Diamond DA 40-TDI G1000

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1 Diamond DA 40-TDI G1000 Diamond DA40-TDI G1000 Dimensions DA40-TDI-G1000 Version 1.1 Dimensions Dimensions 11,94 m 1,97 m 8,01 m 2,97 m 1,68 m Diamond DA40-TDI G1000 ELT and VHF COM 1 Antenna Exterior ELT antenna in fuselage structure VHF COM 1

2 VHF COM 2 antenna VHF NAV + GP Antennas in the horizontal stabilizer Marker Antenna GPS Antennas Fuselage belly Cabin roof DME, TXPDR Antenna ADF antenna Fuselage belly Fuselage belly

3 Pitot/Static Probe Pitot/Static Probe Left wing Static Pitot Lift Detector (Stall Warning) Engine Oil Left wing Engine Oil Air Inlets Intercooler Coolant heat exchanger Oil Cooler

4 Air Inlets Air Inlets Engine air intake RH frontventilation LH front Ventilation Cabin air heater Diamond DA40-TDI G1000 Temperature Limitation Operating Limitation The airplane may only be operated when its temperature prior to operation is not less than -20 C and not higher than 54 C. With the airplane cold soaked and its temperature below -20 C the use of an external pre-heater for the engine and pilot compartment prior to operation is mandatory. Diamond DA40-TDI G1000 Mass (Weight) Mass Empty (typical) Max TKOF Max LDG Max Baggage Max Baggage with Baggage Extension 830 kg 1150 kg 1150 kg 30 kg 45 kg (max 18 kg in aft compartment)

5 Mass (Weight) Attention! JET fuel and Diesel are heavier than AVGAS! Diamond DA40-TDI G1000 Speeds Typical fuel weight: JET A1: 0,8 kg/ltr 3,03 kg/usg Diesel: 0,84 kg/ltr 3,2 kg/usg Characteristic Speeds Characteristic Speeds VNO 129 KIAS VSO 49 KIAS VNE 178 KIAS VS1 52 KIAS VA kg 94 KIAS VFE (Flaps T/O) 108 KIAS VA kg 108 KIAS VFE (Flaps LDG) 91 KIAS Characteristic Speeds Stalling Speeds 980 kg 850 kg 1000 kg 1150 kg VX = VY 54 KIAS 60 KIAS 66 KIAS VSO VS1 V climb 60 KIAS 68 KIAS 73 KIAS VLDG Flaps UP 60 KIAS 68 KIAS 73 KIAS 1150 kg VLDG Flaps LDG 58 KIAS 63 KIAS 71 KIAS

6 Stalling Speeds Stalling Speeds 980 kg 980 kg VSO VS1 VSO VS kg 1150 kg Diamond DA40-TDI G1000 Flight Control Operation Flight Controls Ailerons, Elevator: push rods Rudder: cables Flight Control Operation Flaps: electrically by push rods, left and right mechanically interconnected Intentionally blank

7 Diamond DA40-TDI G1000 Instrument Panel Instrument Panel Garmin 1000 Instrument Panel Instrument Panel Flood Lights Airspeed Horizon Altimeter Backup Instruments Compass Emergency Switch Emergency Battery (non rechargeable) Instrument Panel Instrument Panel Lights ELT Circuit breakers

8 Instrument Panel Instrument Panel Essential Bus Electric Master Starter Engine control Instrument Panel Instrument Panel Avionic Master Fuel x-fer pump, Pitot heat Autopilot Flaps Alternate Static Valve Engine Indication System Default SYSTEM FUEL

9 Diamond DA40-TDI G1000 Hydraulic System Hydraulic brakes Pilot applies brake Pumping Hydraulic brakes Parking brake Parking brake One-way valve is closed Pressure builds up Diamond DA40-TDI G1000 Diamond DA40 TDI Engine Power Plant Thielert Aircraft Engine TAE Previously: TAE Four cylinders, liquid-cooled 1991 ccm (TAE125-01: 1689 ccm) Common-rail direct injection Reduction gear 1:1,69 Dual digital engine control Turbocharger Max. power: 99kW (135 HP) at 2300 RPM Max cont. power: 99kW (135 hp) at 2300 RPM

10 Diamond DA40 TDI Engine Thielert Aircraft Engine TAE125 Four cylinders, liquid-cooled, 1689 ccm Common-rail direct injection Reduction gear 1:1,69 Digital engine control Turbocharger Max. power 99kW (135 PS) at 2300 RPM Max cont. power 99kW (135 PS) at 2300 RPM Digital Engine Control ECU Engine Control Unit this is a FADEC Full Authority Digital Engine Control ECU Engine Control Unit E.O.T. Engine Order Telgraph ( Chadburn ) Diamond DA40 TDI Engine Diamond DA40 TDI Engine Power lever selects power (LOAD in %) RPM automatically determined by selected power Alternate air valve Heat Exchanger for Cabin Heat System Engine air filter

11 Diamond DA40 TDI Engine Diamond DA40 TDI Engine Coolant Reservoir Intercooler CoolantHeatExchanger Reduction Gear Generator Power plant Gear oil Power plant Gear oil Power plant Gear oil Power plant limitations Isthisthelittlebubble? Italic figures are for the old engine Max RPM: 2300 Oil pressure: bar Oil quantity (per engine): liters Max. oil consumption: 0.1 liters/hr Oil temperature: -30 (-32) C 140 C Gearbox temperature: max. 120 C Coolant temperature: -30 (-32) C 105 C Max. restart altitude: 8000 ft (6500 ft), KIAS

12 Power plant fluid specifications Fuel: JET A-1 or JET A (ASTM D 1655) JET No. 3 (GB ) Diesel (EN 590) Oil: SHELL Helix Ultra 5W30 synth. API SL/CF SHELL Helix Ultra 5W40 synth. API SL/CF AERO SHELL Diesel 10W-40 Gearbox oil: SHELL EP 75W90 API GL-4 Coolant: DAI-G30-MIX special water (TAE-125-OM-02-01) + cooler protection 1:1 (BASF Glysantin Alu Protect Plus/G30) (freezing point 36 C)! Diesel limitations Temperature limits Below -5 C no engine start Below +5 C no take-off Be sure that no diesel fuel is in the tanks otherwise temp limitations for diesel ops must be observed Diesel limitations Diesel limitations When is no more diesel in the tanks? each tank to be refilled at least twice with more than 10,6 USG (40 ltrs) (normal tanks) 17,2 USG (65 ltrs) (long range tanks) of Jet fuel otherwise tank must be drained JET fuel Fuel temperature Diesel, Diesel/JET blend or unknown Analogue indication Default page Take-off Engine start FUEL page Diamond DA40-TDI G1000 DA 40 TDI Cooling System Cooling System

13 DA 40 TDI Cooling System DA 40 TDI Cooling System Coolant Temp. < 80 Coolant Temp. > 80 DA 40 TDI Cooling System DA 40 TDI Cabin Heat Cabin Heat DA 40 TDI Ventilation DA 40 TDI Ventilation Cockpit Left wing Cabin Rear cabin ventilation air inlet

14 Diamond DA40-TDI G1000 DA 40 TDI Turbo Charger Turbocharger System Exhaust gas drives turbine Bypass for excess exhaust gas DA 40 TDI Turbo Charger Diamond DA40-TDI G1000 Fuel System Compressor Turbine drives compresses compressor intake air DA 40 TDI Fuel System DA 40 TDI Fuel System 2 x 14 USG usable = 28 USG = 85 kg At 70% power: ~ 5 USG/hr Long Range Tanks: 2 x 19,5 USG usable = 39 USG = 120 kg Max indicated fuel per tank: 15 USG Max. unbalance: 9 USG

15 DA 40 TDI Fuel System DA 40 TDI Fuel System DA 40 TDI Fuel System Fuel cooler Right wing USG/hr Fuel cooler ~60 USG/hr Air inlet Air outlet DA 40 TDI Fuel System DA 40 TDI Fuel System USG/hr U/S Fuel cooler U/S

16 DA 40 Fuel system Fuel vents Alternate means for fuel quantity indication Position: at theborein thestall strip Fuel tank drain Fuel gascolator drain FWD Diamond DA40-TDI G1000 DA40 TDI G1000 Electrical System Electrical System

17 DA40 TDI G1000 Electrical System DA40 TDI G1000 Electrical System Power sources Generator 12-14V 90A ECU Backup Battery 12V 12Ah Excitation Battery 12V 1,3 Ah Power distribution Battery Bus ECU Bus Main Bus Main Battery 12V 45Ah Hot Battery Bus Avionic Bus Essential Bus Electric Master, Essential Bus Engine Master DA40 TDI G1000 Electrical System DA40 TDI G1000 Electrical System Before Engine Start OFF Preparing Engine Start ON ON ON OFF OFF

18 DA40 TDI G1000 Electrical System DA40 TDI G1000 Electrical System Engine Start ON After Engine Start ON ON ON START OFF OFF ON External Power Receptable Emergency Switch DA40-TDI G1000 Switch location The mysterious Essential Bus Switch

19 When is it used? Essential Electrial Power When the generator fails to disconnect unnecessary electrical consumers to supply battery power to essential electrical consumers Essential Bus PFD Horizon *) AHRS ADC Flaps Landing light Pitot Heating Landing Light Flood Light *) COM 1 GPS / NAV Receiver 1 Transponder Engine instruments Hot Battery Bus (Essential Bus) Pilot s map/reading light Auxiliary jack *) Emergency Battery Essential Electrial Power What happens... Main unserviceable systems Fuel x-fer pump MFD Acionic / CDU fan Position light, Strobe lights, Taxi light Instrument lights, Map light Starter (Avionics Bus) COM2, NAV/GPS2, ADF, DME, WX500, Audio, Autopilot... if it is switched ON during normal operation? Will the battery be discharged? NO! DA40-TDI G1000, Ess. Bus switch DA40-TDI G1000, Ess. Bus switch Normal Situation GEN Hot Battery Bus BATT Battery is charged Battery Bus ECU Bus Main Bus Essential Bus Avioniic Bus GEN u/s, Ess. PWR OFF Hot Battery Bus GEN BATT Battery will be discharged Battery Bus ECU Bus Main Bus Essential Bus Avioniic Bus

20 DA40-TDI G1000, Ess. Bus switch DA40-TDI G1000, Ess. Bus switch GEN u/s, Ess. PWR ON Hot Battery Bus GEN BATT Battery will be discharged at slow rate Battery Bus ECU Bus Main Bus Essential Bus Avioniic Bus GEN OK, Ess. PWR ON Hot Battery Bus GEN BATT Battery is still charged Battery Bus ECU Bus Main Bus Essential Bus Avioniic Bus DA40-TDI G1000, Ess. Bus switch DA40-TDI G1000, Ess. Bus switch Essential Bus ON by mistake Hot Battery Bus GEN BATT Battery Bus ECU Bus Fuel x-fer pump MFD Avion./CDU fan FAN / OAT indication Position light Strobe lights Taxi light, Map light Instrument lights Starter Main Bus Essential Bus Avioniic Bus COM2, NAV/GPS2, Audio, ADF, DME, Autopilot WX 500 A very special engine start problem: Start witch ON Nothing happens! Why? Essential Bus switch ON by mistake! DA40 TDI G1000 Electrical System Generator + Battery Fail ON ECU backup battery Intentionally blank

21 Diamond DA40-TDI G1000 Autopilot KAP140 Autopilot KAP 140 has 2 functions: if not engaged: Altitude warning if engaged ( ON ): Autopilot Autopilot Autopilot Stearing signal YES Baro setting NO Heading YES Altitude NO Autopilot limitations Autopilot CWS AP disconnect Manual Electric Trim

22 Autopilot Autopilot ALT ARM AP engaged annunciator Pitch trim annunciator ALT Alert Pitch Wrng AP ON/OFF Baro display/ setting Set Altitude or Baro ALT V/S BARO display Roll Wrng HDG select APR mode ALT Hold NAV mode Backbeam +/- V/S or +/- Alt Autopilot Roll Mode: ROL HDG NAV ARM NAV APR ARM APR REV ARM REV GS ARM Autopilot Altitude Preselect Select Altitude Check ALT ARM Adjust V/S Pitch Mode: VS ALT ARM ALT GS ALT Check ALT ALERT Check ALT Hold Autopilot Altitude preselect Selecting altitude when autopilot is ON: Altitude ARMED automatically Switching autopilot ON with a preselected altitude (e.g. when altitude was preselected before TKOF): Altitude must be ARMed manually! Autopilot Altitude Hold Mode Vertical Speed Mode Toggles between ALT HLD and V/S Toggles between ALT HLD and V/S

23 Diamond DA40-TDI G1000 Performance The DA 40 TDI and Density Altitude Attention! Performance data which are enginepower dependant cannot be determined by just using Density Altitude! Reason: the engine power output does not correspond to density altitude but pressure and temperature have their own, independent influence This is a feature of the ECU controlled, turbocharged Diesel-engine Cruise Power Setting Cruising Speed e.g ft, ISA, 70 % 121 kts TOD TKOF Distance SL, ISA, 1150 kg: 640 m

24 TKOF Run Grass Runway Length of grass -5 cm 5-10 cm >10 cm TKOF roll + 10% + 15% min + 25% Wet grass may be significantly longer Take off climb 66 KIAS Cruise Climb 73 KIAS Attention! Increasing downward ROC to gradient conversion LD, LR tabular format Flaps LDG VREF 71 KIAS Flaps UP VREF 73 KIAS

25 Landing Distance Landing Run Grass Runway Go Around Length of grass -5 cm 5-10 cm >10 cm LDG run + 5% + 15% min + 25% Wet grass may be significantly longer Obstacles? Vöslau RWY 31 d = (RWL + Obst.Dist.) - TOD d = ( ) 650 = 1130 Gradient = ( h / d ) * 100 Gradient = (30 / 1130) * 100 = 2,65 % Acc. Performance Graph: ~ 9 % h 98 ft TOD RWL d Obst. Dist m

26 Diamond DA40-TDI G1000 Empty Mass Mass and Balance Empty Mass includes: Equipment as per Equipment Inventory Brake fluid Coolant fluid Gear oil Engine oil Unusable fuel (2 x 1,0 USG) Center of Gravity Envelope Moment Envelope Moment Arms Typical M+B data Item Front seats Rear seats Lever Arm (m) IFR -version (ADF, WX500) Empty mass 833,5 Moment 2057,7 CG arm 2,469 Wing tanks 2.63 N-VFR -version 826,2 2032,3 2,460 Fwd. baggage 3.89 Aft baggage 4.54

27 M&B Calculation M&B Calculation Lever arm Mass (kg) Moment (kgm) Lever arm Mass (kg) Moment (kgm) Empty mass Empty mass Front seats x 2.30 = Front seats Rear seats x 3.25 = Rear seats Fwd. Baggage Fwd. Baggage Zero Fuel Mass Zero Fuel Mass : 1090 = Fuel ~20 USG Fuel Total TKOF Mass Total TKOF Mass : 1150 = Center of Gravity Envelope M&B Calculation 1150 kg, 2.52 m TOM Lever arm Mass (kg) Moment (kgm) 1090 kg, m ZFM Empty mass Front seats Rear seats Fwd. Baggage Zero Fuel Mass Fuel Total TKOF Mass Moment Envelope 1150 kg, TOM 1090 kg, ZFM Intentionally blank

28 FWD Diamond DA40-TDI G1000 Emergency equipment Emergency Equipment Emergency Exit Emergency Exit FWD Diamond DA40-TDI G1000 Kinds of Operation Equipment List KOEL Kinds of Operation Equipment List (KOEL)

29 Kinds of Operation Equipment List KOEL Kinds of Operation Equipment List KOEL Kinds of Operation Equipment List KOEL Kinds of Operation Equipment List KOEL Additional minimum equipment for the intended operation may be required by national operating rules and also depends on the route to be flown. Diamond DA40-TDI G1000 Scheduled maintenance Servicing Every 100 hours 200 hours 1000 hours 2000 hours Annually

30 Refuelling De-icing Approved de-icing fluids: Kilfrost TKS 80 Aeroshell Compound 07 Procedure: Remove snow with brush Spray de-icing fluid Wipe dry Control surfaces gust lock Mooring Mooring Tow bar

31 Diamond DA40-TDI G1000 TKOF Profile Flight Procedures Rotate at 59 kt LDG Profile Checklists Thechecklistsarenotpartof theafm, and theyarenot officially Diamond-endorsed. They are a recommendation for Operator Checklists published by Diamond Aircraft Flight Training Division. Thank you for your attention!

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