Sélectionne les dossiers auxquels / desquels tu voudrais ajouter / supprimer "MARO HS16"
The slats on the wing's leading edge are protected against ice through the wing anit-ice system. Ice formaiton is prevented by
active heating through telespopic pneumatic tubes with hot air comig from the pneumatic system
The cockpit comprises various panels. List 2 control panels.
OHP (Overhead Panel), Pedestal, Glareshield, Main Instrumental Panel
The Electronic Instrumental System (EIS) comprises
an Electornic Flight Instrument System (EFIS) and an Electronic Centralized Aircraft Monitoring System (ECAM)
The EFIS comprises
The ECAM comprises
What is the purpose of the landing gear shortening mechanism?
It decreases the main landing gear leg length, so that it can go into the main gear bay
The landing gear doors are locked in the closed position by means of
mechanical door uplock assemblies (closed mechanically, opended hydraulically or mechanically)
The landing gear was extended by free fall gravity extension How is this visible when the aircraft has landed?
All landing gear doors stay open
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