faire défiler

by FMA: flight mode annunciator

Ab wann ist der yaw damper aktiv?

Commandes clavier:

= tourner,

= avant/arrière,

= faire défiler

system may be use at any altitude but must be active above 17'000 ft: should be deactivated for T/O and LDG

28V erical system:concists of what?

Commandes clavier:

= tourner,

= avant/arrière,

= faire défiler

1. mary DC system through a dual-fed bus system

2. secondary AC system that powers avionics, yaw rate and some engine instruments

what is the DC electrical power sources?

1. one 24 V, 34 amp-hour battery

2. two 250A, 28V DC starter/generator

3. external power unit

flight controls are

mechanically connected to the control surfaces

trim is activated how?

electrically and has an on-off switch bon the pedestal

Once pitch trim disconnect, hoq you can recovere the trim switch?

reset action==> trim switch on the pedestal to off and on again

what makesthe rudder boost?

directional control in case of an engine failure

how you disengage the rudder boost system?

moving either or both of the bleed air valve switch to the INSTR & ENVIR OFF

how are the flaps operated?

electrically

how you can get the flaps from LDG to APPR?

1. first position up

2. while flaps retract through approach => level to approach

3 Tanks, welche?

1. wing tanks

2. nacelle tanks

3. center section includes teh AUX tanks

fuel quantity in lbs and kg

main tanks: 2560 LB or 1160kg

AUX tank: 1050 LB or 477 kg

Total: 3610 LB or 1637 Kg

1 / 43

Cartes-fiches

how are the engine air inlet lips heated?

heatet by hot exhaust from the engine

wht allows electrically operated ice vanes?

electrically operated ice vanes allow the overboard deflection through a bypass door of moisture particles present in the ram air entering the engine air inlet

how is teh propeller deiced?

an electrically propeller de-ice system heating the propeller de-ice boots

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MCC - Systems

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