GIPPSLAND GA8–ATA 2820 AIRCRAFT FUEL DISTRIBUTION SYSTEM–Attach fitting–Fuel leak. DR 611851746
GIPPSLAND GA8–ATA 2820 AIRCRAFT FUEL DISTRIBUTION SYSTEM–Attach fitting–Fuel leak. DR 611851746
GIPPSLAND GA8–ATA 2820 AIRCRAFT FUEL DISTRIBUTION SYSTEM–Attach fitting–Fuel leak. DR 611851746
CESSNA 210 N–ATA 5510 HORIZONTAL STABILISER STRUCTURE–BRACKET–CRACKED. DR 611851724 During 100-hourly inspection, crack was noted at radius of bend relief on LH bracket. Moreover, RH bracket was found cracked above stabiliser mounting hole as well. Brackets to be replaced with new ones
DE HAVILLAND DHC8 202–ATA 3610 PNEUMATIC DISTRIBUTION SYSTEM–Muscle Pressure Line–FRACTURED. DR 611851653 Number 1 engine experienced power loss of 20 to 25% Tq with climb power set @1050 Np. NH parameter however matched. Open cowl inspection carried out, #1 bleed valve muscle line found fractured. Line replaced. OEM notified.
