ENGINE SYSTEM OPERATION, CONTROL & INDICATING - PART 2

AVIATION WORLD
ENGINE SYSTEM OPERATION, CONTROL & INDICATING - PART 2
IAE VE 2500 ENGINE - T/R DEACTIVATION AND LOCKOUT
PER THE MEL, ONE OR BOTH THRUST REVERSERS MAY BE DEACTIVATED IN THE STOWED POSITION FOR DISPATCH. THE DEACTIVATION PROCEDURE HAS TWO PARTS. FIRST, THE HYDRAULIC CONTROL UNIT (HCU) IS DEACTIVATED. MOVING THE DEACTIVATION LEVER TO THE INHIBIT POSITION PREVENTS THE PRESSURIZING VALVE FROM SUPPLYING HYDRAULIC PRESSURE TO THE REVERSER ACTUATORS. IN THE SECOND PART OF THE DEACTIVATION PROCEDURE EACH TRANSLATING SLEEVE IS SECURED (BOLTED) TO THE REVERSER STRUCTURE PREVENTING ANY MOVEMENT
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Murat Kilciler B1.1/B1.2 licensed Aircraft Technician
(license No : SHY TR66 5612 )
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