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QRH_DA42_V1 2 1 - Sabena Airline Training Center

1. 21 1 1 REDUCE AIRSPEED 2 2 22222222 m INCREASE If oil temperature not returning to green range Be prepared for a loss of oil and engine failure LAND ASAP temperature returning to green range Continue normal operations DA42 sabena 9 AIRLINE TRAINING CENTER INC REV 1 2 4 8 L R GBOX TEMP POWER AFFECTED ENGINE REDUCE AIRSPEED esse E INCREASE f not returning to green range Be prepared for a loss of oil and engine failure LAND ASAP If returning to green range Continue normal operations L R FUEL TEMP POWER AFFECTED ENGINE ase REDUCE AIRSPEED e n INCREASE If not returning to green range LAND ASAP L R STARTER RH DA42 sabena 9 EMER PROC AIRLINE TRAINING CENTER INC REV 1 2 4 9 L R ENGINE TEMP G1000 LOW COOL LVL CHECK If LOW COOL LVL caution light OFF During climb POWER AFFECTED REDUCE BY 10 AIRSPEED corria INCREASE BY 10 KIAS e If coolant temp not returning to green range within 60 seconds POWER AFFECTED REDUCE FURTHER AIRSPEED insti INCREASE Consider level off or descent according to MEA MSA During cruise POWER AFFECTED ENGINE REDUCE as required A
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3. CHECK gt AUXILIARY TANK DRAIN CHECK DRAIN sabena 9 NORM PROC AIRLINE TRAINING CENTER INC REV 1 2 3 1 4 Check for water and sediment drain until no water or sediment comes out RIGHT WING CABIN VENT AIR INLET uz u CHECK CLEAR TANK DRAIN TANK AIR INLET CHECK DRAIN Check for water and sediment drain until no water or sediment comes out TANK AIR OUTLET uu ua ee CHECK OPENINGS ON LOWER 5 1 CHECK Check for foreign objects and for traces of fuel if tank is full fuel may spill over through the tank vent ENTIRE MAIN FUEL TANK CHECK CLOSE WING TIP issa STATIC DISCHARGERS POSITION LIGHT STROBE LIGHT CHECK MES DOWN emm CHECK CLEAR AILERON amp LINKAQGE erronee nnn CHECK FOREIGN OBJECTS IN AILERON PADDIE CHECK FEAP AND LINKAGE iiss a ak CHECK FLAP HINGES amp SAFETY assesses sea CHECK NACELLE UNDERSIDE FUEL COOLER AIR IN amp OUTLET CHECK CLEAR STER Sasa a CHECK AFT CANOPY sess FUSELAGE SKIN ANTENNAS UPPER SIDES anada STANIC PORT eeii 22 2 a QRH DA42
4. CHECK WEAR TREAD DEPTH OF TIRE Tires should be taken out of service when they have one or more flat spots Generally a single flat spot or skid burn does not expose the carcass body and the tire may remain in service unless severe unbalance is reported by the crew Small cuts are acceptable if they do not protrude into the tire carcass Cuts in the side wall are not acceptable Shallow chevron shaped cuts across the tread of a tire pose no problem they are caused by landing on a grooved concrete runway As long as the tread does not wear down into the body plies of the carcass the basic strength of the tire is not affected To provide traction during wet runway operation operators should replace their tires when the tread reaches 1 32 inch 0 79 mm WHEEL amp BRAKES HYDRAULIC BRAKE CHECK When checking the brakes verify that there is even wear on the disc no scratches no grease and no leaks near the brake line SLIP MARKS sa a eaen nieni CHECK LANDING GEAR DOORS CHOCKS M REMOVE RIGHT ENGINE NACELLE AIR INLETS 2 AIR CLEAR ENGINE OIL LEVEL id CHECK CLEAR Check oil level through inspection hole in upper cowling Normal oil quantity is 5 5 quarts Minimum is 4 8 quarts maximum is 6 3 quarts Do not refill when oil quantity is above 5 5 quart When oil quantity is at 5 quarts add
5. CHECK CLEAR M MT P CHECK FUSELAGE RIGHT SIDE UNDERSIDE FUSELAGE SKIN uu uuu ita E Regu RIEN eS ANTENNAS UPPER SIDE sS N STATIC PORT EMPANNAGE STABILIZERS amp CONTROL SURFACES ELEVATOR TIPS HINGES morsa ET ELEVATOR TRIM TAB RUBBER TRIM TAB E E SS ES E O EE TAU SKIOR LOWER EIN A e n p ss STATIC DISGHARGER Sis FUSELAGE LEFT SIDE UNDERSIDE STATIC POR Wasa E s CHECK F SEEAGESKIN pep CHECK FUSELAGE UNDERSIDE a 22 2 CHECK FOR CONTAMINATION ANTENNAS CHECK AFT CANOPY MISCELLANEOUS FOR NIGHT FLIGHT ONLY INTER n n e ec 22 amp CHECK EXTERIOR SS ee tete rec leet assasi sss sag ON amp CHECK ATAN SWITCHES OFF DA42 sabena NORM PROC REV 1 2 3 40 FOR FLIGHT IN IMC ONLY eT ON BITOTHEATZANNUNGIATOR 02052222720 EXTINGUISHED PITON TUBE ST PINOT OFF FOR FLIGHT IN KNOWN ICING CONDITIONS ONLY Iesse Ted RI o eR CHECK QTY ICE LIGET sees 6 ICE GELT E a lios COCKPIT PREPARATION FLOW RUDDER PEDALS lt SG E SN e E ET ADJUSTED amp LOCKED BELG Hie NR OUS cU S PROPER OPERATION SEAMBEL u
6. ee ana puma A OFF LAND ASAP L EMERGENCY DESCENT INITIATE LAND ASAP I DA42 sabena 9 EMER PROC AIRLINE TRAINING CENTER INC REV 1 2 4 1 8 ELECTRICAL FIRE IN FLIGHT l EMERGENCY 5 ua nennen nenne nennen nnns ON jy epe tet INFORM CONSIDER MAYDAY CALL i MASTER ul aa Uu dance OFF ELECTRIC MASTER u u Dau Su sau OFF CABIN HEAT 8 1 EMERGENCY WINDOVSS OPEN AS NECESSARY 1 CANOPY BELOW 120 KIAS UNLATCH IF NECESSARY I LAND ASAP ELECTRIC MASTER uuu luas s aaa POWER LEVERS BOTH ENGINE MASTERS BOTH FUEL SELECTORS BOTH SDS Sau When engine aircraft stopped CANOPY AAA AIRCRAFT p EVACUATE QRH DA42 sabena 9 EMER PROC AIRLINE TRAINING CENTER INC REV 1 2 4 19 UNINTENTIONAL FLIGHT INTO ICING PITOT HEAT MENOR RR TTE ON CABIN HEAT amp DEFROST ON POWER ae INCREASE DE ICE SYSTEMS USE AS APPROPRIATE ALTERNATE AIR Lise u see OPEN AS
7. REDUCE IDLE AIRPLANE REACTION amp PERFORMANCE OBSERVE SPEED E 90 KIAS INBOARD THROTTLE REDUCE TO IDLE AIRPLANE REACTION amp OBSERVE DA42 sabena MANEUVERS AIRLINE TRAINING CENTER INC REV 1 2 2 1 0 e DESCENDING TURN SPEED mE 120 KIAS OUTBOARD REDUCE TO IDLE AIRPLANE REACTION amp PERFORMANCE OBSERVE SPEED SSS mu Pss dildos 120 KIAS INBOARD THROTTLE is ase REDUCE TO IDLE AIRPLANE REACTION amp PERFORMANCE OBSERVE ONE ENGINE FLIGHT BA 4 POWER GOOD ENGINE 1009 SIMULATED FEATHER POWER 202 ABOVE GEAR HORN SET THROTTLE FOR 105 KIAS CLEAN 90 100 DEMONSTRATE LEVEL FLIGHT TURN CLIMB DESCENT EMPHASIZE THROTTLE AND FOOT TOGETHER THROTTLE TRAVEL DOUBLES THE SIDE SLIP INDICATOR SHOULD BE 1 2 WIDTH OUT ON THE SIDE OF THE GOOD ENGINE BANK ANGLE 3 5 TOWARDS THE GOOD ENGINE DA42 sabena MANEUVERS AIRLINE TRAINING CENTER INC REV 1 2 2 1 1 Demonstrate INCREASING BANK ANOLE AWAY Hic ES FROM THE FAILED ENOINE MS 1 Zero bank bad 2 Zero rudder bad 4 A E 3 Zero sideslip good ZERO BANK ZERO SIDESLIP ZERO RUDOER Demonstrate 1 Optimum performance max performance climb at blue li
8. CHECK If unable to latch canopy or rear door or if front baggage doors verified open visually LAND ASAP Never unlatch the rear door in flight QRH DA42 sabena 9 EMER PROC AIRLINE TRAINING CENTER INC REV 1 2 4 23 L R ECU A OR B FAIL ON GROUND TERMINATE FLIGHT PREPARATION IN FLIGHT In case of ECU A fail the system automatically switches to ECU B ECU TEST PRESS FOR MORE THAN 2 SECONDS If ECU B CAUTION MESSAGE re appears and cannot be reset LAND ASAP e If ECU B CAUTION MESSAGE can be reset PEERS CONTINUE Maintenance action required after landing L R COOLLVL ENGINE INSTRUMENTS ANNUNCIATIONS MONITOR COOLANT Continue with ENGINE INSTRUMENT INDICATIONS OUTSIDE GREEN COOLANT TEMPERATURE DA42 69 EMER PROC AIRLINE TRAINING CENTER INC REV 1 2 4 24 L R ALTN FAIL affected BUS VOLTAGE ida MONITOR ELECTRICAL LOAD REDUCE Ifboth ALTN failed BOTH ALTN FAIL CHECKLIST 2 PERFORM BOTH ALTN FAIL an ee OFF TRANSPONDER asa STANDBY LANDING GEAR ee DOWN e When landing gear down amp locked MANUAL GEAR EXTENSION 2 2 PULL STALE
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10. FAIL LIGHT ecce eire ote tit eene PROPELLER W If the L R ECU FAIL do not illuminate and extinguish m during the test sequence there is a malfunction in the engine control system Set ECU swap to ECU B A light shake of the engine may occur but check that other than this the engine keeps running without a change Set ECU swap back to AUTOMATIC Running the engine with the ECU swap ECU other than for this test or in an emergency is prohibited The engines control system redundancy is only given with the swap set to AUTOMATIC sabena 9 NORM PROC AIRLINE TRAINING CENTER INC REV 1 2 3 27 BEFORE TAXI CHECKLIST TAXI TAXILLI HT ON FUEL SELECTORS CROSSFEED Select both FUEL SELECTOR to CROSSFEED for 30 seconds Check the area around the airplane Call out Left is free free right Instructor will reply Right is free In case of solo flights the call out will be Left is free right is free after having verified both sides Then release the parking brake BRAKES suicida ae CHECK Perform brake check immediately after the aircraft starts rolling Apply light and even pressure on both pedals It is not necessary to bring the aircraft to a complete stop As soon as it becomes appar ent that normal brake pressure is available release the brakes again A
11. e IfDE ICE PRES LO light still ON EMER ICE PROTECTION FAILURE CHKLST APPLY e PRES LO OFF TIS EE CONTINUE De icing fluid flow 30 liters hour ICE PROTECTION SYSTEM OPERATION MONITOR DE ICING FLUID CHECK PERIODICALLY DE ICE PRES HI Possible reduced system performance Filter cartridge to be replaced at next scheduled maintenance QRH DA42 sabena 9 EMER PROC AIRLINE TRAINING CENTER INC REV 1 2 4 27 L R FUEL LOW FUEL e nemen nn nenn nn CHECK e IfLH and RH quantities show a remarkable difference Expect fuel leak on side with lower indication FUEL SELECTOR SIDE WITH LOW FUEL INDIC X FEED DA42 sabena 9 EMER PROC AIRLINE TRAINING CENTER INC REV 1 2 4 28 STICK LIMIT 1 OR 2 POWER LEVERS SET FOR MORE THAN 20 LOAD Elevator variable backstop is INOPERATIVE Aviod STALL in any condition 2 POWER LEVERS SET FOR LESS THAT 20 LOAD Elevator variable backstop is ALWAYS ACTIVE Reduced ELEV capacity travel le iii anita 76 78 KIAS RH DA42 Sabena EMER PROC x AIRLINE TRAINING CENTER INC REV 1 2 4 29 FAIL CONTINUOUS OPERATION GEAR INDICATOR Prepare for manual landing gear extension I
12. ii The proper function of the variable elevator backstop is 2 required for the safety of the flight as else handling qualities during power on stalls are significantly ii LARS iiie ici titer tec ondes tes co cosas UP FUEL SELECTORS_ cazas ii it tc ON ELEVATOR TRIM ect etes eterno SET FOR TAKEOFF THROTTLE FRICTION iiss ADJUST AVIONICS MASTER SWITCH ON mc COPY VFR OR IFR CLEARANCE coo uuu as sacan cdi dana COPY AVIONICS MASTER 5 eee n OFF BRIEFING asas ataq usatasussrusasqayquascusssssqsbasshusakuyaqausa qapaq PERFORM Briefing must contain Pilot flying Type of takeoff normal or short field and load Vr and Vclimb Engine failure procedure VFR and IFR departure procedure routing Initial climb instructions safety altitude VFR or IFR altitude Example fly normal takeoff 1009 5 up Vr 75 Vclimb 90 Engine failure below 85 knots abort on the remaining runway and advise ATC Engine failure above 85 knots and above obstacles fly the blue line brief the escape route ER E g VMC visual pattern or IMC ER to MSA then return for IFR ap proach sabena 9 NORM PROC a AIRLINE TRAINING CENTER INC REV 1 2 3 22 VFR departure procedure E g right crosswind departure climb to 3500ft MSA 4500ft or IFR departure procedure E g at 2000 turn R
13. 2 4 8 4 TAKEOFF ABOVE 1 700 8 5 1 ENG INOP UP TO 1 700 KG 8 6 1 ENG INOP ABOVE 1 700 8 7 LANDING DISTANCE 50FT UP 1 700 KG 8 8 LANDING DISTANCE 50FT ABOVE 1 700 KG 8 9 CRUISING TAS as 8 10 S pared SWIM 11 SYM 04 A 0062 Jaod 5 4 suonipuoo lt a 14340400 ONM gt SSv 51 3UNLYAZANEL 3 gt st oF s 08 8 8 8 Bs o sc Ot 02 SL OL Ol 02 62 OF se 004 MAN uia 4 0091 gap y 05 Jano maue Of 006 ansa 4 00 SP duo 3 5 qI 2065 0051 B 2 do 921 2 92 1vO 0061 U on WOOK gt gt apex 0051 3 006 apy Y O z 0041 m m T o 2 10042341 o u 5 on 004 gt LLI 9952 B UO m 009 0042 3 Z o z lt 0062 Es 0015 A 0001 Q 0068 26 67 edu C101 As TE 000 SNLL13S LL 5 00 0 5 oe 8 2 0 06 08 a 08 OS Or OE OZ OL 0 Ol Oe E gt 6 a 6 6 6 6 a lt sau 1
14. CHECK WEAR TREAD DEPTH OF TIRE Tires should be taken out of service when they have one or more flat spots Generally a single flat spot or skid burn does not expose the carcass body and the tire may remain in service unless severe unbalance is reported by the crew Small cuts are acceptable if they do not protrude into the tire carcass Cuts in the side wall are not acceptable Shallow chevron shaped cuts across the tread of a tire pose no problem they are caused by landing on a grooved concrete runway As long as the tread does not wear down into the body plies of the carcass the basic strength of the tire is not affected To provide traction during wet runway operation operators should replace their tires when the tread reaches 1 32 inch 0 79 mm WHEEL amp BRAKES HYDRAULIC BRAKE LINE CHECK sabena 9 NORM PROC pde AIRLINE TRAINING CENTER INC REV 1 2 w 3 1 1 When checking the brakes verify that there is even wear on the disc no scratches no grease and no leaks near the brake line Hide CHECK LANDING GEAR 5 CHECK REMOVE FRONT FUSELAGE AND NOSE LANDING GEAR FRONT CANOPY LEFT amp RIGHT 5 CHECK LEFT AND RIGHT FRONT BAGGAGE DOOR CHECK CLOSE amp LOCK NOSE LANDING GEAR STRUT LOCK amp CENTERING DEVICE CHECK Check
15. a lt o T gt Lu eee es ee sann nn 1 NO S3 19V 1590 30 NV312 1H9IS NI YHL AMH OL N3HM 138 1 392530 E p ssssss a days XON ysyyoayo 507 SVIM 001 A Jea ddy 5 uoeoaddy yal days SWIM OOL A 1950 UO Bae Gp uni eae 6 PATTERNS SVIM 06 01 A 507 sdej4 uni u spuoo s x 001 HOW Jawn WEIS 49v St yueq mL oU 5 ON E 9 lt sabena o PAT LIMITATIONS INTENTIONALLY LEFT BLANK QRH DA42 AIRSPEED LIMITATIONS Speed Definition Limitation Indicator Marking Never Exceed Speed an 194 KIAS 194 KCAS Red radial line Vne Maximum Structural 155 KIAS 155 KCAS of r nd of green arc Cruising Speed Vno 9 Design Maneuvering Above 3 400 Ibs 126 KIAS 126 KCAS Below 3 400 Ibs 120 120 5 Maximum Gear Operating Speed Extension 194 KIAS Retraction 156 KIAS Maximum Flaps 111 KIAS 111 KCAS of white ar n white a Extended Speed SMS 1 Engine Inopera
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18. SURFACES conos CLEAR ANTENNAS uU uu u M M CHECK NN FRONT CANOPY amp REAR DOOR u CHECK FIRE EXTINGUISHER U roo CHECK SECURE CONDITION UPPER SWITCH PANEL aaa ALL SWITCHES OFF ECU SWITCHES a a AUTO ALTERNATOR SWITCHES aa a as a ON LOWER SWITCH PANEL GEAR SELECTOR La aaa PARKING BRAKES U ELECTRIC ME e ON FWEL GAUGES on s E ec CHECK QUANTITY dE LDG ELECTRIC MASTER SWIM cco eoo OFF TERIM LOI LO OE NEUTRAL SUNSCREENS PITOT COVER STALL WARNING COVER amp TIE DOWN REMOVED GHOGKS uuu RN REMOVED TOWBAR PROPERLY STOWED REQUIRED EQUIPMENT ON BOARD FRONT BAGGAGE DOORS aaa SECURE sabena 9 NORM PROC biis AIRLINE TRAINING CENTER INC REV 1 2 3 37 LEFT WING AILERON SS SESE I CHECK AIBERONCANBYEINKAGE lt CHECK ROREIGNIOBJEGES IN AILERON PADDLE 2 2 CHECK STANIE WING TIP Ee E E E E E E E T POSITION LIGHT STROBE LIGHT Noe MAINIEUELE TANK E 3 STALEIWARNINGIDEVIGE U LULU LI asa FUEL TANK AIR OU TEET E WING SUREAGE e A TANK DRAIN TANK AIR INLET UU uu uuu ainia tada ORENINGSIONIEOWERISUREAGE m ee S AIRINLETS 2 AIR OUTLETS ea e ES E
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20. WEIGHT BALANCE DA42 sabena WEIGHT 8 BALANCE AIRLINE TRAINING CENTER INC REV 1 2 7 1 ITEM ARM IN WEIGHT LBS MOMENT IN LBS PILOT amp FRONT PASSENGER AFT PASSENGERS 128 0 NOSE BAG COMP MAX 66 LBS COCKPIT BAG COMP MAX 100 LBS BAG EXTENSION MAX 40 LBS DE ICING FLUID 39 4 1 1 KG LTR OR 9 2 LBS USG ZFW MAX 3638 LBS FUEL IN MAIN TKS 103 5 50 USG 7 01 LBS USG FUEL ALLOWANCE 103 5 START TAXI TOW MAX 3935 LBS TRIP FUEL 103 5 LW MAX 3748LBS DA42 sabena WEIGHT amp BALANCE AIRLINE TRAINING CENTER INC REV 1 2 7 2 Always check aircraft POH for latest weight amp moments shaded area only for 1785 3935 Ib max take off mass MAM 42 088 carried out Flight Mass Ib 4000 Center of Gravity Position in 3800 3600 3400 3200 3000 IIIIII WIL ILLI LI 2800 AIRCRAFT WEIGHT LBS MOMENT IN LBS 2844 80 N4129M 270648 70 N4130M 2836 00 269154 80 N4197D 2833 10 270104 81 dy 2867 30 271666 30 AUX TANKS DE ICE OO SFI DE ICE 2837 00 269175 00 W amp B INTENTIONALLY LEFT BLANK INTENTIONALLY LEFT BLANK QRH DA42 sabena PERFORMANCE AIRLINE TRAINING CENTER INC REV 1 2 8 1 TAKEOFF DISTANCE 50FT UP 1 700 8 2 DISTANCE 50FT ABOVE 1 700 8 3 TAKEOFF UP 1 700
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22. han ee ON FATDISYNERSORLERSEIEARAN 555 5 n sn 2 COPY AMIONIES OFF 5 ENGINE START FLOW STROBE LIGHTS DAY OR POSITION LIGHTS ON ENGINE MASTER SWITCHED uu u runt ri sere ASE EEE eas X RR ON ENGINE ON ENGINE INDICATIONS SSS E aE RA san a CHECK ENGINE GLOW tenor de co daha BRAKESG RAR ARE IGNITIONIKEY e ee cce n ee STARTER ANNUNCIATION OIE PRESSURES E ANNUNCIATIONS ENGINE SYSTEM CHECK REPEAT FOR OTHER ENGINE ANIONIESY MASTIER SWITCHI ON AFTER START CHECKLIST BEFORE TAXI FLOW PAT ee M ss sn n n S G1000 SET UP I F R B ss DA42 sabena NORM PROC AIRLINE TRAINING CENTER INC REV 1 2 3 42 TEST EE os Te mm TEST ECM C en M TM T EE CHECKED AUTO BEFORE TAXI CHECKLIST TAXI FLOW TAXI IGHT EE c FUEL SELECTORS PARKING BRAKE 2 22 22 BRAKES o n n FUEL SELECTORS E O E a S ON BEFORE TAKEOFF FLOW CONTROLS EREE CIRCUIT BREAKERS SSDS EE EREE E
23. sabena 9 NORM PROC AIRLINE TRAINING CENTER INC REV 1 2 3 1 5 STABILIZERS amp CONTROL SURFACES ELEVATOR TIPS CHECK A OR E RR QN DRE CHECK ELEVATOR TRIM TAB teet CHECK RUDDER TRIM tette tees CHECK TIESDOWN a een CHECK CLEAR TAIL SKID AND LOWER FIN ertet CHECK STATIC DISCHARGERS iis camen sete arri CHECK FUSELAGE LEFT SIDE UNDERSIDE STATIC PO Most een een FUSELAGE SKIN iii FUSELAGE UNDERSIDE Check for contamination with hydraulic fluid ANTENNAS UNDERSIDE 2 2 2 rcr tocca sena seb sono anal CHECK AFT CANOPY sabena NORM PROC an AIRLINE TRAINING CENTER INC REV 1 2 3 16 MISCELLANEOUS BATTERY MASTER SWITCH tana aise aua doceas ON For night flight only INTERIOR LIGHTING EXTERIOR LIGHTING ON AND CHECK ALL LIGHTING SWITCHES uuu aa ee OFF For IMC flight only PITOT HEAT 2 Bee Eee ON PITOT HEAT EXTINGUISHED PITOT TUBE PITOT HEAT For flight in known icing conditions only DEICE FLUID co ettet iiie CHECK QUANTITY The minimum de icing fluid quantity for dispatch is 22 liters 5 8 US gal or indication of 4 full on G1000 This minimum allows at least 90 minutes of ice protection with NORM selected The pilot must ensure adequate fluid quantity before each flight Max
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26. GO AROUND GO AROUND FLAPS POWERS bas FULL ee e ROTATE TO 9 FLAPS 20002202 een APP EXCEPT IF FLAPLESS APPROACH ALTIMETER amp VSIL u een POSITIVE CLIMB POSITIVE CLIMB GEAR c UP SPEED idiom CHECK ABOVE 85 KIAS FLAPS sits oi Pr UP SPEED was C MAINTAIN 90 KIAS e Em INFORM AFTER TAKEOFF CHECKLIST DA42 sabena MANEUVERS AIRLINE TRAINING CENTER INC REV 1 2 2 9 EFFECTS OF ASYMMETRICAL POWER EACH DEMO ONCE STRAIGHT AND LEVEL FLIGHT SPEED SI SS aus esse 105 KIAS LEFT OR RIGHT THROTTLE REDUCE TO IDLE AIRPLANE REACTION amp PERFORMANCE OBSERVE CLIMB SPEED E 90 KIAS LEFT OR RIGHT THROTTLE siccade REDUCE IDLE AIRPLANE REACTION PERFORMANCE OBSERVE DESCENT M 120 KIAS REDUCE TO IDLE PE OBSERVE LEVEL TURN SPEEDS c HR 105 KIAS OUTBOARD REDUCE IDLE AIRPLANE REACTION amp PERFORMANCE OBSERVE INBOARD THROTTLE REDUCE IDLE AIRPLANE REACTION amp PERFORMANCE OBSERVE CLIMBING TURN SPEEDS Ya ET EM MEE 90 KIAS OUTBOARD
27. 5 If unsuccessful AIRSPEED Salata asas as MIN 82 KIAS VYSE LANDING GEAR UP FLAPS UP ENGINE MASTER AFFECTED ENGINE OFF ALTERNATOR AFFECTED ENGINE FULE SELECTOR AFFECTED ENGINE LAND ASAP i I QRH DA42 sabena EMER AIRLINE TRAINING CENTER INC REV 1 2 4 13 OSCILLATING RPM POWER LEVER AFFECTED ENGINBEB CHANGE If unsuccessful ECU SWAP AFFECTED ECU B If unsuccessful ECU SWAP AFFECTED AUTO LAND ASAP DA42 sabena 9 EMER PROC AIRLINE TRAINING CENTER INC REV 1 2 4 1 4 RPM OVERSPEED prepared for loss of oil and engine failure POWER LEVER AFFECTEDENCGINE REDUCE I If unsuccessful ECU SWAP AFFECTED ENGINE ECU B I If unsuccessful ECU SWAP AFFECTED 4 I LAND ASAP I AIRSPEED Ysa ee Ss 80 120 KIAS PRESSURE ALTITUDE 6000FT POWER LEVER AFFECTED ENGINE IDLE FUEL SELECTOR AFFECTED 22 ON ALTERNATE AIR caa oie ea AS REQUIRED
28. DAA2 TWINSTAR QUICK REFERENCE HANDBOOK REV 1 2 1 sabena AIRLINE TRAINING CENTER INC DA42 sabena TABLE OF CONTENT sabena e Rev12 01 F PITCH POWER T BEE iiss ideas 1 unduiime 2 NORMAL PROCEDURES Easiness 3 EMERGENCY PROCEDURES 4 gwuld dite 5 LIMITATIONS A 6 WEIGHT AND a as 7 PERFORMANCE ssi a aa S 8 WARNING This QRH is to be used for training purposes only within SATC SFA In case there is a discrepancy between the or this the AFM POH will overrule the procedures limitations performance or systems described in this QRH INTENTIONALLY LEFT BLANK QRH DA42 sabena REVISION HIGHLIGHTS AIRLINE TRAINING CENTER INC REV 1 2 0 3 PPT Revised to be more accurate to match reality MAN Cruise speed gt 5000 145KTAS 1 engine out approach speed amp setting Introduction of Flap retraction speed schedule Steep turn speed 120KIAS Procedure adapted HACL V list items revised height note about seat adjustments removed Introduction of Approach to stall procedure Clean Stall recovery speeds NORM PROC Clarification of callouts config changes Loc amp GS alive Standardisation of cockpit flows items to match che
29. e THE ENGINE FAILURE FIRE AND SHUTDOWN CHECKLIST IN READ DO e WITH 1 PROPELLER FEATHERED STRAIGHT AND LEVEL TURNS BCAA REQUIREMENT e PERFORM THE ENGINE RESTART CHECKLIST UNFEATHERING PROCEDURE IN READ amp DO e RESTART BELOW 6 000 FT AGL SPEED 80 120 KIAS e DO NOT SWITCH OFF THE ALTERNATORS AND FUEL SELECTORS SIMULATE THESE ACTIONS WITHOUT ACTUALLY DOING THEM DA42 sabena MANEUVERS AIRLINE TRAINING CENTER INC REV 1 2 s 2 1 4 TOUCH amp GO e DURING THE TOUCH AND GO ROLL A UP BY THE INSTRUCTOR e VERIFY WITH INSTRUCTOR PRIOR TO RETRACTING FLAPS TAKEOFF YOU HAVE CONTROL GO AROUND 1 ENGINE GO AROUND FLAPS UP kjidqp M BLUE LINE APPROX 6 AFTER TAKEOFF CHECKLIST DA42 sabena 9 MANEUVERS AIRLINE TRAINING CENTER INC REV 1 2 2 1 5 SHORT FIELD TAKEOFF APPROACH FLAPS e TAKEOFF BRAKES E aa HOLD DA it LOWER TO 5 SPEED 85 KIAS E UP Sia a a D CLIMB AT 90 KIAS AFTER TAKEOFF CHECKLIST SHORT FIELD LANDING FINAL TURN COMPLETED E EEA LDG 80 KIAS AIM FOR THRESHOLD POWER em ADJUST FOR 80 KIAS SHORT FINAL CHECKLIST TOUCHDOWN BRAK
30. 1 full oil can 1 quart Maximum oil consumption is 0 1 quart hour sabena 9 NORM PROC en AIRLINE TRAINING CENTER INC REV 1 2 3 1 3 GEARBOX LEVEL irren in CHECK Check oil level through inspection hole in lower cowling COWEING a as CHECK PROPELLER SPINNER Sissies saa em CHECK Check no detrimental nicks cracks or dents in propeller blades and no traces of oil leak in the CSU Check blades no excessive play in CSU sss 5 WARNING a Even in the OFF position an engine may fire Always treat a propeller as potentially dangerous Do not take E gt position underneath a propeller at any time Never push pull the propeller to move the aircraft Never move the propeller by hand p2z2z2z2z2z2z2z22z22z2222z222z222z22z2z22c l EXHAUST u anna CHECK WARNING H The exhaust can cause burns when hot u PITT E 22222 2222222222 222 m m SSS VENTING PIPE sissies CHECK FOR BLOCKAGE GASCOLATOR AIR INLET DRAIN CLEAR Check for water and sediment drain until no water or sediment comes out Do not pour the drained fuel back into the tank NACELEE UNDERSIDE uu uuu een CHECK Check for excessive contamination particularly by oil fuel and other fluids gt AUXILIARY TANK FILLER CHECK CLOSE gt AUXILIARY TANK VENT OUTLET
31. 8282 2 2828288 u AVIONICS MASTER 5 ON AFTER START CHECKLIST BEFORE TAXI HEAT En arme ern CHECK Switch pitot heat ON Verify the amber PITOT HT OFF and STALL HT OFF annunciations disappear from the PFD Note an increase in AMP output Switch pitot heat OFF A A lasweousteas COMPLETE I F R B Initialize Aux Page 4 Check units e g hPa or mbar Check database WGS 84 Check CDI Selected AUTO ILS CDI capture MANUAL Flightplan go to FPL Check Dep AD correct if not enter Dep AD Load DP softkey Enter waypoints Load Apr press softkey then enter AD of arrival Radios Tune fcy Identify if possible on ground Set Nav 1 HSI Nav 2 BRG ADF BRG DME NAVI 2 sabena 9 NORM PROC ipie AIRLINE TRAINING CENTER INC REV 1 2 w 3 25 Bugs speed bugs QNH 3x Altitude bugs 2x Use the VFR and IFR real or simulated clearance each item chronologically as a guideline to set radios and navaids COM1 ground frequency COM1 will be the only radio used for ATC com munications during the whole flight COM2 will be the radio dedi cated to ATIS and company communications during the whole flight NAVI first VOR required by clearance set first radial on HSI NAV2 second VOR required by clearance set BRG 2 optional NAVI and NAV2 will be used as follows at all times VOR or LOC in use on NAVI next VOR on NAV2 DME and ADF as required by clearance At least 1 frequency m
32. Check G1000 for LOW LVL caution light If LOW LVS caution light Reduce power on affected engine Expect loss of coolant fluid Expect ENG FAIL LAND ASAP Refer to EMER L R OIL TEMP Increase power Reduce airspeed Check oil temp and coolant temp If within green range pressure monitor temp indication may be faulty If outside green range Reduce power on affected engine Expect ENG FAIL LAND ASAP Refer to EMER L R OIL PRES Refer to EMER L R FUEL TEMP Increase power Reduce airspeed If not recovered expect ENG FAIL LAND ASAP On ground Check circuit breakers amp increase RPM If not solved terminate flight In flight Check circuit breakers Reduce ELEC load If not solved Refer to ABN L R ALTN FAIL Reduce power Keep RPM in green range If not solved OVERSPEED Refer to EMER QRH DA42 sabena 9 EMER PROC AIRLINE TRAINING CENTER INC REV 1 2 4 7 L R OIL PRESS POWER AFFECTED REDUCE Be prepared for a loss of oil and engine failure LAND ASAP L R OIL TEMP A CHECK If oil pressure is too low POWER AFFECTED ENGINE REDUCE Be prepared for a loss of oil and engine failure LAND ASAP f oil pressure is in green range POWER AFFECTED
33. REQUIRED EMERGENCY WINDOVS OPEN AS REQUIRED If pitot heat fails ALTERNATE STATIC OPEN EMERGENCY WINDOWS ne CLOSE MIM 121 KIAS APPROACH SPEED 82 KIAS LANDING DISTANCE ACTUAL a X 1 4 RH DA42 sabena PROC 5 AIRLINE TRAINING CENTER INC REV 1 2 4 20 LDG WITH DEFECTIVE MAIN TIRE EE INFORM TOUCHDOWN L OR R OF CENTERLINE SIDE OF GOOD TIRE KEEP LOW SIDE OF GOOD TIRE DIRECTIONAL CONTROL MAINTAIN WITH BRAKES LDG WITH DEFECTIVE BRAKES After touchdown if necessary ENGINE MASTERS BOITH enne nenne OFF FUEL SELECTORS BOTH Q u uu uu OFF ELECTRIC MASTER aaa LDG GEAR UNSAFE WARNING If on for more than 20 seconds AIRSPEED 156 KIAS In cold temperature AIRSPEED sess SS MAX 110 KIAS LANDING GFAR saa RECYCLE If landing gear EXTENSION unsuccessful perform MANUAL GEAR EXTENSION If landing gear RETRACTION unsuccessful consider flight with landing gear down sabena 9 EMER PROC AIRLINE TRAINING CENTER INC REV 1 2 4 21 MANUAL GEAR EXTE
34. Sine merecen deco ea ON BEFORE TAKEOFF aeger FREE CIRCUIT BREAKERS comics er IN dE EE AS REQUIRED TRIMS sedsa Xv Dad les CD OR Ree SET FUEL SELECTORS u uuu ON SHORT BRIEFING use PERFORM The short briefing will include of takeoff normal or short or soft Initial heading and altitude Theinstructor answers Confirmed or amends as necessary Example VFR Normal takeoff heading 120 3 500FT confirmed Confirmed FRONT CANOPY secession a sete eec CLOSED amp LOCKED DOOR CHECK OFF sabena 9 NORM PROC ae AIRLINE TRAINING CENTER INC REV 1 2 w 3 29 BEFORE TAKEOFF CHECKLIST LINE UP When ATC clearance if required received and acknowledged to line up FIRST release the parking brake and start to roll to the runway THEN perform the following actions while taxiing Fast taxi turns immediately prior to takeoff should be avoided to prevent unport ing fuel feed lines On request of PF Line up items the starred items may be performed by the PM APPROACH Visually clear the final approach area before entering the runway and call out Approach free LANDING LIGHT TAXI LIGHT asss STROBE LIGHTS ALTIMETER Read threshold elevation from Jeppesen or other airport chart and call out Threshold elevation _____ f
35. e UP FLAPS nn au Du au UP IDENTIPY 22 22 22 cs DEAD FOOT DEAD ENGINE Announce Engine 1 2 failed THROTTLE ENGINE er Verify No yaw sound change I I F CONDITIONS PERMIT A C under control gt 82KIAS above MSA ENGINE TROUBLESHOOTING PERFORM WARNING Never case FIRE Refer to page 4 F CONDITIONS DO NOT PERMIT ENGINE MASTER SWITCH OFF After confirmation AETERNATOR me nee OFF FUEL SELECTOR 3 c X FEED em CONSIDER I Max imbalance 5USG eln case of fire CABIN HEAT AND OFF I ASAP DA42 sabena 9 EMER PROC AIRLINE TRAINING CENTER INC REV 1 2 4 1 2 ENGINE TROUBLESHOOTING POWER LEVER AFFECTED ENGINE IDLE T in conditions ALTERNATE AIR coin tan OPEN FUEL QUANTITY eS act FUEL SELECTOR AFFECTED ENGINE X FEED AS REQUIRED ECU SWAP AFFECTED ENGINBEB ECU B If unsuccessful ECU SWAP AFFECTED ENGINE AUTO CIRCUIT BREAKERS zii saia CHECK
36. hdg 120 intercept IWA R 030 Questions BEFORE START CHECKLIST ENGINE START Starting with the external power source perform procedure in read and do with DA42 AFM Abnormal Operating Procedures 4B 7 i CAUTION If diesel fuel or a blend of diesel Jet A 1 is used or if the fuel grade is unknown the engine must not be started if the fuel temperature indication prior to operation is below 5 C 2375 5 STROBE LIGHTS DAY OR POSITION LIGHTS ON ENGINE MASTER SWITCH ON It is recommended to start the LH engine pilot side first If re quired by operational reasons the RH engine can also be started first ENGINE GLOW m E CHECK ON Verify the L R engine glow annunciation is displayed on the PFD ENGINE INDICATIONS uaa ies meee ade CHECK Check that the engine indications are being powered Red X disap pear ENGINE GLOW sessed CHECK OFF PROPELLER AREA ociosa iris callo ici poda CLEAR sabena 9 NORM PROC T AIRLINE TRAINING CENTER INC REV 1 2 ws 3 23 Check the area around the airplane Open the window momentarily and shout Props clear BRAKES HOLD IGNITION KEY uuu ee einen START Turn the start key left or right as required to start the appropriate engine and release when the engine has started Do not overheat the starter motor Do not operate the starter mot
37. start of any checklist by calling out its title and will read all items out loud with sufficient pause between the items for verifica tion and or answer and will announce the checklist completed by an nouncing its title COMPLETED e PM Pilot Monitoring will be the instructor For single pilot opera tions all items listed in the table below under PM will have to be per formed by the PF All students must be proficient in operating the DA 42 in a single pilot environment e All configuration changes must be announced aloud by the PF E g Gear Up Down Flaps Up Approach Land e During IFR approach procedures the following items must be called out Localiser Alive Glideslope Alive Needle Alive VOR NDB GPS approach e Outer sabena 9 NORM PROC en AIRLINE TRAINING CENTER INC REV 1 2 3 3 FLOW AND CHECKLIST HANDLING Flow Checklist Phase of Flight Loud or Loud or Performed by Performed by Silent Silent Before Start PF Loud PM Loud After Start PF Loud PM Loud Before Takeoff Loud PM Loud Line Up PM Silent N A N A After Takeoff PF Silent by heart Loud Descent Approach Silent by heart Loud Landing Silent by heart Loud After Landing Silent PM Silent Shutdown Loud PM Loud sabena NORM PROC AIRLINE TRAINING CENTER INC REV 1 2 3 4 APPROACHING THE AIRCRAFT e Through flight same day s
38. the student of the correct position The rudder pedals must be adjusted as far as possible with full deflection of the rudder still possible This will enable more force to be applied on the pedal from the lower back and leg and more accurate inputs If required a cushion can be put behind the back FLIGHT CONTROLS Sissies sees PROPER OPERATION Check the flight controls for proper operation Stick left left aileron up right aileron down stick right right aileron up left aileron down Stick aft elevator up stick forward elevator down Left pedal right pedal Aileron and elevator deflections can be visually checked from the pilot s seat Do not push the rudder pedals too hard against system resistance SEATBEETS ge Use of all available seat belts and or harnesses seat is manda tory Seat belts of empty seats will be fastened and crossed over the seat bottom to prevent control interference or passenger injury during flight in turbulent air Fasten belts before closing canopy Do not unlock seat belts during flight or taxi at any time DA42 sabena 9 NORM PROC AIRLINE TRAINING CENTER INC REV 1 2 3 1 8 REAR DOOR iia CLOSED amp SECURED FRONT CANOPY sete POSITION 1 2 When operating the canopy pilots operators must ensure that there are no obstructions between the canopy and the mating frame for example seat belts clothing etc When operating the locking
39. 0 ia ida FULL SPEED ACCELERATING THROUGH 75 KIAS DA ROTATE TO 10 SPEED u uuu sass MAINTAIN 90 KIAS ALTITUDE uuu u uuu tes CLIMB TO INITIAL ALTITUDE HEADING ua tien een TURN BACK TO INITIAL HEADING LEVEL OFF AT INITIAL ALTITUDE p P I GRADUALLY DECREASE 4 SPEED uuu Ee 105 KIAS POWER ii te 50 RPM DA42 Sabena MANEUVERS AIRLINE TRAINING CENTER INC REV 1 2 2 6 TAKEOFF STALL POWER ON CLEAN NO AFM DATA ON EXACT STALL SPEED AVAILABLE EXPECT ACTUAL STALL SPEED TO BE BELOW 50 KIAS 0 BANK e ENTRY eee RAISE 20 POWER asa FULL POWER 65 UP INSTRUCTOR TRIM DO 75 5 e POWER Rt FULL SPEED ACCELERATING THROUGH 75 KIAS ROTATE TO 10 SPEED MAINTAIN 90 KIAS ALTITUDE xii BACK TO INITIAL ALTITUDE HEADING essa TURN BACK TO INITIAL HEADING LEVEL OFF AT INITIAL ALTITUDE SPEED Sauce aaah ide 105 KIAS POWER IEEE 5096 DA42 sabena MANEUVERS AIRLINE TRAINING CENTER INC REV 1 2 2 7 LANDING STALL POWER OFF FLAPS LDG 0 BANK 57 KIAS IDLE FORWARD CG MAX WEIGHT e ENTRY SPEED A hide ET i 105 KIAS A 5096 USE TRAFFIC PATTERN SEQUENCE TO ARRIVE A
40. 9 Wing lt days XON pu os q dO jeu Bejpunoqino 820H 45139349 days mo solu U 2 2 sabena PAT LVd 19V 13 008 MO 138 Q3GN3WIWO233 LON 09 11V LHOI3M NI 318ISSOd LON 13431 QRH DA42 REV 1 2 5 9 H e IW1IWWOOS SVIA 98 dejs JXON EVO LINA SV 907 Sdely 1 aye 1u os p yoay ag 001 eo oiv Jea dO seu ddy sde 4 dvd o1 yuaosap pue uo SWIM 28 aeaf punoug WO Buryseouddy 14001 W0 IV 9 va SBey ON 00Z 14002 VO lv Jamod 51122 sdel3 puno4e 09 L a pessiy SED days v 9 o 2 F F lt days u9eoaddy 9 uan punoquj a lt 933 1x N puaosag WN dO 15190940 v days SVIA SOL A mo saw sa bena 9 SVIM 98 2 A leuy
41. AL TIME IN SERVICE iie ae NOTE Write down the G1 000 total time in service cit a Es BACKUP OR REV MODE Set Engine page on PFD and System page on MFD GEAR WARNING FIRE DETECTOR CHECK The gear warning system is combined with the engine fire detection system push the gear warning fire detector test button and verify you hear the aural alert and observe the warning on the PFD screen If the aural alert or the warning does not appear maintenance ac tion is required MANUAL GEAR EXTENSION HANDLE CHECK PUSHED IN ALTERNATE AIR mi aan CHECK CLOSED ELAP incio clica rca lic CHECK LDG RUDDER TRIM 2 tii CHECK amp SET PARKING BRAKE Sis andauern ten sand caia SET DEFROSTER SWITCH een quwaq OFF BRRERERRRELSPERREREFPFERSFEEFEEHEFEREEREPEHRPERELERETEREFCERPEEEFFEFPGERSSER OFF VARIABLE ELEVATOR BACKSTOP sabena 9 NORM PROC AIRLINE TRAINING CENTER INC REV 1 2 w 3 21 Pull the stick fully aft While holding the stick at the backstop check the flaps in the landing position LDG and set both power levers MAX The stick must move slightly forward during power lever forward movement Set power levers to IDLE The stick must regain full movement during power lever rearward movement Se lect flaps UP For details see Chapter 7 of the AFM
42. CKLIST CRUISE Cruise checklist should be performed every 15 minutes FUEL STATUS m CHECK ENGINE INDICATIONS SYSTEM CHECK sabena 9 NORM PROC ar AIRLINE TRAINING CENTER INC REV 1 2 3 32 DESCENT APPROACH When the altimeter setting for the destination airport is set LANDING LIGHT 25 ee ON AETIMETERS 2 2 m 822220 Bananen SET 3X Set local altimeter setting for the destination airport Complete answer to this checklist item is altimeter setting set ANNUNCIATIONS ENGINE SYSTEM CHECKED GEAR WARNING HORN CHECKED FUEL SELECTORS es a ao ed Ond EOD e OS e dU ON DE ICING SYSTEM CONSIDER DESCENT APPROACH CHECKLIST LANDING Turning base LANDING GEAR cerei ee en DOWN 3 GREENS BRAKES Saed C CHECKED After checking the brakes make sure to slide your feet back to the normal position heels on floor toes on lower part of the pedals LANDING CHECKLIST SHORT FINAL LANDING GEAR 2254 tartans ner DOWN 3 GREENS TOUCHDOWN sabena 9 NORM PROC ne AIRLINE TRAINING CENTER INC REV 1 2 3 33 Maintain desired approach flight path with BA Maintain desired airspeed with power Reduce power to idle during the flare before the main wheels touch
43. E EA CLEAR ENGINES OMHLEMEI SEBE n n GEARBOX OIL LEVEL PROPELLER amp SPININER Se Hark 5 VENTING PIPE u uu CHECK FOR BLOCKAGE GASCOPATORAIR INLET U ara are Sire 24 DRAIN CLEAR NACELLE UNDERSIDE uuu uuu SS ESE eee CHECK CHECK CLOSE PAUXIIARY TANK VENT OUTLET onee a E E CHECK TANK DRAIN 6 aS mex s CHECK DRAIN LEFT MAIN LANDING GEAR LANDING GEAR CHECK DOWNS nn 2 CHECK WEAR TREAD MIRE eee CHECK WHEEL BRAKES HYDRAULIC BRAKE LINE E CHECK SHP MARKS aaah CHECK LANDING GEAR DOORS u CHECK sabena 9 NORM PROC ar AIRLINE TRAINING CENTER INC REV 1 2 3 38 5 Lh FRONT FUSELAGE NOSE LANDING GEAR FRONT CANOPY RIGHT nn LEFT amp RIGHT FRONT BAGGAGE CHECK CLOSE amp LOCK NOSE LDG GEAR STRUT LOCK amp CENTERING DEVICE CHECK DOWN WEAR TREAD amp DEPTH OF TIRE n LANDING GEAR amp UNKACE OAN SENSORS a E EPR CONN ee Mee GD m eU RIGHT MAIN LANDING GEAR LANDIN
44. EEE IN er AS REQUIRED GOOD TRIMS 222522225 SET FUEL SELECTOR uuu E RERA ON SHORT BRIEFING PERFORM RRONRBCANORY O CLOSED amp LOCKED DOOR CHECK OFF BEFORE TAKEOFF CHECKLIST LINE UP FLOW MAYBE PERFORMED BY PM ON REQUEST OF SANDING MGR e ES NS A 5 20 20 a A AEE ete E E a E COMPASS SYSTEM A PUM Oe HEAT a a E ESEE BRAKES POWER LEVERS RARAMETERS Las E elu E ML MI caer er ata CHECK sabena 9 NORM PROC nn AIRLINE TRAINING CENTER INC REV 1 2 3 43 AFTER TAKEOFF FLOW UP au UP ENGINE INSTRUMENTS c e 5 TRANSPONDER E hei ere Gi nce ease use CODE amp ALT MAP SWITCH AFTER TAKEOFF CHECKLIST CRUISE FLOW CHECK ENGINE INDICATIONS SYSTEM PAGE aae UU U a entes teras CHECK DESCENT APPROACH FLOW LANDING LIGHT ees AEN EE EE REE ase SRE SEE EE TE SE ETRS ON ee 250005 SET 3X ANNUNCIATIONS ENGINE SYSTEM PAGE nennen CHECKED GEAR WARNING DE IGING SYSTEM uU DESCENT APPROACH CHECKLIST LANDING FLOW LANDING GEAR DUCATU DOWN 3 GREENS h
45. ENGINE MASTER AFFECTED ENGINE eene ON STARTER essen IF 55 starts POWER AFFECTED ENGINE INSTRUMENTS eee CHECK GREEN RANGE ALTERNATOR AFFECTED ENGINE ON QRH DA42 sabena 9 AIRLINE TRAINING CENTER INC REV 1 2 4 15 L R ALTN AMPS CIRCUIT BREAKERS oi CHECK ELECTRICAL LOAD REDUCE LAND ASAP COMPLETE ELECTRICAL FAILURE CIRCUIT BREAKERS 22 een CHECK If unsuccessful SET ACC TO LEVER POSITION OR NOISE EUER VERIFY POSITION LAND ASAP Landing gear may slowly extend For landing MANUAL LANDING GEAR EXTENSION APPLY DA42 sabena 9 EMER PROC AIRLINE TRAINING CENTER INC REV 1 2 4 1 6 ENGINE FIRE ON GROUND POWER LEVERS IDLE ENGINE MASTERS OFF FUEL SELECTORS BOTH terit rti iter tiere uu ud OFF When engine and aircraft stopped CANOPY ERES OPEN ELECTRIC MASTER EVACUATE RH DA42 Sabena EMER PROC x AIRLINE TRAINING CENTER INC REV 1 2 4 1 7 CABIN SMOKE ABOVE 10 000FT OXYGEN SYSTEM INSTALLED OPTIONAL I A CHECK ON I EMERGENCY DESCENT ne INITIATE When passing 10 0008
46. ER O A Saa 60 Control the roll to repeat exercise in opposite direction RUDDER AS REQUIRED TO CENTER SIDE SLIP QRH DA42 Sabena 69 MANEUVERS AIRLINE TRAINING CENTER INC REV 1 2 24 STALLS e BEFORE EACH STALL EXERCISE VITAL ACTIONS H HEIGHT ABOVE 2300 FT AGL OUT OF CONTROLLED AIRSPACE NOT ABOVE TOWNS OR AIRFIELDS NO LARGE LOOSE ARTICLES SEAT BELTS SECURED ENGINE INSTRUMENTS IN LIMITS 180 OR 2x90 CLEARING TURN S FULL STALL RECOVERY TECHNIQUE VALID FOR ALL STALL EXERCISES e AS THE NOSE STARTS TO DROP 1 BODY ATTITUDE e IFA WING SHOULD DROP RUDDER ee OPPOSITE TO PREVENT YAW CHECK 75 KIAS USE TO LEVEL THE WINGS e FLYING SPEED HAS BEEN REGAINED 3 RECOVERY SEE BELOW ACCORDING TO THE TYPE OF STALL APPROACH TO STALL RECOVERY TECHNIQUE VALID FOR ALL STALL EXERCISES AT THE Ist INDICATION OF THE STALL BUFFET OR STALL WARNING 1 BODY ATTITUDE MAINTAIN e SPEED INCREASING BODY ATTITUDE DECREASE TO MAINTAIN ALTITUDE prm RETRACT ON SCHEDULE Sabena MANEUVERS QRH DA42 AIRLINE TRAINING CENTER INC REV 1 2 25 STALL CLEAN 0 BANK 64 KIAS IDLE FORWARD CG MAX WEIGHT ENTRY SPEED a EE 105 KIAS POWER REDUCE IDLE ALTITUDE u uuu 2 a MAINTAIN TRIM DO TRIM BELOW 75 KIAS POWER 50
47. ES zistan haaa Rs APPLY GRADUALLY INTENTIONALLY LEFT BLANK NORMAL PROC INTENTIONALLY LEFT BLANK sabena 9 NORM PROC DAJE AIRLINE TRAINING CENTER INC REV 1 2 3 1 INTRODUCTION BEFORE EVERY FLIGHT DEPARTING FROM HOME BASE 1 COMPANY INFORMATION CHECK ON WEBSITE BULLETINS WARNINGS LATEST DOCUMENTS 2 WEATHER NOTAMS 5 CHECK USE WEBSITE OR 1 800 WX BRIEF BY PHONE 37 ATIS iue OBTAIN THROUGH RADIO AT DISPATCH 4 FLIGHT RELEASE FORM PRINT amp COMPLETE 5 AIRCRAFT TECHNICAL LOG CHECK SQUAWKS 6 REQUIRED EQUIPMENT e CHECK 7 AIRCRAFT POUCH OBTAIN FROM DISPATCH CHECK CONTENT KEYS FUEL CARD LOGBOOK 8 I M S A F E CHECK 9 MISSION BRIEFING CHECK NOTES gt A black triangle sideways printed in front of a checklist or flow item indi cates optional equipment and must be read as if installed sabena 9 NORM PROC AIRLINE TRAINING CENTER INC 1 2 3 2 PROCEDURES FOR CHECKLISTS AND FLOWS e Student in the left seat Instructor in the right seat Student will perform all flying duties and scans and actions flows and all checklists except the ones shown in the table as PM Pilot Monitoring The reader will announce the
48. G GEAR STRUT amp LOOK 222222222222 CHECK DOWN UPLOGK SWITCHES a WEAR TREAD e CHECK WHEEL BRAKES HYDRAULIC BRAKE LINE CHECK SLIP MARKS LANDING GEAR DOORS CHOCK EA RIGHT ENGINE NACELLE S ARINEETS 2 AROS e e a CLEAR ENGINE CE e COWLING PROPELLER amp SPINNER EXHAUST VENTING PIPE CHECK GASCOLATORYAIR INLET ses EE NS EEE EEEREN DRAIN CLEAR NACELLE UNDERSIDE ERARE E J CHECK AUXILIARY TANK FILLER cs RET CHECK CLOSE PAUXIWARY TANK VENT CHECK AUXILIARY DANK DRAIN ss slapd CHECK DRAIN RIGHT WING CABIN VENT AIRIINDET a CHECK CLEAR TANK DRAINCTANK AIR INDEI ES ss CHECK DRAIN sabena 9 NORM PROC bin AIRLINE TRAINING CENTER INC REV 1 2 3 39 TANK OUTLET OPENINES ON LOWER ENTIREWING SURFACE E MAINIFUEL TANK BIERER cede cian 7 WINGCDIB eere sn u unn N E E STATIE DISCHARGERS tores POSITION LIGHT STROBE LIGHT TIESBOWN essen a iaa SE AIBERONSS LINKAGE nas xe etae due FOREIGN OBJECTS IN AILERON PADDLE e U U U U UU U CHECK ELAF AND LINKAGE 2 20 22 422202222 CHECK FLAP HINGES amp SAFETY PIN UU uu E A E ces CHECK NACELLE UNDERSIDE FUEL COOLER AIR IN amp OUTLET
49. HECKLIST DOWN 3 5 MA 2 2 ON PITOT HEAT OFF STARTED CODE GROUND UP SHUTDOWN CHECKLIST PILOT OVERHEAD READING EIGHT een seen CHECK OFF LIGHTS AVIONIC MASTER SWITCH ENGINE MASTER SWITCHES EVECTRICMASTER SWITCH m 2 OFF ENIMON KEN OUT BARKINGIBRAKE AS REQUIRED INTENTIONALLY LEFT BLANK INTENTIONALLY LEFT BLANK sabena 9 EMER PROC ni iin AIRLINE TRAINING CENTER INC REV 1 2 44 NON NORMAL WORKMETHOD 1 Announce the failure or read the G1000 annunciation E g Engine failure or Hi oil temp 2 Perform Recall items by memory if applicable When completed Recall items completed 3 Brief the Short term plan to PM Aircraft vertical amp lateral flight path altitude amp heading during the checklist reading 1 2min 4 Perform the Emergency checklist confirm recall items completed cor rectly Announce _____V list completed 5 Perform the Normal checklist if applicable 6 Longterm plan Collect all necessary info to make a decision Wx Notams Fuel remaining 7 Annouce Decision to PM ATC Passengers RH DA42 sabena EMER PROC 9 AIRLINE TRAINING CENTER INC REV 1 2 4 2 CHECKLIST TITLE The title of the checklist refer
50. ICE PROTECTION FAILURE LDG WITH DEFECTIVE MAIN TIRE LDG WITH DEFECTIVE BRAKES LDG GEAR UNSAFE WARNING MANUAL GEAR EXTENSION GEAR UP LANDING EMERGENCY DESCENT SUSPICION CARBON MONOXIDE sabena EMER PROC nn AIRLINE TRAINING CENTER INC REV 1 2 4 5 G1000 CAUTIONS Ey 5 Description L R ECU A FAIL 4 23 failed L R ECU FAIL 4 23 ECU B failed L R COOL LVL 4 23 Engine coolant level low L R ALTN FAIL 4 24 Alternator failed L R VOLTS LOW 4 24 Bus voltage too low PITOT FAIL 4 25 Pitot heating system failed PITOT HT OFF 4 25 Pitot heating system OFF STALL HT FAIL 4 25 Stall warning heating failed STALL HT OFF 4 25 Stall warning heating OFF DEICE LVL LO 4 26 De icing fluid level low DEIC PRES LO 4 26 De icing pressure low DEIC PRES HI 4 26 De icing pressure high L R FUEL LOW 4 27 tank fuel quantity low STICK LIMIT 4 27 Stick limiting system failed OTHER ABNORMAL PROC Situation BOTH ALTN FAIL HYD PUMP FAIL OR CONT OPS sabena AIRLINE TRAINING CENTER INC QRH DA42 REV 1 2 4 6 ENGINE IND OUTSIDE GRN RANGE COOLANT TEMP HI COOLANT TEMP LO during low power descent from altitude consider increasing power OIL TEMP HI OIL TEMP LO OIL PRES HI OIL PRES LO FUEL TEMP HI FUEL TEMP LO VOLTS LO RPM HI Refer to L R ENG TEMP
51. K CLEAR MAIN FUEL TANK 110 CHECK CLOSE PITOT PROBE O a Check pitot probe is clean orifices clear cover removed and no deformation STALL WARNING DEVICE TANK AIR OUTLET coo cio cenae e roit noti nee WING SURFACE 2 2 TANK DRAIN TANK AIR INLET CHECK DRAIN Check for water and sediment drain until no water or sediment comes out OPENINGS ON LOWER 5 1 CHECK Check for foreign objects and for traces of fuel if tank is full fuel may spill over through the tank vent sabena 9 NORM PROC AIRLINE TRAINING CENTER INC REV 1 2 3 9 LEFT ENGINE NACELLE AIR INLETS 2 AIR CLEAR ENGINE OIL LEVEL tenerent eene nivea CHECK Check oil level through inspection hole in upper cowling Normal oil quantity is 5 5 quarts Minimum is 4 8 quarts maximum is 6 3 quarts Do not refill when oil quantity is above 5 5 quarts When oil quantity is at 5 quarts add 1 full oil can 1quart Maximum oil consumption is 0 1 quart hour GEARBOX OIL LEVEL coccion a aa CHECK Check oil level through inspection hole in lower cowling COWLDING uu acs na aia aa CHECK PROPELLER amp SPINNER CHECK Check no detrimental nicks cracks or dents in propeller blades and no traces of oil leak in the CSU Check blades no excessive play in CSU WA
52. L POWER PITCH FOR THE BLUE CLIMB 1 ENGINE 82 KIAS LINE NORMAL CRUISE 140 KIAS lt 5 000 FT MSL NORMAL CRUISE 145 KTAS gt 5 000 FT MSL CRUISE 1 ENGINE 105 KIAS 90 100 VFR MANEUVERS 105 KIAS 50 STEEP TURNS 120 KIAS 60 MAX SPEED 155 KIAS Vno LIGHT TURBULENCE MAX SPEED 126 120 KIAS Va ROUGH AIR Gear Down TO EXPEDITE DESCENT 1 000 FPM Maintain speed DA42 Sabena MANEUVERS AIRLINE TRAINING CENTER INC REV 1 2 2 2 SPEEDS IFR HOLDING 120 KIAS 60 POWER CLEAN FLAPS UP 2 ENG 0 PO IFR COURSE REVERSAL 120 KIAS 60 POWER CLEAN FLAPS UP 2 ENG IFR APPROACH SPEED 2 ENG 100 KIAS 55 POWER GEAR DOWN FLAPS APP IFR APPROACH SPEED 1 ENG 100 KIAS 80 POWER GEAR DOWN FLAPS APP FLAPS SPEED SCHEDULE RETRACTION AT SPEED SELECT FLAPS gt 75 KIAS APP DA42 sabena 9 MANEUVERS AIRLINE TRAINING CENTER INC REV 1 2 2 3 SLOW FLIGHT DECELERATION ACCELERATION E FULL MAINTAIN BA M GRADUALLY DECREASE 4 105 KIAS a 50 STEEP TURNS SPEED vaina a 120 KIAS BANK ANGLE NORMAL ROLL RATE TO 45 INCREASE by 2 BA 3 E CN INCREASE 5 RUDDER A habia AS REQUIRED TO CENTER SIDE SLIP Do not trim HEADING 15 BEFORE INITIAL HEADING BANK 2 Em NORMAL ROLL RATE 0 E SR A EE DECREASE TO 1 POW
53. N3NOdAO2 a sSvi sini verint Lue FE 3191590 Y 09 JINVLSIO 33O073 V L lt pared pyeu SvI 64 SvIx ZZ A 0062 59813 suorypuoD INSNOdINOS 5 30 81n0 N 0L gt 002 m 008 g qu 029 Y OS sougsip O L inso 0001 00 su VG OF pumpesH 3 Q 919595 0SZL 0071 4 89 2 51 1vO 4 OO 50 gt E 7 gt 005 lt 5 0081 m 5 000 009 Y 0 te 1232 m 004 u Y ove m 5 m 0095 q m 008 3 Z opz 4 008 kn Ba 6101 541135 200 0075 400004 LLI 2 lt E Y LL LL 8 8 01 00 06 OF OF O9 05 OF OF OF Ob OF lt 50FT ABOVE 1 700KG LN3NOdVIQO ONM 9 SSYN OL 4 39017434181 3018 100 0021 312 1880 Y OS YSAO JONVLSIO 340 3 1 2 9 o OQ u e 44 pesdsury 00 Z oq Jeo sde y suonmpuoo lt 65 SSW HON Sun Lead WEL 3015170 a gt 2 3 5 3 8 8 Ov SE 07 SL OL S 0 C 01 9 02 52 E gt
54. NSION AIRSPEED e E E s MAX 156 KIAS GEAR INDICATOR LIGHTS ae TEST ELECTRIC MASTER mem CHECK ON BUS VOLTAGE ae CHECK NORMAL GEAR SELECTOR ne ee DOWN MANUAL EXTENSION HANDLE PULL f necessary AIRSPEED MAS 110 KIAS pr M APPLY MODERATELY GEAR INDICATOR LIGHTS eee CHECK 3 GREENS GEAR UP LANDING e LANDING GEAR COMPLETELY RETRACTED INFORM NORMAL Just before touchdown POWER LEVERS isses een enn enne IDLE After touchdown ENGINE MASTERS BOTH asas aaa OFF FUEL SELECTORS BOTH aaa OFF ELECTRIC MASTER l issa aad OFF QRH DA42 sabena 9 EMER PROC AIRLINE TRAINING CENTER INC REV 1 2 4 22 EMERGENCY DESCENT dB re Em UP i LANDING GEAR sie ee denen DOWN POWER LEVERS IDLE i AIRSPEED m 5 l LIGHTS Dy cb Level off FL100 10 0000 or MEA MSA whichever is higher SUSPICION CARBON MONOXIDE l CABIN HEAT amp DEFROST VENTILATION 6 OUTLETS i EMERGENCY WINDOWS aes sans sea CANOPY BELOW 120 1 UNLATCH IF NECESSARY I Push lock the cooling position DOOR OPEN AIRSPEED ic REDUCE CANOPY REAR DOOR amp FRONT BAGGAGE DOORS
55. NTENTIONALLY LEFT BLANK PATTERNS PAT INTENTIONALLY LEFT BLANK 2 5 14 SVI406 A ddy sdej4 SVIM S8 9508 se peo1 adojs 5 20 vg 6 Jamod 09 QRH DA42 REV 1 2 5 1 907 sdel3 G3i31dWO9 1 SVIA GZ eye umop Jea 10849 peads IHOHS yoays Jamod Jamod n4 33031 Buipue 1 o 2 2 F F lt 2511429 2 4Joexe ey 381149249 yoeoiddy quaoseg NORMAL SVIA SOL A 9006 96 A BO paa g SVIM06 9008 2 8 v8 SWIM 06 SAydes A 9 dav 3921 aseq uo jueosep 330 13431 SUJENNN INV38V umop 1 909 3SV8 ONINYAL 5 9 SVIM Z8 A dn sea6 joejuoo 5484 28 9 vg asou ay iamo 3NION3 innu sun SHEER ERE E FERE EHE E ERE HERE RR onma HEU SVIMS8 A 08 p p u se peo edo s 10 vg ddy 54 ss 9 Jamod ONNOYYOO QRH DA42 REV 1 2 5 2 SWIM 28 S4 Ie aJeJ0y umop ame paadg 5 yoayo Jamod MELIS Jewod jn 4 3JO3 Vv1
56. PITOT HEAT TE OFF IMP OFF Expect battery power to last for 30 minutes Expect engine stoppage after this time LAND ASAP L R VOLTS LOW Possible reasons are Fault in ELEC PWR supply RPM too low Continue with ENGINE INSTRUMENT INDICATIONS OUTSIDE GREEN RANGE VOLTS LOW QRH DA42 sabena 9 EMER PROC AIRLINE TRAINING CENTER INC REV 1 2 4 25 PITOT FAIL PITOT HT OFF PITOT HEAT is CHECK ON e HEAT cannot be recovered Avoid icing conditions e If icing conditions cannot be avoided Expect failure of the pitot static system 5 VAL VE nel OPEN Leave area with icing conditions see EMER UNINTENTIONAL FLIGHT INTO ICING STALL HT FAIL STALL HT OFF HEAT e If STALL HEAT cannot be recovered Avoid icing conditions e Ificing conditions cannot be avoided Expect loss of aural stall warning Leave area with icing conditions see EMER UNINTENTIONAL FLIGHT INTO ICINC DA42 sabena 9 EMER PROC AIRLINE TRAINING CENTER INC REV 1 2 4 26 DE ICE LVL LO Maximum duration of ice protection NORMAL mode 45 min e HIGH mode 22 min Leave area with icing conditions accordingly DE ICE PRES LO e If DE ICE PRES LO light still ON PUMPT PUMP 2 s SELECT OTHER PUMP If necessary prime pump by activating windshield pump e If DE ICE PRES LO light still ON ALTERNATE
57. RNING Even in the OFF position an engine may fire Always treat a propeller as potentially dangerous Do not take position underneath a propeller at any time Never push pull the propeller to move the aircraft Never move the propeller by hand EXHAUST viii esa CHECK A a EE WARNING H The exhaust can cause burns when hot 1087 lt VENTING PIPE en sn sabena NORM PROC er AIRLINE TRAINING CENTER INC REV 1 2 3 1 0 Check for water and sediment drain until no water or sediment comes out Do not pour the drained fuel back into the tank UNDERSIDE Ses CHECK Check for excessive contamination particularly by oil fuel and other fluids gt AUXILIARY TANK FILLER CHECK CLOSE gt AUXILIARY TANK VENT OUTLET CHECK gt AUXILIARY TANK DRAIN eene nnn CHECK DRAIN Check for water and sediment drain until no water or sediment comes out LEFT MAIN LANDING GEAR LANDING GEAR STRUT amp Check visually and verify strut height is sufficient Typical visible length of bare piston is at least 4cm 1 6 DOWN amp UPLOCK SWITCHES 3
58. RS PAS s 222222 2 AS REQUIRED MU E ACKNOWLEDGED FUEL QUANTITY CHECKED ALTERNATE CLOSED A OO IDLE VARIABLE ELEVATOR BACKSTOP CHECKED EUEIESEEECTOHS ON TRIMS E E E E EE E SET AFTER START CHECKLIST OIE PRESSURE ee eee erate anes sr eases aeons ener CHECKED ANNUNGIATORS ENGINE SYSTEM PAGE emen CHECKED BEFORE TAXI CHECKLIST BIT OR HEANOR CHECKED SE a LE COMPLETED AUTO PILOT TEST uu eee COMPLETED ELECTRICAL TRIM TEST 1 COMPLETED ECU ECU SWAP Er ss AUTO ANN 2 2 EM CHECKED AN ON FLIGHT CONTROLS FREE CANDIDA 22222 222 CLOSED 8 SECURED sabena NORM PROC nn AIRLINE TRAINING CENTER INC REV 1 2 3 47 AFTER TAKEOFF CHECKLIST UP NO LIGHTS 5 UP ENGINE CHECKED LANDING IGEN AS REQUIRED DESCENT APPROACH CHECKLIST These items only when remaining in the pattern LANDING LIGHT ALTIMETERS ANNUNCIATIONS ENGINE SYSTEM PAGE ON aN a ae CONSIDER LANDING C
59. SWITCHES esses dasa nennen OFF STROBE LIGHT esses es OFF ELECTRIC MASTER SWITCHI aa ease OFF IGNITION KEY oe aan OUT PARKING BRAKE AS REQUIRED Never taxi the aircraft facing fuel pumps with engines running park parallel to pumps Stop with plenty of space then pull the aircraft forward into the fueling position Do not set parking brake unless on a slope PILOT OVERHEAD READING OFF SHUTDOWN CHECKLIST MOORING PARKING BRAKE assassins eames eae RELEASE Push aircraft backward or pull aircraft forward into parking space using the tow bar for steering Do not turn the nose gear beyond its steering radius in either direction as this will result in damage to the nose gear and steering mechanism TOW BAR qe STOW PROPERLY SUNSCREENS STALL WARINING COVER PITOT COVER TIE DOWN ee INSTALL Tie down ropes are required when the aircraft is left unattended longer than for a normal crew change If no tie down ropes are available on ramp use the aircraft tie down ropes in flight gear bag Secure tie down ropes to the wing tie down rings and to the tail skid at approximately 45 angles to the ground Use bowline sabena 9 NORM PROC ne AIRLINE TRAINING CENTER INC REV 1 2 3 35 knots square knots or locked slip knots Do not use plain slip knots Parking brake is required when aircraft is n
60. T FINAL CONFIGURATION LDG FLAPS 85KIAS 40 85 KIAS FLIGHT PATH iens ESTABLISH A STABILIZED DESCENT 85 5 POWER es IDLE TO SIMULATE A FLARE TO LAND e RECOVERY POWER cnt pa FULL SPEED ec 75 KIAS m TO 5 ALTIMETER amp VSL nie RR uu la POSITIVE CLIMB POSITIVE CLIMB UP SPEED un O 85 KIAS El aT UP kdo Em MAINTAIN 90 KIAS ALTITUDE iiiter CLIMB TO INITIAL ALTITUDE HEADING 2 isosassssrsspushapayuqushankas TURN BACK TO INITIAL HEADING LEVEL OFF AT INITIAL ALTITUDE H GRADUALLY DECREASE 4 SPEED e EE 105 KIAS POWER 2 nnnmt 50 QRH DA42 Sabena MANEUVERS AIRLINE TRAINING CENTER INC REV 1 2 2 8 FLAPLESS PATTERN SEE ALSO CHAPTER PATTERNS e SPEEDS ALL TARGET PATTERN SPEEDS ADD 5 KNOTS KEYPOINTS BODY ATTITUDES WILL BE HIGHER THAN NORMAL TRIM DOWNWIND sess una EXTEND SLIGHTLY 1 4 MILE SLOPE eiii eei Rer FLY A NORMAL 3 SLOPE TO RWY 1 2 5 a APPLY REDUCED FLARE DON T FLOAT GO AROUND assassin GO AROUND FLAPS UP
61. TEST mode activates the DEICE LVL LO caution immediately if the de ice fluid quantity is low below 10 liters and the DEIC PRES LO caution after 120 seconds PRES Hl rn nes VERIFY NOT ILLUMINATED DESICE mem HIGH PRES LO EXTINGUISHES AFTER 205 If the ambient temperature is above 10 C 50 F the system pressure may not get high enough to disable the DEIC PRES LOW warning pe M OFF 5 asas CIRCUIT 5 soos en IN If a circuit breaker needs resetting check why it has tripped or been pulled 61 000 nicae a qa ACKNOWLEDGE Wait until power up completed Press ENT on MFD to acknowledge Note the engine instruments are not available on the MFD until acknowledged Push the DISPLAY BACKUP button on the audio panel to activate the G1000 reversionary backup mode Push the SYSTEM softkey on the MFD to activate the engine system page sabena NORM PROC nun AIRLINE TRAINING CENTER INC REV 1 2 3 20 FUEL TEMPERATURE 2 2 2 3 aa CHECK Limitation Diesel Fuel Engine start not below 5 C Take Off not below 5 JET A1 fuel Engine start and Take Off not below 30 C Make sure which fuel grade is being used see Section 7 9 5 of the AFM If it is not possible to determine the fuel grade the diesel fuel temperature limitations must be observed FUEL QUANTITY em CHECK FUEL CALCULATOR e SET TOT
62. ame airplane same crew e Through flight walk around fuel oil and tires only e cockpit flows must be read out loud NEARBY OBSTACLES esere eee seserinis CHECK FLAP POSITION Siesta ahaa eas NOTE The flap position should be noted before boarding the airplane SURFACES 2 siones CLEAR Check that all movable surfaces are clear and can be moved without hitting obstacles zx TD li an CHECK Check presence and condition of following antennas COM NAV transponder ELT sabena 9 NORM PROC be AIRLINE TRAINING CENTER INC REV 1 2 u 3 5 PRELIMINARY INSPECTION careful not to use top of the instrument panel as a support when entering or exiting the aircraft Use the dedicated handle behind the glareshield for support Verify that the canopy is clean and undamaged Check for cracks and major scratches Check locking mechanism To avoid scratch ing the paint or damaging the wing do not sit or put any equip ment on the wing Do not use the top of the instrument panel as a shelf for equipment at any time Make sure not to touch the canopy with hands equipment or charts IGNITION KEY uuu ea CHECK OFF amp KEY REMOVED FRONT CANOPY amp REAR DOOR nne FIRE EXTINGUISHER UPPER SWITCH PANEL ECU SWITCHES ALTERNATOR SWITCHES LOWER SWITCH Check pitot heat
63. changes short final lt 500 AGL are not recommended respect the stabilized approach concept Exception is made if landing dis tance is a factor If visual contact with the runway is established prior 500ft AGL LDG flaps may be selected otherwise a flaps APP landing is recom mended if sufficient rwy length is available When becoming visual on an ILS approach you must remain established on the Glide Slope don t dive below the profile until crossing the THR For a Non precision approach you must remain on the PAPI or if no PAPI installed a constant flight path to the aiming marks blocks Diving below the profile is only allowed if landing distance becomes a factor This must be clearly briefed in advance ALTITUDE BUG AND ALTITUDE WARNING Altitude bug gives a visual indication on the G1000 PFD Altitude warning gives an aural warning when approaching 1000ft the selected altitude on the AP When established on GS or leaving the FAF altitude Set Altitude bug on DA MDA rounded up 100ft and the AP altitude on the go around altitude This will give a visual warning when reaching the minima and an aural warning when approaching the level off altitude in the go around PAT ALA YOLOV V SI 39NV1SIGQ ONIONVI 31 1d3X3 LON 33V 19V 13 00 AO138 SHONVHO NOILVS9IJNOO a QRH DA42 REV 1 2 5 6 sdel3 SVIM06 A Anisoq
64. cklist amp flows Added procedures to test De ice system Electrical trim amp Autopilot Overview of flows completely revised to match Norm Proc Normal Checlist revised to match Norm Proc amp Diamond checklist V14 1 EMER PROC Definition of Non normal work method Clarification of Emergency checklists layout Warnings Cautions Recall items Checklists layout adapted Oil Temp emergency checklist corrected according to POH L R Engine fire failure Emergency checklist replaced by Engine failure fire and shutdown Emergency checklist Cabin Smoke and Fire above 10000 Only applicable to aircraft equipped with oxygen system PAT Speeds Settings amp Body attitudes updated for visual patterns Introduction of stabilized approach concept amp configuration changes LDG Checklist performed earlier on instrument approaches W amp B PERF BEW and moments updated Loadsheet Usable fuel 50USG max Introduction of CRUISING TAS graph TOC INTENTIONALLY LEFT BLANK TABLE PPT INTENTIONALLY LEFT BLANK QRH DA42 sabena PITCH POWER REV 1 2 1 1 BODY SPEED CONF ALT ENGINES POWER ATTITUDE TAKEOFF VR 75 KIAS FLAPS UP 2 engines FULL 9 CLIMB 90 KIAS CLEAN 2 engines 100 9 105 KIAS CLEAN 2 engines 90 6 80 KIAS CLEAN 2 engines 100 13 82 KIAS CLEAN 1 engines 100 6 LEVEL 65 KIAS CLEAN 2 e
65. dd M rc EU CHECKED PARKING BRAKE OFF Fe APS Ee ipd AS REQUIRED LANDING CHECKLIST SHORT FINAL FLOW LANDING GEAR scot u nee puse le ERREUR DOWN 3 GREENS AFTER LANDING FLOW MAYBE PERFORMED BY PM ON REQUEST OF PF CANDIA Mao SEM OFF DA42 sabena NORM PROC REV 1 2 3 44 Miser saunter Stansted ON 525 25 55 E CEES t OFF TIME a START ENGINE IDLE TRANSPONDER coca E o i uu a CODE GROUND UP AFTER LANDING CHECKLIST ENGINE SHUTDOWN FLOW PARKING PILOT OVERHEAD READING LIGHT SHUTDOWN CHECKLIST MOORING FLOW PARKING BRAKE ESE sele RELEASE TOWBAR a sn n UE LEE STOW PROPERLY SUNSCREENS STALL WARNING COVER TIE DOWNS PITOT COVER INSTALL SEAN BEES LOCK PERSONAL ITEMS occasion posters db unii etait cocked CLOSE AND LOCK INTENTIONALLY LEFT BLANK sabena NORM PROC AIRLINE TRAINING CENTER INC REV 1 2 3 46 BEFORE START CHECKLIST c COMPLETED RUDDER ADJUSTED AND LOCKED LOCKED PARKING BRAKE u SET GEAECWARNING EIRETDETEGTOR CHECKED AVIONICS MASTER SWITQGH ed OFF EEECTRIGIMASTER SWIICH u u ete Ren re RE REEL ON ALTERNATORS CIRCUIT BREAKE
66. dds INCREASE as required This requires to increase power on the other engine check tem perature or start a descent according to MEA MSA f coolant temperature not returning to green range Be prepared for a loss of oil and engine failure LAND ASAP If LOW COOL LVL caution light ON POWER AFFECTED enn enne REDUCE Expect loss of coolant fluid Be prepared for an engine failure QRH DA42 sabena PROC AIRLINE TRAINING CENTER INC REV 1 2 4 1 0 L R ENGINE FIRE FAILURE AND SHUTDOWN n case of fire CABIN HEAT AND enn enne OFF l DURING PERFORM TAKEOFF RE LANDING I POWER LEVERS ME S IDLE l el quM APPLY E INFORM elf necessary I ENGINE MASTER BOTH OFF FUEL SELECTORS BOTH a anr auraa an eE OFF ELECTRICAL MASTER isma I i I CONTINUED ON NEXT PAGE RH DA42 sabena EMER PROC A AIRLINE TRAINING CENTER INC REV 1 2 41 1 L R ENGINE FIRE FAILURE AND SHUTDOWN IN FLIGHT AIRSPEED ABOVE 68 KIAS POWER LEVERS 2 22 AIRPLANE MAINTAIN 3 5 bank into good engine I Ball delfected into good engine Speed Vyse 82KIAS I GEAR
67. eet This may be done while taxiing out of the run up area Altimeter reading should not differ more than 60 feet from threshold elevation at sea level and 80 feet at 5000 feet pressure altitude COMPASS SYSTEM na RUNWAY HEADING This is a runway compass system check Read runway heading from chart takeoff data QFU and call out Runway heading degrees Check HSI and magnetic compass Maximum difference allowed between published runway heading and any compass sys tem is 6 If a large discrepancy exists do not take off but investi gate the cause first wrong runway compass system malfunction PITOT J T iye AS REQUIRED sabena 9 NORM PROC ar AIRLINE TRAINING CENTER INC REV 1 2 3 30 Switch pitot heat ON Verify the amber PITOT HT OFF and STALL HT OFF annunciations disappear from the PFD TAKE OFF Before applying engine power for takeoff top the timer and call out Takeoff have control The instructor will confirm You have control When the aircraft is lined up perform the available takeoff power check BRAKES 2 uu HOLD POWER LEEVERS u een FULLY FORWARD PARAMETERS cocer me Rennen CHECK Check ANNUNCIA TIONS L L u aaa la pe Ce debo CHECK ij STABILIZES 2240 TO 2300 RPM LOAD esses S TE STABILIZES 90 TO 100 Call out Power checked Note 1 Under high temperature high altitude conditions load indica tio
68. handle DO NOT apply undue force A slight downward pressure on the canopy may be required to ease the handle opera tion FRONT BAGGAGE DOORS a CLOSED Visually check that the front baggage doors are closed AVIONICS MASTER SWITCH ELECTRIC MASTER SWITCH ENGINE MASTER SWITCHES When switching on the electric master switch the electrically driven hydraulic gear pump may activate for 5 to 20 seconds in order to restore system pressure Should the pump operate continuously or intermittently this indicates a malfunction in the landing gear sys tem IGNITION KEY PITOT HEAT u ua nee ande ALTERNATE STATIC Sissies Soe ius OFF ALTERNATORS ECU EE BIMMER CONTROL asas u SET Use the rotary buttons to adjust instrument lighting and flood light Day flight OFF Night flight as required avoid setting the lights too bright LIGHT SWITCHES qe IRR OFF EMERGENCY SWITCH CHECK OFF amp GUARDED NORM PROC DEE AIRLINE TRAINING CENTER INC REV 1 2 3 19 STANDBY INSTRUMENTS uuu a CHECKED MAGNETIC COMPASS assassinate nennen anne CHECK Check magnetic compass for normal reading no bubbles in the fluid and no leaks Deviation chart present DEVIATION CARD u u eritis aquqssssssspasqpasqsssysscasyotqapaqasqkaqas CHECK P DE ICING SYSTEM 2t co ces iocos CHECK ANNUN TEST 22 22 22 ON The ANNUN
69. imum system operating times with full de icing fluid NORM mode 2 hrs 30 min HIGH 2 cet Dau luu usa la saccade 1 hr Mode nennen 30 min Do not operate the main pumps with an empty de icing fluid tank If priming is required use the windshield de icing perse ON ICE Ele CHECK BATTERY MASTER 5 nna OFF sabena 9 NORM PROC ipd AIRLINE TRAINING CENTER INC REV 1 2 w 3 1 7 COCKPIT PREPARATION Before entering the cockpit check Towbar removed Nose baggage doors closed and locked and Rear door closed and secured RUDDER PEDALS et ADJUSTED amp LOCKED The rudder pedals may only be adjusted on the ground The pedals are unlocked by pulling the black handle which is located behind the rear attachment Forward adjustment while keeping the handle pulled push the pedals forward with your feet to the desired posi tion Release the handle and allow the pedals to lock in place Rear ward adjustment using the unlocking handle pull the pedals back to the desired position Release the handle and allow the pedals to lock in place Verify that the pedals are locked by applying pressure to try to move them The instructor should advise
70. ne speed e Show that max climb rate is obtained with 2 to 3 degrees of bank into the good engine 2 Optimum control Vmca demo e Show that lowest is obtained with 8 10 degrees of bank into good engine ZERO ZERO ZERO BANK BANK SIDESLIP RUDDER ANGLE DA42 sabena MANEUVERS AIRLINE TRAINING CENTER INC REV 1 2 2 1 2 VMCA DEMONSTRATION e BEFORE EACH DEMONSTRATION VITAL ACTIONS H HEIGHT ABOVE 4000 FT AGL OUT OF CONTROLLED AIRSPACE NOT ABOVE TOWNS OR AIRFIELDS NO LARGE LOOSE ARTICLES SEATS AND SEAT BELTS SECURES ENGINE INSTRUMENTS IN LIMITS 180 OR 2x90 CLEARING TURN S e SEQUENCE SPEED A 105 KIAS POWER aaasta FULL GOOD ENGINE IDLE DEAD ENGINE BANK ns 5 INTO THE GOOD ENGINE eiie densis SLOWLY INCREASE SPEED DECR 1 SEC RUDDER PRESSURE GRADUALLY INCREASE TO MAINTAIN HEADING WHEN ROLL OFF STALL HORN OR LOSS OF DIRECTIONAL CONTROL OCCURS RUDDER MAXIMUM WHEN DIRECTIONAL CONTROL IS REGAINED POWER ee FULL GOOD ENGINE IDLE DEAD ENGINE DDR 82 KIAS 5 INTO THE GOOD ENGINE E REG TO ORIGINAL HEADING NOTE AIRPLANE PERFORMANCE DA42 sabena 9 MANEUVERS AIRLINE TRAINING CENTER INC REV 1 2 2 1 3 REAL ENGINE SHUTDOWN RESTART IN FLIGHT e STAY WITHIN 10 NM OF A SUITABLE AIRPORT FOR THE DA42 e REMAIN OR ABOVE 4 000 AGL
71. ngines 40 10 105 KIAS CLEAN 2 engines 50 4 120 KIAS CLEAN 2 engines 60 1 lt 5 000FT CLEAN 2 engines 70 0 140 KIAS gt 5 000FT CLEAN 2 engines 7090 7596 0 145 5 105 KIAS CLEAN 1 engine 90 4 APP FLAPS 110 KIAS 2 engines 65 1 GD DESCENT 500FPM 130 KIAS CLEAN 2 engines 50 2 120 KIAS CLEAN 2 engines 40 1 105 KIAS CLEAN 1 engine 75 1 DA42 sabena PITCH POWER SPEED CONF ALT ENGINES POWER BODY ATTITUDE TRAFFIC PATTERN 2 ENGINES 105 KIAS CLEAN DOWNWIND 50 4 95 KIAS APP FLAPS GU DOWNWIND 50 1 90 KIAS APP FLAPS GD BASELEG 50 2 85 KIAS LDG FLAPS GD FINAL 50 4 FLAPLESS PATTERN 2 ENGINES 105 KIAS CLEAN DOWNWIND 50 4 100 KIAS CLEAN GU DOWNWIND 45 5 95 KIAS CLEAN GD BASELEG 35 2 90 KIAS CLEAN GD FINAL 35 1 TRAFFIC PATTERN 1 ENGINE 105 KIAS CLEAN DOWNWIND 9096 T4 95 KIAS CLEAN GD BASELEG 7096 2 95 KIAS APP FLAPS GD FINAL 7096 3 85 KIAS LDG FLAPS GD SHORT FINAL 8096 4 IFR APPROACH 100 KIAS APPFLAPS GD 2 engines 55 4 100 KIAS APP FLAPS GD 1 engine 80 4 MANEUVERS INTENTIONALLY LEFT BLANK QRH DA42 SPEEDS NORMAL CLIMB 90 KIAS lt 1 000 FT AGL NORMAL CLIMB 105 KIAS gt 1 000 FT AGL BEST RATE OF CLIMB 79 KIAS CLEAN VY BEST ANGLE OF CLIMB 79 KIAS CLEAN Vx TO EXPEDITE CLIMB 85 KIAS FUL
72. ns below 9096 are possible If the engine does not stabilize at the target RPM of 2240 to 2300 RPM do not continue take off 2 An engine is warm for takeoff when the throttle can be opened fully without engine faltering backfiring or skipping and without a reduction in engine oil pressure It is important to check takeoff power early in the takeoff run or power appli cation Any sign of rough engine operation or sluggish accel eration is good cause for discontinuing the takeoff 3 Takeoffs are made with full throttle When speed tape comes alive Call out Speed checked At rotation speed 75 knots rotate QRH DA42 sabena 9 NORM PROC AIRLINE TRAINING CENTER INC REV 1 2 3 31 AFTER TAKEOFF POSITIVE CLIMB GEARS ci as Apply stop the spinning of the main wheels before entering the wheel well then select lever up Retract the gear when no more runway is available for an emergency re landing After gear is up and at a safe altitude and speed Perform following actions at 1 000 FT AGL ENGINE INSTRUMENTS ea CHECK LAN DING LIGHT E ee AS REQUIRED TRANSPONDER sss 2 222 2222200000 CODE amp ALT MAP tan ep EE sub Dee rend SWITCH When out of the traffic pattern and congested area switch off the landing lights Do not switch off the landing lights when remaining in the traffic pattern or transiting controlled airspace AFTER TAKEOFF CHE
73. off both engine masters off start key pulled out electric master off and avionics master off GEAR SELECTOR sss eee DOWN To prevent inadvertent gear retraction when the battery master switch is turned on and the squat switch located on the left main gear fails PARKING BRAKE oases aS E s SET To set the parking brake set parking brake on then pump the brake pedals to build up pressure in the brake cylinder sabena 9 NORM PROC an AIRLINE TRAINING CENTER INC REV 1 2 3 6 ELECTRIC MASTER ON When switching on the electric master switch the electrically driven hydraulic gear pump may activate for 5 to 20 seconds in order to restore system pressure Should the pump operate continuously or intermittently this indicates a malfunction in the landing gear sys tem FUELGAUGES sae MAPS ES LDG ELECTRIC MASTER SWITCH voii aslla NEUTRAL Check full control travel of rudder trim and elevator trim then in preparation for the walk around set in neutral position SUNSCREENS PITOT COVER STALL WARNING COVER TIE DOWN CHOCKS EUER REMOVED Put sunscreens if available in their dedicated bag Put pitot cover in the flight gear bag If the aircraft s own tie down ropes and wheel clocks were used put in the flight gear bag TOWBAR
74. or for more than 10 seconds After 1 start cycle apply a cooling period of 20 sec onds After 6 consecutive start cycles apply a cooling period of 30 minutes STARTER ANNUNCIATION If the L R STARTER annunciation does not extinguish after the engine has started and the START KEY has been released set the ENGINE MASTER OFF PRESSURE If the oil pressure has not moved from the red range within 3 sec onds after starting set the ENGINE MASTER OFF When starting a cold engine the oil pressure can be as high as 6 5 bar for a maxi mum of 20 seconds ANNUNCIATIONS ENGINE SYSTEM CHECK Check volts and AMP load Set idle power and verify the RPM is 900 20 Leave power at idle for 2 minutes Thereafter set 1400 RPM until oil temperature above 50 C and coolant temperature above 60 C sabena NORM PROC ee AIRLINE TRAINING CENTER INC REV 1 2 3 24 REPEAT FOR OTHER ENGINE CAUTION With engine running before switching on the engine master for the second engine gt check engine glow for the running engine 15 E extinguished to so may result in engine glow being operated on 2 engines simultaneously which will overload the elec i trical system and will subsequently require a 5 mantenance intervention ILes 2 2 2 2 2 2 2 2 2 2 2 2 2 2 2 82 2
75. ot tied down but with the crew around Do not set parking brake when the brakes are overheated Wheel chocks are required when the aircraft is not tied down and left unattended If no wheel chocks available at the FBO use the aircraft s own wheel chocks in flight gear bag SEAT u saa LOCK Seat belts of all seats will be fastened PERSONAL BELONGINGS AND REMOVE CANOPY AND DOORS CLOSE amp SECURE Lock with key If required fill in strip in aircraft squawk book and report problem to dispatch and maintenance If required fill in ASR Fill out aircraft logbook Return aircraft key to dispatch If required close flight plan sabena 9 NORM PROC ar AIRLINE TRAINING CENTER INC REV 1 2 3 36 FLOWS ARE INTENDED TO PROVIDE A LOGICAL SEQUENCE IN WHICH THE ITEMS CAN BE DONE AND SHOULD BE FOLLOWED BY A CHECK LISTAT ALL TIMES EXCEPT FOR THE WALKAROUND PRE FLIGHT PREPARATION FLOW ALL PERTINENT INFORMATION CONCERNING FLIGHT CHECK FLIGHT RELEASE a a COMPLETE AIRPEANE SOUAWKIBOON er EQUIPMENT REQWIREDIEORIENIGHT o CHECK AIRCRAFT KEYSAND POUCH n Uu usss EMSA F E CHECKLIST CHECK Ee eee ue E CHECK WALKAROUND FLOW APPROACHING THE AIRCRAFT NEARBY
76. s to the type of failure G1000 annunciated failures are between filled boxes Unannunciated failures are not Warnings and Emergencies are RED Cautions and Abnormals are AMBER G1000 WARNINGS OTHER EMER PROC G1000 CAUTIONS OTHER ABNORMAL PROC RECALL ITEMS Some emergency checklist require an immediate response action from the pilot The recall items must be performed quickly without hesitation but without rushing either Recall items are identified in by a dashed line box around the critical items Other checklists that are not boxed must be performed in read and do Sabena EMER PROC 2 AIRLINE TRAINING CENTER INC REV 1 2 4 3 G1000 WARNINGS Warning Page Description L R OIL PRES 4 7 Oil pressure low lt 1 bar L R OIL TEMP 4 7 Oil temp hight gt 140 C L R GBOX TEMP 4 8 Gearbox temp high gt 120 C L R FUEL TEMP 4 8 Fuel temp high gt 75 C L R STARTER 4 8 Starter not disengaging L R ENG TEMP 4 9 Coolant temp high gt 105 C 4 10 Engine fail fire during takeoff L ENG FIRE Engine fail fire in flight Engine fire on ground L R ALTN AMPS 4 15 current gt 60A Unlocked door s DOOR OPEN 4 22 Front Rear Canopy Bag doors not closed and locked sabena EMER PROC nn AIRLINE TRAINING GENTER ING REV 1 2 44 OTHER EMER PROC CABIN FIRE gt 10 000 FT ELECTRICAL FIRE ON GROUND ELECTRICAL FIRE IN FLIGHT UNINTENTIONAL FLIGHT IN ICING
77. sk the pilot in the right seat to perform a brake check as follows Brakes check you have controls check your brakes The right seat pilot will reply I have controls and perform the brake check then he will announce Brakes checked you have controls Pilot flying left seat pilot will reply I have controls and continue taxi Taxi turns can be made using rudder pedal motion only Brakes are only needed to reduce the taxi speed or when maneuvering in tight spaces On the ground and in flight the pilot s feet should be in an almost horizontal position heels on the floor toes on the lower part of the rudder pedals sliding the feet up on the rudder pedals only when required to apply brakes Differential power more power on the engine on the outside of the turn less on the inside engine may be used during turns on the ground FLIGHT INSTRUMENTS oe e 2222er CHECK sabena 9 NORM PROC a0 AIRLINE TRAINING CENTER INC REV 1 2 3 28 In a left turn Turning left lt gt check turn coordinator going left skidding right lt gt check side slip going right and compass decreasing gt check numbers on DG and magnetic compass decreasing horizon level lt gt check attitude indicator level In a right turn Turning right skidding left HDG and compass increasing horizon level The checks need to be done only once in a left turn or a right turn outside congested area FUEL SELECTORS uuu uuu d
78. the runway This gives the gear warning horn a chance to blow if the gear is not locked down After ground contact hold the nose wheel off as long as possible Braking if needed is most effective when back pressure is applied to the con trol wheel putting most of the aircraft weight on the main wheels When the headwind component exceeds 15 knots or when the crosswind component exceeds 10 knots as well as in gusty wind conditions the approach will be flown at a slightly higher than normal speed 5 KIAS with APPROACH FLAPS AFTER LANDING Runway vacated aircraft stopped behind hold short line On re quest of PF After landing items the starred items may be per formed by the PM LANDING HIGHT OFF TAXI LIGHT onaning nien o ee ON PITOT HEAT ec OFF TIME eo cio START ENGINE IDLE Engines have to run at idle power for 2 minutes before shut down Taxi with idle power if possible AFTER LANDING CHECKLIST If the starred items were performed by the PM he she will read the AFTER LANDING checklist silently and announce AFTER LANDING CHECKLIST COMPLETED to the PF SHUTDOWN TAXI osa era OFF sabena 9 NORM PROC npn AIRLINE TRAINING CENTER INC REV 1 2 3 34 TOTAL IN SERVICE 2 2 2 ea NOTE Write down the G1000 total time in service from the FUEL page TIME ee ee ae CHECK 2 MINUTES IN IDLE AVIONICS MASTER SWITCH OFF ENGINE MASTER
79. tive 82 KIAS 82 KCAS Blue radial line ue radial lin Best Rate of Climb Speed Air Minimum Control eT 68 KIAS 68 KCAS Red radial line Speed DA42 sabena LIMITATIONS dn POWERPLANT LIMITATIONS Definition Limitation Indicator Marking Rotational Speed MAX 2300 2500 RPM Red line MAX 75 C Fuel Temp MIN 30 C Oil Temperature MAX 140 C Red line MIN 1 0 MAX 6 5 Pressure Red line BAR BAR Fuel Grade JET A 1 NO ADDITIVES WEIGHT LIMITATIONS Max Ramp Weight 3 935 Ibs Max Takeoff Weight 3 935 Ibs Max Landing Weight 3 748 lbs DA42 sabena 9 LIMITATIONS AIRLINE TRAINING CENTER INC REV 1 2 6 3 WEIGHT LIMITATIONS Max Weights in Baggage Compartments Forward nose 66 lbs Aft cockpit baggage compartment 100 155 Max Zero Fuel Weight 3 638 165 MANEUVER LIMITS All intentional acrobatic maneuvers including spinning are prohibited Avoid abrupt maneuvers FLIGHT MANEUVERING LOAD FACTORS Positive Load Factor Flaps Up Max 3 8G Flaps Down Max 2 0G Negative Load Factor No inverted maneuvers approved QRH DA42 sabena LIMITATIONS AIRLINE TRAINING CENTER INC REV 1 2 w 6 4 FUEL LIMITATIONS Total Fuel Capacity 52 U S Gallons Unusable Fuel 2 U S Gallons Usable Fuel 50 U S Gallons X WIND LIMITATION Maximum demonstrated crosswind component 20 kts
80. u A M PROPERLY STOWED sabena 9 NORM PROC dace AIRLINE TRAINING CENTER INC REV 1 2 3 7 REQUIRED EQIUIPMENT ON BOARD The following equipment must be on board Aircraft pouch containing aircraft flight time log book emergency sick sacs fuel card amp keys Bag containing sunscreens for the windows if available Flight gear bag containing fuel tester flip up training glasses flash light wheel chocks pitot cover 3 tie down ropes first aid kit Fire extinguisher Rescue hammer EASA FAA approved airplane flight manual POH JAA FAA required documents certificate of airworthiness airplane registration Alternate fuel measuring device G1000 User manual FRONT BAGGAGE DOORS SECURE The door must be locked with the key before the flight to prevent opening in flight sabena 9 NORM PROC an AIRLINE TRAINING CENTER INC REV 1 2 3 8 WALK AROUND Walkaround is clockwise around the aircraft LEFT WING WING FLAPS inepte getrennten E sue donde cds CHECK FLAP AND nina CHECK FLAP HINGES AND SAFETY 10 CHECK piEdiepe AILERON AND LINKAGE FOREIGN OBJECTS IN AILERON PADDIE CHECK STATIC DISCHARGERS u u euere CHECK WING E POSITION LIGHT STROBE LIGHT IEE DOWN mcd CHEC
81. um sun Sunan E TTE REAR DOOR _ 0 are nee CLOSED amp SECURED FRONT CANOPY uu u uuu a aaah POSITION 1 OR 2 FRONT BAGGAGE DOORS CLOSED amp LOCKED AVIONICS MASTER SWITCH comarca u uuu us raid OFF ELECTRIC MASTER 222222222222 0 0202 32 ON ENGINE MASTER SWITCHES sss Seas ESE tad xata anna OFF IGNITION KEY sy ALTERNATE STATIC ee ee en A ee CLOSED ico TAM MIERSCONTROR SET LIGHT SWITCHES OFF EMERGENCY 2 22 22 CHECK OFF amp GUARDED STANDBY INSTRUMENTS SES SE TA CHECK MAGNETIC COMPASS cia 2 5200 2202 222 sss CHECK DEVIATION CARD u u u na aparicion WEE SOLANGE IMME Ec n per E FUELSCAEQUEATOR oce ee ee nee len SET TOTAL TIME IN SERVICE HOBBS QRH DA42 sabena NORM PROC REV 1 2 3 41 MANUAL GEAR EXTENSION HANDLE CHECK PUSHED IN ALTERNATE AIRES on EE a e E CHECK CLOSED man M E CHECK LDG 5 PARKING BRAKE SS 20009 SET DEFROSTER SWITCH sra EEE ELE SESS EEE OFF HEATER OFF VARIABLE ELEVATOR BACKSTOP sss dasa E E EEEE EEE CHECK AVIONICS MASTER u sss nan mann
82. ust be set to enable a quick return to the departure airport in case of an emergency AUTOPILOT asas Em TEST 1 Engage feel resistance on stick 2 bug on top 3 Select HDG ALT 4 Turn bug left right monitor stick moving to the left right 5 Press CWS button and check free movement of stick Release CWS button stick goes to the left again Disengage AP by using red disconnect button ELECTRIC A a TEST 1 Push both trim split buttons FWD monitor elev trim moving FWD QU Press red button on stick check elev trim movement stops 3 Repeat steps 1 amp 2 in AFT direction 4 Move left split trim button FWD and AFT check elev trim not moving 5 Repeat step 4 with right split trim button sabena 9 NORM PROC ar AIRLINE TRAINING CENTER INC REV 1 2 3 26 The following test sequence will be executed for both engines si multaneously The whole test procedure must be completed with out any error If any error occurs do not fly even if the engine appears to run smoothly after the test procedure ECU test procedure Set POWER LEVER IDLE Press and hold the ECU TEST BUTTON S and observe following sequence ECU A B FAIL LIGHTS ettet ttes ON PROPELLER RPM INCREASE ECU A B F IL LIGA Soo OFF ECU B FAIL PROPELLER s ECU B FAIL FAIL LIGHT sistas PROPELLER
83. visually and verify strut height is sufficient Typical visible length of bare piston is at least 5 5 9 DOWN amp UPLOCK SWITCHES CHECK WEAR TREAD amp DEPTH OF TIRE CHECK Tires should be taken out of service when they have one or more flat spots Generally a single flat spot or skid burn does not expose the carcass body and the tire may remain in service unless severe unbalance is reported by the crew Small cuts are acceptable if they do not protrude into the tire carcass Cuts in the side wall are not acceptable Shallow chevron shaped cuts across the tread of a tire pose no problem they are caused by landing on a grooved concrete runway As long as the tread does not wear down into the body plies of the carcass the basic strength of the tire is not affected To provide traction during wet runway operation operators should replace their tires when the tread reaches 1 32 inch 0 79 mm SEIP MARKS u een CHECK er REMOVE LANDING GEAR DOOR amp CHECK EPU CONNECTOR uuu een CHECK TOW BAR isso a e a REMOVE RIGHT MAIN LANDING GEAR sabena 9 NORM PROC ar AIRLINE TRAINING CENTER INC REV 1 2 3 1 2 LANDING GEAR STRUT amp LOCK CHECK Check visually and verify strut height is sufficient Typical visible length of bare piston is at least 4cm 1 6 DOWN amp UPLOCK SWITCHES 3

QRH_DA42_V1 2 1 - Sabena Airline Training Center

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