Emergencies - Heli Academy

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HS Issue 1 / Rev. 0 Only the checks and procedures in the AFM are approved. Heli Sitterdorf provides this document as additional material and declines all responsibility. Autorotation procedure -Collective reduce, aft cyclic to get nose up -Set IAS to Vy -Twist grip shut off detent -Maneuver aircraft into wind -At 70ft AGL cyclic flare -At 20ft collective increase and cyclic forward -Collective increase to cushion landing Engine relighting -When Ng < 10% -Normal engine start procedure -Minimum 1000ft AGL required GOV failure NR drop: -Collective reduce to maintain NR in green arc -Twist grip à check in flight position -If necessary apply autorotation NR increase: -Collective increase to maintain NR in green arc -Twist grip slightly reduce -Land as soon as possible -Initiate a shallow approach -Set Torque at around 30% -Set ground speed below 10kts -After touch down reduce twist grip to idle before before lowering collective Smoke in the cabin Source of smoke identified: -Corresponding system OFF -Ventilate the cabin Source of smoke not identified: -Heating/demisting OFF -Battery and Generator OFF -Ventilate the cabin -All consumers OFF -Battery ON à check DC voltage -Generator ON à check DC voltage If DC parameters faulty: -Generator OFF -Unnecessary equipment OFF -Land as soon as practicable If DC parameters correct and no smoke detected: -All consumers one by one ON to identify failed system then keep it off -Continue flight upon equipment failed Flight control servo jam -Maintain attitude -HYDR switch OFF -Set IAS to Vy à apply HYDR failure procedure VEMD failure One screen failure: -Read all information on other screen -Use scroll on display or collective if necessary Both screen failure: -Check battery and generator ON -Set IAS to max 100 kts (-2kts/1000ft) -Carry out a no hover landing Emergencies EC120 HS Issue 1 / Rev. 0 Only the checks and procedures in the AFM are approved. Heli Sitterdorf provides this document as additional material and declines all responsibility. Loss of TR thrust in flight -Indicated by nose left yaw, cannot be stopped by right pedal Hover IGE or within H/V: -Twist grip à IDLE -Collective à INCREASE to cushion landing Hover OGE: -Collective à REDUCE depending on available height -Cyclic à FORWARD to gain airspeed -Airspeed à MAINTAIN Vy or higher -Collective à ADJUST to obtain minimum sideslip angle -Depending on minimum speed, LAND or AR to hard surface In CRUISE: -Airspeed à Maintain Vy or higher -Collective à ADJUST to obtain minimum sideslip angle -Depending on minimum speed, LAND or AR to hard surface HYD system failure -Adjust airspeed for comfortable control -HYD switch à verify ON -If HYD not restored à HYD switch OFF -Land as soon as practical Abnormal NR/NF indications NR indication failure: -Collective à Maintain Tq > 10% -NR is given by NF pointer -Continue flight NF indication failure: -Check in normal operating range with Tq > 0% -Continue flight ENGINE OIL > 110° C -IAS set to Vy -If temperature decreases à land as soon as practicable -Otherwise à land as soon as possible -Check oil pressure gauge -If gauge confirms pressure loss, land immediately Loss of OAT, Ng, Tq, T4 -FLI is replaced by 3-data symbology -Continue flight OAT indicator failure: -Max T/O PWR Ng: 100% -Max cont. PWR Ng: 98.5% Ng indicator failure: -If OAT > -10°C: T4 limited to 760°C -If OAT ≤ -10°C: T4 limited to 750° C -The T4 limitations displayed are the starting limitations Tq meter failure: -Comply with the table: T4 indication failure: -Comply with Ng and Tq limitations -Do not start the engine HS Issue 1 / Rev. 0 Only the checks and procedures in the AFM are approved. Heli Sitterdorf provides this document as additional material and declines all responsibility. ENG FIRE -Indicates fire in engine compartment à procedure -land immediately ENG P -Check oil pressure gauge -If normal à Land as soon as practicable -If low or NIL à land immediately à perform AR MGP P -Excessive temp or low oil pressure of MRGB -Tq à set < 45% -Land as soon as possible (max. 30min flight time) TWT GRIP -Twist Grip à Open to FLIGHT position HYDR -Reduce Collective -Set IAS to Vy -HYD switch à OFF -Land as soon as possible -Shallow approach with slow running landing BATT TEMP -Battery à OFF -Check GEN voltage: Voltage correct: -Check BATT Temp, if decreases à Continue flight -If steady à Land as soon as practicable Voltage > 32V -BATT switch à ON -GENE switch à OFF -Unnecessary equipment OFF GEN 32.0 V -GEN à OFF -CWP à Monitor for BATT TEMP -Apply GENE procedure case A GEN 30.0 V -GEN voltage à MONITOR GEN 24.0 V -GENE procedure à apply -GEN voltage à Check -If > 24V à continue flight -If < 24V à apply GENE procedure case A GEN 210 A -Unnecessary equipment à OFF à Continue flight GENE -GEN voltage on VEMD à CHECK -Verify GENE switch à ON Case A; GENE light rem. on: -Push ELEC RST switch à if light out, apply Case B -Unnecessary equipment à OFF -BAT voltage on VEMD à Monitor -Land as soon as practicable -When battery voltage <18V, NR audio alarm will come on Case B; GENE light out: -Continue flight Warning lights EC120 HS Issue 1 / Rev. 0 Only the checks and procedures in the AFM are approved. Heli Sitterdorf provides this document as additional material and declines all responsibility. ENG CHIP -Metal particles in engine oil circuit -Reduce Power à Land as soon as possible MGB TEMP -IAS à set to Vy -Monitor CWP -MGB Temp remains ON: land a soon as possible -Otherwise: land as soon as practicable GB CHIP -Metal particles in engine MGB or TGB oil circuit -IAS à set to Vy -Land as soon as practicable BATT -Battery is offline -Battery check ON -ELECT RST à PUSH -land as soon as practicable BATT FUSE -Battery fuse has blown à Battery is offline -Land as soon as practicable FUEL -Fuel quantity < 30kg -15min of flight time remaining with MCP -Avoid sideslip over 15° -Land as soon as possible FUEL P -Indicates low fuel pressure