HYDRAULIC SYSTEM USERS
GREEN, BLUE, YELLOW USERSThe three independent hydraulic systems respectively supply the usersindicated on the diagram. Between these systems, the users…
POTABLE WATER SYSTEM CONTROLS & INDICATING
The potable water controls and indicating includes the display on theForward Attendant Panel (FAP) and two panels located at the…
POTABLE WATER SYSTEM
STORAGEThe potable water is stored in one tank installed in the pressurizedunderfloor area of the right hand fuselage, aft of…
FLIGHT CONTROLS – SYSTEM OVERVIEW
SYSTEM OVERVIEWThe control is achieved through the following conventional surfaces.PITCHPitch control is achieved by two elevators and the TrimmableHorizontal Stabilizer…
ENGINE LEAP-1A Power Plant
System Description The primary parts of the powerplant are: · Engine · Engine mounts (forward and aft) · Cowlings. A….
AUTOMATIC DIRECTION FINDER (ADF) SYSTEM
PRINCIPLE The ADF is a radio navigation aid. It provides: – an identification of the relative bearing of the aircraft…
DISTANCE MEASURING EQUIPMENT (DME) SYSTEM
DME SYSTEM PRINCIPLE The DME provides digital readout of the aircraft slant range distance from a selected ground station. The…
AIR TRAFFIC CONTROL (ATC) SYSTEM
ATC SYSTEM PRINCIPLE The Air Traffic Control (ATC) transponder is an integral part of the Air Traffic Control Radar Beacon…
RADIO ALTIMETER SYSTEM
PRINCIPLE The RA system determines the height of the aircraft above the terrain during initial climb, approach and landing phases….
ADIRS ALIGNMENT THROUGH MCDU
GENERAL The Inertial Reference (IR) alignment is carried out when the aircraft is on the ground. To perform the three…