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Showing posts with the label Helicopter

EUROCOPTER EC135 - FOD

EUROCOPTER EC135  29/08/2015        FOD.                                                                                                                   Rag ingested into rotor brake and onto both engine intake grills.  Momentary illumination of the rotor brake caution was observed. Brake handle confirmed in the off position. Caution illuminated again approx 5 secs later for approx 2 secs. All other indications normal. Emergency checklist consulted and flight continued to destination with no further cautions. Post flight inspection with engineer revealed evidence of ingestion of a rag past the rotor brake and onto both engine intake grills.         ...

EC135 - Fuel Indicator

EUROCOPTER EC135  TURBOMECA, FRANCE         11/09/2015                       Fuel indications inaccurate. Main fuel tanks sensors removed and cleaned before aircraft returned to service.                       Main fuel tank indications began to vary to an uncommon amount over two days. The fuel level would differ between 5-10 kilos depending on the altitude of the aircraft in various phases of flight. By the end of my last shift and arriving back at base the main tank fuel level went from 100kg in the main to 64kg whilst taxiing from the runway to the hangar. Throughout all flights over the 2 days the supply tanks indicated full without any change even when the fuel in the main tank became low. In my experience the supply tanks often drop a few kilos then fill back up to capacity.                  MEL con...

DGCA/NEW-MISC/153 Hoist Helicopter

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Subject- Equipment and furnishing- Hoist - Inspection/replacement                  During a maintenance check flight with a MBB-BK 117 C-2 helicopter , a dummy load of 552 lbs (250kg) was picked up in order to conduct a “maximum load cycle” on the rescue hoist. The cable reeled-out without further command of the operator, causing the test dummy load to impact the ground.               The results of further examinations on the subject hoist determined that the overload clutch had failed. The overload clutch design is common to all Goodrich externally mounted rescue hoists listed in Appendix 1 of  EASA AD 2013-0065-E                         This condition, if not detected and corrected, could lead to further cases of in-flight loss of the hoist load, possibly resulting in injury to persons on the ground or in a hoisting accident. For ...