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Thrust Reverser


Aft movement of reverser sleeves causes blocker doors to deflect fan air forward through fixed cascade vanes.


Hydraulic system

Hydraulic pressure for the operation of engine 1 and engine 2 thrust reversers comes from hydraulic systems A and B respectively. In the event of a failure, the affected thrust reverser can be operated using the standby hydraulic system.


Deployment

  • either RA <10'; or
  • air/ground sensor in ground mode

Indications

LocationReason
REVupper DUreverser sleeve has moved from stowed position
REVupper DUreverser in deployed position
REVERSEaft overhead panelreverser is commanded to stow until isolation valve closes (~10s)
*note that if illuminated for >12s, MASTER CAUTION and ENG annunciator lights illuminate
(recycling to clear the fault is allowed)

Categories: Boeing 737NG | Engines & APU



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