![]() ![]() One engine Inoperative: MCT to idle Mode: NAV NAV laterally guides the aircraft along the FMS flight plan Mode:LOC LOC tracks the localizer beam Mode: HDG/TRACK HDG/TRACK laterally guides the aircraft along the AFS CP selected heading/track CLB/DES CLB/DES climbs/descends the aircraft along the FMS flight plan to the AFS CP selected altitude, by taking into account all FMS altitude constraints. Move thrust levers from active Detent A/THR active range All engines operative: CL to Idle Thrust Levers placed in the active Detent How do you disengage the A/THR Press A/THR Push button on AFS Panel When can the A/THR operate interdependently from the AP A/THR controls speed even when AP is off What flight phases is the A/THR Active all phases except takeoff In what Detents is the A/THR Active CL and FLEX/MCT How do you arm the A/THR Engage A/THR push button on AFS panel Holds thrust and performs thrust reduction during flare Ensures protection against excessive angle-of-attack (alpha floor). What is Autothrust Autothrust Controls the thrust of the two engines via orders to the FADEC When performing an approach with the FD OFF, the FD is automatically re-engaged in the case of a go around What Is a flight director The Flight Directors display: guidance orders on the PFDs via pitch, roll and yaw bars The FD enables the flight crew to manually fly the aircraft or to monitor the flight guidance orders when the autopilot is engaged. Autopilot engagement/use The AP can be engaged 5 seconds after takeoff and can be used for climb, cruise and approach, landing and rollout phase Flight Director The FD is automatically: Engaged at power-up Įngaged in case of a Resolution Advisory (RA) situation Guidance of the aircraft at initial climb by holding runway axis and speed Automatic landing Īutomatic TCAS Resolution Advisory (RA). Navigation information Fuctions of the Autopilot Stabilization of the aircraft around its center of gravity when the AP is engaged What does the ND display The ND displays:ĭisplay lateral and vertical parts of flight plans ![]() What does the PFD display? Primary flight parameters Guidance targets Īrmed and engaged modes on the Flight Mode Annunciator The FE is used by the FG and by the flight controls to prevent the aircraft from exiting the envelope. MTOW 268000kg MLW 205000kg MZFW 192000kg Vmo (IAS) 340kt Mmo 0.89M Vd (Max Dive Speed) 375 kt Vlo (IAS) 250kt IAS Vle (IAS) 250 kt IAS Conf 0/ Clean flight Phase CRZ Conf 1 flight Phase Hold/APP Conf 1+F flight Phase TO/APP Conf 2 flight Phase TO/APP Conf 3 flight Phase TO/APP/LDG FULL flight Phase LDG L Wing Tank Fuel Cap KG 23693Kg Center Tank Fuel Cap KG 65937Kg R Wing Tank Fuel Cap KG 23695Kg Total usable fuel capacity Kg 113327kg Engine type RR Trent XWB-84 Max Takeoff thrust kN 374.5kN ETOPS 180min Min Turn Radius 51m Number of Cabin Doors 8 1L, 1R, 2L, 2R, 3L, 3R, 4R, 4L Min Crew 9 Total Jumpseats 13 Define: The Flight Management System (FMS) The FMS manages the flight plan, defined by the flight crew, and provides flight parameters to the flight guidance Define: The Flight Envelope (FE) The FE computes the aircraft normal flight envelope. ![]()
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