Aerosoft DA20-100 Manual Download

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Neither the software nor the documentation may
be used for real aviation and training purposes.

04<07

page

DA20-100 ‘Katana’ 4X Manual

NORMAL OPERATION

CAUTION:

Visually inspect for the following conditions: Defects, contamination,
cracks, delaminations, excessive play, insecure or improper
mounting and general condition. Additionally, check the control
surfaces for freedom of movement.

CAUTION:

Set PARKING brake prior to removing wheel chocks

Left Main Landing Gear

Landing Gear Strut

Wheel Fairing

visual inspection

Tire Pressure (33 psi / 2.3 bar)

Wheel Chocks

check

remove

Tire, Wheel, Brake

visual inspection

Left Wing

Entire Wing

Stall Warning

Wing Tip, Position Lights and Strobe

check (suck on opening)

visual inspection

Pitot-Static Probe

Aileron Balancing Weight

Taxi and Landing Lights

Wing Flap including Inspection Panel

clean, holes open

visual inspection

Tie down

Aileron including Inspection Panel

remove

visual inspection

Summary of Contents for DA20-100

Page 1: ...MANUAL DA20 100 Katana ...

Page 2: ......

Page 3: ...Neither the software nor the documentation may be used for real aviation and training purposes ...

Page 4: ...Diamond Aircraft Diamond Air Service Hanseatischer Fliegerclub andAerosoft the pilots and testers our families and friends that had to stand back from time to time while we were working on this project 1 2 DEVELOPMENT TEAM DA20 100 Katana 4X Manual Neither the software nor the documentation may be used for real aviation and training purposes 01 04 page 1 2 1 DEVELOPERS 1 2 2 SUPPORT 1 2 3 TEST TEA...

Page 5: ... cockpit Advanced animations need to be enabled for skin animations and special effects Enable automixture has to be untagged as the Katana features a carburetor simulation Many systems of the Diamond DA20 100 Katana 4x were implemented beyond the possibilities of FSX So there are some keyboard shortcuts that won t work on the Katana For example CTRL E for autostarting the engine or SHIFT M to tur...

Page 6: ...EOFF CLIMB FLIGHT DESCEND LANDING APPROACH PARKED PARKED LONGTERM PARKED RANDOM Ok 1 3 3 INITIATION WINDOW The information part shows accumulated flight hours and landings in realistic mode the operation mode and the detected aircraft status The systems ok message indicates that the add on modules are working properly If you do not want to change the systems setup click None to close the Initiatio...

Page 7: ...center position Before using new or other hardware it is recommended to delete the functions on this device before changing to another If the device is not available anymore it may be the only solution to delete the settings in the config files If the Katana suffers low engine power heavy drag or the engine won t even start or keep running also the aircraft has been maintained it is possibly some ...

Page 8: ...ther windows This menu offers options for preparing the aircraft before your flight refueling and cleaning Only available with parked aircraft Preflight Maintaining the aircraft servicing and changes of the equipment Only available with parked aircraft Maintenance These windows are only available if the add on is operated in Instructor Mode and offer the possibility to influence the aircraft syste...

Page 9: ...e maintained Damages and wear may occur and will be stored with other data Special features are enabled Realistic Simple Instructor The aircraft is brand new every time when loaded No damages and wear no special features No data stored The aircraft is brand new every time when loaded Damages and wear can occur but will not be stored Systems can be influenced with a special user interface REALISTIC...

Page 10: ... The aircraft has been parked for a while so you should check all the systems carefully and prepare the aircraft for the flight The aircraft shall be set into the appropriate condition If it is not able to figure out ist situation it will be forced into a status with engine and all systems running Automatic AUTOMATIC Aircraft tries to figure out the situation of flight and configures iteslf Aircra...

Page 11: ...g movable as in reality Compatible 1 4 6 SETTINGS AVIONICS The avionics can be switched to simple operation for autotune function or compatibility issues with hard and software In simple mode all special functions will be disabled and the radio units operate like the default radios in FSX FLAP LEVER COMPATIB Animation not correct but may be necessary for some hardware Animation realistic but only ...

Page 12: ...eadlights By activating this option the FSX default landing and taxi light cones are enabled Enhanced Headlights More subtle and realistic headlights can be engaged with this selection 1 4 8 SETTINGS EFFECTS CUSTOM SOUNDS This add on comes with over 120 custom sounds to enhance the simulation experience You can enable disable all or just some of the custom sound effects with this menu These option...

Page 13: ...01 13 page DA20 100 Katana 4X Manual 1 4 9 SETTINGS EFFECTS VIBRATION Especially small airplanes get rattled and shaken by the engine and the propeller wind This add on features several vibration and motion effects that can be enabled and disabled in this menu section INTRODUCTION AND DESCRIPTION ...

Page 14: ...1 5 PREFLIGHT DA20 100 Katana 4X Manual Neither the software nor the documentation may be used for real aviation and training purposes 01 14 page INTRODUCTION AND DESCRIPTION ...

Page 15: ...ks Fixations and Equipment can be applied or removed with this window 1 5 2 PREFLIGHT TOW BAR After the area around the airplane has been cleared the Katana can be towed in proper position for further preflight preparations Clicking on the Tow Bar button will open a circle icon in the middle of the screen Note Through FSX limitations moving straight forward after a turn is not possible anymore It ...

Page 16: ...nspection of the aircraft Click on the circled numbers to open the respective checklist Items that need attention are colored blue Some of them can be done in this window others are achieved through actions on other windows for example the oil quantity check The propeller pitch can be tested via dragging the drawing of the blade in horizontal direction as indicated by the arrow INTRODUCTION AND DE...

Page 17: ...r indicator Right click will increase left click will decrease the digit 1 Choose the type of fuel you want to fill into the aircraft s tank 2 Open the fuel tank cap 3 Pull the fuel nozzle to the aircraft and into the tank filler neck 4 Press and hold the button to refuel It will automatically stop when the fuel reaches the maximum capacity Remove the fuel nozzle when done 5 Press the draining ven...

Page 18: ...n it is possible to turn the propeller from within the virtual cockpit 4 Draw the dipstick into the tank and pull it out again after a few moments On the enlarge view the oil should be running from within the flat and light gray area That area indicates the maximum and minimum oil levels 5 To refill oil first choose one of the oil cans and it will be highlighted If there is no yellow stripe indica...

Page 19: ...tically if the aircraft is getting prepared for flight 1 5 8 PREFLIGHT CLEANING Use the water faucet to fill the bucket 1 1 2 3 4 5 Pull the bucket to the aircraft and below the sponge 2 Move the sponge down into the bucket until it is full of water Pull it up again 3 As long as the sponge is wet wipe with the mouse over the areas you want to clean Some sorts of dirt need more work than others For...

Page 20: ...1 6 MAINTENANCE DA20 100 Katana 4X Manual Neither the software nor the documentation may be used for real aviation and training purposes 01 20 page INTRODUCTION AND DESCRIPTION ...

Page 21: ...red device the replacing icon will apear and the status bar should indicate the progress As soon as the process has been finished the unit is available in the virtual cockpit 1 6 2 MAINTENANCE EQUIPMENT WHEEL FAIRINGS Wheel Fairings are reducing drag of the landing gear and make the aircraft faster But they are not suitable for all terrain The fairings can be mounted or unmounted just by clicking ...

Page 22: ...nance is necessary Markings will disapear as soon as maintenance action has been started So this does not mean that the system is back in good condition Another inspection can be done to be sure The Tool Button is used to start the maintenance of a system That is indicated my the moving icon and can be observed by the progress on the bar There can only be one action at a time The progress bar does...

Page 23: ...perating in Realistic Mode The only button that has not yet been described in the maintenance section is for Recharging the battery The action can be interrupted at every time but the battery may not be completely charged Depending on the type of fuel that is used in the aircraft the Oil Filter should be changed regularly The Inlet Baffle should be installed at cold air temperatures If the fuel ta...

Page 24: ...umentation may be used for real aviation and training purposes 01 24 page The Instructor Windows are only available if the add on is operated in Instructor Mode They can be used to easily influence the aicraft s and system s status and conditions INTRODUCTION AND DESCRIPTION ...

Page 25: ...aft Status can be set with a single click on the different status boxes The corresponding box will be colored blue for an active setting process and stays green for a few moments if the status has been successfully set This will only affect aircraft settings not the position airspeed etc The Systems Status can be fixed easily with the the three boxes on the right Within a second all systems can be...

Page 26: ... Deiced with a single click The content of the Oil and Cooland Liquid reservoirs can be changed by dragging the content bars or clicking the button At the bottom it is possible to engage and set a Leak for each system It can be adjusted by dragging the value display or by clicking the buttons A right click on the bar will set the optimum filling level Neither the software nor the documentation may...

Page 27: ...of Pumps and the Filter can be be set by dragging the status bar or by using the buttons Additionally the contamination by water can be adjusted in the same way Clicking the Draining Water bar will drain away accumulated water at the bottom of the tank Clicking a bar with the right mouse button will repair the corresponding system Neither the software nor the documentation may be used for real avi...

Page 28: ...e drawing of the Electric System is interactive switches and circuit breakers can be set with a right click and the charge of the battery can be changed by dragging the status bar 1 7 4 INSTRUCTOR AVIONICS AND INSTRUMENTS The pitot and and static system gyros and avionics can be set to Fault or back to Ok by clicking the corresponding boxes INTRODUCTION AND DESCRIPTION ...

Page 29: ...ual Neither the software nor the documentation may be used for real aviation and training purposes 01 29 page This chapter is about how to control and handle elements of the cockpit with the help of the input devices INTRODUCTION AND DESCRIPTION ...

Page 30: ...n like in the real aircraft Wheel down Wheel up toggle switch position move switch into the lower position move switch into the upper position Left click 3 POS SWITCHES click a side of the switch to hold it down Elevator trim switch Left click SELECTORS and ROTARIES with steps Wheel down Wheel up turning knob left Right click turning knob right turning knob left turning knob right Left Drag ROTARI...

Page 31: ...d Fine movement backward Fine movement forward Hint The friction wheel increases decreases the dragging sensitivity Hint The propeller lever may also be moved by dragging or rotating the mouse wheel over the RPM indicator Left Drag forward back LEVERS at the console Wheel down Wheel up Move lever forward backward Fine movement backward Fine movement forward Right click Move the lever to the opposi...

Page 32: ... there are nearly 100 variables available to control the DA20 100 with buttons switches and levers All controls are named with 4X DA20 100 so they are easy to find INTRODUCTION AND DESCRIPTION Select the Buttons Switches Key Presses oder Axis Assignment window and activate the control There are different ways to assign buttons and switches please have a look into the documentation of FSUIPC for fu...

Page 33: ...SET and using the Parameters 0 and 1 Or you can use just one button to toggle it ON OFF with L BUTTON_BATTERY_MASTER It is possible to use a lever for the carburetor heat with L LEVER_CARB_HEAT Or to use two buttons to push and pull the lever with L BUTTON_CARB_HEAT and the parameters 0 and 1 Or to use just one button Assign the parameter 1 under Control sent when button pressed and parameter 0 in...

Page 34: ...t Manual addresses the operating limitations instrument markings airspeed indicator markings and the limitation placards which are necessary for the safe operation of the airplane its engine and standard systems and equipment 2 1 INTRODUCTION WARNING These limitations must be complied with for all operations page DA20 100 Katana 4X Manual LIMITATIONS ...

Page 35: ...ntrol movement Do not exceed this speed with flaps extended Do not exceed this speed except in smooth air and then only with caution Do not exceed this speed in any operation VA Maneuvering Speed VFE Maximum Flap Extended Speed VNO Maximum Structural Cruising Speed VNE Never Exceed Speed IAS Marking kts mph km h Explanation 37 81 43 93 69 150 Operating range with extended flaps White Arc 41 118 47...

Page 36: ...ible T O RPM 58 kW 78 hp Max Continuous Power 2420 RPM MaMax Permissible Continuous RPM d Oil Pressure 22 psi 1 5 bar Minimum 73 psi 5 0 bar Maximum 102 psi bar 7 0 Max in case of Cold start short term e Fuel Pressure 2 psi 0 15 bar Minimum 6 psi 0 40 bar Maximum f Oil Temperature 122 F 50 C Minimum 284 F 140 C Maximum NOTE The propeller is driven by the engine via a reduction gear with a ratio of...

Page 37: ...ive Fuel 95 RON 91 AKI Approved Fuel Grades i Oil Grades 4 stroke motorcycle oil of a registered brand with gear additives that meets or exceedes API classification SF or SG are highly recommended a Propeller Manufacturer Hoffmann Propeller Rosenheim Germany b Propeller Type HO V352F 170FQ OR c Propeller Diameter 1 70 m 5 ft 6 9 in d Propeller Pitch at 3 4 radius 10 35 e Propeller Speed Limitation...

Page 38: ...r Oil Pressure Indicator 600 2260 RPM 2260 2385 RPM 2385 RPM 122 F 50 C 122 266 F 50 130 C 266 F 130 C 275 F 135 C 12 psi 0 8 bar 29 73 psi 2 5 bar above 1440 RPM 12 29 psi 0 8 2 bar below 1440 RPM 73 102 psi 5 7 bar 102 psi 7 bar Powerplant instrument markings and their color code significance are shown below Recommended nominal idle speed 950 RPM Instrument Red Line Lower Limit Green Arc Normal ...

Page 39: ... RD Most rearward CG all weights The reference datum RD for the center of gravity CG calculation is tangent to the leading edge of the wing at the root rib This plane is vertical when the fuselage is horizontal The procedure used to determine the center of gravity is described in Chapter 6 WARNING Exceeding the weight limitations may lead to overloading of the airplane as well as degrading of the ...

Page 40: ...ht maneuvers b Stalls except WHIPstalls c Lazy Eight s Entry speed 116 kts 215 km h Chandelles Entry speed 116 kts 215 km h Steep turns in which the angle of bank does not exceed 60 d Spinning with Wing Flaps UP Table of structural maximum permissible load factors 4 4 4 4 2 0 2 2 2 2 0 at vA at vNE with fully ext flaps Positive Negative Exceeding the maximum load factors will result in overstressi...

Page 41: ...ompass Turn and Bank Indicator not mandatory for Day VFR only Instrument Panel and Map Lighting not mandatory for Day VFR only Minimum Equipment Powerplant Instruments Fuel Quantity Indicator Oil Pressure Indicator Oil Temperature Indicator Manifold Pressure Indicator Cylinder Head Temperature Indicator Tachometer Fuel Pressure Warning Light Voltmeter Ammeter Generator Warning Light 2 12 FLIGHT CR...

Page 42: ...20 1 US gal 76 litres Usable Fuel 19 5 US gal 74 litres Unusable Fuel 0 6 US gal 2 litres Intentionally left out 2 16 DEMONSTRATED CROSSWIND COMPONENT The maximum demonstrated crosswind component is 15 kts 27 km h 2 15 TEMPERATURE LIMITS Limits for outside air temperature and temperature of the structure for the operation of the airplane 131 F 55 C Structural Temperature Limit Maximum T O Temperat...

Page 43: ...l EMERGENCY PROCEDURES 3 2 AIRSPEEDS DURING EMERGENCY PROCEDURES IAS kts mph km h 60 68 110 Engine failure after take off with flaps in T O position 104 120 193 Manoeuvering Speed 73 66 84 76 135 121 Airspeed for best glide angle Wing Flaps in T O Position 1653 lbs 750kg Wing Flaps in T O Position 1322 lbs 600kg 57 66 106 Precautionary Landing with power and Wing Flaps in LDG position 57 66 106 Em...

Page 44: ... 7 Airspeed VIAS Carburetor Heat Fuel Shut off Valve Electric Fuel Pump 60 kts 68 mph 110 km h ON OPEN ON 2 4 6 8 Throttle Choke Ignition Switch Propeller Speed Control Lever FULL OFF BOTH max RPM I INSUFFICIENT ENGINE POWER WARNING If adequate engine performance cannot be restored immediately prepare for an emergency landing If possible land straight ahead avoiding obstacles Shortly before landin...

Page 45: ...FF cycle L BOTH R BOTH reduce throttle to minimum required power land as soon as possible 2 4 6 Electric Fuel Pump Fuel Shut off Valve Throttle ON check OPEN at present position I ENGINE RUNNING ROUGHLY 1 Oil Temperature check 2 If Oil Pressure drops below Green Arc but Oil Temperature is normal land at nearest airfield II LOSS OF OIL PRESSURE If Oil Pressure drops below Green Arc and Oil Temperat...

Page 46: ... and emergency landing II LOSS OF FUEL PRESSURE 1 As long as the airspeed V is at least 54 kts 62 mph 100 km h the propeller will continue to windmill IAS 3 5 7 Airspeed VIAS Propeller Speed Control Lever Ignition Switch Throttle 70 kts 81 mph 130 km h max RPM BOTH 3 4 in 2 cm forward 2 4 6 Wing Flaps Fuel Shut off Valve Electric Fuel Pump T O Position OPEN ON IV RESTARTING THE ENGINE WITH PROPELL...

Page 47: ...Switch Battery Fuel Shut off Valve Throttle ON OPEN IDLE After successful re start 9 11 Oil Pressure Electrically Powered Equipment check ON if required 10 Choke OFF Cold Start 3 4 in 2 cm forward Warm Start 7 Choke ON pulled Cold Start OFF Warm Start 8 Ignition Switch START NOTE The engine may also be re started by increasing the airspeed by pushing the airplane into a descent and accelerating to...

Page 48: ...Switch Battery secured OFF EMERGENCY PROCEDURES 65 kts 75 mph 120 km h b Precautionary Landing with Engine Power Available 1 Search for a suitable place to land Special attention must be given to wind direction and obstacles in the approach path 2 Safety Belts secured 3 5 Initiate Descent Trim as required 4 6 Throttle Wing Flaps observe permissible speed as required as required NOTE A precautionar...

Page 49: ...bstacles DA20 100 Katana 4X Manual EMERGENCY PROCEDURES Neither the software nor the documentation may be used for real aviation and training purposes 03 07 page Throttle Propeller Speed Control Lever Carburetor Heat Electric Fuel Pump Wing Flaps 57 kts 66 mph 106 km h Airspeed VIAS 13 Touch down is to be made with minimum airspeed nose wheel should be kept above ground as long as possible 14 Afte...

Page 50: ...4 Ignition Switch OFF EMERGENCY PROCEDURES CAUTION If fire extinguisher is used the cabin must be aerated b Engine Fire during Flight 1 Fuel Shut off Valve 2 Airspeed VIAS 70 kts 81 mph 130 km h CLOSED 3 5 7 Flaps Electric Fuel Pump Perform emergency landing with engine off according to paragraph 3 3 2 T O 4 6 Throttle Cabin Heat FULL OFF CLOSED c Electrical Fire including Smoke during Flight 1 Ma...

Page 51: ...re including Smoke on the Ground 1 Master Switch Battery 2 3 Cabin Air Fire Extinguisher OPEN deploy as required OFF 3 5 Cabin Heat Land as soon as possible CLOSED 8 Radio 7 9 Avionics Master Switch Land as soon as possible ON ON In case the fire is extinguished and electric power is required for continuation of the flight 1 Master Switch Battery OFF If engine running 2 3 4 5 6 Throttle Fuel Shut ...

Page 52: ...ange of altitude or change of flight direction to reach area with higher outside air temp 2 Continue to move control surfaces to maintain their moveability 3 5 Carburetor Heat Cabin Heat ON OPEN 4 Increase RPM to avoid icing of propeller blades observe maximum RPM CAUTION In case of icing on the leading edge of the wing the stall speed will increase CAUTION In case of icing on wing leading edge er...

Page 53: ...ected during final rolling Land with wing slightly tipped in the direction of the non defective tire To increase the maneuvrability during rolling the nose wheel should be brought to the ground as soon as possible after touch down 2 Rudder fully applied opposite to direction of spin IDLE 3 5 Control Stick Wing Flaps ease forward 4 6 Rudder Elevator neutral after rotation has stopped UP pull cautio...

Page 54: ...nd by 1968 ft 0 6 km The glide distance from 1000 ft altitude decreases for each 10 kts head wind by 2296 ft 0 7 km 3 3 9 ELECTRICAL POWER FAILURE a Total Electrical Power Failure 1 Battery Circuit Breaker 2 Master Switch Gen Battery check ON 3 If unsuccessful Land at nearest suitable airport If tripped reset GEN Annunciator Illuminated b Generator Failure 1 2 3 4 Master Switch Generator Gen Circu...

Page 55: ...le remains in the yellow arc and the ammeter is indicating to the left of centre discharge Increase RPM until needle is in the Green Arc This should occur before exceeding 1350 RPM Discontinue any planned flight activity 2 Non flight essential electrical consumers Switch OFF consumers until needle is in the Green Arc 1 II LOW VOLTAGE INDICATION NEEDLE IN YELLOW ARC DURING FLIGHT 1 All non flight e...

Page 56: ...ll positions of the flap toggle switch flap stops are fail safe raise approach speed by 5 kts modify approach and landing as follows After landing proceed in accordance with paragraph 3 3 9 c WARNING If at any time the Voltmeter needle indicates in the red arc you should land at the nearest suitable airfield and service the aircraft accordingly before continuing the flight 3 3 10 FLAP SYSTEM FAILU...

Page 57: ...NICS SYSTEM FAILURE TOTAL AVIONIC FAILURE 1 Avionic Master Circuit Breaker If tripped re engage and monitor status If it trips again land at nearest suitable airport 2 Avionic Master Switch Toggle avionic master switch if avionic system remains off line pull avionic master control circuit breaker and land at nearest suitable airport RADIO SYSTEM OPERATIVE NO RECEPTION 1 Microphone Key check for st...

Page 58: ...onal regulations 3 3 13 TRIM SYSTEM FAILURE STUCK TRIM 1 Circuit breaker check reset if it is tripped depress in both directions wait 5 minutes try again 2 Rocker switch NOTE Full range of travel is available for elevator but expect forces up to 20 lbs on control stick 3 Land at nearest suitable airport RUNAWAY OF TRIM 1 Control Stick Grip stick and maintain control of airplane Pull circuit breake...

Page 59: ...sful NOTE With propeller speed control lever at least inch 10mm aft of full forward position the Max Permissible Continuous RPM 2260 RPM cannot be exceeded at any throttle setting and airspeed However maximum engine power may not be available Expect electrical power failure Ref 3 3 9 3 3 15 TACHOMETER FAILURE 1 Airspeed Do not exceed 110 KIAS Operation at T O 5 minute power 1 Propeller Speed Contr...

Page 60: ...l aviation and training purposes 04 01 4 0 NORMAL OPERATION Chapter 3 of this Flight Manual deals with normal operating procedures and contains checklists and descriptions how to operate the aircraft 4 1 INTRODUCTION page DA20 100 Katana 4X Manual NORMAL OPERATION ...

Page 61: ...ed crosswind speed during take off and landing Maximum permissible speed with Wing Flaps extended VFE DA20 100 Katana 4X Manual NORMAL OPERATION Neither the software nor the documentation may be used for real aviation and training purposes 04 02 page Unless stated otherwise the following table contains the applicable airspeeds for maximum take off and landing weight The airspeeds may also be used ...

Page 62: ...t in the seat shell backs At temperatures below the 55 C 131 F limit the indicator appears all red with a faint indication of 55 C At temperatures exceeding the 55 C 131 F limit the indicator displays a clearly contrasting red 55 C on a black background NOTE FSX OPERATION At temperatures approaching the limit the background will progressively darken prior to turning black this indicates acceptable...

Page 63: ...uctural Temp does not exceed 55 C 131 F removed pulled out free 2 4 6 8 Airplane Documents Flight Controls Carburetor Heat Choke check check for proper direction of movement free OFF free self resetting 9 11 Parking Brake Propeller Speed Control Lever free free max RPM 10 12 Throttle Master Switch Battery free IDLE ON 13 15 Warning Lights Gen Fuel Press and Canopy Engine Gauges Ammeter and Voltmet...

Page 64: ...cator Lights Master Switch Battery Emergency Locator Transmitter ELT EBC Model 502 EBC Model 102A NEUTRAL operational and dimmable OFF OFF ARM 20 22 24 26 Wing Flaps Indicator and Flap Actuation Exterior Lights Foreign Object Inspection Fire Extinguisher check extend and retract fully operational as required done check 27 Baggage stowed baggage net attached 28 Canopy clean undamaged ...

Page 65: ...Neither the software nor the documentation may be used for real aviation and training purposes 04 06 page DA20 100 Katana 4X Manual NORMAL OPERATION II Walk Around Check and Visual Inspection ...

Page 66: ...o removing wheel chocks 1 Left Main Landing Gear a Landing Gear Strut b Wheel Fairing visual inspection visual inspection c e Tire Pressure 33 psi 2 3 bar Wheel Chocks check remove d Tire Wheel Brake visual inspection 2 Left Wing a Entire Wing b f Stall Warning Wing Tip Position Lights and Strobe check suck on opening visual inspection c g e i Pitot Static Probe Aileron Balancing Weight Taxi and L...

Page 67: ...nspection d Fuel Quantity visual inspection use fuel pipette 4 Empennage a Stabilizers and Control Surfaces b Tie down remove visual inspection c Trim Tabs visual inspection 5 Right Wing a Entire Wing b f Wing Flap including Inspection Panel Tie down visual inspection visual inspection c e Aileron including Inspection Panel Wing Tip Position Lights and Strobe visual inspection remove visual inspec...

Page 68: ...ction 7 Nose a Oil b g f k Cowling Nose Gear Spinner Wheel Chocks visual inspection visual inspection check level by using dip stick min max range is indicated by flat area of stick c h e j Air Intakes five Wheel Fairing Propeller Blades Tire and Wheel free visual inspection towbar removed visual inspection remove perform Pitch Check by Hand visual inspection d i Propeller Tire Pressure 26 psi 1 8...

Page 69: ...9 11 Throttle Friction Device of Throttle Quadrant IDLE adjust 10 12 Propeller Speed Control Lever Avionics Master Switch max RPM OFF 13 15 Master Switch Battery Generator Fuel Pressure Warning Light ON illuminated 14 16 17 18 19 Generator Warning Light Exterior Lights Instrument Panel Lighting Canopy Canopy Locking Warning Light illuminated as required as required Close and Secure OFF NOTE Under ...

Page 70: ...Light Propeller Area Choke OFF Clear OFF 9 Throttle maximum 1500 RPM 10 Oil Pressure within green range after maximum of 10 seconds NOTE NOTE Extremely low temperatures require that the engine be preheated prior to engine start Satisfactory engine starts have been demonstrated at 31ºF 35ºC OAT after a 2 hour preheat with the TannisTAS100 27 preheat system During extremely cold weather starts hold ...

Page 71: ...ssure may advance to the yellow arc until Oil Temp reaches normal operating temperatures Activate starter for max 10 sec only followed by a cooling period of 2 min 4 4 4 BEFORE TAXIING 1 3 5 4 Avionics Master Switch Engine Gauges Warning Lights Gen Fuel Press Canopy Voltmeter ON check push to test check ensure needle is in the green arc Increase RPM to achieve or turn OFF non flight essential elec...

Page 72: ...r RPM the propeller may be damaged by loose sand gravel or water 4 4 6 BEFORE TAKE OFF ENGINE RUN UP 1 3 6 8 9 4 Toe Brakes Canopy Fuel Quantity Indicator Trim Controls Fuel Pressure Warning Light hold closed and locked check NEUTRAL free OFF If light illuminates maintenance action is required and flight should not be initiated 2 5 7 Safety Belts Fuel Shut off Valve Engine Gauges fastened check OP...

Page 73: ... DA20 100 Katana 4X Manual DA20 100 Katana 4X Manual NORMAL OPERATION 13 14 Throttle Carburetor Heat 1500 RPM ON RPM drop max 50 RPM 15 16 17 19 18 20 Throttle Carburetor Heat Circuit Breakers Wing Flaps Electric Fuel Pump Parking Brake IDLE OFF check pressed IN T O ON release 4 4 7 TAKE OFF 1 5 3 7 4 Electric Fuel Pump Wing Flaps Ignition Switch Throttle Check RPM Carburetor Heat check ON check T...

Page 74: ...t using the brakes for directional control increases the take off roll distance 10 11 Rotate VIAS Climb Speed VIAS 51 kts 59 mph 95 km h 57 kts 66 mph 106 km h CAUTION CAUTION For the shortest possible take off distance to clear a 15 m 50 ft obstacle Lift off Speed VIAS Climb Speed VIAS 54 kts 62 mph 100 km h 57 kts 66 mph 106 km h 12 13 Propeller Speed Control Lever Electric Fuel Pump 2260 RPM af...

Page 75: ... decreases with increasing altitude Electric fuel pump ON above 13 000 ft 4 4 8 CLIMB 1 3 5 4 6 Propeller Speed Control Lever Engine Gauges Airspeed Wing Flaps Trim 2260 RPM within green range 65 kts 75 mph 120 km h T O adjust 2 Throttle FULL Speeds VIAS kts mph km h 69 79 128 65 75 120 0 4000 7000 10 000 4000 7000 ALTITUDE feet kts mph km h 65 75 120 63 73 117 62 71 115 Flaps T O Flaps UP 7000 10...

Page 76: ...r to Chapter 5 Electric fuel pump ON above 13 000 ft To achieve a fast descent 4 4 9 CRUISE 1 Throttle as required 2 Propeller Speed Control Lever 1700 2260 RPM 3 Wing Flaps UP 4 Trim as required 5 Engine Gauges check 4 4 10 DESCENT 1 3 Flight Instruments and Avionics Propeller Speed Control Lever adjust 1700 2260 RPM 2 4 Throttle Carburetor Heat as required as required Propeller Speed Control Lev...

Page 77: ...ises suspect carburetor icing and leave Carb Heat ON Otherwise turn Carb Heat OFF Wing Flaps UP Airspeed 118 kts 135 mph 218 km h 4 4 11 LANDING APPROACH 1 3 5 Seat Belts Lights Ignition Switch fastened as required check BOTH 2 4 6 Electric Fuel Pump Master Switch Battery Generator Carburetor Heat ON check ON ON 5 6 7 9 Throttle Wing Flaps as required T O 8 10 Airspeed Trim max 81 kts 93 mph 150 k...

Page 78: ...lence a higher approach speed should be selected 4 4 12 4 4 13 4 4 14 BALKED LANDING AFTER LANDING ENGINE SHUT DOWN 1 1 1 3 3 3 5 5 Propeller Speed Control Lever Throttle Throttle Carburetor Heat Carburetor Heat ELT Airspeed Electric Fuel Pump max RPM as required IDLE OFF OFF Check by listening to 121 5 MHZ for signal 57 kts 66 mph 106 km h OFF 2 2 2 4 4 Throttle Wing Flaps Parking Brake Wing Flap...

Page 79: ...heel Chocks as required 8 Master Switch Battery OFF NOTE In case of post ignition due to hot weather conditions the ignition should be switched on choke pulled and after approximately 3 seconds ignition should be turned off again 4 4 15 Flight in Rain NOTE Flight performance might be reduced especially for the T O distance and the maximum horizontal air speed The influence on flight characteristic...

Page 80: ...5 7 9 Loose Items Altitude and Airspace Wing Flaps Throttle Reduce speed with elevator stowed check UP IDLE speed reduction rate 2 3 kts sec 2 4 6 8 10 Seat Belts Electric Fuel Pump Carburetor Heat Entry Speed When stall warning sounds fastened OFF ON trim to 65 kts 75 mph 120 km h apply simultaneously full aft stick and full rudder a Spin Entry CAUTION Intentional spinning is only permitted with ...

Page 81: ...e 1 3 5 Throttle Control Stick Wing Flaps IDLE ease stick forward until spinning stops check UP 2 4 6 Rudder Rudder Control Stick fully applied opposite to direction of spin neutral immediately after rotation has stopped ease stick backward cautiously Bring airplane from descent into level flight position Do not exceed maximum permissible speed VNE b Recovery from Spinning ...

Page 82: ...mance tables do not take into account the expertise of the pilot or the maintenance condition of the airplane The performance illustrated in the tables can be achieved if the indicated procedures are followed and the airplane is in good maintenance condition Note that the flight duration data does not include a fuel reserve The fuel consumption during cruise is based on propeller RPM and manifold ...

Page 83: ...d for real aviation and training purposes 05 02 page PERFORMANCE The performance data is shown in the form of tables and diagrams to illustrate the influence of the different variables These tables contain sufficiently detailed information to plan any flight with the necessary precision and safety on the conservative side ...

Page 84: ...P VIAS kts VCAS kts Example v 93 kts equals v 95 kts IAS CAS 5 3 PERFORMANCE TABLE AND DIAGRAMS DA20 100 Katana 4X Manual PERFORMANCE Neither the software nor the documentation may be used for real aviation and training purposes 05 03 page 5 3 1 AIRSPEED SYSTEM CALIBRATION Assumes zero indicator error ...

Page 85: ...19 19 20 21 22 22 6 22 6 24 7 24 0 23 3 22 0 21 0 19 7 18 0 17 0 13 6 14 4 15 6 16 8 18 0 19 2 20 4 21 5 3 6 3 8 4 1 4 4 4 8 5 1 5 4 5 7 20 20 21 22 22 22 6 25 7 24 7 23 3 22 7 21 7 20 3 15 6 16 0 16 8 19 6 21 2 22 4 4 1 4 2 4 4 5 2 5 6 5 9 Pressure altitude Standard Temp 75 85 Ft M C F RPM X100 MP In Hg Fuel Flow L hr Gal hr RPM X100 MP In Hg Fuel Flow L hr Gal hr 0 2000 4000 6000 8000 0 600 1200...

Page 86: ...5 37 33 41 47 49 52 59 62 Stall speeds in kts Flaps UP T O LDG Bank Angle 0 30 45 60 IAS CAS IAS CAS IAS CAS IAS CAS 47 57 53 62 63 68 79 81 45 52 51 56 59 62 72 75 43 50 47 54 56 60 68 72 Stall speeds in mph Flaps UP T O LDG Bank Angle 0 30 45 60 IAS CAS IAS CAS IAS CAS IAS CAS 76 93 85 99 101 109 127 130 72 84 81 91 94 100 117 120 69 81 76 87 91 96 109 115 Stall speeds in km h Configuration Idle...

Page 87: ...5 20 0 10 20 30 40 160 150 140 130 120 170 HEADWIND COMPONENT 10 0 10 20 30 km h kts 0 10 20 30 0 5 10 15 20 km h kts 50 60 70 80 90 100 110 FLIGHT DIRECTION max demonstrated crosswind a n g l e b e t w e e n w i n d a n d f l i g h t d i r e c t i o nw i n d s p e e d i n k t s Example Wind speed Angle between wind direction and flight direction Headwind component Crosswind component 11 kts 20 km...

Page 88: ... 800 700 600 500 400 300 200 m ft 3200 2200 1200 3000 2000 1000 2800 1800 800 2600 1600 2400 1400 Take Off Distance Example Pressure altitude 3000 ft Outside temperature 15 C 59 F Weight 725 kg 1598 lbs Wind 10 kts Result Take Off roll distance 312 m 1025 ft Take Off distance to clear a 15 m 50 ft obstacle 434 m 1425 ft DA20 100 Katana 4X Manual PERFORMANCE 5 3 5 TAKE OFF DISTANCE Conditions Maxim...

Page 89: ...ep 10 increase in take off roll distance Grass 5 to 10cm 2 to 4in deep 15 increase in take off roll distance Grass deeper than 10cm 4in 25 increase in take off roll distance On wet soft grass covered runways with grass deeper than 10cm 4in the take off roll distance might be increased by as much as 40 This information is provided for guidance purposes only and has not been demonstrated The dashed ...

Page 90: ...kg Temperature C 20 10 0 10 20 30 Pressure Altitude ft 0 2000 2000 4000 6000 8000 10000 12000 14000 16000 18000 4 14 32 50 68 86 Temperature F Standard Temperature 4 6 900 1000 1653lbs 750kg Example PressureAltitude 5000 ft 1524 m OAT 46 F 8 C Weight 1477 lbs 670 kg Result Climb performance 554 ft min 2 82 m s CAUTION In case of operation without wheel fairings the climb performance is reduced by ...

Page 91: ... In case of operation without wheel fairings the maximum cruising speed is reduced by approximately 5 Neither the software nor the documentation may be used for real aviation and training purposes 05 10 page Temperature C 20 10 0 10 20 30 Pressure Altitude ft 0 2000 2000 4000 6000 8000 10000 12000 14000 4 14 32 50 68 86 Temperature F 95 170 180 190 200 210 220 230 240 250 True Airspeed km h True A...

Page 92: ...erve 2 11 h min Possible flight time with reserve of 45 mins 1 26 h min Neither the software nor the documentation may be used for real aviation and training purposes 05 11 page 80 70 60 50 40 30 20 10 0 1 2 3 4 5 6 0 4 8 12 16 20 6 0 0 m 2 0 0 0 f t Fuel quantity in litres Flight time hour no reserve 1800m 6000ft 1200m 4000ft 600m 2000ft 1800m 6000ft 1200m 4000ft 600m 2000ft 95 75 55 Fuel quantit...

Page 93: ...sult Climb performance during balked landing 320 ft min 1 63 m sec CAUTION In case of operation without wheel fairings the climb performance is reduced by approximately 3 Neither the software nor the documentation may be used for real aviation and training purposes 05 12 page 2000 1000 0 3000 4000 5000 6000 7000 8000 9000 10000 PRESSURE ALTITUDE Hp ft 0 500 1000 1500 2000 2500 3000 PRESSURE ALTITU...

Page 94: ...5 ft m 748 228 770 235 793 242 817 249 842 257 868 265 NOTE Poor maintenance condition of the airplane deviation from the given procedures as well as unfavourable outside conditions high temperature rain unfavourable wind conditions including cross wind could increase the landing distance considerably For landings on dry short cut grass covered runways the following corrections must be taken into ...

Page 95: ...ation and training purposes 05 14 page DA20 100 Katana 4X Manual PERFORMANCE 5 4 NOISE DATA a Noise limit according to FAR 36 Appendix G 75 0 dB A Noise value measured 63 8 dB A b Noise limit according to ICAOAnnex 16 Chapter 10 79 1 dB A Noise value measured 71 7dB A ...

Page 96: ...may be used for real aviation and training purposes 07 01 7 0 DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS 7 1 INTRODUCTION page DA20 100 Katana 4X Manual DESCRIPTION This Chapter provides description and operation of the airplane and its systems ...

Page 97: ...and flaps are made from CFRP and are attached to the wings using aluminum hinges The wing fuselage connection is made with three bolts each The so called A and B bolts are fixed to the fuselage s root rib The A bolt is placed in front of the spar tunnel the B bolt lies near the trailing edge The two main bolts are placed in the middle of the spar tunnel main bulkhead They are accessible between th...

Page 98: ...ons up UP take off T O and landing LDG and are electrically operated The switch is located on the instrument panel In addition the flap control circuit is provided with a manually triggerable circuit breaker Elevator forces may be balanced using the electric trim system The flaps are driven by an electric motor The flaps are controlled by a three position flap operating switch on the instrument pa...

Page 99: ... illuminated at the same time the flaps are between these two positions This is the case while the flaps are in motion The pedals for rudder and brakes are unlocked by pulling the T grip located on the rudder pedal sled aft pedestal Forward adjustment Push both pedals forward with your feet while pulling theT grip Backward adjustment Pull pedals backward to desired position by pulling onT grip 7 3...

Page 100: ...should be installed whenever the aircraft is parked 7 3 5 FLIGHT CONTROL LOCK NOTE Failure to install the flight control lock whenever the aircraft is parked may result in control system damage due to gusts or turbulence FSX The Flight Control Lock red band is stored in the baggage compartment if not applied to the controls and can be used by a click with the mouse Another click will move it back ...

Page 101: ...meter Annunciator Lights Map Light Switch CDI Hobbs Meter Trim Ind Dimmer Stall Warning Horn GPS Unit Carb Heat Knob Turn and Bank Ind Radio Choke Knob Directional Gyro Transponder Cabin Heat Knob Vertical Speed Ind Not Used Parking Brk Knob Not used Intercom Power Lever Microphone Jack Manifold Pressure Prop RPM Lever Air Vent Tachometer Lever Tension Fuel Pump Switch Oil Pressure Ind Trim Switch...

Page 102: ...eat knob located in front of the center console is used to regulate the flow of heated air Knob pulled cabin heat ON 7 4 2 CABIN HEAT The cabin aeration is controlled by two adjustable air vent nozzles The two sliding windows in the canopy can be opened for additional ventilation 7 4 3 CABIN AIR 7 5 LANDING GEAR SYSTEM The landing gear system consists of the two main landing gear wheels mounted to...

Page 103: ... pilot s brakes fail too The same applies to a failure on the co pilot s side in this case also the pilot s brakes fail CAUTION When placing the feet on the brake pedals care should be taken to not contact the structure above the pedals which could prevent effective application of the brake s 7 5 2 PARKING BRAKE The knob is located on the center console in front of the throttle quadrant and is pus...

Page 104: ...ent loose objects to foul the controls The seats are equipped with removable cushions Manually triggered seat type parachutes may be used instead of cushions For automatically triggered parachutes it is possible to install suitable fastening loops on the A bolts under the seats Every seat is equipped with four point safety belt The locking of the safety belt occurs by slipping the lap belt through...

Page 105: ...outside LH side by sliding the locking handle backward and pulling the emergency release lever forward to a stop and lifting up To lock Push both LH and RH locking handles forward To unlock Pull both LH and RH locking handles backwards Neither the software nor the documentation may be used for real aviation and training purposes 07 10 page DA20 100 Katana 4X Manual DESCRIPTION 7 8 CANOPY CAUTION B...

Page 106: ...ot s side The ignition switch is present in form of a key switch The ignition is turned on by turning the key to position BOTH The starter is operated by further turning against spring load to the right position START The engine is shut off by the ignition switch Due to the backlash in the reduction gear the propeller can be easily turned approximately 30 by hand Sudden throttle movements should b...

Page 107: ...opeller Pitch Control Lever Lever with blue notched knob right of throttle Lever forward max RPM fine pitch Lever rearward min RPM coarse pitch also see page 7 10 Small black knob below the center instrument panel self resetting Knob pulled choke ON 7 9 3 CHOKE The HO V352F Hoffmann Propeller is used on the DA 20 100 KATANA The infinitely variable pitch is hydraulically controlled by a Woodward Go...

Page 108: ... keeps the selected RPM constant regardless of airspeed or throttle setting If the engine power level selected with the throttle is insufficient to keep the selected RPM constant the propeller blades will move to the smallest possible pitch The propeller governor is mounted on the engine It is driven directly by the engine The propeller governor oil circuit is part of the engine oil circulation sy...

Page 109: ...he process is finished when crankcase air can be heard being forced back to the oil tank The sound will be noticed as a gurgle coming from the oil tank with the oil cap removed The sound verifies that the crankcase has been purged of residual oil Remove the oil dip stick clean and reinsert Let the oil dip stick sit for a few seconds then remove verifying the oil level is in the middle of the level...

Page 110: ...ller on the left side of the fuselage behind the canopy is connected to the tank with a rubber hose The tank vent line runs from the filler connection piece through the fuselage bottom skin to the exterior of the airplane Afinger filter is installed at the bottom of the tank From there the fuel is fed to the electric fuel pump and from there through the middle tunnel to the fuel shut off valve Fro...

Page 111: ...e fuel filler cap WARNING The fuel shut off valve should only be closed during engine fire or fuel system maintenance After reopening the locking detent should be checked to ensure it performs the proper safety function Otherwise the danger of operating the airplane with the fuel shut off valve closed engine failure is possible 7 10 2 TANK DRAIN 7 10 3 FUEL PIPETTE NOTE Electric fuel gauges may ma...

Page 112: ...the generator circuit breaker 50Amps Both circuit breakers can be triggered manually The generator warning light is activated by the voltage regulator monitoring circuit and illuminates when the generator is not charging the battery 7 11 1 POWER SUPPLY The engine is provided with two independent ignition systems The two magnetos are independent from the power supply system and are in operation as ...

Page 113: ...ion 7 4 for a illustration of the instrument panel 7 11 3 ELECTRICAL POWERED EQUIPMENT The voltmeter indicates the status of the electrical bus It consists of a dial that is marked numerically from 8 16 volts in divisions of 2 The scale is divided into three colored arcs to indicate the seriousness of the bus condition These arcs are Red for 8 0 11 0 volts Yellow for 11 0 12 5 volts Green for 12 5...

Page 114: ...onsequently the needle deflection to change Oil pressure indicator cylinder head temperature indicator and fuel pressure warning light are supplied with power through one circuit breaker Oil temperature indicator and fuel quantity indicator are also protected together by one circuit breaker 7 11 8 INSTRUMENTS 7 11 9 INTERNAL LIGHTING ON OFF INSTRUMENT PANEL LIGHT MAP LIGHT The internal lighting of...

Page 115: ...he aircraft is parked to prevent contamination and subsequent malfunction of the aircraft systems relying on its proper functioning 7 13 STALL WARNING SYSTEM When the airspeed drops below 1 1 times the stall speed a horn sounds in the left instrument panel The horn grows louder as the speed approaches the stall speed The horn is activated by suction on a hose that leads from a hole in the leading ...

Page 116: ...Neither the software nor the documentation may be used for real aviation and training purposes 09 01 9 0 AVIONICS page DA20 100 Katana 4X Manual AVIONICS ...

Page 117: ... channels within a 25 kHz raster Frequency range for navigation from 108 00 to 117 95 MHz consists of 200 VOR LOC channels within a 50 kHz raster The COM NAV unit is mounted in the center instrument panel the communications antenna on the vertical tail and the antenna for navigation within the elevator Both the navigation and the communication part of the unit feature two frequencies One active an...

Page 118: ...d with the Instruments Light switch on the center console 9 1 5 TURNING ON Turning the ON OFF Volume knob out of the OFF position will engage the radio The unit will be instantly be operational displaying the frequencies that have been set before 9 1 6 TUNING Turning the COM and NAV rotaries will set the standby frequencies The larger rotary will set the frequency in 1 MHz steps the smaller one in...

Page 119: ...The NAV volume knob can be pulled to enable the identification of the tuned station via morse code 9 1 8 OPERATION MODES If a VOR frequency has been tuned as active frequency the NAV mode button can be used to cycle the three available modes for Nav information window Course Deviation Indicator CDI Bearing BRG Radial RAD When the unit has been switched on CDI is the default mode CDI MODE While ope...

Page 120: ...l be displayed Instead the TO marker will appear and a three digit number will indicate the direct bearing direction to the station In the case the unit does not receive a signal three dashes will be displayed instead of the bearing digits RAD MODE Selecting the Radial mode allows radial from information to be shown Neither the course deviation indicator nor OBS will be displayed Instead the FR ma...

Page 121: ...e will be displayed OBS TO and FR markers will be hidden and the OBS windows displays the LOC marker If the unit receives a signal the deviation will be indicated by the vertical bars If there is no signal all bars will be shown and the FLAG marker will appear NOTE Power surges at engine startup can damage the avionic devices So it is necessary to ensure the avionic to be switched off before start...

Page 122: ...urposes 09 07 page 9 1 9 FSX OPERATION Left and Right Drag Turn knob left and right COMM Volume Pull Test Knob Left and Right Drag Turn knob left and right NAV Volume Pull Ident Knob 188 88 188 88 188 88 188 88 888 OBS FLAG TO FR KX TSO COMM 125 OFF PULL TEST PULL 25K MODE IDENT PULL S B Y S B Y NAV PULL OBS 0 0 COMM Frequency Selection Knobs NAV Frequency Selection Knobs Left Turn knob left Right...

Page 123: ... the software nor the documentation may be used for real aviation and training purposes 09 08 page Left Push knob in Right Pull knob out All marked knobs can be pulled out or pushed in by a click on the faceplate 188 88 188 88 188 88 188 88 888 OBS FLAG TO FR KX TSO COMM 125 OFF PULL TEST PULL 25K MODE IDENT PULL S B Y S B Y NAV PULL OBS 0 0 Left Press and or hold buttons ...

Page 124: ...e Bendix King KT76A is a radio transmitter and receiver working on the basis of radar frequencies It receives radar signals from ground stations at 1030 MHz and send them back Encoding in the range from 0000 to 7777 results in 4096 possible combinations The KT76Atransponder unit is mounted in the center instrument panel The antenna is placed at the bottom of the fuselage between the wings 9 2 3 PR...

Page 125: ... about 60 seconds in SBY mode for warming up and stabilizing the radio tube Skipping the SBY knob position will not reduze the warming time a Turn and hold mode selector knob to the TEST position The Reply light should illuminate b Return mode selector knob to the SBYposition c NOTE The coding switches shall only be operated in SBY mode to avoid the accidently setting and transmitting of an emerge...

Page 126: ...To extend the life time of the transponder it should be switched off while starting up or shutting down the engine These operations could lead to voltage peaks in the on board power supply that may damage the device NOTE The coding switches shall only be operated in SBY mode to avoid the accidently setting and transmitting of an emergency code The transponder shall not be operated with code number...

Page 127: ...ation and training purposes 09 12 page OFF ON SBY ALT TST IDENT KT76A 0 0 0 0 Left Turn knob left Right Turn knob right Mode Selector TST position is springloaded Coding Switches Up Turn knob right Down Turn knob left The transponder integrated lighting is linked to the instrumentation lighting and is toggled with the switch on the center console 9 2 10 LIGHTING NOTE The warming of the radio tube ...

Page 128: ...tion For operation instructions please refer to the FSX documentation 9 3 2 DESCRIPTION 9 3 3 PROTECTION The GPS circuit breaker protects the on board power supply from high voltage in the case of a short circuit 9 3 4 HANDLING Engage main battery generator and avionic switches switched off on and dimmed with the master knob Integrated lighting can be switched with the Instruments Light switch on ...

Page 129: ...OC D MENU CLR ENT RNG GPS500 DEFAULT NAV GPS C 9 2 9 FSX OPERATION Left and Right Drag Decrease increase brightness and turn on off the GPS unit Master Knob Rotaries Button The smaller rotary can be pressed by a click on the faceplate Left Turn knob left Right Turn knob right Up Turn knob right Down Turn knob left Buttons All buttons can be pres sed by a left click ...

Page 130: ...d to the main bus and will be operative as soon as the master switch is enganged Three buttons are available for operation and settings O A T VOLTS SELECT CONTROL 14 3E 03 1 1 UT FT LT ET Red button Cycle through Voltage E Outside Air Temperature Fahrenheit F and Outside Air Temperature Celsius C SEL button Selection what is displayed Universal Time UT Local Time LT Flight Time FT and Elapsed Time...

Page 131: ... the SEL button to select the LT display Press both the SEL and the CTL button at the same time to enter the set mode The tens of hours digit will start flashing Setting the time is the same as descriped at LT except that the minutes are synchronized with UTand can not be set O A T VOLTS SELECT CONTROL 14 3E 7 1 1 UT FT LT ET 9 5 5 SETTING FLIGHT TIME ALERT Use the SEL button to select the FT disp...

Page 132: ... will then be switched to hours and minutes counting up to 99 hours and 59 minutes Pressing the CTL button again will reset ETto zero O A T VOLTS SELECT CONTROL 14 3E 2 50 UT FT LT ET 9 5 8 ELAPSED TIME COUNT DOWN Use the SEL button to select theET display Press both the SEL and the CTL button at the same time to enter the set mode A countdown from a maximum of 59 minutes and 59 seconds can be set...

Page 133: ... T VOLTS SELECT CONTROL 88 88 88 88 UT FT LT ET 9 5 10 OAT AND VOLTAGE Pressing the red button will cycle through E F and C displays Voltage will always be displayed when the clock is powerd up O A T VOLTS SELECT CONTROL 71F 2 50 UT FT LT ET 9 5 11 FSX OPERATION O A T VOLTS SELECT CONTROL 14 3E 0 0 1 UT FT LT ET 0 0 Left Right Press or hold the button until release The button will be hold for 3 se...

Page 134: ...Neither the software nor the documentation may be used for real aviation and training purposes 10 01 10 0 PAINTKIT page DA20 100 Katana 4X Manual PAINTKIT ...

Page 135: ...een the basis for all Katana paintings adding color and details with different layers and blending modes MF_DA20_EXT_FUS_000 bmp Cowling spinner propeller and wheel fairings MF_DA20_EXT_FUS_001 bmp Left fuselage and details MF_DA20_EXT_FUS_002 bmp Right fuselage and details Letterings has to be mirrored MF_DA20_EXT_FUS_003 bmp Elevator MF_DA20_EXT_WNG_001 bmp Both wings The lightly shaded sides or...

Page 136: ...raft ID and some more labels in german and english There are 4 position frames at the top for the aircrafts ID label Every frame stands for another position on the panel and you can choose which one to use Don t forget to create an alpha mask for all lettering objects and export as psd file The alpha channel is used for transparency 10 3 CONVERTING FILES Once the graphical work has been completed ...

Page 137: ... DA20 100 Katana folder NOTE If the nose or tail of your repaint are just white it is not necessary to copy MF_DA20_EXT_FUS_000 dds and MF_DA20_EXT_FUS_003 dds into the folder of your livery Missing textures in your folder will be loaded from the main texture folder This will keep filesizes small If you want to have german panel labeling even the MF_DA20_INT_PNL_001 dds does not have to be in your...

Page 138: ...n menu in FSX and your fresh painted Katana should be ready to fly Be carefull the color could still be wet 10 6 LAST STEP As a last step you can add an image of your painting into the thumbnail jpg This picture will be shown in the aircraft selection menu 10 7 PUBLISHING You are not allowed to publish any other files than those textures and files in the texture folder of your painting You may onl...

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