Diamond DA40 NG Manual Download

Page: 98 / 156

Compiled by Peter Schmidleitner

DA40 NG

191

When is it used ?

When the alternator fails

to disconnect unnecessary

electrical consumers

to supply battery power to

essential electrical consumers

Compiled by Peter Schmidleitner

DA40 NG

192

Main unserviceable systems

Starter control

MFD

Fuel x-fer pump

Avionic-, CDU-cooling fans

Instrument lights

Taxi + map lights

Position lights

Strobe lights

Avionics Bus

COM2, NAV/GPS2, Audio, Autopilot, DME, ADF,
WX500, TAS

Essential Electrial Power

Summary of Contents for DA40 NG

Page 1: ...DA40 NG Version 5 2 Handout DA40 NG Systems ...

Page 2: ...INTENTIONALLY BLANK ...

Page 3: ...1 Diamond DA40 NG Compiled by Peter Schmidleitner 1 Dimensions Compiled by Peter Schmidleitner DA40 NG 2 Dimensions 11 63 m ...

Page 4: ...2 Compiled by Peter Schmidleitner DA40 NG 3 Dimensions 8 01 m 1 97 m 1 68 m 1 85 with increased MLW Compiled by Peter Schmidleitner DA40 NG 4 Dimensions 2 97 m 1 90 m ...

Page 5: ...3 Diamond DA40 NG Compiled by Peter Schmidleitner 5 Exterior Compiled by Peter Schmidleitner DA40 NG Antenna locations ...

Page 6: ...4 Compiled by Peter Schmidleitner DA40 NG ELT and VHF COM 1 Antenna ELT antenna in fuselage structure VHF COM 1 Compiled by Peter Schmidleitner DA40 NG VHF COM 2 antenna ...

Page 7: ...5 Compiled by Peter Schmidleitner DA40 NG 9 VHF NAV GP Antennas in the horizontal stabilizer Compiled by Peter Schmidleitner DA40 NG 10 Marker Antenna Fuselage belly ...

Page 8: ...6 Compiled by Peter Schmidleitner DA40 NG 11 GPS antennas 11 Cabin roof Compiled by Peter Schmidleitner DA40 NG 12 DME TXPDR TAS Antenna DME Transponder TAS ...

Page 9: ...7 Compiled by Peter Schmidleitner DA40 NG 13 ADF antenna ADF Compiled by Peter Schmidleitner DA40 NG 14 Pitot Probe Left wing ...

Page 10: ...8 Compiled by Peter Schmidleitner DA40 NG 15 Static Ports Both sides of fuselage Compiled by Peter Schmidleitner DA40 NG 16 Lift Detector Stall Warning Left wing ...

Page 11: ...9 Compiled by Peter Schmidleitner DA40 NG 17 Landing Taxi Light Left wing Compiled by Peter Schmidleitner DA40 NG 18 Engine Oil and Gear Oil ...

Page 12: ...10 Compiled by Peter Schmidleitner DA40 NG 19 Engine Oil and Gear Oil Compiled by Peter Schmidleitner DA40 NG 20 Engine Oil and Gear Oil ...

Page 13: ...11 Compiled by Peter Schmidleitner DA40 NG 21 Engine Oil Compiled by Peter Schmidleitner DA40 NG 22 Gear Oil ...

Page 14: ...A40 NG 23 Air Inlets Intercooler Coolant heat exchanger Cabin air heater and Reduction Gear cooling Compiled by Peter Schmidleitner DA40 NG 24 Air Inlets Cabin air heater and Reduction Gear cooling Cabin air heater Reduction Gear cooling ...

Page 15: ...tner DA40 NG 25 Coolant Radiator Inlet Baffle Must be installed when OAT at take off is below 30 C but operation with baffle only up to 0 C Compiled by Peter Schmidleitner DA40 NG 26 RH frontVentilation Engine air intake Air Inlets ...

Page 16: ...A40 NG 27 LH front Ventilation Air Inlets Compiled by Peter Schmidleitner DA40 NG 28 Air Inlets Rear Ventilation May be closed in cold weather with Ventilation inlet baffle With ventilation inlet baffle installed max OAT for Take off 15 C ...

Page 17: ...engine until oil temp above 20 C between 15 C and 10 C recommended and cockpit Below 30 C Batteries must be pre heated Below 40 C Operation prohibited Outside Air Temperature at TKOF Below 30 C Coolant radiator inlet baffle must be installed Above 0 C Coolant radiator inlet baffle must be removed Above 15 C Ventilation inlet baffle must be removed Above 20 C Fuel cooler inlet baffle must be remove...

Page 18: ...aximum operating altitude 16 400 ft 5 000 m Pressure Altitude Compiled by Peter Schmidleitner DA40 NG 32 Other Limitations Aerobatics spinning more than 60 bank are prohibited Canopy and passenger door must be unlocked during operation Max demonstrated crosswind 25 kts ...

Page 19: ...R or IFR with an empty main batttery No engine start with external power because of an empty main battery if IFR or Night VFR flight is planned Battery must be charged first No IFR flight if seal on the Emergency Switch is broken Compiled by Peter Schmidleitner DA40 NG Intentionally blank ...

Page 20: ...d by Peter Schmidleitner 35 Mass Compiled by Peter Schmidleitner DA40 NG 36 Mass Option 574 Option 662 Empty typical 900 kg Max TKOF 1280 kg 1310 kg Max Ramp 4 kg Max LDG 1216 kg 1280 kg Max ZFW 1200 kg 1265 kg Min flight 940 kg ...

Page 21: ...280 kg is an Abnormal Operating Procedure Same as the Normal Procedure observing higher speed 77 KIAS Compiled by Peter Schmidleitner DA40 NG 38 Max Baggage Load Standard Options Baggage Extension Short Baggage Extension Standard compartment 30 kg 45 kg 30 kg Max in tube if installed 5 kg Baggage Extension 18 kg 15 kg Total 35 kg 45 kg 45 kg ...

Page 22: ...20 Compiled by Peter Schmidleitner DA40 NG 39 Mass Option Baggage Tray Extended Compartment BAGGAGE TRAY Compiled by Peter Schmidleitner DA40 NG 40 Short Baggage Extension BAGGAGE TRAY ...

Page 23: ...Schmidleitner DA40 NG 41 Mass Attention JET fuel and Diesel are heavier than AVGAS Typical fuel weight JET A1 0 8 kg ltr 3 03 kg USG Diesel 0 84 kg ltr 3 2 kg USG Compiled by Peter Schmidleitner DA40 NG Intentionally blank ...

Page 24: ... DA40 NG Compiled by Peter Schmidleitner 43 Speeds Compiled by Peter Schmidleitner DA40 NG 44 Characteristic Speeds VNO 130 KIAS VNE 172 KIAS VO 1180 kg 101 KIAS VO 1081 1180 kg 108 KIAS VO 1181 1280 kg 113 KIAS ...

Page 25: ...66 KIAS VFE Flaps T O 110 KIAS VFE Flaps LDG 98 KIAS Compiled by Peter Schmidleitner DA40 NG 46 Characteristic Speeds KIAS at 940 kg 1000 kg 1100 kg 1200 kg 1280 kg above VR Flaps T O 56 58 61 65 67 V50 up to 50 ft Flaps T O 62 65 67 70 72 VY up to safe altitude Flaps T O 72 V cruise climb Flaps UP 88 ...

Page 26: ...f Approach Flaps LDG 66 68 72 76 76 77 Vref Approach Flaps T O 68 70 74 77 77 78 Vref Approach Flaps UP 71 73 78 82 82 83 Minimum V Go Around Flaps T O 72 Compiled by Peter Schmidleitner DA40 NG 48 Characteristic Speeds Best gliding Flaps UP prop windmilling 88 KIAS 1 9 7 1 59 NM 1000 ft Without wheel fairings 1 9 4 1 54 NM 1000 ft ...

Page 27: ...25 Compiled by Peter Schmidleitner DA40 NG 49 Stalling Speeds 1000 kg 1310 kg VS1 VSO 55 58 60 66 Compiled by Peter Schmidleitner DA40 NG 50 Stalling Speeds VS1 VSO 56 59 63 68 1000 kg 1310 kg ...

Page 28: ...26 Compiled by Peter Schmidleitner DA40 NG 51 Stalling Speeds VS1 VSO 61 64 69 74 1000 kg 1310 kg Compiled by Peter Schmidleitner DA40 NG 52 Stalling Speeds VS1 VSO 72 76 82 88 1000 kg 1310 kg ...

Page 29: ...27 Diamond DA40 NG Compiled by Peter Schmidleitner 53 Flight Controls Compiled by Peter Schmidleitner DA40 NG 54 Flight Control Operation Rudder cables Ailerons Elevator push rods ...

Page 30: ... Compiled by Peter Schmidleitner DA40 NG 55 Flight Control Operation Flaps electrically by push rods left and right mechanically interconnected Compiled by Peter Schmidleitner DA40 NG Intentionally blank ...

Page 31: ...29 Diamond DA40 NG Compiled by Peter Schmidleitner 57 Instrument Panel Compiled by Peter Schmidleitner DA40 NG 58 Instrument Panel Garmin 1000 ...

Page 32: ...nel Backup Instruments Horizon Altimeter Airspeed Compass Compiled by Peter Schmidleitner DA40 NG 60 Instrument Panel Emergency Battery non rechargeable Flood Lights Emergency Switch IFR flights are not permitted when the seal on the emergency switch is broken ...

Page 33: ...31 Compiled by Peter Schmidleitner DA40 NG 61 Instrument Panel ELT Lights Compiled by Peter Schmidleitner DA40 NG 62 Instrument Panel Circuit breakers ...

Page 34: ...32 Compiled by Peter Schmidleitner DA40 NG 63 Instrument Panel Essential Bus Electric Master Starter Compiled by Peter Schmidleitner DA40 NG 64 Instrument Panel Engine control ...

Page 35: ...33 Compiled by Peter Schmidleitner DA40 NG 65 Instrument Panel Avionic Master Fuel x fer pump Pitot heat Compiled by Peter Schmidleitner DA40 NG 66 Instrument Panel Flaps ...

Page 36: ...34 Compiled by Peter Schmidleitner DA40 NG 67 Alternate Static Valve Compiled by Peter Schmidleitner DA40 NG 68 Alternate Static Valve ...

Page 37: ... Schmidleitner 69 Garmin 1000 EIS Engine Instrument System Compiled by Peter Schmidleitner DA40 NG 70 Garmin 1000 For a detailed description of the G1000 integrated instrument system consult the instruction modules DA42 G1000 parts 1 to 3 ...

Page 38: ...d by Peter Schmidleitner DA40 NG 71 Garmin 1000 MFD Audio Panel PFD Primary Flight Display Multi Function Display Compiled by Peter Schmidleitner DA40 NG 72 MFD EIS Engine Indication System Multi Function Display ...

Page 39: ...ay when pushing the SYSTEM softkey Display when pushing the FUEL softkey Upper part always the same LOAD is not measured but calculated from common rail fuel pressure ECU commanded injection time manifold pressure and Prop RPM Fuel Flow is not measured but calculated from fuel pressure and ECU commanded injection time Readouts and labels and pointers appear white to indicate normal operation yello...

Page 40: ...38 Compiled by Peter Schmidleitner DA40 NG 75 Engine Indication System Default SYSTEM FUEL Compiled by Peter Schmidleitner DA40 NG Engine Indication System with G1000 NXi ...

Page 41: ...39 Diamond DA40 NG Compiled by Peter Schmidleitner 77 Brake System Compiled by Peter Schmidleitner DA40 NG 78 Hydraulic brakes Pilot applies brake ...

Page 42: ...by Peter Schmidleitner DA40 NG 79 Hydraulic brakes Copilot applies brake Compiled by Peter Schmidleitner DA40 NG 80 Hydraulic brakes One way valve is closed Parking brake Pressure is trapped Apply brake pressure 80 ...

Page 43: ...41 Compiled by Peter Schmidleitner DA40 NG 81 Parking brake Compiled by Peter Schmidleitner DA40 NG Intentionally blank ...

Page 44: ...Austro Engine E4 A Four cylinders liquid cooled 1991 ccm Common rail direct injection Reduction gear 1 1 69 Dual digital engine control Turbocharger Torsion vibration damper isolates engine from propeller Max power 100 5 minutes time limit 123 5 kW 165 6 DIN HP at 2300 RPM Max cont power 92 113 6 kW 152 3 DIN HP at 2100 RPM ...

Page 45: ...ed by Peter Schmidleitner DA40 NG 85 Austro Engine E4 A Compiled by Peter Schmidleitner DA40 NG 86 Austro Engine E4 A Fuel High Pressure Pump Turbo Charger Oil Sump Alternator Gearbox Propeller Shaft Front View ...

Page 46: ...Oil Filter Housing Alternator Starter Oil Filler Cap Heat Exchanger Top View Propeller Shaft Compiled by Peter Schmidleitner DA40 NG 88 Austro Engine E4 A High Pressure Pump Starter Side glass of Gearbox Oil Level Alternator Water Pump Heat Exchanger Rip Belt Turbo Charger Engine Oil Level and Refill Cap Left Hand View Engine Oil Filter Housing Propeller Shaft ...

Page 47: ...itner DA40 NG 89 Austro Engine E4 A Gearbox Oiltank Alternator Intercooler Coolant reservoir Compiled by Peter Schmidleitner DA40 NG 90 Austro Engine E4 A Cabin heat exchanger Turbocharger Engine air filter and alternate air valve ...

Page 48: ...Compiled by Peter Schmidleitner DA40 NG 91 Alternate air lever Alternate air valve Alternate air Compiled by Peter Schmidleitner DA40 NG 92 Alternate air Alternate air lever pulled Alternate air valve open ...

Page 49: ...47 Compiled by Peter Schmidleitner DA40 NG 93 Use of Alternate Air Compiled by Peter Schmidleitner DA40 NG 94 Austro Engine E4 A Prop governor ...

Page 50: ...48 Compiled by Peter Schmidleitner DA40 NG 95 ECU Engine Control Unit Compiled by Peter Schmidleitner DA40 NG 96 E O T Engine Order Telegraph ...

Page 51: ...97 Engine Control Unit ECU VOTER switch Normally in AUTO position Working ECU is automatically selected according operating hours or in case of malfunction Compiled by Peter Schmidleitner DA40 NG 98 ECU test button Test on ground PWR lever idle ...

Page 52: ...ance of air fuel or electrical supply system e g air filter icing Depending on the type of failure the ECU failure cautions are either non latched i e the caution message disappears after the cause of the caution is no longer present or latched i e the caution massage remains until cleared through maintenance action and Austro Engine has to be informed Clearing of non latched caution on the active...

Page 53: ...51 Compiled by Peter Schmidleitner DA40 NG 101 ECU FAIL Caution Compiled by Peter Schmidleitner DA40 NG 102 ECU FAIL Caution ...

Page 54: ...ner DA40 NG 104 0 100 92 20 1600 1650 1700 1750 1800 1850 1900 1950 2000 2050 2100 2150 2200 2250 2300 2350 2400 0 10 20 30 40 50 60 70 80 90 100 Power Lever Propeller Speed rpm Power lever selects LOAD in RPM automatically determined by selected power Power plant Recommended Cruise Power Setting 75 ...

Page 55: ...ooden propeller Constant speed Prop pitch set by ECU via an electro mechanical actuator on the governor Governor operated by gearbox oil Oil pressure up pitch up RPM down Oil pressure down pitch down RPM up Compiled by Peter Schmidleitner DA40 NG 106 RPM malfunctions ...

Page 56: ...chmidleitner DA40 NG 107 RPM malfunctions Compiled by Peter Schmidleitner DA40 NG 108 Fuel pumps 1 engine driven pump this high pressure pump feeds the common rail additional electrical fuel pumps are part of the fuel system ...

Page 57: ...bar Normal 2 5 6 bar Oil quantity 5 0 7 0 liters Max oil consumption 0 1 liters hr Oil temperature 30 C 140 C Normal 50 C 125 C Compiled by Peter Schmidleitner DA40 NG Gearbox temperature Min 30 C Min at full load 35 C Max 120 C 110 Power plant limitations The yellow cautionary range is for information only There is no time limit associated with the cautionary temperature range ...

Page 58: ...ed by Peter Schmidleitner DA40 NG Max restart altitude 16 400ft PA for immediate restart 15 000ft PA for immediate restart with engine software V33_1_05_19 or later 10 000ft PA for restart within 2 minutes After more than 2 minutes cooldown a succesful restart may not be possible Restart airspeed The propeller will be windmilling Airspeed 88 KIAS If propeller has stopped mechanical engine defect D...

Page 59: ...er Schmidleitner DA40 NG 113 Power plant limitations Intentional negative g manoeuvers are not permitted Compiled by Peter Schmidleitner DA40 NG 114 Starter limitations Operation max 10 seconds 60 seconds cool down time ...

Page 60: ...mum cetane number of 36 EN ISA 5165 ASTM D613 recommended For additives see AFM Diesel Fuel No additives permitted Compiled by Peter Schmidleitner DA40 NG 116 Engine oil e g SHELL Helix Ultra AEROSHELL Oil Diesel Ultra AUSTRO ENGINE Aero For more oil types see AFM Gearbox oil Shell Spirax GSX 75W 80 Shell Spirax S6 GXME 75W 80 Coolant Destilled water cooler protection BASF Glysantin Protect Plus G...

Page 61: ...59 Compiled by Peter Schmidleitner DA40 NG 117 Engine operation after line up Compiled by Peter Schmidleitner DA40 NG 118 Engine operation ...

Page 62: ...60 Compiled by Peter Schmidleitner DA40 NG 119 Power plant warnings Compiled by Peter Schmidleitner DA40 NG 120 Power plant abnormals ...

Page 63: ...61 Diamond DA40 NG Compiled by Peter Schmidleitner 121 Cooling System Compiled by Peter Schmidleitner DA40 NG 122 Cooling system ...

Page 64: ...62 Compiled by Peter Schmidleitner DA40 NG 123 Cooling system Coolant Temp 80 C Compiled by Peter Schmidleitner DA40 NG 124 Cooling system Coolant Temp 80 C ...

Page 65: ...63 Compiled by Peter Schmidleitner DA40 NG 125 Cooling system Compiled by Peter Schmidleitner DA40 NG 126 Cooling system ...

Page 66: ...64 Compiled by Peter Schmidleitner DA40 NG 127 Cabin heat Compiled by Peter Schmidleitner DA40 NG 128 Cabin heat Cabin Heat ...

Page 67: ...65 Compiled by Peter Schmidleitner DA40 NG 129 Ventilation Cockpit Front ventilation Compiled by Peter Schmidleitner DA40 NG 130 Ventilation Cabin Rear ventilation ...

Page 68: ...66 Diamond DA40 NG Compiled by Peter Schmidleitner 131 Turbocharger System Compiled by Peter Schmidleitner DA40 NG 132 Turbo Charger Exhaust gas drives turbine Bypass for excess exhaust gas ...

Page 69: ...67 Compiled by Peter Schmidleitner DA40 NG 133 Turbo Charger Turbine drives compressor Compressor compresses intake air Compiled by Peter Schmidleitner DA40 NG Intentionally blank ...

Page 70: ...nd DA40 NG Compiled by Peter Schmidleitner 135 Fuel System Compiled by Peter Schmidleitner DA40 NG 136 Standard Tanks Capacity 2 x 15 USG 2 x 14 USG usable 28 USG usable 85 kg At 75 power 6 5 USG hr Fuel System ...

Page 71: ...dleitner DA40 NG 137 Long Range Tanks Capacity 2 x 20 5 USG 2 x 19 5 USG usable 39 USG 120 kg Max indicated fuel per tank 14 USG Max unbalance 9 USG Fuel System Compiled by Peter Schmidleitner DA40 NG 138 Fuel System Fuel valve ...

Page 72: ...70 Compiled by Peter Schmidleitner DA40 NG 139 Fuel System Compiled by Peter Schmidleitner DA40 NG 140 Fuel System Up to 71 USG hr Average 45 USG hr 60 USG hr Fuel cooler ...

Page 73: ...idleitner DA40 NG Fuel System The transfer pump is switched OFF automatically when the auxiliary tank is empty the main tank is full 14 USG Compiled by Peter Schmidleitner DA40 NG 142 Fuel cooler Right wing Air inlet Air outlet ...

Page 74: ...eter Schmidleitner DA40 NG 143 Fuel System 45 USG hr Fuel cooler U S Transfer Compiled by Peter Schmidleitner DA40 NG 144 Fuel system Alternate means for fuel quantity indication Position at the bore in the stall strip ...

Page 75: ...und with wings level Therefore Fuel indicator II is available for pitch angle measurement Place it on top of fuselage in front of vertical tail Read pitch angle and use table to determine exact fuel quantity 145 Compiled by Peter Schmidleitner DA40 NG Fuel system Fuel Qantity Indicator II Qantity scale Level scale 146 ...

Page 76: ...74 Compiled by Peter Schmidleitner DA40 NG Fuel system 147 Compiled by Peter Schmidleitner DA40 NG Fuel system Conversion tables in the AFM 148 ...

Page 77: ...75 Compiled by Peter Schmidleitner DA40 NG 149 Fuel vents Compiled by Peter Schmidleitner DA40 NG 150 Fuel tank drain FWD ...

Page 78: ...76 Compiled by Peter Schmidleitner DA40 NG 151 Fuel gascolator drain FWD Compiled by Peter Schmidleitner DA40 NG 152 Fuel gascolator drain ...

Page 79: ...ECU B pump B normal Ops only one pump working when ECU switches over fuel pumps switch over as well When pump fails low fuel pressure automatic switch over to other pump by switching to the other ECU For TKOF LDG and with fuel pressure failure both pumps switched ON manually with FUEL PUMP switch 153 Compiled by Peter Schmidleitner DA40 NG 154 Fuel pumps ...

Page 80: ...78 Compiled by Peter Schmidleitner DA40 NG 155 Fuel pumps Compiled by Peter Schmidleitner DA40 NG 156 Fuel pressure warning Warning annunciation FUEL PRESS ...

Page 81: ...79 Compiled by Peter Schmidleitner DA40 NG 157 Fuel pressure warning Compiled by Peter Schmidleitner DA40 NG Intentionally blank ...

Page 82: ...80 Diamond DA40 NG Compiled by Peter Schmidleitner 159 Diesel Operation Compiled by Peter Schmidleitner DA40 NG 160 DA40NG Diesel Operation ...

Page 83: ...ner DA40 NG 161 DA40NG Diesel Operation Fuel Temperature Diesel Operation Minimum 30 C Maximum 60 C Modified G1000 Software Compiled by Peter Schmidleitner DA40 NG 162 DA40NG Diesel Operation Operational Limitations Fuel Temperature ...

Page 84: ... zones other classes Winter Diesel Class F Compiled by Peter Schmidleitner DA40 NG 164 DA40NG Diesel Operation If JET Fuel is used make sure that no Diesel Fuel is remaining in the tanks neither in the left nor in the right tank Otherwise the temperature limitations for Diesel Fuel operation must be observed The fuel filter is not heated ...

Page 85: ...tank must be refilled at least twice with more than 17 2 US gal 65 l of JET Fuel Otherwise both tanks must be drained before refueling with JET Fuel NOTE In order to provide information about the fuel grade it is recommended to enter the fuel grade in the airplane log each time fuel is refilled Compiled by Peter Schmidleitner DA40 NG 166 DA40NG Diesel Operation TKOF Ground Roll Add 6 TKOF Distance...

Page 86: ...iamond DA40 NG Compiled by Peter Schmidleitner 167 Electrical System Compiled by Peter Schmidleitner DA40 NG 168 Electrical system 168 General information 2 types of amperemeter can be installed in aircraft ...

Page 87: ...85 Compiled by Peter Schmidleitner DA40 NG 169 Electrical system 169 Observe The Amperemeter on the G1000 is a Compiled by Peter Schmidleitner DA40 NG 170 Electrical system ...

Page 88: ...Alternator 28V 70A Main Battery 24V 13 6Ah ECU Backup Battery 2x14V 7 2Ah Electrical system Compiled by Peter Schmidleitner DA40 NG 172 Power distribution Hot Battery Bus Battery Bus 1 Main Bus Essential Bus ENG ECU Bus Avionic Bus Battery Bus 2 Electrical system ...

Page 89: ...V 7 2 Ah Avionic Bus Hot Battery Bus Battery Bus 1 Battery power supply Electrical system Compiled by Peter Schmidleitner DA40 NG 174 Battery Bus 2 Main Bus Essential Bus Main Battery 24V 13 6Ah Alternator Starter ECU A B ECU Bus ECU backup battery 24V 7 2 Ah Avionic Bus Hot Battery Bus Battery Bus 1 Electrical system External power supply ELECTRIC MASTER OFF EPU ...

Page 90: ...ry 24V 7 2 Ah Avionic Bus Hot Battery Bus Battery Bus 1 Electrical system External power supply ELECTRIC MASTER ON EPU Compiled by Peter Schmidleitner DA40 NG 176 Battery Bus 2 Main Bus Essential Bus Main Battery 24V 13 6Ah Alternator ECU A B ECU Bus ECU backup battery 24V 7 2 Ah Avionic Bus Hot Battery Bus Battery Bus 1 Normal power supply Electrical system ...

Page 91: ...4V 7 2 Ah Avionic Bus Hot Battery Bus Battery Bus 1 Electrical system Essential power supply Alternator Compiled by Peter Schmidleitner DA40 NG 178 Battery Bus 2 Main Bus Essential Bus ECU A B ECU Bus ECU backup battery 24V 7 2 Ah Avionic Bus Hot Battery Bus Battery Bus 1 Electrical system Alternator Total electric fail Main Battery 24V 13 6Ah ...

Page 92: ...Hot battery bus Accessory power plug ELT Compiled by Peter Schmidleitner DA40 NG 180 Battery bus 1 and 2 Battery Bus 1 starter heavy duty power Battery Bus 2 ECU BUS Main Bus Electric Master ON ESS BUS OFF Essential Bus Electric Master ON ESS BUS ON ...

Page 93: ...ontrol MFD Fuel x fer pump Avionic CDU cooling fans Instrument lights Taxi map lights Position lights Strobe lights Compiled by Peter Schmidleitner DA40 NG 182 Essential bus PFD Horizon Air Data Computer AHRS COM 1 GPS NAV 1 Flood light Landing light Transponder Pitot heat Flap system Engine instruments ...

Page 94: ...2 Compiled by Peter Schmidleitner DA40 NG 183 Avionic bus COM 2 GPS NAV 2 Audio panel Autopilot DME ADF WX 500 TAS Compiled by Peter Schmidleitner DA40 NG 184 Essential Bus Avionic Master Electric Master ...

Page 95: ...93 Compiled by Peter Schmidleitner DA40 NG 185 Engine Master Compiled by Peter Schmidleitner DA40 NG 186 External Power Receptable ...

Page 96: ...94 Compiled by Peter Schmidleitner DA40 NG 187 External Power Receptable Compiled by Peter Schmidleitner DA40 NG 188 External Power Receptable 28 V ...

Page 97: ...95 Compiled by Peter Schmidleitner DA40 NG 189 The mysterious Essential Bus Switch Essential bus switch Compiled by Peter Schmidleitner DA40 NG 190 Switch location ...

Page 98: ...o supply battery power to essential electrical consumers Compiled by Peter Schmidleitner DA40 NG 192 Main unserviceable systems Starter control MFD Fuel x fer pump Avionic CDU cooling fans Instrument lights Taxi map lights Position lights Strobe lights Avionics Bus COM2 NAV GPS2 Audio Autopilot DME ADF WX500 TAS Essential Electrial Power ...

Page 99: ...97 Compiled by Peter Schmidleitner DA40 NG 193 Autopilot GFC700 Diamond DA40 NG Compiled by Peter Schmidleitner DA40 NG 194 GFC 700 AFCS AFCS Automatic Flight Control System Flight Director Autopilot ...

Page 100: ...98 Compiled by Peter Schmidleitner DA40 NG 195 GFC 700 AFCS Compiled by Peter Schmidleitner DA40 NG 196 GFC 700 AFCS ...

Page 101: ...y Peter Schmidleitner DA40 NG 197 GFC 700 AFCS GFC 700 functions Flight Director FD AUTO Pilot AP Manual Electric Trim MET Compiled by Peter Schmidleitner DA40 NG 198 Autopilot AP disconnect CWS Manual Electric Trim ...

Page 102: ...99 Autopilot GA button Compiled by Peter Schmidleitner DA40 NG 200 GFC 700 AFCS Aircraft Attitude Symbol Flight Director Command Bars Image reproduced with the permission of Garmin Copyright 2006 Garmin Ltd or its subsidiaries All Rights Reserved ...

Page 103: ... its subsidiaries All Rights Reserved Second push deactivates the mode Vertical NAV GFC 700 AFCS Compiled by Peter Schmidleitner DA40 NG FLC Flight Level Change Mode FLC IAS hold A target altitude must be selected first FLC does not initiate the level change to the selected altitude Current altitude is maintained until either engine power or IAS reference are adjusted FLC does not allow the aircaf...

Page 104: ...ion Image reproduced with the permission of Garmin Copyright 2006 Garmin Ltd or its subsidiaries All Rights Reserved Compiled by Peter Schmidleitner DA40 NG 204 GFC 700 AFCS Image reproduced with the permission of Garmin Copyright 2006 Garmin Ltd or its subsidiaries All Rights Reserved ...

Page 105: ...min Copyright 2006 Garmin Ltd or its subsidiaries All Rights Reserved When FD or AP is engaged Compiled by Peter Schmidleitner DA40 NG 206 GFC 700 AFCS Flight Mode Annunciators AFCS Status Box Image reproduced with the permission of Garmin Copyright 2006 Garmin Ltd or its subsidiaries All Rights Reserved ...

Page 106: ...Copyright 2006 Garmin Ltd or its subsidiaries All Rights Reserved Compiled by Peter Schmidleitner DA40 NG 208 Armed modes white Active modes green GFC 700 AFCS Flight Mode Annunciators AFCS Status Box AP status Lateral mode Vertical mode Image reproduced with the permission of Garmin Copyright 2006 Garmin Ltd or its subsidiaries All Rights Reserved ...

Page 107: ...rol Wheel Steering Image reproduced with the permission of Garmin Copyright 2006 Garmin Ltd or its subsidiaries All Rights Reserved Compiled by Peter Schmidleitner DA40 NG 210 GFC 700 AFCS Flight Mode Annunciators AFCS Status Box Vertical mode Image reproduced with the permission of Garmin Copyright 2006 Garmin Ltd or its subsidiaries All Rights Reserved ...

Page 108: ...FC 700 AFCS Vertical modes Compiled by Peter Schmidleitner DA40 NG 70 to165 kt 212 GFC 700 AFCS Image reproduced with the permission of Garmin Copyright 2006 Garmin Ltd or its subsidiaries All Rights Reserved Vertical mode range and change increments ...

Page 109: ...s Box Roll mode Image reproduced with the permission of Garmin Copyright 2006 Garmin Ltd or its subsidiaries All Rights Reserved Compiled by Peter Schmidleitner DA40 NG 214 GFC 700 AFCS Image reproduced with the permission of Garmin Copyright 2006 Garmin Ltd or its subsidiaries All Rights Reserved ...

Page 110: ...0 AFCS GA mode active Wings level 7 pitch up Compiled by Peter Schmidleitner DA40 NG 216 GFC 700 AFCS Image reproduced with the permission of Garmin Copyright 2006 Garmin Ltd or its subsidiaries All Rights Reserved What the FD AP flies What the pilot wants ...

Page 111: ... with the permission of Garmin Copyright 2006 Garmin Ltd or its subsidiaries All Rights Reserved Compiled by Peter Schmidleitner DA40 NG 218 GFC 700 AFCS IAS Hold Mode Flight Level Change Selected Airspeed Airspeed Reference Bug Image reproduced with the permission of Garmin Copyright 2006 Garmin Ltd or its subsidiaries All Rights Reserved ...

Page 112: ...dleitner DA40 NG 219 GFC 700 AFCS flashing Overspeed Protection Image reproduced with the permission of Garmin Copyright 2006 Garmin Ltd or its subsidiaries All Rights Reserved Compiled by Peter Schmidleitner DA40 NG GFC 700 AFCS ...

Page 113: ...nual electric trim is available GIA No 1 The Autopilot disconnects and Autopilot Flight Director and manual electric trim are inoperative GIA No 2 The Autopilot disconnects and Autopilot and manual electric trim are inoperative Flight Director is available GPS No 1 and 2 The Autopilot and Flight Director operates in NAV modes only LOC BC VOR VAPP with reduced accuracy ADC The Autopilot disconnects...

Page 114: ... Schmidleitner DA40 NG 223 G 1000 System Loss Effect upon Autopilot Operation AP FD MET 9 Limited functionality 9 9 Compiled by Peter Schmidleitner DA40 NG 224 G 1000 System Loss Effect upon Autopilot Operation AP FD MET 9 ...

Page 115: ...ter Schmidleitner DA40 NG 225 G 1000 System Loss Effect upon Autopilot Operation AP FD MET HDG 9 9 9 Compiled by Peter Schmidleitner DA40 NG 226 G 1000 System Loss Effect upon Autopilot Operation AP FD MET 9 9 ALT VS FLC ...

Page 116: ...piled by Peter Schmidleitner DA40 NG 227 G 1000 System Loss Effect upon Autopilot Operation AP FD MET Compiled by Peter Schmidleitner DA40 NG 228 G 1000 System Loss Effect upon Autopilot Operation AP FD MET 9 ...

Page 117: ...mpiled by Peter Schmidleitner DA40 NG 229 G 1000 System Loss Effect upon Autopilot Operation AP FD MET 9 GPS 1 GPS 2 VHF NAV only reduced accuracy 9 Compiled by Peter Schmidleitner DA40 NG Intentionally blank ...

Page 118: ...116 Diamond DA40 NG Compiled by Peter Schmidleitner 231 Performance Compiled by Peter Schmidleitner DA40 NG 232 TKOF LDG Performance general ...

Page 119: ...ompiled by Peter Schmidleitner DA40 NG 234 Performance Tables Fuel Flow Stalling Speeds TKOF Ground Roll TKOF Distance Climb Performance Take off climb Cruise climb Time Fuel Distance to Climb Cruise Performance LDG Ground Roll LDG Distance Flaps LDG Abnormal Flap Position Go Around Climb Performance 234 ...

Page 120: ...118 Compiled by Peter Schmidleitner DA40 NG 235 Peter Schmidleitner Fuel Flow 6 6 USG hr Compiled by Peter Schmidleitner DA40 NG 236 Stalling Speeds ...

Page 121: ... for each 12 kt Tailwind TKOF distance plus 10 for each 2 kt Uphill slope Ground roll plus 15 for each 1 of slope Without wheel fairings Ground roll plus 20 m TKOF distance plus 30 m Compiled by Peter Schmidleitner DA40 NG 238 TKOF on Grass RWY Length of grass TKOF roll Wet grass 5 cm 10 additional 20 5 10 cm 30 10 25 cm 45 25 cm TKOF should not be attempted 50 on soft ground 238 ...

Page 122: ...chmidleitner Climb performance Available tables Take Off Climb Flaps T O 1310 kg 1280 kg 1200 kg 1100 kg Compiled by Peter Schmidleitner DA40 NG 240 Peter Schmidleitner Climb performance Available tables Cruise Climb Flaps UP 1310 kg 1280 kg 1200 kg 1100 kg ...

Page 123: ...e of climb Conversion to gradient with TAS still air gradient For operation without wheel fairings a climb rate decreased by 40 ft min must be expected 241 Compiled by Peter Schmidleitner DA40 NG 242 Peter Schmidleitner Time Fuel Dist to climb Available tables Flaps UP 1310 kg 1280 kg 1200 kg 1100 kg ...

Page 124: ...d fuel 10 to distance for each 10 increase of OAT Method of calculation 1 get values for airfield altitude 2 get values for for cruise altitude Result subtract 1 from 2 243 Time Fuel Dist to climb Compiled by Peter Schmidleitner DA40 NG 244 Peter Schmidleitner True Air Speed Up to 16000 ft Only one table for 1310kg ...

Page 125: ...aps T O or UP 1310 kg 1280 kg 1200 kg 1100 kg Headwind LDG distance minus 10 for each 20 kt Tailwind LDG distance plus 10 for each 3 kt Downhill slope Ground roll plus 10 for each 1 of slope Compiled by Peter Schmidleitner DA40 NG 246 LDG on wet or Grass RWY LDG roll Paved RWY WET 15 Length of grass Wet grass or soft ground 5 cm 30 additional 15 5 cm min 45 246 ...

Page 126: ...0 NG 247 Go around Available tables Flaps LDG 1310 kg 1280 kg 1200 kg 1100 kg Compiled by Peter Schmidleitner DA40 NG 248 Glide Best gliding Flaps UP prop windmilling 88 KIAS 1 9 7 1 59 NM 1000 ft Without wheel fairings 1 9 4 1 54 NM 1000 ft ...

Page 127: ...Obst Dist d h d RWL Obst Dist TOD Gradient h d 100 ROC Gradient x TAS 0 98 50 ft 50 ft assumed Effective Obst Dist Compiled by Peter Schmidleitner DA40 NG 250 Vöslau RWY 31 950 600 830 m 1180 98 ft d 950 830 600 1180 Gradient 30 1180 100 2 54 200 fpm At 1280 kg 380 fpm d ...

Page 128: ...d by Peter Schmidleitner 251 Mass and Balance Compiled by Peter Schmidleitner DA40 NG 252 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 ...

Page 129: ...f Gravity Envelope 2 46 2 53 2 469 Compiled by Peter Schmidleitner DA40 NG 254 Moment Arms Item Lever Arm m Front seats 2 30 Rear seats 3 25 Wing tanks 2 63 Standard baggage 3 65 Baggage tube 4 32 Short bagge extension 3 97 Extended baggage FWD 3 89 AFT 4 54 ...

Page 130: ... Peter Schmidleitner DA40 NG 255 Baggage Compartments Option Baggage Tray Extended Compartment BAGGAGE TRAY Compiled by Peter Schmidleitner DA40 NG 256 Baggage Compartments BAGGAGE TRAY Option Short Baggege Extension ...

Page 131: ... 80 170 10 1160 60 1220 391 0 260 0 38 9 2870 7 157 8 3028 5 170 x 2 30 391 0 80 x 3 25 260 0 20 USG Compiled by Peter Schmidleitner DA40 NG 258 M B Calculation 2 47 2 48 Lever arm Mass kg Moment kgm Empty mass 2 42 900 2180 8 Front seats 2 30 Rear seats 3 25 Fwd baggage 3 89 Aft baggage 4 54 Zero Fuel Mass Fuel 2 63 Total TKOF Mass 80 170 10 1160 60 1220 391 0 260 0 38 9 2870 7 157 8 3028 5 2870 ...

Page 132: ...130 Compiled by Peter Schmidleitner DA40 NG 259 ZFM 1160 kg 2 47 m Center of Gravity Envelope TOM 1220 kg 2 48 m Compiled by Peter Schmidleitner DA40 NG Intentionally blank ...

Page 133: ...131 Diamond DA40 NG Compiled by Peter Schmidleitner 261 Emergency Equipment Compiled by Peter Schmidleitner DA40 NG 262 Emergency equipment ...

Page 134: ...132 Compiled by Peter Schmidleitner DA40 NG 263 Emergency Exit FWD 1 2 Compiled by Peter Schmidleitner DA40 NG 264 Emergency Exit FWD 1 2 ...

Page 135: ...133 Compiled by Peter Schmidleitner DA40 NG 265 Egress Hammer 265 Compiled by Peter Schmidleitner DA40 NG Intentionally blank ...

Page 136: ...134 Diamond DA40 NG Compiled by Peter Schmidleitner 267 Kinds of Operation Equipment List KOEL Compiled by Peter Schmidleitner DA40 NG 268 Kinds of Operation Equipment List KOEL ...

Page 137: ...135 Compiled by Peter Schmidleitner DA40 NG 269 Kinds of Operation Equipment List KOEL Compiled by Peter Schmidleitner DA40 NG 270 Kinds of Operation Equipment List KOEL ...

Page 138: ... 271 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 Compiled by Peter Schmidleitner DA40 NG Intentionally blank ...

Page 139: ...137 Diamond DA40 NG Compiled by Peter Schmidleitner 273 Servicing Compiled by Peter Schmidleitner DA40 NG 274 Scheduled maintenance Every 100 hours 200 hours 1000 hours Annually ...

Page 140: ...y Peter Schmidleitner DA40 NG 275 Unscheduled maintenance Hard landings Propeller strike Engine fire Lightning strike Occurence of other malfunctions and damage Compiled by Peter Schmidleitner DA40 NG 276 Refuelling ...

Page 141: ...ith brush Spray de icing fluid Wipe dry Compiled by Peter Schmidleitner DA40 NG 278 Parking Short term parking Parking brake ON Flaps UP Extended or unattended parking unpredictable wind Mooring or placing in hangar Outside parking at OAT below 38 C Water Coolant mixture ratio 40 to 60 If battery heating system installed Recommended to be used if OAT below 0 C ...

Page 142: ...140 Compiled by Peter Schmidleitner DA40 NG 279 Control surfaces gust lock Compiled by Peter Schmidleitner DA40 NG 280 Mooring ...

Page 143: ...141 Compiled by Peter Schmidleitner DA40 NG 281 Mooring Compiled by Peter Schmidleitner DA40 NG 282 Tow bar ...

Page 144: ...142 Diamond DA40 NG Compiled by Peter Schmidleitner 283 Airconditioning Compiled by Peter Schmidleitner DA40 NG 284 RACC Recirculating Air Cabin Cooling ...

Page 145: ...refore only Short baggage compartment Compiled by Peter Schmidleitner DA40 NG 286 RACC Elements AUX Power switch Control panel on center console Central unit aft of baggage compartment Additional alternator engine compartment belt driven from propeller shaft Not connected to the electrical system ...

Page 146: ...144 Compiled by Peter Schmidleitner DA40 NG 287 RACC Controls Compiled by Peter Schmidleitner DA40 NG 288 Addititional Alternator ...

Page 147: ...eitner DA40 NG 289 Addititional Alternator Compiled by Peter Schmidleitner DA40 NG 290 RACC Concept Cabin air is circulated through the RACC and thereby cooled Cabin air and outside air is also needed for the operation of the RACC ...

Page 148: ...146 Compiled by Peter Schmidleitner DA40 NG 291 RACC Central Unit Compiled by Peter Schmidleitner DA40 NG 292 RACC Central Unit Front and left side ...

Page 149: ...147 Compiled by Peter Schmidleitner DA40 NG 293 RACC Central Unit Back and right side Compiled by Peter Schmidleitner DA40 NG 294 RACC Schematic ...

Page 150: ...148 Compiled by Peter Schmidleitner DA40 NG 295 RACC Schematic Compiled by Peter Schmidleitner DA40 NG 296 RACC Installation Cooled air outlets ...

Page 151: ... Emergencies during Take off Landing Go Around RACC may be ON with modification 40 394 but for flight masses above 1280 kg only when wheel fairings are installed during Abnormal Operating Procedures at OAT below 10 C 50 F above 10 000 ft MSL when ADF system is used for navigation RACC effects accuracy of the ADF system and the WX 500 Stormscope Minimum flight mass 988 kg ...

Page 152: ...GINE MASTER check OFF Connect external power RACC ON On ground with engine running Keep RPM above 800 AUX POWER ON RACC ON Power Off RACC OFF press button for 1 sec AUX POWER OFF Compiled by Peter Schmidleitner DA40 NG 300 RACC Operation In flight switching RACC System ON AUX POWER ON RACC ON switching RACC System OFF RACC OFF AUX POWER OFF ...

Page 153: ...ter Schmidleitner DA40 NG 301 Take off RACC ON ground roll increased by 30 m TKOF distance increased by 40 m Compiled by Peter Schmidleitner DA40 NG 302 Climb and Cruise RACC ON reduced by 4 RACC ON reduced by 25 ft min ...

Page 154: ...Peter Schmidleitner DA40 NG 303 Moment Arms Item Lever Arm m Front seats 2 30 Rear seats 3 25 Wing tanks 2 63 Standard bagge 3 65 Short baggage extension 3 97 Compiled by Peter Schmidleitner DA40 NG Intentionally blank ...

Page 155: ...dures Compiled by Peter Schmidleitner DA40 NG 306 TKOF Profile Safe altitude Circuit altitude Climb to cruise altitude Vy 72 KIAS 88 KIAS 110 KIAS 88 KIAS Flaps UP Climb Power 60 Rotate 56 67 KIAS V50 up to 50 ft 62 72 KIAS 50 ft Climb Check Fuel pumps are switched OFF ...

Page 156: ... Power MAX Flaps T O 66 77 KIAS Continue with TKOF profile Descent Approach Check Fuel pumps are switched ON Compiled by Peter Schmidleitner DA40 NG 308 Checklists The checklists are not part of the AFM and they are not officially Diamond factory endorsed They are published and used by Diamond Flight Training and are a also a recommendation for an Operator Checklist ...

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