Sennheiser SI 234 - ANNEXE 802 Operations Instructions

Introduction DA 42 NG AFMPage 0 - 8 Rev. 3 01-Apr-2014 Doc. # 7.01.16-ECh. Page Date4A 4A-28 01-Apr-2014'4A-29 01-Apr-2014'4A-30 01-Apr-2014

EmergencyProceduresDA 42 NG AFMPage 3 - 16 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E3.4 G1000 SYSTEM WARNINGS3.4.1 RED XA red X through any display field

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 173.4.5 VERT SPEED FAILVERT SPEED FAILThe display system is not receivi

EmergencyProceduresDA 42 NG AFMPage 3 - 18 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E3.5 G1000 FAILURES3.5.1 NAVIGATION INFORMATION FAILUREIf Garmin G1000

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 19(b) DISPLAY BACKUP button on audio panel ... PUSH (button will be I

EmergencyProceduresDA 42 NG AFMPage 3 - 20 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E3.5.4 AIR DATA COMPUTER (ADC) FAILURENOTEComplete loss of the Air Dat

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 213.5.6 ERRONEOUS OR LOSS OF WARNING/CAUTION ANNUNCIATORSNOTELoss of an

EmergencyProceduresDA 42 NG AFMPage 3 - 22 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E3.6 ABNORMAL ENGINE BEHAVIOUR1. Full power ...

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 233.7 ONE ENGINE INOPERATIVE PROCEDURESWARNINGIn certain combinations of

EmergencyProceduresDA 42 NG AFMPage 3 - 24 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E3.7.1 DETECTING THE INOPERATIVE ENGINENOTEOne engine inoperative mean

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 253.7.2 ENGINE TROUBLESHOOTINGWARNINGControl over the flight attitude h

DA 42 NG AFM IntroductionDoc. # 7.01.16-E Rev. 3 01-Apr-2014 Page 0 - 9Ch. Page Date4B 4B-1 01-Apr-2014'4B-2 01-Apr-2014'4B-3 01-Apr-2014&ap

EmergencyProceduresDA 42 NG AFMPage 3 - 26 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EWARNINGDo not increase the POWER lever past the propeller speedof 1975

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 27If either ECU A or B setting restores normal engine operation then mai

EmergencyProceduresDA 42 NG AFMPage 3 - 28 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E3.7.3 ENGINE SECURING (FEATHERING) PROCEDUREShut down and feathering

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 293.7.4 UNFEATHERING & RESTARTING THE ENGINE IN FLIGHTIf the reason

EmergencyProceduresDA 42 NG AFMPage 3 - 30 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ENOTEAt airspeeds below 100 KIAS it is possible that the propellermay w

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 31Restarting the Engine by WindmillingIf the reason for the shutdown has

EmergencyProceduresDA 42 NG AFMPage 3 - 32 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ENOTEBelow 125 KIAS it is possible that the propeller may notwindmill c

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 333.7.5 ENGINE FAILURE DURING TAKE-OFFa) Engine Failure During Ground R

EmergencyProceduresDA 42 NG AFMPage 3 - 34 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-Eb) Engine Failure After Lift OffIf the landing gear is still extended

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 356. Inoperative engine ... secure according to 3.7.3 -

Introduction DA 42 NG AFMPage 0 - 10 Rev. 3 01-Apr-2014 Doc. # 7.01.16-ECh. Page Date5 5-1 01-Apr-2014'5-2 01-Apr-2014'5-3 01-Apr-2014'

EmergencyProceduresDA 42 NG AFMPage 3 - 36 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E3.7.6 ENGINE FAILURES IN FLIGHT(a) Engine Failure During Initial Cli

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 37(b) Engine Failure During Flight1. Rudder ...

EmergencyProceduresDA 42 NG AFMPage 3 - 38 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E3.7.7 LANDING WITH ONE ENGINE INOPERATIVEPreparation:CAUTIONFor emerg

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 39Not before being certain of "making the field“:8. Airspeed ...

EmergencyProceduresDA 42 NG AFMPage 3 - 40 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ENOTEHigher approach speeds result in a significantly longer landingdis

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 41If the approach to land is not successful you may consider:3.7.8 GO-A

EmergencyProceduresDA 42 NG AFMPage 3 - 42 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EIf a positive rate of climb cannot be established:- Land so as to keep

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 43If landing with landing gear extended:10.LANDING GEAR...

EmergencyProceduresDA 42 NG AFMPage 3 - 44 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E3.7.9 FLIGHT WITH ONE ENGINE INOPERATIVECAUTIONEven if a positive fli

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 453.8 ENGINES OUT LANDING1. ENGINE MASTER ... both OFF2

DA 42 NG AFM IntroductionDoc. # 7.01.16-E Rev. 3 01-Apr-2014 Page 0 - 11Ch. Page Date6 6-1 01-Apr-2014'6-2 01-Apr-2014'6-3 01-Apr-2014'

EmergencyProceduresDA 42 NG AFMPage 3 - 46 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EIf landing with landing gear extended:9. LANDING GEAR...

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 473.9 LANDING GEAR SYSTEM FAILURES3.9.1 LANDING GEAR UNSAFE WARNINGNOTE

EmergencyProceduresDA 42 NG AFMPage 3 - 48 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ENOTEIf the landing gear cannot be retracted to the final up positionyo

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 493.9.2 MANUAL EXTENSION OF THE LANDING GEARNOTEIn case of a failure of

EmergencyProceduresDA 42 NG AFMPage 3 - 50 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E7. Gear indicator lights ... check 3 green lightsNOTE

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 513.9.3 LANDING WITH GEAR UPNOTEThis procedure applies if the landing g

EmergencyProceduresDA 42 NG AFMPage 3 - 52 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E3.9.4 LANDING WITH A DEFECTIVE TIRE ON THE MAIN LANDING GEARCAUTIONA

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 533.9.5 LANDING WITH DEFECTIVE BRAKESConsider the greater rolling dista

EmergencyProceduresDA 42 NG AFMPage 3 - 54 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E3.10 FAILURES IN THE ELECTRICAL SYSTEM3.10.1 COMPLETE FAILURE OF THE

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 55NOTEThe backup artificial horizon and the flood light will haveelectri

Introduction DA 42 NG AFMPage 0 - 12 Rev. 3 01-Apr-2014 Doc. # 7.01.16-ECh. Page Date7 7-19 01-Apr-2014'7-20 01-Apr-2014'7-21 01-Apr-2014&ap

EmergencyProceduresDA 42 NG AFMPage 3 - 56 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E3.10.3 STARTER MALFUNCTIONIf the starter does not disengage from the

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 573.11 SMOKE AND FIRENOTEThe cabin hand fire extinguisher is located ins

EmergencyProceduresDA 42 NG AFMPage 3 - 58 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E3.11.2 ENGINE FIRE DURING TAKE-OFF1. Cabin heat & Defrost ...

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 593.11.3 ENGINE FIRE IN FLIGHT1. Cabin heat & Defrost ...

EmergencyProceduresDA 42 NG AFMPage 3 - 60 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E3.11.4 ELECTRICAL FIRE ON GROUND1. ELECT. MASTER ...

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 613.11.5 ELECTRICAL FIRE IN FLIGHT1. EMERGENCY SWITCH ...

EmergencyProceduresDA 42 NG AFMPage 3 - 62 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E3.12 OTHER EMERGENCIES3.12.1 SUSPICION OF CARBON MONOXIDE CONTAMINATI

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 633.12.2 UNLOCKED DOORS1. Airspeed ... reduce

EmergencyProceduresDA 42 NG AFMPage 3 - 64 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EFront Baggage Door Open5. Airspeed ... reduce

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 653.12.3 DEFECTIVE PROPELLER RPM REGULATING SYSTEMCAUTIONThe POWER leve

DA 42 NG AFM IntroductionDoc. # 7.01.16-E Rev. 3 01-Apr-2014 Page 0 - 13Ch. Page Date7 7-73 01-Apr-2014'7-74 01-Apr-2014'7-75 01-Apr-2014&ap

EmergencyProceduresDA 42 NG AFMPage 3 - 66 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E(b) Propeller OverspeedNOTEThis procedure applies for continued prope

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 67(c) Fixed RPM1. POWER setting ... changeIf the prob

EmergencyProceduresDA 42 NG AFMPage 3 - 68 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E3.12.4 UNINTENTIONAL FLIGHT INTO ICING1. Leave the icing area (by cha

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 693.12.5 FUEL SUPPLY FAILURE1. FUEL SELECTOR ... CROS

EmergencyProceduresDA 42 NG AFMPage 3 - 70 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E3.12.6 RECOVERY FROM AN UNINTENTIONAL SPINCAUTIONSpin recovery has NO

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 71When rotation has stopped:6. Rudder ... neut

EmergencyProceduresDA 42 NG AFMPage 3 - 72 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E3.12.7 EMERGENCY DESCENT1. FLAPS... UP2. G

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 733.12.9 AUTOPILOT OR ELECTRIC TRIM MALFUNCTION / FAILURENOTEAn autopil

EmergencyProceduresDA 42 NG AFMPage 3 - 74 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ENOTEAccomplish items 1 and 2 simultaneously!1. Airplane control stick

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 1CHAPTER 4ANORMAL OPERATING PROCEDURESPage4A.1 INTRODUCTION ...

Introduction DA 42 NG AFMPage 0 - 14 Rev. 3 01-Apr-2014 Doc. # 7.01.16-E0.4 TABLE OF CONTENTSChapterGENERAL(a non-approved chapter) ...

Normal OperatingProceduresDA 42 NG AFMPage 4A - 2 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4A.6.13 AFTER LANDING ... 4A-594A.6.

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 34A.1 INTRODUCTIONChapter 4A contains checklists and describes p

Normal OperatingProceduresDA 42 NG AFMPage 4A - 4 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4A.2 AIRSPEEDS FOR NORMAL OPERATING PROCEDURESFLAPS up to 1900

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 54A.3 ADVISORY ALERTS ON THE G1000The G1000 provides the followi

Normal OperatingProceduresDA 42 NG AFMPage 4A - 6 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4A.4 FLIGHT CHARACTERISTICSThe DA 42 NG is to be flown with &qu

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 74A.6 CHECKLISTS FOR NORMAL OPERATING PROCEDURES4A.6.1 PRE-FLIG

Normal OperatingProceduresDA 42 NG AFMPage 4A - 8 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EOn the instrument panel:a) ALTERNATOR ... c

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 9b) Fuel quantity ... check indication, ve

Normal OperatingProceduresDA 42 NG AFMPage 4A - 10 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-Eh) POWER lever ... set MAXi) Variable ele

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 11II. Walk-around check, visual inspectionCAUTIONA visual inspe

DA 42 NG AFM GeneralDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 1 - 1CHAPTER 1GENERALPage1.1 INTRODUCTION ...1-21.2

Normal OperatingProceduresDA 42 NG AFMPage 4A - 12 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E2. Left engine nacelle:a) 4 air inlets / 2 air outlets ...

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 13j) Nacelle underside ... check for excessive

Normal OperatingProceduresDA 42 NG AFMPage 4A - 14 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-El) Tie-down ... check, clearm) Ailero

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 156. Fuselage, right side:a) Fuselage skin ...

Normal OperatingProceduresDA 42 NG AFMPage 4A - 16 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-Ee) Openings on lower surface ... check for foreign

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 17f) Venting pipe ... check for blockageg)

Normal OperatingProceduresDA 42 NG AFMPage 4A - 18 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E10. Front fuselage and nose landing gear:a) Left and right fro

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 194A.6.2 BEFORE STARTING ENGINE1. Preflight inspection ...

Normal OperatingProceduresDA 42 NG AFMPage 4A - 20 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ENOTEThe pilot must ensure that a passenger sitting on a front

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 2116. G1000 ... wait until power-up c

General DA 42 NG AFMPage 1 - 2 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E1.1 INTRODUCTIONThis Airplane Flight Manual has been prepared in order to provide

Normal OperatingProceduresDA 42 NG AFMPage 4A - 22 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4A.6.3 STARTING ENGINENOTEAt ambient temperatures below -22°C

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 23CAUTIONDo not overheat the starter motor. Do not operate the s

Normal OperatingProceduresDA 42 NG AFMPage 4A - 24 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4A.6.4 BEFORE TAXIING1. AVIONIC MASTER ... O

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 25NOTEThe AFCS system automatically conducts a preflight self-te

Normal OperatingProceduresDA 42 NG AFMPage 4A - 26 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4A.6.5 TAXIING1. Parking brake ... relea

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 274A.6.6 BEFORE TAKE-OFF1. Position airplane into wind if possi

Normal OperatingProceduresDA 42 NG AFMPage 4A - 28 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E9. Annunciations / Engine / System Page ... check OK / norma

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 29ECU / fuel pumps test sequence:CAUTIONIf the L/R ECU A/B FAIL

Normal OperatingProceduresDA 42 NG AFMPage 4A - 30 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E1. Power lever ... IDLE2. Propeller RPM

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 318. ECU TEST button... releaseNOTEBy switchin

DA 42 NG AFM GeneralModification Source InstalledDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 1 - 3Garmin GWX 68 Weather Radar OÄM 42-119 9 yes 9 noIc

Normal OperatingProceduresDA 42 NG AFMPage 4A - 32 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EAvailable power check:1. POWER lever ...

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 334A.6.7 TAKE-OFFa) Standard Procedure (Take-off with Flaps UP)

Normal OperatingProceduresDA 42 NG AFMPage 4A - 34 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EWhen safe climb is established:7. LANDING GEAR...

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 35NOTEIn strong crosswinds steering can be augmented by use ofth

Normal OperatingProceduresDA 42 NG AFMPage 4A - 36 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4A.6.8 CLIMBInitial Climb Check1. Landing light ...

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 37GFC 700 Operation During ClimbNOTEThe NOSE UP and NOSE DN butt

Normal OperatingProceduresDA 42 NG AFMPage 4A - 38 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-Eb) Flight Level Change (FLC)1. Altitude preselect ...

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 39c) To Capture a Selected Altitude1. Altimeter setting ...

Normal OperatingProceduresDA 42 NG AFMPage 4A - 40 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-Ed) Navigation Capture and Track:1. Navigation source ...

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 414A.6.9 CRUISE 1. POWER lever ... up to

DA 42 NG AFM IntroductionPage 0 - 0a Rev. 3 01-Apr-2014 Doc. # 7.01.16-EIntentionally left blank.

General DA 42 NG AFMPage 1 - 4 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ECAUTIONThe DA 42 NG is a twin engine airplane. When the operatinglimitations and m

Normal OperatingProceduresDA 42 NG AFMPage 4A - 42 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E2. Transfer the second half of the auxiliary fuel:Repeat the p

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 43NOTEIf the altitude preselect is not changed before selecting

Normal OperatingProceduresDA 42 NG AFMPage 4A - 44 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ENOTEIf the altitude preselect is not changed before selecting

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 45NOTEIn ALT mode, the autopilot will maintain the reference alt

Normal OperatingProceduresDA 42 NG AFMPage 4A - 46 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-Ee) Navigation Capture and Track:1. Navigation source ...

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 474A.6.10 DESCENT1. POWER lever ... as req

Normal OperatingProceduresDA 42 NG AFMPage 4A - 48 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ENOTEIf the altitude preselect is not changed before selecting

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 49NOTEIf the altitude preselect is not changed before selecting

Normal OperatingProceduresDA 42 NG AFMPage 4A - 50 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ENOTEIn ALT mode, the autopilot will maintain the reference alt

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 51NOTEIf the Course Deviation Indicator (CDI) is greater than on

DA 42 NG AFM GeneralDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 1 - 51.2 CERTIFICATION BASISThe certification basis is JAR-23, published on 11-Mar-1994

Normal OperatingProceduresDA 42 NG AFMPage 4A - 52 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4A.6.11 APPROACH & LANDINGApproach:CAUTIONFor landing the

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 53Before landing:12. Airspeed:Up to 1900 kg (4189 lb) ...

Normal OperatingProceduresDA 42 NG AFMPage 4A - 54 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EGFC 700 Operation During Approach and Landinga) VOR1. Navigati

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 55b) ILS1. Navigation source... select LOC usi

Normal OperatingProceduresDA 42 NG AFMPage 4A - 56 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-Ec) GPS1. Navigation source ... select GPS us

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 57NOTEThe course pointer must be at least 115° from the currentm

Normal OperatingProceduresDA 42 NG AFMPage 4A - 58 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4A.6.12 GO AROUND1. POWER lever ... MAX2

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 59At an appropriate safe altitude:6. Autopilot mode controller .

Normal OperatingProceduresDA 42 NG AFMPage 4A - 60 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4A.6.14 SHUT-DOWN1. Parking brake ... se

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 614A.6.15 EXIT AIRPLANEExit the airplane to the aft on designat

General DA 42 NG AFMPage 1 - 6 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E1.4 DIMENSIONSNOTEAll dimensions shown below are approximate.Overall DimensionsSpa

Normal OperatingProceduresDA 42 NG AFMPage 4A - 62 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4A.6.18 FLIGHT IN RAIN, SNOW OR VISIBLE MOISTURE1. ALTERNATE

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 634A.6.19 REFUELINGCAUTIONBefore refueling, the airplane must b

Normal OperatingProceduresDA 42 NG AFMPage 4A - 64 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ETypical Dosing Quantities:%(a) KATHON FP 1.5%Fuel Quantity% Fu

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 65(c) PRIST Hi-Flash%Fuel Quantity%Fuel Additive *,**%PRIST Hi-F

Normal OperatingProceduresDA 42 NG AFMPage 4A - 66 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4A.6.20 FLIGHT AT HIGH ALTITUDEAt high altitudes the provisio

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 67NOTEAt airspeeds below 100 KIAS it is possible that the propel

Normal OperatingProceduresDA 42 NG AFMPage 4A - 68 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ERestarting the Engine by WindmillingMinimum restart airspeed .

DA 42 NG AFMNormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4A - 691. Altitude ... stabilize in level f

Normal OperatingProceduresDA 42 NG AFMPage 4A - 70 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EIntentionally left blank.

DA 42 NG AFMAbnormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4B - 1CHAPTER 4BABNORMAL OPERATING PROCEDURESPage4B.1 PRECAUTIONARY

DA 42 NG AFM GeneralDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 1 - 7Wing FlapsArea (total, left + right) : 2.18 m² 23.5 sq.ft.Horizontal TailArea : 2.

Abnormal OperatingProceduresDA 42 NG AFMPage 4B - 2 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4B.4.11 STICK LIMIT ... 4B-234

DA 42 NG AFMAbnormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4B - 34B.1 PRECAUTIONARY LANDINGNOTEA landing of this type is only

Abnormal OperatingProceduresDA 42 NG AFMPage 4B - 4 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ECAUTIONIf sufficient time is remaining, the risk of fire in t

DA 42 NG AFMAbnormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4B - 54B.2 CANOPY IN COOLING GAP POSITIONCAUTIONIf take-off was ina

Abnormal OperatingProceduresDA 42 NG AFMPage 4B - 6 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4B.3 ENGINE INSTRUMENT INDICATIONS OUTSIDE OF GREENRANGE ON T

DA 42 NG AFMAbnormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4B - 74B.3.2 COOLANT TEMPERATURE(a) High Coolant TemperatureProce

Abnormal OperatingProceduresDA 42 NG AFMPage 4B - 8 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4B.3.3 OIL TEMPERATURE(a) High Oil TemperatureProceed accor

DA 42 NG AFMAbnormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4B - 94B.3.4 OIL PRESSURE(a) High Oil Pressure- Check oil tempera

Abnormal OperatingProceduresDA 42 NG AFMPage 4B - 10 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4B.3.5 GEARBOX TEMPERATUREHigh Gearbox TemperatureProceed a

DA 42 NG AFMAbnormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4B - 114B.3.7 VOLTAGE(a) Low Voltage Indication on the Ground wit

General DA 42 NG AFMPage 1 - 8 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E1.5 DEFINITIONS AND ABBREVIATIONS(a) AirspeedsCAS: Calibrated Airspeed. Indicated

Abnormal OperatingProceduresDA 42 NG AFMPage 4B - 12 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4B.4 CAUTION-ALERTS ON THE G1000The G1000 provides the follo

DA 42 NG AFMAbnormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4B - 13NOTEAn ECU FAIL CAUTION is caused by various types ofmalfunc

Abnormal OperatingProceduresDA 42 NG AFMPage 4B - 14 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4B.4.3 L/R ECU B FAILL/R ECU B FAIL* Left / Right engine EC

DA 42 NG AFMAbnormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4B - 15NOTEIf additional engine problems are observed refer to 3.7.

Abnormal OperatingProceduresDA 42 NG AFMPage 4B - 16 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4B.4.4 L/R FUEL LOWL/R FUEL LOWLeft / Right engine main tan

DA 42 NG AFMAbnormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4B - 174B.4.5 LOW VOLTAGE CAUTION (LOW VOLTS)L/R VOLTS LOWLeft / R

Abnormal OperatingProceduresDA 42 NG AFMPage 4B - 18 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4B.4.6 L/R ALTN FAILL/R ALTN FAILLeft / Right engine altern

DA 42 NG AFMAbnormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4B - 194B.4.7 L/R COOL LVLL/R COOL LVLLeft / Right engine coolant

Abnormal OperatingProceduresDA 42 NG AFMPage 4B - 20 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4B.4.8 PITOT FAIL / HT OFFPITOT FAILPitot heating system ha

DA 42 NG AFMAbnormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4B - 214B.4.9 STALL HT FAIL / OFFSTAL HT FAILStall warning heat ha

DA 42 NG AFM GeneralDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 1 - 9vNO: Maximum Structural Cruising Speed. This speed may be exceeded only insmooth a

Abnormal OperatingProceduresDA 42 NG AFMPage 4B - 22 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4B.4.10 L/R AUXILIARY FUEL TANK EMPTY (if installed)L/R AUX

DA 42 NG AFMAbnormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4B - 234B.4.11 STICK LIMITSTICK LIMITControl stick limiting system

Abnormal OperatingProceduresDA 42 NG AFMPage 4B - 24 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4B.4.12 CHECK GEARCHECK GEARLanding gear is not down and loc

DA 42 NG AFMAbnormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4B - 254B.4.14 AHRS ALIGNING - KEEP WINGS LEVELAHRS ALIGN:Keep Win

Abnormal OperatingProceduresDA 42 NG AFMPage 4B - 26 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4B.5 FAILURES IN FLAP OPERATING SYSTEMFailure in Position In

DA 42 NG AFMAbnormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4B - 274B.6 FAILURES IN ELECTRICAL RUDDER PEDAL ADJUSTMENTRunaway o

Abnormal OperatingProceduresDA 42 NG AFMPage 4B - 28 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4B.7 FAILURES IN HYDRAULIC SYSTEM4B.7.1 CONTINUOUS HYDRAULI

DA 42 NG AFMAbnormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4B - 294B.7.2 HYDRAULIC PUMP FAILURE1. Landing gear indication lig

Abnormal OperatingProceduresDA 42 NG AFMPage 4B - 30 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4B.8 STARTING ENGINE WITH EXTERNAL POWER4B.8.1 BEFORE START

DA 42 NG AFMAbnormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4B - 31CAUTIONWhen switching the external power unit ON, the electr

General DA 42 NG AFMPage 1 - 10 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EQNH: Theoretical atmospheric pressure at MSL, calculated from the elevationof the

Abnormal OperatingProceduresDA 42 NG AFMPage 4B - 32 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4B.8.2 STARTING ENGINE1. Strobe lights (ACL) ...

DA 42 NG AFMAbnormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4B - 33CAUTIONDo not overheat the starter motor. Do not operate the

Abnormal OperatingProceduresDA 42 NG AFMPage 4B - 34 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4B.9 LIGHTNING STRIKE1. Airspeed ...

DA 42 NG AFMAbnormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4B - 354B.10 FAILURES IN THE AUTOPILOT SYSTEM4B.10.1 AUTOPILOT DIS

Abnormal OperatingProceduresDA 42 NG AFMPage 4B - 36 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4B.10.3 LOSS OF NAVIGATION INFORMATION (Yellow VOR, VAPP, G

DA 42 NG AFMAbnormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4B - 374B.10.4 AUTOPILOT OUT OF TRIM (Yellow 7AIL, 6AIL, 8ELE, 9E

Abnormal OperatingProceduresDA 42 NG AFMPage 4B - 38 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E2. Airplane attitude ... maintain / rega

DA 42 NG AFMAbnormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4B - 39If annunciation remains:2. Control stick ...

Abnormal OperatingProceduresDA 42 NG AFMPage 4B - 40 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4B.10.5 FLASHING YELLOW MODE ANNUNCIATIONNOTEAbnormal mode

DA 42 NG AFMAbnormal OperatingProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4B - 414B.10.6 EFFECTS OF G1000 LOSSES UPON AUTOPILOT OPERATIONG10

DA 42 NG AFM GeneralDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 1 - 11MET: Weather, weather advice.NAV: Navigation, route planning.RoC: Rate of Climb.(

Abnormal OperatingProceduresDA 42 NG AFMPage 4B - 42 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E4B.11 L/R AUX FUEL TRANSFER FAIL (IF AUX. TANKS ARE'INS

DA 42 NG AFM PerformanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 5 - 1CHAPTER 5PERFORMANCEPage5.1 INTRODUCTION ...

Performance DA 42 NG AFMPage 5 - 2 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E5.1 INTRODUCTIONThe performance tables and diagrams on the following pages are

DA 42 NG AFM PerformanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 5 - 35.3 PERFORMANCE TABLES AND DIAGRAMS5.3.1 AIRSPEED CALIBRATIONNOTEThe position

Performance DA 42 NG AFMPage 5 - 4 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E5.3.2 FUEL FLOW'CAUTIONThe table shows the fuel flow per hour for one en

DA 42 NG AFM PerformanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 5 - 55.3.3 INTERNATIONAL STANDARD ATMOSPHERE

Performance DA 42 NG AFMPage 5 - 6 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E5.3.4 STALLING SPEEDSStalling Speeds at Various Flight MassesAirspeeds, most

DA 42 NG AFM PerformanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 5 - 71999 kg(4407 lb)Bank Angle''0°' 30°' 45°' 60°'Ge

Performance DA 42 NG AFMPage 5 - 8 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E0° 10° 20° 30° 40°32°50°60°70°80°90°100°110°120°130°160°180°010 201630 40Cross

DA 42 NG AFM PerformanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 5 - 95.3.6 TAKE-OFF DISTANCEConditions:- Power lever ... bot

General DA 42 NG AFMPage 1 - 12 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EMaximum Landing Mass:The highest mass for landing conditions at the maximum desce

Performance DA 42 NG AFMPage 5 - 10 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EWARNINGFor a safe take-off the available runway length must be atleast equal

DA 42 NG AFM PerformanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 5 - 11Take-Off Distance - Normal Procedure - 1999 kg / 4407 lb' Weight: 1999

Performance DA 42 NG AFMPage 5 - 12 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ETake-Off Distance - Normal Procedure - 1900 kg / 4189 lb Weight: 1900 kg /

DA 42 NG AFM PerformanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 5 - 13Take-Off Distance - Normal Procedure - 1700 kg / 3748 lb Weight: 1700 kg /

Performance DA 42 NG AFMPage 5 - 14 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ETake-Off Distance - Short Field Procedure - 1999 kg / 4407 lb' Weight:

DA 42 NG AFM PerformanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 5 - 15Take-Off Distance - Short Field Procedure - 1900 kg / 4189 lb Weight: 1900

Performance DA 42 NG AFMPage 5 - 16 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ETake-Off Distance - Short Field Procedure - 1700 kg / 3748 lb Weight: 1700

DA 42 NG AFM PerformanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 5 - 17GradientROC fpmTAS KTAS [%] .[][]0985.3.7 CLIMB PERFORMANCE (ALL ENGINE

Performance DA 42 NG AFMPage 5 - 18 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EAll Engines Operating Climb - Flaps UP Flaps: UP Power: 92%vY: 92 KIAS abov

DA 42 NG AFM PerformanceAll Engines Operating Climb - Flaps UP Flaps: UP Power: 92%vY: 92 KIAS above 1900 kg (4189 lb)' 90 KIAS up to 1900

DA 42 NG AFM GeneralDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 1 - 13(f) Designation of the Circuit Breakers on the Instrument PanelLH MAIN BUS:COM1

Performance DA 42 NG AFMPage 5 - 20 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EAll Engines Operating Climb - Flaps APP Flaps: APP Power: 92% vY: 85

DA 42 NG AFM PerformanceAll Engines Operating Climb - Flaps APP Flaps: APP Power: 92% vY: 85 KIAS Gear: retractedWeight [kg] / [lb]Press.Al

Performance DA 42 NG AFMPage 5 - 22 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EGradientROC fpmTAS KTAS [%] .[][]0985.3.8 ONE ENGINE INOPERATIVE CLIMB

DA 42 NG AFM PerformanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 5 - 23One Engine Inoperative Climb' Flaps: UP Power: feathered / 92% vYS

Performance DA 42 NG AFMOne Engine Inoperative Climb' Flaps: UP Power: feathered / 92% vYSE: 85 KIAS Gear: retractedWeight [kg] /

DA 42 NG AFM PerformanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 5 - 255.3.9 TIME, FUEL AND DISTANCE TO CLIMB'Conditions:'- Power lever .

Performance DA 42 NG AFMPage 5 - 26 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ETime, Fuel and Distance to Climb' Flaps: UP' vY: 92 KIAS (abo

DA 42 NG AFM PerformanceTime, Fuel and Distance to Climb' Flaps: UP' vY: 92 KIAS (above 1900 kg / 4189 lb)' vY: 90 KIAS (up

Performance DA 42 NG AFMPage 5 - 28 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E5.3.10 CRUISE PERFORMANCE'Conditions:- Flaps ...

DA 42 NG AFM PerformanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 5 - 29Cruise Performance'Press. Alt.'[ft] / [m]'Outside Air Temperat

DA 42 NG AFM IntroductionDoc. # 7.01.16-E Rev. 3 01-Apr-2014 Page 0 - 1FOREWORDWe congratulate you on the acquisition of your new DIAMOND DA 42 NG.Ski

General DA 42 NG AFMPage 1 - 14 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EAVIONICS BUS:COM2 COM Radio No. 2GPS/NAV2 Global Positioning System and NAV Recei

Performance DA 42 NG AFMCruise Performance'Press. Alt.'[ft] / [m]'Outside Air Temperature - [°C]''ISA-10' ISA' ISA+

DA 42 NG AFM PerformanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 5 - 315.3.11 LANDING DISTANCES'Conditions:- Power lever ...

Performance DA 42 NG AFMPage 5 - 32 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EWARNINGFor a safe landing the available runway length must be atleast equal t

DA 42 NG AFM PerformanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 5 - 33Landing Distance - Flaps LDG - 1999 kg / 4407 lb'Weight:' 1999 kg /

Performance DA 42 NG AFMPage 5 - 34 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ELanding Distance - Flaps LDG - 1900 kg / 4189 lbWeight: 1900 kg / 4189 lb Fla

DA 42 NG AFM PerformanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 5 - 35Landing Distance - Flaps LDG - 1805 kg / 3979 lbWeight: 1805 kg / 3979 lb Fla

Performance DA 42 NG AFMPage 5 - 36 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ELanding Distance - Flaps LDG - 1700 kg / 3748 lbWeight: 1700 kg / 3748 lb Fla

DA 42 NG AFM PerformanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 5 - 37Landing Distance - Abnormal Flap Position - 1999 kg / 4407 lb'Weight:&ap

Performance DA 42 NG AFMPage 5 - 38 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ELanding Distance - Abnormal Flap Position - 1900 kg / 4189 lbWeight: 1900 kg

DA 42 NG AFM PerformanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 5 - 39Landing Distance - Abnormal Flap Position - 1805 kg / 3979 lbWeight: 1805 kg

DA 42 NG AFM GeneralDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 1 - 15RH ENG ECU BUS:ECU BUS RH ECU BusECU B RH ECU BECU A RH ECU ARH BUS:ALT.RH RH Alt

Performance DA 42 NG AFMPage 5 - 40 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ELanding Distance - Abnormal Flap Position - 1700 kg / 3748 lbWeight: 1700 kg

DA 42 NG AFM PerformanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 5 - 41GradientROC fpmTAS KTAS [%] .[][]0985.3.12 GO-AROUND CLIMB PERFORMANCE&

Performance DA 42 NG AFMPage 5 - 42 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EGo-Around Climb Performance Flaps: LDG Power: MAX vREF: 86 KIAS above 1900

DA 42 NG AFM PerformanceGo-Around Climb Performance Flaps: LDG Power: MAX vREF: 86 KIAS above 1900 kg (4189 lb) '84 KIAS up to 1900 kg (4189 lb

Performance DA 42 NG AFMPage 5 - 44 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E5.3.13 APPROVED NOISE DATA'Max. Flight Mass 1900 kg (4189 lb)ICAO Annex

DA 42 NG AFM Mass and BalanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 6 - 1CHAPTER 6MASS AND BALANCEPage6.1 INTRODUCTION ...

Mass and Balance DA 42 NG AFMPage 6 - 2 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E6.1 INTRODUCTIONIn order to achieve the performance and flight characteri

DA 42 NG AFM Mass and BalanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 6 - 32196 mmfloor of nose baggage compartmenthorizontal(86.46 in)DatumPlaneRoo

Mass and Balance DA 42 NG AFMPage 6 - 4 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E6.3 MASS AND BALANCE REPORTThe empty mass and the corresponding CG positi

DA 42 NG AFM Mass and BalanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 6 - 5MASS AND BALANCE REPORTPage No.:Current emptymassMo-ment Mo-mentArmMassRe

General DA 42 NG AFMPage 1 - 16 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E(i) MiscellaneousACG: Austro Control GmbH (Austrian Airworthiness Authority)ATC:

Mass and Balance DA 42 NG AFMPage 6 - 6 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E6.4 FLIGHT MASS AND CENTER OF GRAVITYThe following information enables yo

DA 42 NG AFM Mass and BalanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 6 - 7CAUTIONIf the auxiliary tanks are in use, both tanks must be refueledto t

Mass and Balance DA 42 NG AFMPage 6 - 8 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E6.4.1 MOMENT ARMSThe most important lever arms aft of the Datum Plane:It

DA 42 NG AFM Mass and BalanceItemLever Arm[m] [in]Doc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 6 - 9Baggage incompartments Standard:Nose 0.60 23.6Cabin

Mass and Balance DA 42 NG AFMPage 6 - 10 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E255010012515017520022575[kg][lb]Load Mass10,000 20,000 30,000 40,000 50,

DA 42 NG AFM Mass and BalanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 6 - 11

Mass and Balance DA 42 NG AFMPage 6 - 12 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E6.4.3 CALCULATION OF LOADING CONDITIONNOTEIt the optional de-icing syst

DA 42 NG AFM Mass and BalanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 6 - 133. Locate the values in the diagram in Section 6.4.4 - PERMISSIBLE CENTE

Mass and Balance DA 42 NG AFMCALCULATION OFLOADING CONDITIONDA 42 NG (Example)Your DA 42 NGMass[kg][lb]Moment[kgm][in.lb]Mass[kg][lb]Moment[kgm][in.lb

DA 42 NG AFM Mass and BalanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 6 - 15The CG's shown in the following diagrams are those from the example

DA 42 NG AFM GeneralDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 1 - 171.6 UNITS OF MEASUREMENT1.6.1 CONVERSION FACTORSDimension SI-Units US Units Conv

Mass and Balance DA 42 NG AFMPage 6 - 16 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E6.4.4 PERMISSIBLE CENTER OF GRAVITY RANGE'''''

DA 42 NG AFM Mass and BalanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 6 - 17The flight CG position must be within the following limits:Most forward

Mass and Balance DA 42 NG AFMPage 6 - 18 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E6.4.5 PERMISSIBLE MOMENT RANGE''''''&apos

DA 42 NG AFM Mass and BalanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 6 - 196.5 EQUIPMENT LIST AND EQUIPMENT INVENTORYAll equipment that is approved

DA 42 NG AFM Mass and BalanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 6 - 20Airplane Serial No.: Registration: Date: Mass Lever ArmDescription Type

DA 42 NG AFM Mass and BalanceAirplane Serial No.: Registration: Date: Mass Lever ArmDescription Type Part No. Manufacturer S/N installed lb kg in mDoc

DA 42 NG AFM Mass and BalanceAirplane Serial No.: Registration: Date: Mass Lever ArmDescription Type Part No. Manufacturer S/N installed lb kg in mDoc

DA 42 NG AFM Mass and BalanceAirplane Serial No.: Registration: Date: Mass Lever ArmDescription Type Part No. Manufacturer S/N installed lb kg in mDoc

DA 42 NG AFM Mass and BalanceAirplane Serial No.: Registration: Date: Mass Lever ArmDescription Type Part No. Manufacturer S/N installed lb kg in mDoc

DA 42 NG AFM Mass and BalanceAirplane Serial No.: Registration: Date: Mass Lever ArmDescription Type Part No. Manufacturer S/N installed lb kg in mDoc

General DA 42 NG AFMDimension SI-Units US Units ConversionPage 1 - 18 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EIntensity ofelectriccurrent[A] ampères --El

DA 42 NG AFM Mass and BalanceAirplane Serial No.: Registration: Date: Mass Lever ArmDescription Type Part No. Manufacturer S/N installed lb kg in mDoc

DA 42 NG AFM Mass and BalanceAirplane Serial No.: Registration: Date: Mass Lever ArmDescription Type Part No. Manufacturer S/N installed lb kg in mDoc

DA 42 NG AFM Mass and BalanceAirplane Serial No.: Registration: Date: Mass Lever ArmDescription Type Part No. Manufacturer S/N installed lb kg in mDoc

DA 42 NG AFM Mass and BalanceAirplane Serial No.: Registration: Date: Mass Lever ArmDescription Type Part No. Manufacturer S/N installed lb kg in mDoc

DA 42 NG AFM Mass and BalanceAirplane Serial No.: Registration: Date: Mass Lever ArmDescription Type Part No. Manufacturer S/N installed lb kg in mDoc

DA 42 NG AFM Mass and BalanceAirplane Serial No.: Registration: Date: Mass Lever ArmDescription Type Part No. Manufacturer S/N installed lb kg in mDoc

DA 42 NG AFM Mass and BalanceAirplane Serial No.: Registration: Date: Mass Lever ArmDescription Type Part No. Manufacturer S/N installed lb kg in mDoc

DA 42 NG AFM Mass and BalanceAirplane Serial No.: Registration: Date: Mass Lever ArmDescription Type Part No. Manufacturer S/N installed lb kg in mDoc

DA 42 NG AFM Mass and BalanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 6 - 341. The Amerex A 620 T is UL approved and can be used in airplanes regist

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 1CHAPTER 7DESCRIPTION OF THE AIRPLANEAND ITS SYSTEMSPage7.1 INTRODUCTI

DA 42 NG AFM GeneralDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 1 - 191.6.2 CONVERSION CHART LITERS / US GALLONSLiters US Gallons US Gallons Liters5 1

Airplane Description DA 42 NG AFMPage 7 - 2 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E7.12 STALL WARNING SYSTEM ... 7-647.13 GARM

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 37.1 INTRODUCTIONChapter 7 contains a description of the airplane and

Airplane Description DA 42 NG AFMPage 7 - 4 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E7.3 FLIGHT CONTROLSThe ailerons, elevator and wing flaps are operated

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 5FlapsThe flaps are a two piece construction. The inner part of the fl

Airplane Description DA 42 NG AFMPage 7 - 6 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EThe flaps are operated by means of a 3-position flap selector switch

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 7ElevatorConstruction: GFRP sandwich.Hinges: 5 hinges.Operation: Steel

Airplane Description DA 42 NG AFMPage 7 - 8 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ERudderConstruction: GFRP sandwich.Hinges: Upper hinge: One bolt.Lower

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 9Elevator TrimThe trim control is a black wheel in the center console

Airplane Description DA 42 NG AFMPage 7 - 10 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EElectrical Pedal Adjustment (Optional Equipment, OÄM 42-070)NOTEThe

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 116871623910 11 18 24 19 2120 2522263016171227322829132134351431157.4

General DA 42 NG AFMPage 1 - 20 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E2205 mm(7 ft 3 in)1950 mm(6 ft 5 in)2490 mm(8 ft 2 in)1735 mm (5 ft 8 in)8560 mm

Airplane Description DA 42 NG AFMPage 7 - 12 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EMajor Instruments and Controls1 Electric master switch 17 Circuit br

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 137.5 LANDING GEARThe landing gear is a fully retractable, hydraulical

Airplane Description DA 42 NG AFMPage 7 - 14 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ETo test the gear warning system (refer to 4A.6.1 - PRE-FLIGHT INSPEC

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 15Hydraulic Gear Extension System SchematicThe main landing gear of th

Airplane Description DA 42 NG AFMPage 7 - 16 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EThe operating mode for the retraction of the landing gear is shown i

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 17For an emergency extension of the landing gear, the hydraulic fluid

Airplane Description DA 42 NG AFMPage 7 - 18 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-Ebrake pedals,pilotbrake pedals,co-pilotparking brakevalvebrake cylin

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 197.6 SEATS AND SAFETY HARNESSESTo increase passive safety, the seats

Airplane Description DA 42 NG AFMPage 7 - 20 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EOutboard HingeInboard HingeLamella PackageFriction AdjustmentScrewSe

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 217.7 BAGGAGE COMPARTMENTThere are two baggage compartments. One is lo

DA 42 NG AFM GeneralDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 1 - 211.8 G1000 AVIONICS SYSTEM1. The G1000 Integrated Avionics System is a fully integ

Airplane Description DA 42 NG AFMPage 7 - 22 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EWARNINGThe airplane may be operated with the front canopy in the“coo

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 23Heating and VentilationHeating and ventilation are operated using tw

Airplane Description DA 42 NG AFMPage 7 - 24 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EFloor PanelEmergency AxeEmergency AxeIf OÄM 42-205 is incorporated a

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 257.9 POWER PLANT7.9.1 ENGINES, GENERALThere are two Austro Engine E4

Airplane Description DA 42 NG AFMPage 7 - 26 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E7.9.2 PROPELLERTwo mt-Propeller MTV-6-R-C-F / CF 190-69 hydraulical

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 27Pressure Accumulator:The pressure accumulator is a nitrogen oil type

Airplane Description DA 42 NG AFMPage 7 - 28 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EUnfeathering:To unfeather the propeller, the associated ENGINE MASTE

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 297.9.3 OPERATING CONTROLSPower LeverEngine performance is controlled

Airplane Description DA 42 NG AFMPage 7 - 30 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ECAUTIONThe power lever should be moved slowly, in order to avoidover

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 31ECU VOTERThere are two VOTER switches, one for each engine. For norm

General DA 42 NG AFMPage 1 - 22 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E(b) RNAV (GPS) Approaches - The G1000 GPS meets the requirements ofAC 20-138(A) f

Airplane Description DA 42 NG AFMPage 7 - 32 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EAlternate AirIn the event of power loss because of icing or blocking

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 337.9.4 ENGINE INSTRUMENTSThe engine instruments are displayed on the

Airplane Description DA 42 NG AFMPage 7 - 34 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ENOTEThe figure on previous page is a general demonstration ofa typic

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 357.9.5 FUEL SYSTEMGeneralENGINEReturn LineFUSELAGECross-FeedLinesNOT

Airplane Description DA 42 NG AFMPage 7 - 36 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EFuel is stored in the tanks which are located in the wings.Normally

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 37Fuel Selector ValvesFor each engine one fuel selector valve is provi

Airplane Description DA 42 NG AFMPage 7 - 38 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EScheme of the Fuel Selector Valve Positions:Possible operating modes

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 39Fuel Selector ValveFuel SelectorFigure 1:Normal OperationRH EngineRe

Airplane Description DA 42 NG AFMPage 7 - 40 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EMain Fuel TanksEach tank consists of three aluminum chambers which a

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 41Auxiliary Fuel Tanks (if installed)The auxiliary fuel tanks are opti

DA 42 NG AFM GeneralDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 1 - 231.9 SOURCE DOCUMENTATIONThis section lists documents, manuals and other literatur

Airplane Description DA 42 NG AFMPage 7 - 42 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EWhen one auxiliary pump is defective, the fuel stored in the related

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 43Alternate Means for Fuel QuantityIndication for the Fuel Tank:The al

Airplane Description DA 42 NG AFMPage 7 - 44 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EFuel TemperatureMax. fuel temperature: 60 °C (140 °F)Fuel GradeAppro

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 45CoolantHeatExchangerCoreEngineExpansionTankThermostatic ValveWater P

Airplane Description DA 42 NG AFMPage 7 - 46 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E7.9.7 OIL SYSTEMSEach engine has two separate oil systems.Lubricati

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 47IntercoolerEngineWaste GateTurbineChargerExhaustAlternate Air ValveA

Airplane Description DA 42 NG AFMPage 7 - 48 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E7.9.9 FIRE DETECTION SYSTEMThe fire detection system in the DA 42 N

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 497.10 ELECTRICAL SYSTEM

Airplane Description DA 42 NG AFMPage 7 - 50 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E7.10.1 GENERALThe DA 42 NG has 28 Volt DC system, which can be sub-

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 51Alternator Control:Each alternator has an alternator control unit. I

Introduction DA 42 NG AFMPage 0 - 2 Rev. 3 01-Apr-2014 Doc. # 7.01.16-E0.1 APPROVALThe content of approved chapters is approved by EASA. All other con

General DA 42 NG AFMPage 1 - 24 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E1.9.2 PROPELLERAddress: mt-propellerAirport Straubing WallmühleD-94348 AttingGER

Airplane Description DA 42 NG AFMPage 7 - 52 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EDistributionElectrical power is distributed via the HOT BATTERY BUS,

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 53MAIN BUS:The LH (RH) MAIN BUS is connected to the BATTERY BUS via a

Airplane Description DA 42 NG AFMPage 7 - 54 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EPosition and Strobe LightsCombined position and strobe lights (anti

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 55External Power SocketThe DA 42 NG has an external 28 Volt DC power s

Airplane Description DA 42 NG AFMPage 7 - 56 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E7.10.2 ELECTRICAL ENGINE CONTROL UNIT / ECUEngine Control and Regula

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 57In accordance with the received signals and a comparison with the pr

Airplane Description DA 42 NG AFMPage 7 - 58 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E7.10.3 WARNING, CAUTION AND ADVISORY MESSAGESCrew Alerting System (

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 59Alert LevelsLevelText Color Importance Audible ToneWarning RedMay re

Airplane Description DA 42 NG AFMPage 7 - 60 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EWarning Alerts on the G1000Warning Alerts Meaning / CauseL/R ENG TEM

DA 42 NG AFM Airplane DescriptionWarning Alerts Meaning / CauseDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 61VERT SPEEDFAILThe annunciation is acti

DA 42 NG AFM Operating LimitationsDoc. No. 7.01.16-E Rev. 3 01-Apr-2014EASAapprovedPage 2 - 1CHAPTER 2OPERATING LIMITATIONSPage2.1 INTRODUCTION ...

Airplane Description DA 42 NG AFMPage 7 - 62 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ECaution Alerts on the G1000Caution Alerts Meaning / CauseL/R ECU A

DA 42 NG AFM Airplane DescriptionCaution Alerts Meaning / CauseDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 63DEICE LVL LO De-icing fluid level is

Airplane Description DA 42 NG AFMPage 7 - 64 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E7.11 PITOT-STATIC SYSTEMTotal pressure is measured at the leading ed

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 657.13 GARMIN G1000 INTEGRATED AVIONICS SYSTEM7.13.1 GENERALThe Gamin

Airplane Description DA 42 NG AFMPage 7 - 66 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E7.13.2 PRIMARY FLIGHT DISPLAY (PFD)The primary flight display (PFD;

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 67The PFD displays the crew alerting (annunciator) system. When a warn

Airplane Description DA 42 NG AFMPage 7 - 68 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EAdvisory messages related to G1000 system status are shown in white

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 697.13.4 AUDIO PANELThe audio panel contains traditional transmitter

Airplane Description DA 42 NG AFMPage 7 - 70 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E7.14 AVIONICS7.14.1 AUTOPILOT SYSTEMGeneralThe GFC 700 automatic f

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 71The GFC 700 may be manually disconnected by any of the following mea

Operating Limitations DA 42 NG AFMPage 2 - 2 Rev. 3 01-Apr-2014EASAapprovedDoc. No. 7.01.16-E2.16.6 GARMIN G1000 AVIONICS SYSTEM ... 2-38

Airplane Description DA 42 NG AFMPage 7 - 72 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E- Loss of the MFD will not cause the autopilot to disconnect, and wi

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 73VS (Vertical speed mode on/off)FLC (Flight level change mode on/off)

Airplane Description DA 42 NG AFMPage 7 - 74 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-EAnnunciation of the flight director and autopilot modes is shown in

DA 42 NG AFM Airplane DescriptionDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 757.14.2 AUTOMATIC FLIGHT CONTROL SYSTEM ANNUNCIATIONS ANDALERTSAuto

Airplane Description DA 42 NG AFMPage 7 - 76 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ECaution Alerts on the Automatic Flight Control System (AFCS)Caution

DA 42 NG AFMHandling, Care,MaintenanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 8 - 1CHAPTER 8AIRPLANE HANDLING, CARE AND MAINTENANCEPage8.1 INTRODUC

Handling, Care,MaintenanceDA 42 NG AFMPage 8 - 2 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E8.1 INTRODUCTIONChapter 8 contains the manufacturer's recom

DA 42 NG AFMHandling, Care,MaintenanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 8 - 38.3 AIRPLANE ALTERATIONS OR REPAIRSAlterations or repairs to the

Handling, Care,MaintenanceDA 42 NG AFMPage 8 - 4 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-ECAUTIONUse only approved fuel types given in Chapter 2.1. Ground

DA 42 NG AFMHandling, Care,MaintenanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 8 - 58.4.4 TIRE INFLATION PRESSURE CHECK1. Remove dust cap from valv

DA 42 NG AFM Operating LimitationsDoc. No. 7.01.16-E Rev. 3 01-Apr-2014EASAapprovedPage 2 - 32.1 INTRODUCTIONChapter 2 of this Airplane Flight Manual

Handling, Care,MaintenanceDA 42 NG AFMPage 8 - 6 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E8.5 GROUND HANDLING / ROAD TRANSPORT8.5.1 GROUND HANDLINGFor pu

DA 42 NG AFMHandling, Care,MaintenanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 8 - 7CAUTIONTowing with towing vehicles is not approved.NOTEIf the en

Handling, Care,MaintenanceDA 42 NG AFMPage 8 - 8 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E

DA 42 NG AFMHandling, Care,MaintenanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 8 - 98.5.3 MOORINGNear the lower end of the tail fin of the airplane

Handling, Care,MaintenanceDA 42 NG AFMPage 8 - 10 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E8.6 CLEANING AND CARECAUTIONThe airplane must be kept clean. Th

DA 42 NG AFMHandling, Care,MaintenanceDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 8 - 118.6.2 CANOPY AND REAR DOORThe canopy, rear door and rear windo

Handling, Care,MaintenanceDA 42 NG AFMPage 8 - 12 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E8.7 GROUND DE-ICINGApproved deicing fluids are:Manufacturer Nam

DA 42 NG AFM SupplementsDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 9 - 1CHAPTER 9SUPPLEMENTSPage9.1 INTRODUCTION ...

Supplements DA 42 NG AFMPage 9 - 2 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E9.1 INTRODUCTIONChapter 9 contains information concerning additional (optional

DA 42 NG AFM SupplementsDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 9 - 39.2 LIST OF SUPPLEMENTSAirplane S/N: Registration: Date:Sup.No.TitleRev.No.Dat

Operating Limitations DA 42 NG AFMPage 2 - 4 Rev. 3 01-Apr-2014EASAapprovedDoc. No. 7.01.16-E2.2 AIRSPEEDAirspeed KIAS RemarksvOOperatingmaneuveringsp

Supplements DA 42 NG AFMAirplane S/N: Registration: Date:Sup.No.TitleRev.No.DateapplicableYES NOPage 9 - 4 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E999999

DA 42 NG AFM Operating LimitationsDoc. No. 7.01.16-E Rev. 3 01-Apr-2014EASAapprovedPage 2 - 52.3 AIRSPEED INDICATOR MARKINGSMarking KIAS SignificanceW

Operating Limitations DA 42 NG AFMPage 2 - 6 Rev. 3 01-Apr-2014EASAapprovedDoc. No. 7.01.16-E2.4 POWER-PLANT LIMITATIONSa) Number of engines : 2b) Eng

DA 42 NG AFM Operating LimitationsDoc. No. 7.01.16-E Rev. 3 01-Apr-2014EASAapprovedPage 2 - 7h) Oil temperatureMinimum : - 30 °CMaximum : 140 °CNorma

Operating Limitations DA 42 NG AFMPage 2 - 8 Rev. 3 01-Apr-2014EASAapprovedDoc. No. 7.01.16-Ek) Fuel temperatureMinimum : - 30 °CMaximum : 60 °Cl) F

DA 42 NG AFM Operating LimitationsDoc. No. 7.01.16-E Rev. 3 01-Apr-2014EASAapprovedPage 2 - 9t) Oil specification : SAE Grade 5W-30:SHELL HELIX ULTRA

DA 42 NG AFM IntroductionDoc. # 7.01.16-E Rev. 3 01-Apr-2014 Page 0 - 3Rev.No.ReasonChap-ter Page(s)Date ofRevisionEASAApproval No.Approval'Date&

Operating Limitations DA 42 NG AFMPage 2 - 10 Rev. 3 01-Apr-2014EASAapprovedDoc. No. 7.01.16-ECAUTIONOnly engine oils conforming to MB 229.5 specifica

DA 42 NG AFM Operating LimitationsDoc. No. 7.01.16-E Rev. 3 01-Apr-2014EASAapprovedPage 2 - 112.5 ENGINE INSTRUMENT MARKINGSEngine instrument markings

Operating Limitations DA 42 NG AFMPage 2 - 12 Rev. 3 01-Apr-2014EASAapprovedDoc. No. 7.01.16-E2.6 WARNING, CAUTION AND ADVISORY ALERTS2.6.1 WARNING,

DA 42 NG AFM Operating LimitationsWarning alerts (red)Meaning / CauseDoc. No. 7.01.16-E Rev. 3 01-Apr-2014EASAapprovedPage 2 - 13L/R ALTN AMPS Left /

Operating Limitations DA 42 NG AFMPage 2 - 14 Rev. 3 01-Apr-2014EASAapprovedDoc. No. 7.01.16-EColor and Significance of the Caution Alerts on the G100

DA 42 NG AFM Operating LimitationsCaution alerts(amber)Meaning / CauseDoc. No. 7.01.16-E Rev. 3 01-Apr-2014EASAapprovedPage 2 - 15CHECK GEAR Landing g

Operating Limitations DA 42 NG AFMPage 2 - 16 Rev. 3 01-Apr-2014EASAapprovedDoc. No. 7.01.16-E2.6.2 OTHER WARNING ALERTSWarning Alerts on the Instrum

DA 42 NG AFM Operating LimitationsDoc. No. 7.01.16-E Rev. 3 01-Apr-2014EASAapprovedPage 2 - 172.7 MASS (WEIGHT)ValueMass (Weight)Minimum flight mass 1

Operating Limitations DA 42 NG AFMPage 2 - 18 Rev. 3 01-Apr-2014EASAapprovedDoc. No. 7.01.16-ENOTEIn some countries the beginning of a flight is defin

DA 42 NG AFM Operating LimitationsDoc. No. 7.01.16-E Rev. 3 01-Apr-2014EASAapprovedPage 2 - 192.8 CENTER OF GRAVITYDatum PlaneThe datum plane (DP) is

Introduction DA 42 NG AFMPage 0 - 4 Rev. 3 01-Apr-2014 Doc. # 7.01.16-E0.3 LIST OF EFFECTIVE PAGESCh. Page Date0 0-0 19-Jun-20120-0a 01-Apr-2014'

Operating Limitations DA 42 NG AFMPage 2 - 20 Rev. 3 01-Apr-2014EASAapprovedDoc. No. 7.01.16-EWARNINGExceeding the center of gravity limitations reduc

DA 42 NG AFM Operating LimitationsDoc. No. 7.01.16-E Rev. 3 01-Apr-2014EASAapprovedPage 2 - 212.9 APPROVED MANEUVERSThe airplane is certified in the N

Operating Limitations DA 42 NG AFMPage 2 - 22 Rev. 3 01-Apr-2014EASAapprovedDoc. No. 7.01.16-E2.10 MANEUVERING LOAD FACTORSNOTEThe tables below show s

DA 42 NG AFM Operating LimitationsDoc. No. 7.01.16-E Rev. 3 01-Apr-2014EASAapprovedPage 2 - 232.11 OPERATING ALTITUDEThe maximum operating altitude is

Operating Limitations DA 42 NG AFMPage 2 - 24 Rev. 3 01-Apr-2014EASAapprovedDoc. No. 7.01.16-ENOTEMany of the items of minimum equipment listed in the

DA 42 NG AFM Operating Limitationsfor daytime VFR flightsin addition for night VFR flightsin addition for IFR flightsDoc. No. 7.01.16-E Rev. 3 01-Apr-

Operating Limitations DA 42 NG AFMfor daytime VFR flightsin addition for night VFR flightsin addition for IFR flightsPage 2 - 26 Rev. 3 01-Apr-2014EAS

DA 42 NG AFM Operating LimitationsDoc. No. 7.01.16-E Rev. 3 01-Apr-2014EASAapprovedPage 2 - 272.14 FUELApproved fuel grades: JET A, JET A-1 (ASTM D 16

Operating Limitations DA 42 NG AFMPage 2 - 28 Rev. 3 01-Apr-2014EASAapprovedDoc. No. 7.01.16-EAny mixture of the different types of fuel additives is

DA 42 NG AFM Operating LimitationsDoc. No. 7.01.16-E Rev. 3 01-Apr-2014EASAapprovedPage 2 - 29OPERATION WITH ANTI-ICING FUEL ADDITIVES'The applic

DA 42 NG AFM IntroductionDoc. # 7.01.16-E Rev. 3 01-Apr-2014 Page 0 - 5Ch. Page Date2 appr. 2-1 01-Apr-2014'appr. 2-2 01-Apr-2014'appr. 2-3

Operating Limitations DA 42 NG AFMPage 2 - 30 Rev. 3 01-Apr-2014EASAapprovedDoc. No. 7.01.16-E2.15 LIMITATION PLACARDSAll limitation placards are show

DA 42 NG AFM Operating LimitationsDoc. No. 7.01.16-E Rev. 3 01-Apr-2014EASAapprovedPage 2 - 31LANDING GEARvLE / vLOE = 188 KIASvLOR = 152 KIAS GPS NO

Operating Limitations DA 42 NG AFMPage 2 - 32 Rev. 3 01-Apr-2014EASAapprovedDoc. No. 7.01.16-EOILSHELL HELIX ULTRA5W30or see Airplane Flight ManualWAR

DA 42 NG AFM Operating LimitationsDoc. No. 7.01.16-E Rev. 3 01-Apr-2014EASAapprovedPage 2 - 33UPFlapsAPP133 KIASLDG 113 KIASNext to the Flap Selector

Operating Limitations DA 42 NG AFMPage 2 - 34 Rev. 3 01-Apr-2014EASAapprovedDoc. No. 7.01.16-EIf OÄM 42-207 is carried out:In the Cabin, on the Left F

DA 42 NG AFM Operating LimitationsDoc. No. 7.01.16-E Rev. 3 01-Apr-2014EASAapprovedPage 2 - 35In the Nose Baggage Compartment:Beside the Door Locking

Operating Limitations DA 42 NG AFMPage 2 - 36 Rev. 3 01-Apr-2014EASAapprovedDoc. No. 7.01.16-E2.16 OTHER LIMITATIONS2.16.1 FUEL TEMPERATUREFrom -30 °

DA 42 NG AFM Operating LimitationsDoc. No. 7.01.16-E Rev. 3 01-Apr-2014EASAapprovedPage 2 - 372.16.5 ELECTRONIC EQUIPMENTThe use and switching on of

Operating Limitations DA 42 NG AFMPage 2 - 38 Rev. 3 01-Apr-2014EASAapprovedDoc. No. 7.01.16-E2.16.6 GARMIN G1000 AVIONICS SYSTEM1. The Garmin G1000

DA 42 NG AFM Operating LimitationsDoc. No. 7.01.16-E Rev. 3 01-Apr-2014EASAapprovedPage 2 - 39NOTEThe database version is displayed on the MFD power-u

Introduction DA 42 NG AFMPage 0 - 6 Rev. 3 01-Apr-2014 Doc. # 7.01.16-ECh. Page Date3 3-1 01-Apr-2014'3-2 01-Apr-2014'3-3 01-Apr-2014'3

Operating Limitations DA 42 NG AFMPage 2 - 40 Rev. 3 01-Apr-2014EASAapprovedDoc. No. 7.01.16-E(d) When an alternate airport is required by the applica

DA 42 NG AFM Operating LimitationsDoc. No. 7.01.16-E Rev. 3 01-Apr-2014EASAapprovedPage 2 - 416. When AHRS is required to meet the items listed in the

Operating Limitations DA 42 NG AFMPage 2 - 42 Rev. 3 01-Apr-2014EASAapprovedDoc. No. 7.01.16-E2.16.7 AUTOPILOT LIMITATIONS1. It is the responsibility

DA 42 NG AFM Operating LimitationsDoc. No. 7.01.16-E Rev. 3 01-Apr-2014EASAapprovedPage 2 - 4310. The GFC 700 components must utilize the following or

Operating Limitations DA 42 NG AFMPage 2 - 44 Rev. 3 01-Apr-2014EASAapprovedDoc. No. 7.01.16-E2.16.8 SMOKINGSmoking in the airplane is not permitted.

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 1CHAPTER 3EMERGENCY PROCEDURESPage3.1 INTRODUCTION ...

EmergencyProceduresDA 42 NG AFMPage 3 - 2 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E3.5 G1000 FAILURES ... 3-183.5.1 NAV

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 33.10.1 COMPLETE FAILURE OF THE ELECTRICAL SYSTEM . . 3-543.10.2 HIGH

EmergencyProceduresDA 42 NG AFMPage 3 - 4 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E3.1 INTRODUCTION3.1.1 GENERALThis chapter contains checklists as well

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 53.1.2 CERTAIN AIRSPEEDS IN EMERGENCIESEventOne engine inoperative mini

DA 42 NG AFM IntroductionDoc. # 7.01.16-E Rev. 3 01-Apr-2014 Page 0 - 7Ch. Page Date3 3-55 01-Apr-2014'3-56 01-Apr-2014'3-57 01-Apr-2014&apo

EmergencyProceduresDA 42 NG AFMPage 3 - 6 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E3.2 AIRPLANE-RELATED G1000 WARNINGS3.2.1 WARNINGS / GENERAL"Warni

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 7During cruise:- Reduce power on affected engine.- Increase airspeed.- C

EmergencyProceduresDA 42 NG AFMPage 3 - 8 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E3.2.3 L/R OIL TEMPL/R OIL TEMPLeft / Right engine oil temperature is i

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 9CAUTIONIf high oil temperature is announced and the oil pressureindicat

EmergencyProceduresDA 42 NG AFMPage 3 - 10 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E3.2.5 L/R GBOX TEMPL/R GBOX TEMPLeft / Right engine gearbox temperatu

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 113.2.6 L/R FUEL TEMPL/R FUEL TEMPLeft / Right fuel temperature is in t

EmergencyProceduresDA 42 NG AFMPage 3 - 12 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E3.2.7 L/R FUEL PRESSL/R FUEL PRESSLeft / Right engine fuel pressure i

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 133.2.9 L/R ENG FIREL/R ENG FIRELeft / Right engine fire detected.Engin

EmergencyProceduresDA 42 NG AFMPage 3 - 14 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E3.2.10 L/R STARTERL/R STARTERLeft / Right engine starter is engaged.Pr

DA 42 NG AFMEmergencyProceduresDoc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 3 - 153.3 AIRPLANE-RELATED G1000 CAUTIONS3.3.1 L/R ALTN FAILL/R ALTN FAILLe