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18-01-18 THRUST REVERSER SYSTEM DESCRIPTION The thrust reversers help stop the aircraft on landing and during a rejected takeoff (RTO). The system is operable on the ground only; the reversers will not deploy in flight. COMPONENTS AND OPERATION THRUST REVERSER The thrust reverser is powered by the left hydraulic system for the left reverser and the right hydraulic system for the right reverser and is controlled by the FADEC and electrical signals from the airplane. The hydraulic system has: -Isolation control unit -Directional control unit -Hydraulic and electro-hydraulic primary locks -Door actuators -Tertiary actuator locks The electrical system comprises: UPPER DOOR UPPER ACTUATOR LOWER TERTIARY LOCK LOWER DOOR THRUST REVERSER SYSTEM (Cont) CFO1801002_010 When reverse thrust is desired, the thrust levers are drawn aft to the IDLE position, where the thrust reverser levers may be lifted, thus allowing the main thrust levers to be pulled further rearward to the REV soft detent. This rearward movement signals the FADEC (via the RVDTs) and the thrust reversers (via the microswitches in the TQA) that thrust reverser de-ployment has been commanded. Once in the REV detent, it is unnecessary to hold the thrust reverse levers up, as they stay in place until the pilot selects forward operation. Interlock balks will prevent movement of the levers rearward beyond REV until the thrust reverser deploy switches provide feedback that the thrust reverser doors are fully deployed. During the de-ployment sequence, a white REV icon is displayed on the EICAS, and N1 target and bug are removed from the display. Once the doors are fully deployed, the REV icon changes to a green color, and the interlock baulk is released. This will allow for thrust lever modulation between the REV and MAX REV positions. N1 target and bug are set to the maximum reverser N1 setting. |