Diamond DA42 NG Handout DA42 NG Systems INTENTIONALLY BLANK Diamond DA42 NG Vers. 4 ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r Dimensions 13,42 m Span: 13,55 m with ACL (strobe lights) ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 1 Dimensions 2,20 m 2,49 m 8,56 m 1,74 m ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r Dimensions 1,87 m Dash-6: 1,90 m 2,95 m ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 2 Minimum width for 180° turn Full nosewheel deflection, no brake 2,95 m 9,5 m 46 cm safety margin ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r Minimum width for 180° turn Full nosewheel deflection, max. brake on inner wheel (wheel blocked) 2,95 m 6,0 m 30cm safety margin ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 3 Nose bagge compartment ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r ELT and VHF COM 1 antenna ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 4 VHF COM 2 antenna ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r VHF NAV + GP antennas in the stabilizer ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 5 Stormscope antenna ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r GPS antennas Cabin roof With SBAS ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 6 Marker antenna Fuselage belly ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r DME, TXPDR antennas Fuselage belly ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 7 ADF antenna Fuselage belly ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r TAS antennas Fuselage belly ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 8 OAT Sensor Battery vent OAT sensor ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r Intentionally blank ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 9 Mass ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r Mass (Weight) Empty (typical) 1450 kg Max TKOF 1900 kg Max Ramp + 8 kg Max Zero Fuel 1765 kg Max LDG 1805 kg ! Min for flight 1510 kg ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 10 Max Landing Mass Landing with a mass higher than 1805 kg is an „Abnormal Operating Procedure“ However: „Hard LDG Check“ only required after a hard LDG, regardless of LDG mass ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r Max. Baggage Load Nose compartment 30 kg „Short“ Standard Baggage Extension Standard 45 kg 30 kg compartment Baggage 18 kg 15 kg Extension Total 45 kg 45 kg ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 11 CABIN BAGGAGE TRAY ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r „Short“ Baggage Extension BAGGAGE TRAY ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 12 Mass Attention! JET fuel and Diesel are heavier than AVGAS! Typical fuel weight: JET A1: Diesel: 0,8 kg/ltr 0,84 kg/ltr 3,03 kg/USG 3,2 kg/USG ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r Intentionally blank ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 13 Speeds ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r Characteristic speeds VNO 151 KIAS VNE 188 KIAS 112 KIAS 1700 kg VO 119 KIAS 1800 kg 122 KIAS ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 14 Characteristic speeds „NG“ 62 KIAS VSO „Dash-6“ 62 KIAS „NG“ 69 KIAS VS1 „Dash-6“ 68 KIAS Flaps UP Flaps APP „NG“ 76 KIAS 73 KIAS VMCA „Dash-6“ 71 KIAS 68 KIAS For short field take-off Vops ice 118-156 KIAS ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r Characteristic speeds For short field take-off Flaps UP Flaps APP „NG“ 80 KIAS 76 KIAS VR „Dash-6“ 76 KIAS 71 KIAS „NG“ --- 82 KIAS VX „Dash-6“ --- 77 KIAS VY 90 KIAS 85 KIAS VYSE 85 KIAS Vyse „ice“ 88 KIAS VCRZ CLB 90 KIAS ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 15 Characteristic speeds VFE (Flaps APP) 133 KIAS VFE (Flaps LDG) 113 KIAS VLO E (= VNE) 188 KIAS Emergency extension 152 KIAS VLO R (=~VNO) 152 KIAS VLE (= VNE) 188 KIAS ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r Characteristic speeds Approach Speeds VREF FLAPS UP 86 KIAS VREF FLAPS APP 84 KIAS VREF FLAPS LDG 84 KIAS VGA FLAPS UP 90 KIAS ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 16 Diamond DA42 NG Instrument Panel ComCompiledpiled by byPeterPeter Schmidleitne Schmidleitner r Instrument panel ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 17 Instrument Panel Garmin 1000 ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r Instrument Panel Airspeed Horizon Altimeter Compass Backup Instruments ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 18 Instrument Panel Flood Lights Emergency Switch Emergency Battery (non rechargeable) IFR flights not permitted when seal on Emergeny Switch is broken ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r Instrument Panel Lights ELT ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 19 Instrument Panel Circuit breakers ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r Instrument Panel Alternators + ECU Control ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 20 Digital Engine Control ECU (EECU) Engine Control Unit Electric Engine Control Unit this is a FADEC Full Authority Digital Engine Control ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r Digital Engine Control Will be explained in the „Power Plant“ chapter ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 21 Instrument Panel Fuel Pumps Pitot heat Engine master switches, Electric Master, Engine start Avionic Master ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r Instrument Panel Landing gear Flaps ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 22 Instrument panel („Upgrade NG“ with KAP140) Fuel pumps New ECU panel Fuel pump CBs ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r Instrument panel („Upgrade NG“ with KAP140) ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 23 Pitot probe ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r Static ports ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 24 Alternate static valve ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r Lift detector (Stall warning) ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 25 Diamond DA42 NG Garmin 1000 Engine Indication System ComCompiledpiled by byPeterPeter Schmidleitne Schmidleitner r DA42 Garmin 1000 PFD MFD Primary Flight Display Multi Function Display Image reproduced with the permission of Garmin. © Copyright 2006 Garmin Ltd. or its subsidiaries. All Rights Reserved. ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 26 Garmin 1000 MFD EIS / Engine Indication System Image reproduced with the permission of Garmin. © Copyright 2006 Garmin Ltd. or its subsidiaries. All Rights Reserved. ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r Engine Indication System Display when Display when pushing the pushing the Default page SYSTEM softkey FUEL softkey Image reproduced with the permission of Garmin. © Copyright 2006 Garmin Ltd. or its subsidiaries. All Rights Reserved. ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 27 Engine Indication System Display when Display when pushing the pushing the Default page SYSTEM softkey FUEL softkey Upper part always the same Image reproduced with the permission of Garmin. © Copyright 2006 Garmin Ltd. or its subsidiaries. All Rights Reserved. ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r Engine Indication System Default SYSTEM FUEL Image reproduced with the permission of Garmin. © Copyright 2006 Garmin Ltd. or its subsidiaries. All Rights Reserved. ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 28 Diamond DA42 NG Hydraulic System ComCompiledpiled by byPeterPeter Schmidleitne Schmidleitner r Hydraulic brakes Pilot applies brake ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 29 Hydraulic brakes Parking brake Locked ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r Hydraulic brakes Parking brake „Pumping“ One-way valve is closed Pressure builds up ©Peter Schmidleitner ComCompiledpiled by bPetery Peter Schmidleitne Schmidleitner r 30 Landing gear ©Peter