Checklist für Diamond DA 42 Twin Star

01.07.2006 Peter Schmidleitner Page 2 Edition # 12 Does not replace the Airplane Flight Manual * if optional ice protection is installed ** if optional AUX tanks are installed PREFLIGHT INTERIOR + EXTERIOR. 1 Check airplane documents 2 Remove pitot cover 3 Check interior for foreign objects 4 Check circuit breakers 5 Start key PULLED OUT 6 Gear selector CHECKED DOWN 7 Electric Master ON 8 Gear 3 greens CHECKED 9 Check fuel quantity + temp 10 ** Fuel transfer ON – if L/R AUX FUEL E caution ON: AUX tank(s) empty Fuel transfer OFF 11 * Check de-ice fluid quantity 12 * De-ice HIGH (if required) 13 External (* ice) lights ON 14 Pitot heat ON 15 Check external lights 16 Check stall warning 17 Check pitot/static tube heat 18 * Check de-ice function 19 Pitot heat OFF 20 External lights OFF 21 * De-ice, ice lights OFF 22 Electric Master OFF PREFLIGHT EXTERIOR Canopy left side Left main gear Strut (min 4cm bare piston) & downlock Tire condition, pressure (4,5 bar), position mark Brake, hydraulic line Gear door & linkage Left engine nacelle Drain cascolator 3 air inlets / 2 air outlets Spinner, propeller Gearbox oil level Engine oil level Cowling Nacelle underside Venting pipe Exhaust ** Check AUX tank full ? Left wing Wing leading edge, top- and bottom surface Tank drain Stall warning Tank air vent Fuel filler cap Pitot, static probe (cover removed) Wing tip, position light Static dischargers Aileron (freedom of movement, hinges, control linkage, security) Wing flap Fuel cooler air in- & outlet ** AUX tank vent ** Drain AUX tank Left fuselage Step Rear cabin door Fuselage left side Antennas Attention! For refuelling with JET A1 no additives (e.g. „Aerojet“) are permitted. DA42 Twin Star PREFLIGHT PROCEDURES 01.07.2006 Peter Schmidleitner Page 3 Edition # 12 Does not replace the Airplane Flight Manual Tail Elevator & rudder (freedom of movement, hinges) Elevator & rudder trim - tabs Tail skid & lower fin Static dischargers Right fuselage Fuselage right side Rear window Step Right wing Fuel cooler air in- & outlet ** AUX tank vent ** Drain AUX tank Wing flap Aileron (freedom of movement, hinges, control linkage, security) Static dischargers Wing tip, position light Wing leading edge, top- and bottom surface Fuel filler cap Tank air vent Tank drain Canopy right side Right engine nacelle ** Check AUX tank full ? 3 air inlets / 2 air outlets Spinner, propeller Gearbox oil level Engine oil level Cowling Nacelle underside Venting pipe Exhaust Drain cascolator Ventilation air inlet Right main gear Strut (min 4cm bare piston) & downlock Tire condition, pressure (4,5 bar), position mark Brake, hydraulic line Gear door & linkage Nose section * De-ice fluid tank L + R front baggage door locked OAT sensor EPU connection Landing / Taxi light Nose gear Strut (min 15cm bare piston) & lock Tire condition, pressure (6 bar), position mark Gear door & linkage Chocks removed Tow bar removed DA42 Twin Star NORMAL PROCEDURES 01.07.2006 Peter Schmidleitner Page 4 Edition # 12 Does not replace the Airplane Flight Manual CHECK BEFORE ENGINE START 1 Preflight check ............................COMPLETED 1 2 Baggage and tow bar ...................... SECURED 2 3 Fuel selectors (2)..................................... ON 3 4 Power levers (2) .................................... IDLE 4 5 Parking brake......................................... SET 5 6 Alternate Air .................................... CLOSED 6 7 Manual gear extension handle ............ PUSHED 7 8 Gear selector ..................................... DOWN 8 9 Avionic master ....................................... OFF 9 10 Electric master ....................................... OFF 10 11 Engine masters (2) ................................. OFF 11 12 Pitot heat .............................................. OFF 12 13 Alternate static................................. CLOSED 13 14 Alternators (2) ........................................ ON 14 15 ECU swap (2) .......................................AUTO 15 16 All light switches..................................... OFF 16 17 Emergency switch.................... OFF/GUARDED 17 18 ELT ...................................................ARMED 18 19 Circuit breakers .......................... CHECKED IN 19 20 Flap selector ............................................ UP 20 If starting with external power: a Prop area ....................... CHECK CLEAR a b External power...................... CONNECT b 21 Electric master ........................................ ON 21 22 Rudder pedals ............................... ADJUSTED 22 23 Flight controls ................................ CHECKED 23 24 Trims ............................................ CHECKED 24 25 Gear warning, fire detector .....................TEST 25 26 * De-ice ANNUN TEST .............................. ON 26 27 * DEICE LVL LO caution . CHECKED ON if applic. 27 28 * Windshield de-icing ..... PUMP 1 + 2 CHECKED 28 Checklist continued next page DA42 Twin Star NORMAL PROCEDURES 01.07.2006 Peter Schmidleitner Page 5 Edition # 12 Does not replace the Airplane Flight Manual CHECK BEFORE ENGINE START continued 29 Flaps.....................................................LDG 29 30 Variable elevator backstop ................... CHECK 30 Control stick ............................... AFT and HOLD Power levers ............................................. MAX Check backstop limit decreasing Power levers .............................................IDLE Check backstop limit increasing 31 Flaps....................................................... UP 31 32 Passengers ............................... INSTRUCTED 32 33 Seat belts ..................................... FASTENED 33 34 Rear door .................... CLOSED and LATCHED 34 35 Front Canopy ................................POS 1 or 2 35 36 G1000.................POWERED, ACKNOWLEDGED 36 37 PFD/MFD ................................ BACKUP MODE 37 38 MFD...................................... ENGINE – FUEL 38 39 Fuel Quantity .....CHECKED, RESET/SET if requ. 39 40 Fuel temperature ............................ CHECKED 40 41 Total time in service............................NOTED 41 42 MFD..................................ENGINE – SYSTEM 42 43 * DEIC PRESS LO caution ........... CHECKED ON 43 44 * De-ice ANNUN TEST ............................. OFF 44 45 Power levers (2) .................................... IDLE 45 46 ACL (strobe) ........................................... ON 46 End of Checklist ENGINE START PROCEDURE Normal sequence: first start LH engine Engine Master ............................................. ON Annunciations / Eng.Instr. ................... CHECKED Glow indication .......................................... OFF Propeller area ........................................ CLEAR Start key............................................... START Oil pressure ............... OUTSIDE RED within 3 sec Voltage, Electrical load ......... CHECK INDICATION Annunciations / Eng.Instr. .......................CHECK If external power was used: External power................. DISCONNECT Start RH engine, procedure as above DA42 Twin Star NORMAL PROCEDURES 01.07.2006 Peter Schmidleitner Page 6 Edition # 12 Does not replace the Airplane Flight Manual CHECK AFTER ENGINE START 1 Oil pressure ................................... CHECKED 1 2 RPM 900 +/- 20.............................. CHECKED 2 3 Warm up time .................................... START 3 Warm up: Idle ................................................. 2 minutes 1400RPM ............. until Oil > 50°C and Coolant > 60°C 4 Fuel selectors (2)............................... X-FEED 4 5 Pitot heat ....ON, annunciation + Amps checked 5 6 Pitot heat .............................................. OFF 6 7 PFD/MFD ............................... NORMAL MODE 7 8 Avionics master ....................................... ON 8 FMS SETUP I nitialize profile (AUX 4, MAP, MFD FPL, PFD FPL) F light plan R adios (COM, NAV, ADF, DME, CDI, BRG 1/2) P erformance (speed bugs) 9 FMS setup ..................................COMPLETED 9 AUTOPILOT TEST DISCONN press, check electric trim not working AP ON, check overpowering servos DISCONN press, check AP off 10 Autopilot test ..............................COMPLETED 10 11 Flood light .............. CHECKED, ON as required 11 12 Position lights..........................ON as required 12 13 Fuel Selectors (2) .................................... ON 13 14 Altimeters (3) ........................................ SET 14 15 Standby horizon ............................. CHECKED 15 16 Transponder ..............CODE / MODE CHECKED 16 17 Parking brake................................ RELEASED 17 End of Checklist DURING TAXI Check Brakes Check nose wheel steering Check flight instruments DA42 Twin Star NORMAL PROCEDURES 01.07.2006 Peter Schmidleitner Page 7 Edition # 12 Does not replace the Airplane Flight Manual BEFORE TAKE OFF CHECK 1 Parking brake......................................... SET 1 2 Seat belts ..................................... FASTENED 2 3 Rear door ....................... CLOSED + LATCHED 3 4 Front canopy................... CLOSED + LATCHED 4 5 Front baggage doors ........... CHECKED CLOSED 5 6 Door warning light .................................. OFF 6 7 Engine instruments ......................... CHECKED 7 8 Fuel temperature (Diesel min. +5°)... CHECKED 8 9 Circuit breakers .............................. CHECKED 9 10 Electric elevator trim ..........CHECKED, T/O SET 10 11 Fuel selectors (2)....................... CHECKED ON 11 12 Rudder trim ............................. AS REQUIRED 12 13 Flaps........................................ CHECKED UP 13 14 Flight controls ................................ CHECKED 14 15 Power levers (2) .................................... IDLE 15 16 ECU test (2)................................... PERFORM 16 ECU TEST ECU test button........................... press and hold “L/R ECU A/B fail”........ON / RPM increasing / OFF “L/R ECU B fail”..............ON / prop cycling / OFF “L/R ECU A fail”...............ON / prop cycling / OFF RPM......................................... decrease to idle ECU test button..................................... release 17 ECU swap (2) ......... ECU B, ENGINES CHECKED 17 18 ECU swap (2) .......................................AUTO 18 19 Pitot heat ................................ AS REQUIRED 19 20 * Ice protection ........................ AS REQUIRED 20 21 Transponder ..............CODE / MODE CHECKED 21 22 Parking brake................................ RELEASED 22 End of Checklist LINE UP PROCEDURE Landing light............................................... ON Approach sector ..................................... CLEAR Runway..........................................IDENTIFIED Power lever max (100% / 10 sec) ........................... CHECK LOAD / RPM / FUEL FLOW / OP DA42 Twin Star NORMAL PROCEDURES 01.07.2006 Peter Schmidleitner Page 8 Edition # 12 Does not replace the Airplane Flight Manual AFTER TAKE-OFF PROCEDURE Brakes ...................................................APPLY Gear ...........................................................UP Landing light.............................................. OFF CLIMB TO CRUISE CHECK 1 Gear ........................................ CHECKED UP 1 2 Flaps........................................ CHECKED UP 2 3 Landing light ............................ CHECKED OFF 3 End of Checklist PERIODICALLY DURING CRUISE Fuel Radio Engine Direction Altitude DESCENT / APPROACH CHECK 1 Landing data ................................. RECEIVED 1 2 Altimeters (3) ........................................ SET 2 3 COM / NAV / FMS ................................... SET 3 4 Seatbelts ...................................... FASTENED 4 5 Fuel selectors (2)....................... CHECKED ON 5 6 Parking brake..................CHECKED RELEASED 6 7 Gear warning horn .......................... CHECKED 7 End of Checklist BEFORE LANDING PROCEDURE Downwind, latest base leg: Flaps ........................................................ APP Gear ...........................DOWN, CHECK 3 GREENS Landing light............................................... ON On final when landing assured: FINAL CHECK 1 Flaps.....................................................LDG 1 2 Gear .............................. 3 GREENS CHECKED 2 DA42 Twin Star NORMAL PROCEDURES 01.07.2006 Peter Schmidleitner Page 9 Edition # 12 Does not replace the Airplane Flight Manual GO AROUND PROCEDURE Power ...................................................... MAX Flaps ........................................................ APP Positive rate of climb: Gear ...........................................................UP Continue with take-off profile At safe altitude: Flaps ..........................................................UP Landing light.............................................. OFF AFTER LANDING CHECK When clear of runway 1 Flaps....................................................... UP 1 2 Pitot heat .............................................. OFF 2 3 Alternate air..................................... CLOSED 3 4 * De-ice systems .................................... OFF 4 5 Landing/Taxi light ..................... AS REQUIRED 5 End of Checklist PARKING CHECK 1 Parking brake......................................... SET 1 2 Power levers (2) ..................... IDLE for 2 min. 2 3 ELT ...................................... 121,5 CHECKED 3 4 Engine / System page ..................... CHECKED 4 5 Engine / Fuel page ..... TTL TIME IN SVC NOTED 5 6 Avionic master ....................................... OFF 6 7 Electrical consumers except ACL (strobe) ... OFF 7 8 Engine Masters (2).................................. OFF 8 9 ACL (strobe) .......................................... OFF 9 10 Electric Master........................................ OFF 10 11 Interior light ............................ CHECKED OFF 11 12 Start key .......................................REMOVED 12 End of Checklist SECURING THE AIRCRAFT Release parking brake, use chocks. Attach tie down ropes to mooring points. DA42 Twin Star IMPORTANT DATA AND LIMITATIONS 01.07.2006 Peter Schmidleitner Page 10 Edition # 12 Does not replace the Airplane Flight Manual OPERATING SPEEDS KIAS for MTOM 1785 1400 kg 1785 kg Stalling speed (VS0) Flaps LDG 49 57 Stalling speed (VS) Flaps APP 53 61 Stalling speed (VS) clean 56 64 In Ice: + 4 Kt Best gliding angle (Flaps UP) 82 Best angle of climb (VX) 79 Best rate of climb (VY ) 79 Best rate of climb 1-eng. (VYSE ) 82 Min. control speed (VMCA) 68 Min. control speed for TRG(V SSE) 82 Min. control speed (VMCA) in ice 72 Operating speed in ice 121 - 160 Cruising climb speed 86 Rotation speed 72 Max. flap speed (VFE) Flaps APP 137 Max. flap speed (VFE) Flaps LDG 111 Max. LG extension (VLOE ) 194 Max. LG extended (VLE) 194 Max. LG retraction (V LOR) 156 1700 kg 1785 kg Min. Landing speed Flaps UP 85 86 Min. Landing speed Flaps APP 82 82 Min. Landing speed Flaps LDG 76 78 Min. Go-around speed Flaps UP 82 82 Max. cruising speed (VNO) 155 Never exceed speed (VNE ) 194 up to 1542 kg above - 1542 kg Manoeuvring speed (V A) 120 126 MASS Max. TKOF mass 1785 kg Max ZF mass 1650 kg Max. LDG mass 1700 kg Empty mass 1295 kg Max. baggage in NOSE 30 kg Max. baggage in COCKPIT 45 kg Max. baggage in rear EXTENSION 18 kg 45 kg DA42 Twin Star 01.07.2006 Peter Schmidleitner Page 1 Edition #12 Does not replace the Airplane Flight Manual EMERGENCY + ABNORMAL CHECKLIST G1000 Warnings ............................................... page 2 Engine Engine fire / failure during take-off ...... page 4 Engine fire / failure in flight ................ page 4 Engine troubleshooting ...................... page 5 Engine restart .................................. page 5 Oscillating RPM ................................. page 6 RPM overspeed ................................. page 6 Landing Gear Landing with defective main gear tire .. page 6 Landing with defective brakes ............. page 6 Landing gear unsafe warning .............. page 7 Manual extension of landing gear ........ page 7 Landing gear up landing..................... page 7 Smoke and fire Engine fire on ground ........................ page 8 Electrical fire on ground ..................... page 8 Electrical fire in flight......................... page 8 Cabin smoke, cabin fire abv 10.000 ft .. page 9 Other Emergencies Oxygen pressure loss above 10.000 ft . page 9 Emergency descent ........................... page 9 Suspicion of carbon monoxide............. page 9 Unintentional flight into icing .............page 10 Ice protection failure ........................page 10 Electrical Syste Complete electrical failure .................page 10 For conditions to use this Emergency + Abnormal Checklist see page 1 of the Normal Checklist. All such conditions are fully applicable also for this checklist. DA42 Twin Star EMERGENCY PROCEDURES 01.07.2006 Peter Schmidleitner Page 2 Edition #12 Does not replace the Airplane Flight Manual G1000 WARNINGS L/R OIL PRES Pg. 2 Oil pressure low (red range) L/R OIL TEMP Pg. 2 Oil temperature high (red range) L/R GBOX TEMP Pg. 2 Gearbox temperature high (red range) L/R ENG TEMP Pg. 3 Coolant temperature high (red range) L/R FUEL TEMP Pg. 3 Fuel temperature high (red range) L/R ALTN AMPS Pg. 3 High Current (red range) L/R STARTER Pg. 3 Starter not disengaging DOOR OPEN Pg. 3 Unlocked doors L/R ENG FIRE Pg. 4 Pg. 4 Pg. 8 Engine fail/fire during take-off Engine fail/fire in flight Engine fire on ground For other parameters “out of green range” see Abnormal Checklist Abnormal Checklist starts at page 11 L/R OIL PRES OIL PRESSURE LOW ¾ Reduce power on affected engine ¾ Be prepared for loss of oil and an engine failure; land ASAP L/R OIL TEMP OIL TEMPERATURE HIGH ¾ Check oil pressure ™ If oil pressure too low (outside green range): Ÿ Reduce power on affected engine Ÿ Expect loss of engine oil Ÿ Be prepared for an engine failure ™ If oil pressure in green range Ÿ Reduce power on affected engine Ÿ Increase airspeed ™ If oil temperature not returning to green range: Ÿ Be prepared for an engine failure; land ASAP L/R GBOX TEMP GEARBOX TEMPERATURE HIGH ¾ Reduce power on affected engine ¾ Increase airspeed ™ If not returning to green range: Ÿ Be prepared for an engine failure; land ASAP DA42 Twin Star EMERGENCY PROCEDURES 01.07.2006 Peter Schmidleitner Page 3 Edition #12 Does not replace the Airplane Flight Manual L/R ENG TEMP COOLANT TEMPERATURE HIGH ¾ Check G1000 for LOW COOL LVL caution light ™ If LOW COOL LVL caution light OFF ™ During climb: Ÿ Reduce power on affected engine by 10% or more as rqrd Ÿ Increase airspeed by 10 KIAS or more as required Ÿ If coolant temp. not returning to green range within 60”: reduce power on affected engine as much as possible and increase airspeed ™ During cruise: Ÿ Reduce power on affected engine Ÿ Increase airspeed Ÿ If coolant temp. not returning to green range: Be prepared for an engine failure; land ASAP ™ If LOW COOL LVL caution light ON Ÿ Reduce power on affected engine Ÿ Expect loss of coolant fluid Ÿ Be prepared for an engine failure L/R FUEL TEMP FUEL TEMPERATURE HIGH ¾ Reduce power on affected engine ¾ Increase airspeed ¾ Transfer fuel from AUX to MAIN tank if applicable ™ If not returning to green range: land ASAP L/R ALTN AMPS HIGH CURRENT ¾ Check circuit breakers ¾ Reduce electrical load and land ASAP L/R STARTER STARTER NOT DISENGAGING ¾ Affected power lever IDLE ¾ Affected engine master OFF ¾ Electric master OFF DOOR OPEN UNLOCKED DOORS ¾ Reduce Airspeed ¾ Check canopy and rear door visually ™ If unable to latch: land ASAP ¾ Check front baggage doors visually ™ If one or both open: land ASAP Never unlatch rear door during flight DA42 Twin Star EMERGENCY PROCEDURES 01.07.2006 Peter Schmidleitner Page 4 Edition #12 Does not replace the Airplane Flight Manual ENGINE FAILURE ENGINE FIRE DURING TAKE-OFF REJECTED TAKE-OFF OR EMERGENCY RE-LANDING 1 Power .................................................... OFF 1 2 Brakes ................................................ APPLY 2 3 ATC ................................................. INFORM 3 If necessary: 4 Engine Masters (2) .................................. OFF 4 5 Fuel selectors (2) .................................... OFF 5 6 Electric Master ........................................ OFF 6 In case of fire: 7 Cabin heat & defrost ................................ OFF 7 ENGINE FAILURE ENGINE FIRE IN FLIGHT If airspeed below 68 KIAS: Perform Vmca recovery procedure Airspeed above 68 KIAS: 1 Power ............................ INCREASE up to MAX 1 2 Airspeed..............................min Vyse 82 KIAS 2 3 Landing gear ............................................ UP 3 4 Flaps ....................................................... UP 4 5 Engine Master (dead engine)..................... OFF 5 6 Alternator (dead engine) .......................... OFF 6 7 Fuel selector (dead engine)....................... OFF 7 In case of fire: 8 Cabin heat & defrost ................................ OFF 8 9 Canopy ......................... UNLATCH if necessary 9 Max airspeed 120 KIAS DA42 Twin Star EMERGENCY PROCEDURES 01.07.2006 Peter Schmidleitner Page 5 Edition #12 Does not replace the Airplane Flight Manual ENGINE TROUBLESHOOTING 1 Power ................................................... MAX 1 If in icing conditions: 2 Alternate air ......................................... OPEN 2 3 Fuel quantity ...................................... CHECK 3 4 AUX transfer ..................................CONSIDER 4 5 Fuel selector ............................. ON or X-FEED 5 6 ECU swap............................................ ECU B 6 If unsuccessful: 7 ECU swap.............................................AUTO 7 8 Circuit breakers....................... CHECK / RESET 8 x If CB reset restored engine power: land ASAP x If all unsuccessful: continue with ENGINE FAILURE IN FLIGHT checklist ENGINE RESTART 1 Airspeed.................... 80 KIAS - max 120 KIAS 1 2 Pressure Altitude ..........................max 6000 ft 2 3 Power (affected engine) .......................... IDLE 3 4 Fuel selector (affected engine) ................... ON 4 5 Alternate air ............................. AS REQUIRED 5 6 Engine Master (affected engine) ................. ON 6 7 Starter........................... if necessary ENGAGE 7 If engine started: 8 Power (affected engine) ................. MODERATE 8 9 Engine instruments.......... check GREEN RANGE 9 10 Alternator (affected engine) ....................... ON 10 DA42 Twin Star EMERGENCY PROCEDURES 01.07.2006 Peter Schmidleitner Page 6 Edition #12 Does not replace the Airplane Flight Manual OSCILLATING RPM 1 Power lever ............................. change setting 1 If no success: 2 ECU swap............................................ ECU B 2 If no success: 3 ECU swap.............................................AUTO 3 Land ASAP RPM OVERSPEED 1 Power setting.................................... REDUCE 1 If no success: 2 ECU swap............................................ ECU B 2 If no success: 3 ECU swap.............................................AUTO 3 Land ASAP Be prepared for ENGINE FAILURE IN FLIGHT LANDING WITH DEFECTIVE MAIN GEAR TIRE 1 ATC ............................................. INFORMED 1 For landing: x Land on RWY side with “good” tire x Keep wing on “good” side low x Support directional control with brake LANDING WITH DEFECTIVE BRAKES After touchdown (if necessary): 1 Engine Masters (2) .................................. OFF 1 2 Fuel selectors (2) .................................... OFF 2 3 Electric Master ........................................ OFF 3 DA42 Twin Star EMERGENCY PROCEDURES 01.07.2006 Peter Schmidleitner Page 7 Edition #12 Does not replace the Airplane Flight Manual LANDING GEAR UNSAFE WARNING If on for more than 20 seconds: 1 Airspeed...................................max 156 KIAS 1 In cold temperature: 2 Airspeed...................................max 110 KIAS 2 3 Gear selector ................................... RECYCLE 3 If landing gear extension unsuccessful: Continue with MANUAL EXTENSION If landing gear retraction unsuccessful: Consider flight with landing gear down MANUAL EXTENSION OF LANDING GEAR 1 Airspeed...................................max 156 KIAS 1 2 Gear indicator lights ...............................TEST 2 3 Electric master ............................... CHECK ON 3 4 Bus voltage ........................... CHECK NORMAL 4 5 Circuit breaker .................................... CHECK 5 6 Gear selector ...................................... DOWN 6 7 Manual extension handle ......................... PULL 7 If necessary 8 Airspeed...................................max 110 KIAS 8 Apply moderate yawing 9 Gear indicator lights ............. CHECK 3 GREENS 9 LANDING GEAR UP LANDING (Landing gear completely retracted) 1 Approach .........................................NORMAL 1 Just before touchdown: 2 Power lever ........................................... IDLE 2 After touchdown: 3 Engine Masters (2) .................................. OFF 3 4 Fuel selectors (2) .................................... OFF 4 5 Electric Master ........................................ OFF 5 DA42 Twin Star EMERGENCY PROCEDURES 01.07.2006 Peter Schmidleitner Page 8 Edition #12 Does not replace the Airplane Flight Manual ENGINE FIRE ON GROUND 1 Power levers (2)..................................... IDLE 1 2 Engine masters (2) .................................. OFF 2 3 Fuel selectors (2) .................................... OFF 3 4 Mayday call ...................................CONSIDER 4 5 Electric master ........................................ OFF 5 When engine and aircraft stopped: 6 Canopy ................................................ OPEN 6 Evacuate ELECTRICAL FIRE ON GROUND 1 Mayday call ...................................CONSIDER 1 2 Electric Master ........................................ OFF 2 3 Power levers (2)..................................... IDLE 3 4 Engine Masters (2) .................................. OFF 4 5 Fuel selectors (2) .................................... OFF 5 When engine and aircraft stopped: 6 Canopy ................................................ OPEN 6 Evacuate ELECTRICAL FIRE IN FLIGHT 1 Emergency switch .................................... ON 1 2 Mayday call ...................................CONSIDER 2 3 Avionic master ........................................ OFF 3 4 Electric master ........................................ OFF 4 5 Cabin heat & defrost ................................ OFF 5 6 Emergency windows ........... OPEN as necessary 6 7 Canopy ......................... UNLATCH if necessary 7 Max airspeed 120 KIAS Land ASAP DA42 Twin Star EMERGENCY PROCEDURES 01.07.2006 Peter Schmidleitner Page 9 Edition #12 Does not replace the Airplane Flight Manual CABIN SMOKE ABOVE 10.000 FT 1 Oxygen ......................................... CHECK ON 1 2 Emergency descent .......................... INITIATE 2 When passing 10.000 ft 3 Oxygen .................................................. OFF 3 Land ASAP CABIN FIRE ABOVE 10.000 FT 1 Oxygen ..........................................PUSH OFF 1 2 Emergency descent ........................ INTITIATE 2 Land ASAP OXYGEN PRESSURE LOSS ABOVE 10.000 FT 1 Oxygen ..........................................PUSH OFF 1 2 Oxygen pressure .............CHECKED, note down 2 3 Emergency descent ........................... INTIATE 3 When passing 10.000 FT: 4 Oxygen pressure ....................... CHECK AGAIN 4 x If oxygen pressure constant: ... Continue flight x If oxygen pressure dropped: ........ Land ASAP EMERGENCY DESCENT 1 Flaps ....................................................... UP 1 2 Landing Gear ...................................... DOWN 2 3 Power levers .......................................... IDLE 3 4 Airspeed................................... AS REQUIRED 4 SUSPICION OF CARBON MONOXIDE 1 Cabin heat & defrost ................................ OFF 1 2 Ventilation............................................ OPEN 2 3 Emergency windows .............................. OPEN 3 4 Airspeed...................................max 120 KIAS 4 5 Canopy .......................................... UNLATCH 5 Push up and lock in cooling gap position DA42 Twin Star EMERGENCY PROCEDURES 01.07.2006 Peter Schmidleitner Page 10 Edition #12 Does not replace the Airplane Flight Manual UNINTENTIONAL FLIGHT INTO ICING 1 Pitot heat ................................................ ON 1 2 Cabin heat & defrost ................................. ON 2 3 Power ........................................... INCREASE 3 4 * De-ice systems................ USE as appropriate 4 5 Alternate air ........................ OPEN as required 5 6 Emergency windows ............. OPEN as required 6 When pitot heat fails: 7 Alternate static valve ............................. OPEN 7 8 Emergency windows .......................... CLOSED 8 ICE PROTECTION FAILURE 1 Airspeed................................... MIN 121 KIAS 1 2 Flaps .............................................. MAX APP 2 3 Approach with residual ice .................. 82 KIAS 3 4 Landing distance ................................... x 1,4 4 COMPLETE ELECTRICAL FAILURE 1 Circuit breakers...........................CHECK all IN 1 If no success: 2 Emergency switch .................................... ON 3 3 Flood light ............................................... ON 4 4 Power .................................................... SET 5 according power lever position and/or engine noise 5 Flaps ..................................VERIFY POSITION 6 Land ASAP Landing gear may slowly extend For landing apply “Manual extension of landing gear” DA42 Twin Star ABNORMAL PROCEDURES 01.07.2006 Peter Schmidleitner Page 11 Edition # 12 Does not replace the Airplane Flight Manual G1000 CAUTION LIGHTS L/R ECU A FAIL Page 12 ECU A failed L/R ECU B FAIL Page 12 ECU B failed L/R ALTN FAIL Page 12 Alternator failed L/R VOLTS LOW Page 12 Bus voltage too low L/R COOL LVL Page 13 Engine coolant level low PITOT FAIL Page 13 Pitot heating system failed PITOT HT OFF Page 13 Pitot heating system OFF STALL HT FAIL Page 13 Stall warning heating failed STALL HT OFF Page 13 Stall warning heating OFF L/R FUEL LOW Page 13 Main tank fuel qty low L/R AUX FUEL E Page 13 L/R auxiliary fuel tank empty STICK LIMIT Page 13 Stick limiting system failed DEICE LVL LO Page 14 De-icing fluid level low DEIC PRES LO Page 14 De-icing pressure low DEIC PRES HI Page 14 De-icing pressure high Engine instrument indications outside of green range COOLANT temperature high/low .................. page 15 OIL temperature high/low........................... page 15 OIL pressure high/low ................................ page 15 FUEL temperature high/low......................... page 15 VOLT low.................................................. page 16 RPM high.................................................. page 16 Other abnormal situations Both Alternators failed .......................... page 16 Hydraulic pump fail or continuous ops... page 16 AUX fuel transfer fail ............................. page 16 DA42 Twin Star ABNORMAL PROCEDURES 01.07.2006 Peter Schmidleitner Page 12 Edition # 12 Does not replace the Airplane Flight Manual CAUTION ALERTS ON THE G1000 L/R ECU A OR B FAIL ON GROUND ¾ Discontinue operation, terminate flight preparation L/R ECU A FAIL DURING FLIGHT Remark: in case of ECU A fail the system automatically switches to ECU B ¾ Press ECU TEST button for more than 2 seconds ™ If ECU A caution message re-appears or cannot be reset: Ÿ Land ASAP ™ If ECU A caution message can be reset Ÿ Continue flight. Engine must be serviced after LDG L/R ECU B FAIL DURING FLIGHT ¾ Press ECU TEST button for more than 2 seconds ™ If ECU B caution message re-appears or cannot be reset: Ÿ Land ASAP ™ If ECU B caution message can be reset Ÿ Continue flight. Engine must be serviced after LDG L/R ALTN FAIL ALTERNATOR FAILED ¾ Alternator on affected side OFF ¾ Monitor bus voltage ¾ Reduce electrical consumers ™ If both alternators failed: Ÿ See Abnormal Checklist “Both Alternators failed”, page 16 L/R VOLTS LOW BUS VOLTAGE TOO LOW Remark: possible reasons are - fault in the electrical power supply - RPM too low ¾ Continue with “Engine instrument indications outside of green range” – VOLTS low, page 16 DA42 Twin Star ABNORMAL PROCEDURES 01.07.2006 Peter Schmidleitner Page 13 Edition # 12 Does not replace the Airplane Flight Manual L/R COOL LVL ENGINE COOLANT LEVEL LOW ¾ Monitor annunciations / engine instruments ¾ Check coolant temperature ¾ See “Engine instrument indications outside of green range” – COOLANT TEMPERATURE PITOT FAIL PITOT HT OFF STALL HT FAIL STALL HT OFF ¾ check pitot heat ON, if in icing conditions Ÿ expect failure of the pitot-static-system Ÿ alternate static valve: OPEN Ÿ expect loss of aural stall warning ¾ leave area with icing conditions (see Emergency Checklist page 10 “Unintentional flight into icing”) L/R FUEL LOW MAIN TANK FUEL QTY LOW ¾ Check fuel quantity ™ If LH & RH quantities show remarkable difference: Ÿ Expect loss of fuel on side with lower indicaton Ÿ Use x-feed: Fuel selector to x-feed on side with LOW FUEL indication L/R AUX FUEL E AUXILIARY FUEL TANK EMPTY Ÿ L/R auxiliary fuel pump OFF STICK LIMIT VARIABLE ELEVATOR BACKSTOP SYSTEM FAILED ™ 1 or 2 power levers set for MORE than 20% load: Ÿ Elevator variable backstop is INOP Ÿ Do not stall in any configuration! ™ 2 power levers set for LESS than 20% load: Ÿ Elevator variable backstop always ACTIVE Ÿ Reduced elevator capacity Ÿ For approach min V REF 76/78 KIAS DA42 Twin Star ABNORMAL PROCEDURES 01.07.2006 Peter Schmidleitner Page 14 Edition # 12 Does not replace the Airplane Flight Manual DEICE LVL LO DE-ICING FLUIS LEVEL LOW ¾ Maximum duration of ice protection in NORMAL mode: 45 min, in HIGH mode: 22 min DEIC PRES LO DE-ICING PRESSURE LOW ¾ Switch DE-ICE to HIGH ™ If DEIC PRES LO light still ON Ÿ PUMP1 / PUMP2: select other pump Ÿ If necessary prime pump by activating windshield pump ™ If DEIC PRES LO light still ON Ÿ Activate ALTERNATE switch ™ If DEIC PRES LO light still ON Ÿ Go to Emergency Checklist page 10 ICE PROTECTION FAILURE ™ ™ ™ If DEIC PRES LO light OFF Ÿ Continue flight (de-icing fluid flow: 30 lt/hr) Ÿ Monitor ice protection system operation Ÿ Check de-icing fluid level periodically DEIC PRES HI DE-ICING PRESSURE HIGH ¾ Possible reduced system performance ¾ Filter cartridge to be replaced at next scheduled maintenance DA42 Twin Star ABNORMAL PROCEDURES 01.07.2006 Peter Schmidleitner Page 15 Edition # 12 Does not replace the Airplane Flight Manual ENGINE INSTRUMENT INDICATIONS OUTSIDE OF GREEN RANGE COOLANT temperature high ¾ Refer to Emergency Checklist page 3, “L/R ENG TEMP” COOLANT temperature low Remark: During low power descent from high altitude coolant temperature may decrease. Consider increasing power. ¾ Check G1000 for LOW COOLANT LVL caution light ™ If “LOW COOLANT LVL caution light” ON Ÿ Reduce power on affected engine Ÿ Expect loss of coolant fluid Ÿ Be prepared for an engine failure OIL temperature high ¾ Refer to Emergency Checklist page 2, “L/R OIL TEMP” OIL temperature low ¾ Increase power ¾ Reduce airspeed OIL pressure high ¾ Check oil temperature and coolant temperature ™ If within green range Ÿ Oil pressure indication may be faulty; watch temperatures ™ If outside of green range Ÿ Reduce power on affected engine; Ÿ Be prepared for an engine faiure; Land ASAP OIL pressure low ¾ Refer to Emergency Checklist page 2, “L/R OIL PRES” FUEL temperature high ¾ Refer to Emergency Checklist page 3, “L/R FUEL TEMP” FUEL temperature low ¾ Increase power on affected engine ¾ Reduce airspeed ™ If not returning to green range: Ÿ Be prepared for an engine failure;Land ASAP DA42 Twin Star ABNORMAL PROCEDURES 01.07.2006 Peter Schmidleitner Page 16 Edition # 12 Does not replace the Airplane Flight Manual VOLTS low ™ On ground: Ÿ Check circuit breakers Ÿ Increase RPM ™ If LOW VOLTS CAUTION still indicated on the G1000: Ÿ Discontinue operation; terminate flight preparation ™ In flight: Ÿ Check circuit breakers Ÿ Switch off unnecessary electrical equipment ™ If LOW VOLTS CAUTION still indicated on the G1000: Ÿ Apply L/R ALTN FAIL caution procedure, page 12 RPM high ¾ Reduce power on affected engine ¾ Keep RPM in green range with appropriate power lever setting ™ If problem not solved: Ÿ Refer to Emergency Checklist page 6 “RPM overspeed” Ÿ Land ASAP OTHER ABNORMAL SITUATIONS Both alternators failed ¾ Avionic Master: OFF ¾ LH/RH Alternator: OFF ¾ Transponder: STBY ¾ Gear: DOWN ™ When down and locked: Ÿ Pull manual gear extension handle ¾ Stall/Pitot heat: OFF ¾ All lights:OFF Ÿ Expect battery power to last for 30 minutes Ÿ Expect engine stoppage after this time Ÿ Land ASAP Hydraulic pump: failure or continuous operation ¾ Check gear indication lights ¾ Prepare for manual landing gear extension L/R Auxiliary fuel XFER FAIL ¾ Check fuel quantity ¾ Use X-feed to keep LH and RH fuel levels equal ¾ Amend flight plan to allow for reduced amount of available fuel FMS Intitialization – AUX 4 page Recommended and compulsory settings TIME FORMAT UTC NAV ANGLE AUTO DIS. SPD NAUTICAL ALT. VS FEET PRESSURE HECTOPASCAL TEMP CELSIUS FUEL, FF GALLONS POSITION HDDD°MM.MM’ MAP DATUM WGS 84 AIRSPACE ALERTS As desired ARRIVAL ALERT As desired VOICE As Desired MFD DATA BAR FIELDS 1 GS 2 DIS 3 ETE 4 MSA GPS CDI SELECTED AUTO ILS CDI CAPTURE If coupled ILS APCH planned : MANUAL COM CHANNEL SPACING 25,0 KHZ NEAREST APT RWY SURFACE As desired Compulsory: ARINC 424 Distance Coding: A B C D E 1 2 3 4 5 F G H I J 6 7 8 9 10 K L M N O 11 12 13 14 15 P Q R S T 16 17 18 19 20 U V W X Y 21 22 23 24 25 PFD Flight Plan ETA ESA MFD Flight Plan DTK DIS