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 Best Regards Murat Kilciler B1.1/B1.2 licensed Aircraft Technician (license No : SHY TR66 5612 ) kilcilermurat@ 905383120629 whatsapp