| AIRCRAFT ABOVE 5700kg (35) | ||
| AIRBUS A320 232 – ATA 2913 HYDRAULIC PUMP, (ELECTRIC/ENGINE), MAIN – PUMP – FAILED. DR 611954106 | ||
| Crew observed “HYD B ELEC PUMP LO PR” and “HYD SYS LO PR” ECAM indications during cruise. Root cause: Blue electric hydraulic pump found failed. Blue electric hydraulic pump to be replaced. |
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| EMBRAER EMB120 ER – ATA 3441 INERTIAL GUIDANCE SYSTEM – AHRS – Connectors contaminated. DR 611954121 | ||
| Pitch attitude comparator warning flag on EADI2.
Root cause: Contamination of connectors was observed when DPU and AHRS were removed. DPU and AHRS #1- and #2-unit connectors cleaned of contamination. Units Refitted and functional check c/o serviceable. |
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| AIRBUS A330 202 – ATA 5330 FUSELAGE MAIN, PLATES/SKIN – SKIN – DAMAGED. DR 611954141 | ||
| During walk around check, Engineer found scratch mark of 1.8 inch in length and through hole with approximately 3mm diameter at DR 2L area prior Aerobridge connection. Approved repairs completed. |
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| AIRBUS A320 232 – ATA 2210 AUTOPILOT SYSTEM – RUDDER – UNCOMMANDED ACTIVATE. DR 611954154 | ||
| While in cruise, Autopilot #1 engaged, aircraft experienced right yaw. Autopilot remained engaged. Once in cruise and twice on descent, a noticeable and abnormal yaw input was experienced with autopilot engaged. Flight data has been forwarded to Airbus for assessment and troubleshooting advice has been requested.
Resolution: Rudder Trim Actuator, FAC 1 replaced. Wiring checks completed. |
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| SAAB 340 B – ATA 3010 AIRFOIL ANTI-ICE/DE-ICE SYSTEM – De Icer Boot – PUNCTURED. DR 611954181 | ||
| During scheduled inspection of horizontal stabilizer, de-icer boot found boot with 130mm of stitching damage. It appears that stitching failure was initiated by impact damage.
Under investigation. |
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| AIRBUS A320 232 – ATA 3240 LANDING GEAR BRAKE SYSTEM – Brake fan – DAMAGED. DR 611954187 | ||
| During pre-flight walkaround inspection, #2-wheel, brake and brake fan shroud support found to be damaged. #2 Brake assy and #2 MWA replaced. MEL applied to brake fan. |
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| IAI 1124 – ATA 3220 NOSE/TAIL LANDING GEAR – CONTROL ROD – CORRODED. DR 611954191 | ||
| NLG control rods failed during NDT. External corrosion found on the shafts as well. NLG door shaft replaced IAW AMM32-20-00. Landing gear functional check carried out IAW AMM 32-10-03. | ||
| AIRBUS A320 232 – ATA 2730 ELEVATOR CONTROL SYSTEM – SERVO CONTROL – LEAKING. DR 611954196 | ||
| During Cruise, ECAM showed “HYD B RSVR LO LVL & HYD B SYS LO PR” message. Leak traced to L/H elevator servocontrol actuator 34CE3 between piston barrel and actuator body. Aircraft AOG, with actuator replaced and investigation ongoing. | ||
| BOEING 717 200 – ATA 3610 PNEUMATIC DISTRIBUTION SYSTEM – FAN AIR VALVE – UNSERVICEABLE. DR 611954197 | ||
| “Air Return” – due crew report of F.A.V. fault on climb. P.S.C. (Pneumatic System Controller), flags LH Fan air Valve to be defective. F.A.V. replaced, tested serviceable. | ||
