Diamond DA 40-TDI G1000

Compiled by Peter Schmidleitner 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 © Peter Schmidleitner Compiled by Peter Schmidleitner Digital Engine Control „ ECU „ Engine Control Unit this is a „ FADEC „ Full Authority Digital Engine Control © Peter Schmidleitner Compiled by Peter Schmidleitner ECU – Engine Control Unit © Peter Schmidleitner Compiled by Peter Schmidleitner E.O.T. – Engine Order Telgraph („Chadburn“) © Peter Schmidleitner Compiled by Peter Schmidleitner • Power lever selects power (LOAD in %) • RPM automatically determined by selected power Diamond DA40 TDI Engine © Peter Schmidleitner Compiled by Peter Schmidleitner Diamond DA40 TDI Engine Engine air filter Alternate air valve Heat Exchanger for Cabin Heat System © Peter Schmidleitner Compiled by Peter Schmidleitner Intercooler Diamond DA40 TDI Engine © Peter Schmidleitner Compiled by Peter Schmidleitner Diamond DA40 TDI Engine Coolant Heat Exchanger Reduction Gear Coolant Reservoir Generator © Peter Schmidleitner Compiled by Peter Schmidleitner Power plant – Gear oil © Peter Schmidleitner Compiled by Peter Schmidleitner Power plant – Gear oil © Peter Schmidleitner Compiled by Peter Schmidleitner Power plant – Gear oil Is this the little bubble ? © Peter Schmidleitner Compiled by Peter Schmidleitner Power plant limitations „ Italic figures are for the „old“ 125-01 engine „ Max RPM: 2300 „ Oil pressure: 1.0 – 6.5 bar „ Oil quantity (per engine): 4.5 – 6.0 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), 73–120 KIAS © Peter Schmidleitner Compiled by Peter Schmidleitner „ Fuel: JET A-1 or JET A (ASTM D 1655) JET No. 3 (GB6537-94) 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) ! Power plant fluid specifications © Peter Schmidleitner Compiled by Peter Schmidleitner „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 © Peter Schmidleitner Compiled by Peter Schmidleitner „ 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 „Diesel“ limitations © Peter Schmidleitner Compiled by Peter Schmidleitner JET fuel -30 +75 +70 +5 -5 Fuel temperature Diesel, Diesel/JET blend or unknown Engine start Take-off Analogue indication FUEL page „Diesel“ limitations Default page Diamond DA40-TDI G1000 Compiled by Peter Schmidleitner Cooling System © Peter Schmidleitner Compiled by Peter Schmidleitner DA 40 TDI Cooling System © Peter Schmidleitner Compiled by Peter Schmidleitner DA 40 TDI Cooling System Coolant Temp. < 80° © Peter Schmidleitner Compiled by Peter Schmidleitner DA 40 TDI Cooling System Coolant Temp. > 80° © Peter Schmidleitner Compiled by Peter Schmidleitner DA 40 TDI Cooling System Cabin Heat © Peter Schmidleitner Compiled by Peter Schmidleitner DA 40 TDI Cabin Heat © Peter Schmidleitner Compiled by Peter Schmidleitner Cockpit DA 40 TDI Ventilation Cabin Cabin © Peter Schmidleitner Compiled by Peter Schmidleitner DA 40 TDI Ventilation Left wing Rear cabin ventilation air inlet Diamond DA40-TDI G1000 Compiled by Peter Schmidleitner Turbocharger System © Peter Schmidleitner Compiled by Peter Schmidleitner DA 40 TDI Turbo Charger Exhaust gas drives turbine Bypass for excess exhaust gas © Peter Schmidleitner Compiled by Peter Schmidleitner DA 40 TDI Turbo Charger Turbine drives compressor Compressor compresses intake air Diamond DA40-TDI G1000 Compiled by Peter Schmidleitner Fuel System © Peter Schmidleitner Compiled by Peter Schmidleitner „ 2 x 14 USG usable „ = 28 USG „ = 85 kg „ At 70% power: ~ 5 USG/hr DA 40 TDI Fuel System © Peter Schmidleitner Compiled by Peter Schmidleitner „ Long Range Tanks: 2 x 19,5 USG usable „ = 39 USG „ = 120 kg „ Max indicated fuel per tank: 15 USG „ Max. unbalance: 9 USG DA 40 TDI Fuel System © Peter Schmidleitner Compiled by Peter Schmidleitner DA 40 TDI Fuel System © Peter Schmidleitner Compiled by Peter Schmidleitner DA 40 TDI Fuel System © Peter Schmidleitner Compiled by Peter Schmidleitner DA 40 TDI Fuel System 18-21 USG/hr ~60 USG/hr Fuel cooler © Peter Schmidleitner Compiled by Peter Schmidleitner Fuel cooler Right wing Air inlet Air outlet © Peter Schmidleitner Compiled by Peter Schmidleitner DA 40 TDI Fuel System U/S © Peter Schmidleitner Compiled by Peter Schmidleitner DA 40 TDI Fuel System 18-21 USG/hr U/S Fuel cooler © Peter Schmidleitner Compiled by Peter Schmidleitner DA 40 Fuel system „Alternate means for fuel quantity indication“ Position: at the bore in the stall strip © Peter Schmidleitner Compiled by Peter Schmidleitner Fuel vents © Peter Schmidleitner Compiled by Peter Schmidleitner Fuel tank drain FWD © Peter Schmidleitner Compiled by Peter Schmidleitner Fuel gascolator drain Diamond DA40-TDI G1000 Compiled by Peter Schmidleitner Electrical System © Peter Schmidleitner Compiled by Peter Schmidleitner DA40 TDI G1000 Electrical System © Peter Schmidleitner Compiled by Peter Schmidleitner DA40 TDI G1000 Electrical System Power sources Generator 12-14V 90A Main Battery 12V 45Ah ECU Backup Battery 12V 12Ah Excitation Battery 12V 1,3 Ah © Peter Schmidleitner Compiled by Peter Schmidleitner DA40 TDI G1000 Electrical System Power distribution Hot Battery Bus Battery Bus Main Bus Essential Bus ECU Bus Avionic Bus © Peter Schmidleitner Compiled by Peter Schmidleitner Electric Master, Essential Bus © Peter Schmidleitner Compiled by Peter Schmidleitner Engine Master © Peter Schmidleitner Compiled by Peter Schmidleitner DA40 TDI G1000 Electrical System OFF ON OFF Before Engine Start © Peter Schmidleitner Compiled by Peter Schmidleitner DA40 TDI G1000 Electrical System ON OFF Preparing Engine Start ON © Peter Schmidleitner Compiled by Peter Schmidleitner DA40 TDI G1000 Electrical System ON OFF ON Engine Start START © Peter Schmidleitner Compiled by Peter Schmidleitner DA40 TDI G1000 Electrical System ON OFF ON ON After Engine Start © Peter Schmidleitner Compiled by Peter Schmidleitner External Power Receptable © Peter Schmidleitner Compiled by Peter Schmidleitner Emergency Switch © Peter Schmidleitner Compiled by Peter Schmidleitner The mysterious Essential Bus Switch DA40-TDI G1000 © Peter Schmidleitner Compiled by Peter Schmidleitner Switch location © Peter Schmidleitner Compiled by Peter Schmidleitner When is it used ? „ When the generator fails „ to disconnect unnecessary electrical consumers „ to supply battery power to essential electrical consumers © Peter Schmidleitner Compiled by Peter Schmidleitner Essential Electrial Power „ Essential Bus „ PFD „ Horizon *) „ AHRS „ ADC „ Flaps „ Landing light „ Pitot Heating „ Landing Light „ Flood Light *) *) Emergency Battery „ COM 1 „ GPS / NAV Receiver 1 „ Transponder „ Engine instruments „ Hot Battery Bus „ (Essential Bus) „ Pilot‘s map/reading light „ Auxiliary jack © Peter Schmidleitner Compiled by Peter Schmidleitner „ 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 Essential Electrial Power © Peter Schmidleitner Compiled by Peter Schmidleitner What happens ... „ ... if it is switched ON during normal operation? „ Will the battery be discharged? „ NO ! © Peter Schmidleitner Compiled by Peter Schmidleitner Normal Situation Hot Battery Bus Battery Bus Essential Bus GEN BATT Avioniic Bus ECU Bus Main Bus Battery is charged DA40-TDI G1000, Ess. Bus switch © Peter Schmidleitner Compiled by Peter Schmidleitner GEN u/s, Ess. PWR OFF Hot Battery Bus Battery Bus Essential Bus GEN BATT Avioniic Bus ECU Bus Main Bus Battery will be discharged DA40-TDI G1000, Ess. Bus switch © Peter Schmidleitner Compiled by Peter Schmidleitner GEN u/s, Ess. PWR ON Hot Battery Bus Battery Bus Essential Bus GEN BATT Avioniic Bus ECU Bus Main Bus Battery will be discharged at slow rate DA40-TDI G1000, Ess. Bus switch © Peter Schmidleitner Compiled by Peter Schmidleitner GEN OK, Ess. PWR ON Hot Battery Bus Battery Bus Essential Bus GEN BATT Avioniic Bus ECU Bus Main Bus Battery is still charged DA40-TDI G1000, Ess. Bus switch © Peter Schmidleitner Compiled by Peter Schmidleitner Hot Battery Bus Battery Bus Essential Bus GEN BATT Avioniic Bus ECU Bus Main Bus DA40-TDI G1000, Ess. Bus switch Essential Bus ON by mistake COM2, NAV/GPS2, Audio, ADF, DME, Autopilot WX 500 Fuel x-fer pump MFD Avion./CDU fan FAN / OAT indication Position light Strobe lights Taxi light, Map light Instrument lights Starter © Peter Schmidleitner Compiled by Peter Schmidleitner „ A very special engine start problem: „ Start witch ON „ Nothing happens! „ Why? „ Essential Bus switch ON by mistake! DA40-TDI G1000, Ess. Bus switch © Peter Schmidleitner Compiled by Peter Schmidleitner DA40 TDI G1000 Electrical System Generator + Battery Fail ON ECU backup battery © Peter Schmidleitner Compiled by Peter Schmidleitner Intentionally blank Diamond DA40-TDI G1000 Compiled by Peter Schmidleitner Autopilot KAP140 © Peter Schmidleitner Compiled by Peter Schmidleitner „ KAP 140 has 2 functions: „ if not engaged: Altitude warning „ if engaged („ON“): Autopilot Autopilot © Peter Schmidleitner Compiled by Peter Schmidleitner Autopilot Heading YES Stearing signal YES © Peter Schmidleitner Compiled by Peter Schmidleitner Autopilot Altitude NO Baro setting NO © Peter Schmidleitner Compiled by Peter Schmidleitner Autopilot limitations © Peter Schmidleitner Compiled by Peter Schmidleitner Autopilot AP disconnect CWS Manual Electric Trim © Peter Schmidleitner Compiled by Peter Schmidleitner Autopilot Roll Wrng AP ON/OFF HDG select NAV mode APR mode Backbeam ALT Hold +/- V/S or +/- Alt Set Altitude or Baro Baro display/ setting ALT ARM Pitch Wrng © Peter Schmidleitner Compiled by Peter Schmidleitner Autopilot ALT V/S BARO display ALT Alert Pitch trim annunciator AP engaged annunciator © Peter Schmidleitner Compiled by Peter Schmidleitner Autopilot Pitch Mode: VS ALT ARM ALT GS Roll Mode: ROL HDG NAV ARM NAV APR ARM APR REV ARM REV GS ARM © Peter Schmidleitner Compiled by Peter Schmidleitner ALT Autopilot Altitude Preselect Select Altitude Check ALT ARM Adjust V/S Check ALT ALERT Check ALT Hold © Peter Schmidleitner Compiled by Peter Schmidleitner 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! © Peter Schmidleitner Compiled by Peter Schmidleitner Autopilot Altitude Hold Mode Toggles between ALT HLD and V/S Vertical Speed Mode Toggles between ALT HLD and V/S Diamond DA40-TDI G1000 Compiled by Peter Schmidleitner Performance © Peter Schmidleitner Compiled by Peter Schmidleitner The „DA 40 TDI“ and „Density Altitude“ „ Attention! „ Performance data which are engine- power 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 © Peter Schmidleitner Compiled by Peter Schmidleitner Cruise Power Setting © Peter Schmidleitner Compiled by Peter Schmidleitner Cruising Speed e.g. 6000 ft, ISA, 70 % 121 kts © Peter Schmidleitner Compiled by Peter Schmidleitner TOD SL, ISA, 1150 kg: 640 m © Peter Schmidleitner Compiled by Peter Schmidleitner TKOF Distance © Peter Schmidleitner Compiled by Peter Schmidleitner TKOF Run © Peter Schmidleitner Compiled by Peter Schmidleitner Grass Runway min + 25% >10 cm + 15% 5 - 10 cm may be significantly longer + 10% - 5 cm Wet grass TKOF roll Length of grass © Peter Schmidleitner Compiled by Peter Schmidleitner Take off climb 66 KIAS Attention! Increasing downward © Peter Schmidleitner Compiled by Peter Schmidleitner Cruise Climb 73 KIAS © Peter Schmidleitner Compiled by Peter Schmidleitner ROC to gradient conversion © Peter Schmidleitner Compiled by Peter Schmidleitner LD, LR tabular format Flaps LDG V REF 71 KIAS Flaps UP V REF 73 KIAS © Peter Schmidleitner Compiled by Peter Schmidleitner Landing Distance © Peter Schmidleitner Compiled by Peter Schmidleitner Landing Run © Peter Schmidleitner Compiled by Peter Schmidleitner Grass Runway min + 25% >10 cm + 15% 5 - 10 cm may be significantly longer + 5% - 5 cm Wet grass LDG run Length of grass © Peter Schmidleitner Compiled by Peter Schmidleitner Go Around © Peter Schmidleitner Compiled by Peter Schmidleitner Obstacles ? RWL TOD Obst. Dist. „d“ „h“ „d“= (RWL + Obst.Dist.) - TOD Gradient = („h“ / „d“) * 100 © Peter Schmidleitner Compiled by Peter Schmidleitner Vöslau RWY 31 950 650 830 m 1130 98 ft „d“= (950 + 830) – 650 = 1130 Gradient = (30 / 1130) * 100 = 2,65 % Acc. Performance Graph: ~ 9 % Diamond DA40-TDI G1000 Compiled by Peter Schmidleitner Mass and Balance © Peter Schmidleitner Compiled by Peter Schmidleitner Empty Mass „ Empty Mass includes: „ Equipment as per Equipment Inventory „ Brake fluid „ Coolant fluid „ Gear oil „ Engine oil „ Unusable fuel (2 x 1,0 USG) © Peter Schmidleitner Compiled by Peter Schmidleitner Center of Gravity Envelope 2.46 2.59 © Peter Schmidleitner Compiled by Peter Schmidleitner Moment Envelope © Peter Schmidleitner Compiled by Peter Schmidleitner Moment Arms 4.54 Aft baggage 3.89 Fwd. baggage 2.63 Wing tanks 3.25 Rear seats 2.30 Front seats Lever Arm (m) Item © Peter Schmidleitner Compiled by Peter Schmidleitner Typical M+B data 2,460 2032,3 826,2 „N-VFR“-version 2,469 2057,7 833,5 „IFR“-version (ADF, WX500) CG arm Moment Empty mass © Peter Schmidleitner Compiled by Peter Schmidleitner M&B Calculation 2.63 3.89 3.25 2.30 2.47 Lever arm Total TKOF Mass Fuel Zero Fuel Mass Fwd. Baggage Rear seats Front seats 2050.1 830 Empty mass Moment (kgm) Mass (kg) 80 170 10 1090 60 1150 391.0 260.0 38.9 2740.0 157.8 2897.8 170 x 2.30 = 391.0 80 x 3.25 = 260.0 ~20 USG © Peter Schmidleitner Compiled by Peter Schmidleitner M&B Calculation 2.63 3.89 3.25 2.30 2.47 Lever arm Total TKOF Mass Fuel Zero Fuel Mass Fwd. Baggage Rear seats Front seats 2050.1 830 Empty mass Moment (kgm) Mass (kg) 80 170 10 1090 60 1150 391.0 260.0 38.9 2740.0 157.8 2897.8 2740.0 : 1090 = 2.514 2897.8 : 1150 = 2.52 2.514 2.52 © Peter Schmidleitner Compiled by Peter Schmidleitner ZFM 1090 kg , 2.514 m TOM 1150 kg , 2.52 m Center of Gravity Envelope © Peter Schmidleitner Compiled by Peter Schmidleitner M&B Calculation 2.63 3.89 3.25 2.30 2.47 Lever arm Total TKOF Mass Fuel Zero Fuel Mass Fwd. Baggage Rear seats Front seats 2050.1 830 Empty mass Moment (kgm) Mass (kg) 80 170 10 1090 60 1150 391.0 260.0 38.9 2740.0 157.8 2897.8 © Peter Schmidleitner Compiled by Peter Schmidleitner Moment Envelope ZFM 1090 kg , 2740.0 TOM 1150 kg , 2897.8 © Peter Schmidleitner Compiled by Peter Schmidleitner Intentionally blank Diamond DA40-TDI G1000 Compiled by Peter Schmidleitner Emergency Equipment © Peter Schmidleitner Compiled by Peter Schmidleitner Emergency equipment © Peter Schmidleitner Compiled by Peter Schmidleitner Emergency Exit FWD 1 2 © Peter Schmidleitner Compiled by Peter Schmidleitner Emergency Exit FWD 1 2 Diamond DA40-TDI G1000 Compiled by Peter Schmidleitner Kinds of Operation Equipment List (KOEL) © Peter Schmidleitner Compiled by Peter Schmidleitner Kinds of Operation Equipment List KOEL © Peter Schmidleitner Compiled by Peter Schmidleitner Kinds of Operation Equipment List KOEL © Peter Schmidleitner Compiled by Peter Schmidleitner Kinds of Operation Equipment List KOEL © Peter Schmidleitner Compiled by Peter Schmidleitner Kinds of Operation Equipment List KOEL © Peter Schmidleitner Compiled by Peter Schmidleitner Additional minimum equipment for the intended operation may be required by national operating rules and also depends on the route to be flown. Kinds of Operation Equipment List KOEL Diamond DA40-TDI G1000 Compiled by Peter Schmidleitner Servicing © Peter Schmidleitner Compiled by Peter Schmidleitner Scheduled maintenance „ Every „ 100 hours „ 200 hours „ 1000 hours „ 2000 hours „ Annually © Peter Schmidleitner Compiled by Peter Schmidleitner Refuelling © Peter Schmidleitner Compiled by Peter Schmidleitner De-icing „ Approved de-icing fluids: „ Kilfrost TKS 80 „ Aeroshell Compound 07 „ Procedure: „ Remove snow with brush „ Spray de-icing fluid „ Wipe dry © Peter Schmidleitner Compiled by Peter Schmidleitner Control surfaces gust lock © Peter Schmidleitner Compiled by Peter Schmidleitner Mooring © Peter Schmidleitner Compiled by Peter Schmidleitner Mooring © Peter Schmidleitner Compiled by Peter Schmidleitner Tow bar Diamond DA40-TDI G1000 Compiled by Peter Schmidleitner Flight Procedures © Peter Schmidleitner Compiled by Peter Schmidleitner TKOF Profile Rotate at 59 kt © Peter Schmidleitner Compiled by Peter Schmidleitner LDG Profile © Peter Schmidleitner Compiled by Peter Schmidleitner Checklists The checklists are not part of the AFM, and they are not „officially Diamond-endorsed“. They are a recommendation for „Operator Checklists“ published by „Diamond Aircraft Flight Training Division“. © Peter Schmidleitner Compiled by Peter Schmidleitner Thank you for your attention!