Diamond DA 40-TDI G1000
Transcript of Diamond DA 40-TDI G1000
1
Diamond DA 40-TDIG1000
DA40-TDI-G1000 Version 1.1
Diamond DA40-TDI G1000
Compiled by Peter Schmidleitner
Dimensions
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Dimensions
11,94 m
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Dimensions
8,01 m
1,97 m
1,68 m
2,97 m
Diamond DA40-TDI G1000
Compiled by Peter Schmidleitner
Exterior
© Peter SchmidleitnerCompiled by Peter Schmidleitner
ELT and VHF COM 1 Antenna
ELT antenna in fuselage structure
VHF COM 1
2
© Peter SchmidleitnerCompiled by Peter Schmidleitner
VHF COM 2 antenna
© Peter SchmidleitnerCompiled by Peter Schmidleitner
VHF NAV + GP Antennas
in the horizontal stabilizer
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Marker Antenna
Fuselage belly
© Peter SchmidleitnerCompiled by Peter Schmidleitner
GPS Antennas
Cabin roof
© Peter SchmidleitnerCompiled by Peter Schmidleitner
DME, TXPDR Antenna
Fuselage belly
© Peter SchmidleitnerCompiled by Peter Schmidleitner
ADF antenna
Fuselage belly
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© Peter SchmidleitnerCompiled by Peter Schmidleitner
Pitot/Static Probe
Left wing
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Pitot/Static Probe
PitotStatic
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Lift Detector (Stall Warning)
Left wing
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Engine Oil
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Engine Oil
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Air Inlets
Intercooler Coolant heatexchanger
Oil Cooler
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© Peter SchmidleitnerCompiled by Peter Schmidleitner
RH frontVentilation
Engine air intake
Cabin air heater
Air Inlets
© Peter SchmidleitnerCompiled by Peter Schmidleitner
LH front Ventilation
Air Inlets
Diamond DA40-TDI G1000
Compiled by Peter Schmidleitner
Operating Limitation
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Temperature Limitation
The airplane may only be operated whenits temperature prior to operation is notless than -20°C and not higher than54°C.With the airplane cold soaked and itstemperature below -20°C the use of an external pre-heater for the engine and pilot compartment prior to operation ismandatory.
Diamond DA40-TDI G1000
Compiled by Peter Schmidleitner
Mass
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Mass (Weight)
45 kg(max 18 kg in
aftcompartment)
Max Baggage with„BaggageExtension“
30 kgMax Baggage
1150 kg Max LDG
1150 kgMax TKOF
830 kgEmpty (typical)
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© Peter SchmidleitnerCompiled by Peter Schmidleitner
Mass (Weight)
Attention!
JET fuel and Diesel are heavier thanAVGAS!
Typical fuel weight:
Diesel:0,84 kg/ltr3,2 kg/USG
JET A1: 0,8 kg/ltr3,03 kg/USG
Diamond DA40-TDI G1000
Compiled by Peter Schmidleitner
Speeds
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Characteristic Speeds
108 KIASVA 980-1150 kg
94 KIASVA 780-980 kg
178 KIASVNE
129 KIASVNO
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Characteristic Speeds
52 KIASVS1
49 KIASVSO
91 KIASVFE (Flaps LDG)
108 KIASVFE (Flaps T/O)
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Characteristic Speeds
71 KIAS
73 KIAS
73 KIAS
66 KIAS
1150 kg
63 KIAS
68 KIAS
68 KIAS
60 KIAS
1000 kg850 kg
58 KIASVLDG Flaps LDG
60 KIASVLDG Flaps UP
60 KIASV climb
54 KIASVX = VY
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Stalling Speeds
980 kg
1150 kg
VS1VSO
42 47
49 52
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© Peter SchmidleitnerCompiled by Peter Schmidleitner
Stalling Speeds
VS1VSO
57 58
62 66
980 kg
1150 kg
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Stalling Speeds
VS1VSO
71 73
76 79
980 kg
1150 kg
Diamond DA40-TDI G1000
Compiled by Peter Schmidleitner
Flight Controls
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Flight Control Operation
Rudder:cables
Ailerons, Elevator:push rods
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Flight Control Operation
Flaps:electrically by push rods,
left and right mechanicallyinterconnected
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Intentionally blank
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Diamond DA40-TDI G1000
Compiled by Peter Schmidleitner
Instrument Panel
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Instrument Panel
Garmin 1000
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Instrument Panel
Backup Instruments
Horizon AltimeterAirspeed Compass
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Instrument Panel
Emergency Battery(non rechargeable)
Flood Lights
Emergency Switch
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Instrument Panel
ELTLights
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Instrument Panel
Circuit breakers
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© Peter SchmidleitnerCompiled by Peter Schmidleitner
Instrument Panel
Essential BusElectric Master
Starter
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Instrument Panel
Engine control
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Instrument Panel
AvionicMaster
Fuel x-fer pump,Pitot heat
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Instrument Panel
FlapsAutopilot
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Alternate Static Valve
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Engine Indication SystemDefault SYSTEM FUEL
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Diamond DA40-TDI G1000
Compiled by Peter Schmidleitner
Hydraulic System
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Hydraulic brakes
Pilot applies brake
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Hydraulic brakes
One-way valve is closed
Parking brake
„Pumping“
Pressure builds up
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Parking brake
Diamond DA40-TDI G1000
Compiled by Peter Schmidleitner
Power Plant
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Thielert Aircraft Engine TAE125-02-99Previously: TAE125-01
Four cylinders, liquid-cooled1991 ccm (TAE125-01: 1689 ccm)
Common-rail direct injectionReduction gear 1:1,69Dual digital engine controlTurbochargerMax. power: 99kW (135 HP) at 2300 RPMMax cont. power: 99kW (135 hp) at 2300 RPM
Diamond DA40 TDI Engine
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© Peter SchmidleitnerCompiled by Peter Schmidleitner
Diamond DA40 TDI Engine
Thielert Aircraft Engine TAE125Four cylinders, liquid-cooled, 1689 ccmCommon-rail direct injectionReduction gear 1:1,69Digital engine controlTurbochargerMax. power 99kW (135 PS) at 2300 RPMMax cont. power 99kW (135 PS) at 2300 RPM
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Digital Engine Control
ECUEngine Control Unit
this is a
FADECFull Authority Digital EngineControl
© Peter SchmidleitnerCompiled by Peter Schmidleitner
ECU – Engine Control Unit
© Peter SchmidleitnerCompiled by Peter Schmidleitner
E.O.T. – Engine Order Telgraph („Chadburn“)
© Peter SchmidleitnerCompiled by Peter Schmidleitner
• Power lever selects power (LOAD in %)
• RPM automatically determined by selected power
Diamond DA40 TDI Engine
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Diamond DA40 TDI Engine
Engine air filter
Alternate air valve
Heat Exchanger for Cabin Heat System
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© Peter SchmidleitnerCompiled by Peter Schmidleitner
Intercooler
Diamond DA40 TDI Engine
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Diamond DA40 TDI Engine
Coolant Heat Exchanger
Reduction Gear
Coolant Reservoir
Generator
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Power plant – Gear oil
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Power plant – Gear oil
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Power plant – Gear oil
Is this the little bubble ?
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Power plant limitations
Italic figures are for the „old“ 125-01 engine
Max RPM: 2300Oil pressure: 1.0 – 6.5 barOil quantity (per engine): 4.5 – 6.0 litersMax. oil consumption: 0.1 liters/hrOil temperature: -30 (-32) °C – 140 °CGearbox temperature: max. 120 °CCoolant temperature: -30 (-32) °C – 105 °CMax. restart altitude: 8000 ft (6500 ft),73–120 KIAS
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© Peter SchmidleitnerCompiled 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/CFSHELL Helix Ultra 5W40 synth. API SL/CFAERO SHELL Diesel 10W-40
Gearbox oil: SHELL EP 75W90 API GL-4
Coolant: DAI-G30-MIXspecial 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 SchmidleitnerCompiled by Peter Schmidleitner
„Diesel“ limitations
Temperature limitsBelow -5° C no engine startBelow +5° C no take-off
Be sure that no diesel fuel is in thetanks – otherwise temp limitationsfor diesel ops must be observed
© Peter SchmidleitnerCompiled by Peter Schmidleitner
When is no more diesel in the tanks?each tank to be refilled at least twice withmore than
10,6 USG (40 ltrs) (normal tanks)17,2 USG (65 ltrs) (long range tanks)
of Jet fuelotherwise
tank must be drained
„Diesel“ limitations
© Peter SchmidleitnerCompiled by Peter Schmidleitner
JET fuel
-30 +75+70+5-5Fuel 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 SchmidleitnerCompiled by Peter Schmidleitner
DA 40 TDI Cooling System
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© Peter SchmidleitnerCompiled by Peter Schmidleitner
DA 40 TDI Cooling System
Coolant Temp.< 80°
© Peter SchmidleitnerCompiled by Peter Schmidleitner
DA 40 TDI Cooling System
Coolant Temp.> 80°
© Peter SchmidleitnerCompiled by Peter Schmidleitner
DA 40 TDI Cooling System
Cabin Heat
© Peter SchmidleitnerCompiled by Peter Schmidleitner
DA 40 TDI Cabin Heat
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Cockpit
DA 40 TDI Ventilation
CabinCabin
© Peter SchmidleitnerCompiled by Peter Schmidleitner
DA 40 TDI Ventilation
Left wing
Rear cabin ventilation air inlet
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Diamond DA40-TDI G1000
Compiled by Peter Schmidleitner
TurbochargerSystem
© Peter SchmidleitnerCompiled by Peter Schmidleitner
DA 40 TDI Turbo Charger
Exhaust gas drives turbineBypass for excess exhaust gas
© Peter SchmidleitnerCompiled by Peter Schmidleitner
DA 40 TDI Turbo Charger
Turbine drives compressorCompressor compresses intake air
Diamond DA40-TDI G1000
Compiled by Peter Schmidleitner
Fuel System
© Peter SchmidleitnerCompiled by Peter Schmidleitner
2 x 14 USG usable= 28 USG= 85 kgAt 70% power: ~ 5 USG/hr
DA 40 TDI Fuel System
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Long Range Tanks:2 x 19,5 USG usable= 39 USG= 120 kgMax indicated fuel per tank: 15 USGMax. unbalance: 9 USG
DA 40 TDI Fuel System
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© Peter SchmidleitnerCompiled by Peter Schmidleitner
DA 40 TDI Fuel System
© Peter SchmidleitnerCompiled by Peter Schmidleitner
DA 40 TDI Fuel System
© Peter SchmidleitnerCompiled by Peter Schmidleitner
DA 40 TDI Fuel System
18-21 USG/hr
~60 USG/hrFuel cooler
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Fuel cooler
Right wing
Air inletAir outlet
© Peter SchmidleitnerCompiled by Peter Schmidleitner
DA 40 TDI Fuel System
U/S
© Peter SchmidleitnerCompiled by Peter Schmidleitner
DA 40 TDI Fuel System
18-21 USG/hr
U/SFuel cooler
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© Peter SchmidleitnerCompiled by Peter Schmidleitner
DA 40 Fuel system
„Alternate means forfuel quantity indication“
Position:at the bore in the stall strip
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Fuel vents
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Fuel tank drain
FWD
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Fuel gascolator drain
Diamond DA40-TDI G1000
Compiled by Peter Schmidleitner
Electrical System
© Peter SchmidleitnerCompiled by Peter Schmidleitner
DA40 TDI G1000 Electrical System
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© Peter SchmidleitnerCompiled by Peter Schmidleitner
DA40 TDI G1000 Electrical System
Power sources
Generator12-14V 90A
Main Battery12V 45Ah
ECU Backup Battery12V 12Ah
Excitation Battery12V 1,3 Ah
© Peter SchmidleitnerCompiled by Peter Schmidleitner
DA40 TDI G1000 Electrical System
Power distribution
Hot Battery Bus
Battery Bus Main Bus
Essential Bus
ECU Bus
Avionic Bus
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Electric Master, Essential Bus
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Engine Master
© Peter SchmidleitnerCompiled by Peter Schmidleitner
DA40 TDI G1000 Electrical SystemOFF
ON
OFF
Before Engine Start
© Peter SchmidleitnerCompiled by Peter Schmidleitner
DA40 TDI G1000 Electrical System
ON
OFF
Preparing Engine StartON
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© Peter SchmidleitnerCompiled by Peter Schmidleitner
DA40 TDI G1000 Electrical System
ON
OFF
ONEngine Start
START
© Peter SchmidleitnerCompiled by Peter Schmidleitner
DA40 TDI G1000 Electrical System
ON
OFF
ON
ON
After Engine Start
© Peter SchmidleitnerCompiled by Peter Schmidleitner
External Power Receptable
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Emergency Switch
© Peter SchmidleitnerCompiled by Peter Schmidleitner
The mysteriousEssential Bus
Switch
DA40-TDI G1000
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Switch location
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© Peter SchmidleitnerCompiled by Peter Schmidleitner
When is it used ?
When the generator failsto disconnect unnecessaryelectrical consumersto supply battery power to essential electrical consumers
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Essential Electrial Power
Essential BusPFDHorizon *)AHRSADCFlapsLanding lightPitot HeatingLanding LightFlood Light *)
*) Emergency Battery
COM 1GPS / NAV Receiver 1TransponderEngine instruments
Hot Battery Bus(Essential Bus)Pilot‘s map/reading lightAuxiliary jack
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Main unserviceable systemsFuel x-fer pumpMFDAcionic / CDU fanPosition light, Strobe lights, Taxi lightInstrument lights, Map lightStarter(Avionics Bus)
COM2, NAV/GPS2, ADF, DME, WX500, Audio, Autopilot
Essential Electrial Power
© Peter SchmidleitnerCompiled by Peter Schmidleitner
What happens ...
... if it is switched ON duringnormal operation?Will the battery be discharged?
NO !
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Normal Situation
Hot
Bat
tery
Bus
Batt
ery
Bus
Esse
ntia
l Bus
GEN
BATT
Avio
niic
Bus
ECU
Bus
Mai
n Bu
s
Battery is charged
DA40-TDI G1000, Ess. Bus switch
© Peter SchmidleitnerCompiled by Peter Schmidleitner
GEN u/s, Ess. PWR OFF
Hot
Bat
tery
Bus
Batt
ery
Bus
Esse
ntia
l Bus
GEN
BATT
Avio
niic
Bus
ECU
Bus
Mai
n Bu
s
Battery will bedischarged
DA40-TDI G1000, Ess. Bus switch
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© Peter SchmidleitnerCompiled by Peter Schmidleitner
GEN u/s, Ess. PWR ONH
ot B
atte
ryBu
s
Batt
ery
Bus
Esse
ntia
l Bus
GEN
BATT
Avio
niic
Bus
ECU
Bus
Mai
n Bu
s
Battery will bedischargedat slow rate
DA40-TDI G1000, Ess. Bus switch
© Peter SchmidleitnerCompiled by Peter Schmidleitner
GEN OK, Ess. PWR ON
Hot
Bat
tery
Bus
Batt
ery
Bus
Esse
ntia
l Bus
GEN
BATT
Avio
niic
Bus
ECU
Bus
Mai
n Bu
s
Battery is still charged
DA40-TDI G1000, Ess. Bus switch
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Hot
Bat
tery
Bus
Batt
ery
Bus
Esse
ntia
l Bus
GEN
BATT
Avio
niic
Bus
ECU
Bus
Mai
n Bu
s
DA40-TDI G1000, Ess. Bus switch
Essential Bus ON by mistake
COM2, NAV/GPS2,Audio,ADF, DME, AutopilotWX 500
Fuel x-fer pumpMFDAvion./CDU fanFAN / OAT indicationPosition lightStrobe lightsTaxi light, Map light Instrument lightsStarter
© Peter SchmidleitnerCompiled by Peter Schmidleitner
A very special engine start problem:Start witch ONNothing happens!
Why?Essential Bus switch ON by mistake!
DA40-TDI G1000, Ess. Bus switch
© Peter SchmidleitnerCompiled by Peter Schmidleitner
DA40 TDI G1000 Electrical System
Generator + Battery FailON
ECU backup battery
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Intentionally blank
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Diamond DA40-TDI G1000
Compiled by Peter Schmidleitner
AutopilotKAP140
© Peter SchmidleitnerCompiled by Peter Schmidleitner
KAP 140 has 2 functions:if not engaged: Altitude warningif engaged („ON“): Autopilot
Autopilot
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Autopilot
HeadingYES
Stearing signalYES
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Autopilot
AltitudeNO
Baro settingNO
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Autopilot limitations
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Autopilot
AP disconnectCWS
Manual Electric Trim
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© Peter SchmidleitnerCompiled by Peter Schmidleitner
Autopilot
Roll Wrng
AP ON/OFF
HDG select
NAV mode
APR mode
Backbeam
ALT Hold +/- V/Sor
+/- Alt
SetAltitude
orBaro
Barodisplay/setting
ALT ARM
Pitch Wrng
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Autopilot
ALTV/S
BARO
display
ALT Alert
Pitch trimannunciator
AP engagedannunciator
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Autopilot
PitchMode:
VSALT ARM
ALTGS
Roll Mode:
ROLHDG
NAV ARMNAV
APR ARMAPR
REV ARMREV
GS ARM
© Peter SchmidleitnerCompiled by Peter Schmidleitner
ALT
AutopilotAltitude Preselect
Select Altitude
Check ALT ARM
Adjust V/S
Check ALT ALERT
Check ALT Hold
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Autopilot – Altitudepreselect
Selecting altitude when autopilot is ON:Altitude ARMED automatically
Switching autopilot ON with a preselected altitude (e.g. when altitudewas preselected before TKOF):
Altitude must be ARMed manually!
© Peter SchmidleitnerCompiled by Peter Schmidleitner
AutopilotAltitude Hold Mode
Toggles between ALT HLD and V/S
Vertical Speed Mode
Toggles between ALT HLD and V/S
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Diamond DA40-TDI G1000
Compiled by Peter Schmidleitner
Performance
© Peter SchmidleitnerCompiled by Peter Schmidleitner
The „DA 40 TDI“ and „Density Altitude“
Attention!Performance data which are engine-power dependant cannot bedetermined by just using „DensityAltitude“!Reason: the engine power output doesnot correspond to density altitude butpressure and temperature have theirown, independent influenceThis is a feature of the ECU controlled, turbocharged Diesel-engine
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Cruise Power Setting
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Cruising Speed
e.g. 6000 ft, ISA, 70 %
121 kts
© Peter SchmidleitnerCompiled by Peter Schmidleitner
TOD
SL, ISA, 1150 kg: 640 m
© Peter SchmidleitnerCompiled by Peter Schmidleitner
TKOF Distance
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© Peter SchmidleitnerCompiled by Peter Schmidleitner
TKOF Run
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Grass Runway
min + 25%>10 cm
+ 15%5 - 10 cmmay be
significantlylonger
+ 10%- 5 cm
Wet grassTKOF rollLength of grass
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Take off climb66 KIAS
Attention!Increasingdownward
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Cruise Climb
73 KIAS
© Peter SchmidleitnerCompiled by Peter Schmidleitner
ROC to gradient conversion
© Peter SchmidleitnerCompiled by Peter Schmidleitner
LD, LR tabular format
Flaps LDGVREF 71 KIAS
Flaps UPVREF 73 KIAS
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© Peter SchmidleitnerCompiled by Peter Schmidleitner
Landing Distance
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Landing Run
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Grass Runway
min + 25%>10 cm
+ 15%5 - 10 cmmay be
significantlylonger
+ 5%- 5 cm
Wet grassLDG runLength of grass
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Go Around
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Obstacles ?
RWLTOD
Obst. Dist.„d“
„h“
„d“= (RWL + Obst.Dist.) - TOD
Gradient = („h“ / „d“) * 100
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Vöslau RWY 31
950650
830 m1130
98 ft
„d“= (950 + 830) – 650 = 1130
Gradient = (30 / 1130) * 100 = 2,65 %
Acc. Performance Graph:~ 9 %
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Diamond DA40-TDI G1000
Compiled by Peter Schmidleitner
Mass and Balance
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Empty Mass
Empty Mass includes:Equipment as per Equipment InventoryBrake fluidCoolant fluidGear oilEngine oilUnusable fuel (2 x 1,0 USG)
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Center of Gravity Envelope
2.46 2.59
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Moment Envelope
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Moment Arms
4.54Aft baggage
3.89Fwd. baggage
2.63Wing tanks
3.25Rear seats
2.30Front seats
LeverArm (m)
Item
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Typical M+B data
2,4602032,3826,2„N-VFR“-version
2,4692057,7833,5„IFR“-version (ADF, WX500)
CG armMomentEmpty mass
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© Peter SchmidleitnerCompiled by Peter Schmidleitner
M&B Calculation
2.63
3.89
3.25
2.30
2.47
Leverarm
Total TKOF Mass
Fuel
Zero Fuel Mass
Fwd. Baggage
Rear seats
Front seats
2050.1830 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 SchmidleitnerCompiled by Peter Schmidleitner
M&B Calculation
2.63
3.89
3.25
2.30
2.47
Leverarm
Total TKOF Mass
Fuel
Zero Fuel Mass
Fwd. Baggage
Rear seats
Front seats
2050.1830 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 SchmidleitnerCompiled by Peter Schmidleitner
ZFM1090 kg , 2.514 m
TOM1150 kg , 2.52 m
Center of Gravity Envelope
© Peter SchmidleitnerCompiled by Peter Schmidleitner
M&B Calculation
2.63
3.89
3.25
2.30
2.47
Leverarm
Total TKOF Mass
Fuel
Zero Fuel Mass
Fwd. Baggage
Rear seats
Front seats
2050.1830 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 SchmidleitnerCompiled by Peter Schmidleitner
Moment Envelope
ZFM1090 kg , 2740.0
TOM1150 kg , 2897.8
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Intentionally blank
28
Diamond DA40-TDI G1000
Compiled by Peter Schmidleitner
EmergencyEquipment
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Emergency equipment
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Emergency Exit
FWD
1
2
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Emergency Exit
FWD
1
2
Diamond DA40-TDI G1000
Compiled by Peter Schmidleitner
Kinds of Operation Equipment List
(KOEL)
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Kinds of Operation Equipment List KOEL
29
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Kinds of Operation Equipment List KOEL
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Kinds of Operation Equipment List KOEL
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Kinds of Operation Equipment ListKOEL
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Additional minimum equipment for theintended operationmay be required by
national operating rulesand also depends on the
route to be flown.
Kinds of Operation Equipment ListKOEL
Diamond DA40-TDI G1000
Compiled by Peter Schmidleitner
Servicing
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Scheduled maintenance
Every100 hours200 hours1000 hours2000 hours
Annually
30
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Refuelling
© Peter SchmidleitnerCompiled by Peter Schmidleitner
De-icing
Approved de-icing fluids:Kilfrost TKS 80Aeroshell Compound 07
Procedure:Remove snow with brushSpray de-icing fluidWipe dry
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Control surfaces gust lock
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Mooring
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Mooring
© Peter SchmidleitnerCompiled by Peter Schmidleitner
Tow bar
1
Diamond DA40-TDI G1000
Compiled by Peter Schmidleitner
Flight Procedures
© Peter SchmidleitnerCompiled by Peter Schmidleitner
TKOF Profile
Rotate at 59 kt
© Peter SchmidleitnerCompiled by Peter Schmidleitner
LDG Profile
© Peter SchmidleitnerCompiled 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 SchmidleitnerCompiled by Peter Schmidleitner
Thank you for your attention!