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Diamond Aircraft DV 20 KATANA 100, Flight Manual

The Diamond Aircraft DV 20 KATANA 100 is a sleek and reliable aircraft perfect for training and recreational flying. Ensure you have all the necessary information for safe flying by downloading the free Flight Manual from manualshive.com. Make sure to have your manual on hand before takeoff.

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Summary of Contents for DV 20 KATANA 100

Page 1: ...tana 100 and must be carried on board at all times Scope and revision status can be found in the List of Effective Pages and in the Record of Revisions The pages identified as ACG appr in the List of...

Page 2: ...00 airplane We ask that you carefully read this Airplane Flight Manual and to pay special attention to the recommendations given A careful study of the manual will reward you with many hours of troubl...

Page 3: ...PERATING LIMITATIONS 2 EMERGENCY PROCEDURES 3 NORMAL OPERATING PROCEDURES 4 PERFORMANCE 5 MASS WEIGHT AND BALANCE I EQUIPMENT LIST 6 DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS 7 HANDLING PREVENTIVE A...

Page 4: ...g 1999 1 11 20 Aug 1999 ACG appr 4 7 20 Aug 1999 1 12 20 Aug 1999 ACG appr 4 8 20 Aug 1999 1 13 20 Aug 1999 ACG appr 4 9 20 Aug 1999 1 14 20 Aug 1999 ACG appr 4 10 20 Aug 1999 1 15 20 Aug 1999 ACG app...

Page 5: ...999 6 6 20 Aug 1999 6 7 20 Aug 1999 6 8 20 Aug 1999 ACG appr 6 9 20 Aug 1999 6 10 20 Aug 1999 6 11 20 Aug 1999 6 12 20 Aug 1999 6 13 20 Aug 1999 6 14 20 Aug 1999 6 15 20 Aug 1999 6 16 20 Aug 1999 6 17...

Page 6: ...r amended text will be indicated by a bold black vertical line in the left hand margin of a revised page Revision No and reference will be shown on the bottom of the page The airplane may only be oper...

Page 7: ...DV 20 Flight Manual Oiamond AIRCRAFT Intra Rev No Chapter Pages Date of Approval Date of Date of Signature I Initials Amendment Remarks Approval by Issue Authority Doc 4 01 20 E 20 Aug 1999 Page 0 6...

Page 8: ...GENERAL INTRODUCTION CERTIFICATION BASIS WARNINGS CAUTIONS AND NOTES THREE VIEW DRAWING OF AIRPLANE DIMENSIONS ENGINE PROPELLER FUEL LUBRICANT AND COOLANT MASS WEIGHT LIST OF ABBREVIATIONS CONVERSION...

Page 9: ...ation of optional equipment the Operation Manual of the respective vendor must be used For permissible accessories refer to the equipment list Section 6 5 1 2 CERTIFICATION BASIS The basic version of...

Page 10: ...ervation of the corresponding procedure leads to an immediate or important degradation of the flight safety CAUTION means that the non observation of the corresponding procedure leads to a minor or to...

Page 11: ...DV 20 Flight Manual Diamond AIRCRAFT General 1 4 THREE VIEW DRAWING OF AIRPLANE 23 ft 10 6 in I I I I I I 5ft 8 9 in I I I I I I 3 2 in 6 ft 2 8 in 35 ft 4 3 in I Doc 4 01 20 E I 20 Aug 1999 1 4...

Page 12: ...ABILIZER Area Rudder Area LANDING GEAR Track Wheelbase Nose wheel Main wheel IDoc 4 01 20 E I Diamond AIRCRAFT 10 78 m 35 ft 4 3 in 10 84 m 35 ft 6 7 in 7 28 m 23 ft 10 6 in 1 76 m 5 ft 9 3 in Wortman...

Page 13: ...POWER AT 1 7 PROPELLER 2 43 1 1 352 liters 82 5 cu in 73 5 kW 100 HP 5800 RPM engine RPM Two bladed variable pitch propeller manufactured by HOFFMANN model HO V352F 170FQ or model HO V352F C170FQ Cons...

Page 14: ...clutch during normal operation Heavy duty 4 stroke motor cycle oils meet all the requirements These oils are usually no mineral oils but semi or fully synthetic oils Oils primarily used for Diesel en...

Page 15: ...ailing climatic conditions using the following table Avoid using single grade oils climatic 0C O F multi grade oils conditions 40 J tropical 30 80 0 0 II t I 20 0 0 f 60 II t N N I W W 0 oq I 0 0 10 U...

Page 16: ...SO pure water shall be used or alternatively an equivalently premixed coolant NOTE If problems are encountered with boiling after engine stop gradually increase the percentage of antifreeze concentra...

Page 17: ...ximum mass weight in baggage compartment Maximum useful load including fuel WING LOADING At maximum take off mass weight Perfonmance load at max take off mass weight IDoc 4 01 20 E I 730 kg 1609 Ibs 7...

Page 18: ...lane relative to air TAS is CAS corrected for altitude and temperature errors VA Maneuvering speed Maximum speed at which the airplane is not overstressed at full deflection of control surfaces VFE Ma...

Page 19: ...Indicated Pressure Altitude Altitude reading with altimeter set to 1013 25 mbar 29 92 inHg air pressure Pressure Altitude Altitude measured at standard pressure at MSL 1013 25 mbar 29 92 inHg using a...

Page 20: ...itude at which the maximum rate of climb is 0 5 m s 100 ftlmin e Mass and Center of Gravity Reference Datum RD Station An imaginary vertical plane from which all horizontal distances for the center of...

Page 21: ...e operated within Usable Fuel The amount of fuel available for the flight plan calculation Unusable Fuel The amount of fuel remaining in the tank determined in accordance with to the requirements of t...

Page 22: ...AIRCRAFT General 1 12 CONVERSION FACTORS LENGTH OR ALTITUDE 1 ft 0 3048 m 1 in 25 4 mm SPEED 1 kts 1 852 km h 1 mph 1 609 km h PRESSURE 1 hPa 100 N m 1 mbar 1 in Hg 33 865 hPa 1 psi 68 97 mbar IDoc 4...

Page 23: ...INDICATOR MARKINGS POWERPLANT LIMITATIONS POWERPLANT INSTRUMENT MARKINGS MISCELLANEOUS INSTRUMENT MARKINGS MASS WEIGHT CENTER OF GRAVITY PERMISSIBLE MANEUVERS MANEUVERING LOAD FACTORS OPERATING ALTITU...

Page 24: ...Civil Aviation BAZ WARNING These limitations must be complied with for all operations 2 2 AIRSPEED LIMITATIONS lAS Speed kts mph km h Remarks VA 104 120 193 Do not make full or abnupt control Maneuver...

Page 25: ...te Arc 38 81 44 93 70 150 Operating range with extended flaps Green Arc 43 117 49 135 80 217 Normal Operating Range Yellow Arc 117 161 135 185 21 7 298 Maneuvers must be conducted with caution and onl...

Page 26: ...his manual contrary to the engine manual are propeller speeds c Engine Operating Limitations Max TIO power 5 min Max permissible TIO RPM Max continuous power Max permissible continuous RPM d Oil Press...

Page 27: ...rer I Propeller Type m Propeller Diameter n Propeller Pitch at 0 75 R 0 Propeller Speed Limitations max TIO RPM max 5 min Max Continuous RPM Doc 4 01 20 E AVGAS 100LL Automotive Fuel ROZ minimum 95 oc...

Page 28: ...n Range Upper Limit Range Limit Tachometer 600 2260 RPM 2260 2385 RPM 2385 RPM Oil temperature 50 C 50 130 C 130 C indicator 122 O F 122 266 O F 266 O F Cylinder head 135 C temperature 275 O F indicat...

Page 29: ...the airplane as well as degrading of the handling characteristics and flight performance 2 8 CENTER OF GRAVITY The reference datum RD for the center of gravity CG calculation is tangent to the leadin...

Page 30: ...does not exceed 60 NOTE Aerobatics as well as flight maneuvers with bank angles of more than 60 are prohibited 2 10 MANEUVERING LOAD FACTORS Table of structural maximum permissible load factors Positi...

Page 31: ...m Equipment Flight and Navigation Instruments Airspeed Indicator Altimeter Magnetic Compass Minimum Equipment Powerplant Instruments Fuel Quantity indicator Oil Pressure indicator Oil Temperature indi...

Page 32: ...d See Flight Manual for other limitations I No smoking b In the baggage compartment Baggage max 20 kg 44 Ibs only with baggage harness NOTE For further placards refer to the Maintenance Manual Doc No...

Page 33: ...lling V Restarting The Engine With Propeller At Full Stop Emergency Landing a Emergency Landing With Engine Off b Precautionary Landing Fire a Fire On Ground b Fire During Take Off c Fire In Flight Ic...

Page 34: ...sed to rectify such problems Since it is impossible to present in the Flight Manual all emergency situations which may occur knowledge of the airplane and experience of the pilot are essential in rect...

Page 35: ...NE POWER 1 2 3 4 5 6 7 8 9 10 11 Airspeed V AS Throttle Carburetor Heat Choke Fuel Shut off Valve Ignition Switch Electric Fuel Pump Propeller Speed Control Lever 59 kts 168 mph 1 110 kmlh FULL OFF OF...

Page 36: ...emperature is normal If oil pressure drops below green arc and oil temperature is rising III LOSS OF FUEL PRESSURE 1 Electric Fuel Pump 2 If Fuel Pressure Warning Light does not extinguish Doc 4 01 20...

Page 37: ...will continue to windmill 1 Airspeed V AS 2 Wing Flaps 3 Propeller Speed Control Lever 4 Electric Fuel Pump 5 Ignition switch 6 Fuel Shut off Valve 7 Throttle 70 kts 181 mph 1130 km h T O Position ma...

Page 38: ...2 cm 3 4 in forward 6 Choke Cold Start ON pulled Warm Start OFF 7 Ignition Switch START NOTE The engine may also be re started by increasing the airspeed by pushing the airplane into a descent and ac...

Page 39: ...OTE Such a landing would only be required if reasonable suspicion of a defect of the airplane or its systems or bad weather raises doubts that the destination airfield can be reached without endangeri...

Page 40: ...buretor Heat 11 Electric Fuel Pump 12 Wing Flaps 13 Airspeed VIAS 14 Touch down is to be made with minimum airspeed nose wheel should be kept above ground as long as possible 15 After touch down Fuel...

Page 41: ...Master Switch Battery OFF 4 Ignition Switch OFF 5 Evacuate Airplane immediately II ELECTRICAL FIRE INCLUDING SMOKE ON THE GROUND 1 Master Switch If engine is running 2 Throttle 3 Fuel Shutt off Valve...

Page 42: ...on as possible bring airplane to standstill take further action as in a FIRE ON GROUND II NO SUFFICIENT RUNWAY LENGTH AVAILABLE FOR NORMAL LANDING 1 Look for a suitable field 2 Airspeed lAS 59 kts 168...

Page 43: ...AL FIRE INCLUDING SMOKE IN FLIGHT 1 2 3 4 Master Switch Battery Cabin Heat Cabin Air Fire Extinguisher OFF CLOSED OPEN use only if smoke development continues CAUTION While fire extinguisher is being...

Page 44: ...mond AIRCRAFT Emergency Procedures II CABIN FIRE IN FLIGHT 1 Master Switch Battery OFF 2 Cabin Air OPEN 3 Cabin Heat CLOSED 4 Fire Extinguisher use as required 5 Land as soon as possible Doc 4 01 20 E...

Page 45: ...ion to reach area with higher outside air temperature 2 Continue to move control surfaces to maintain their movability 3 Carburetor Heat 4 Increase RPM to avoid icing of propeller blades observe maxim...

Page 46: ...cautiously Bring airplane from descent into level flight position Do not exceed maximum permissible speed VNE NOTE Due to the excellent low speed and stability characteristics of the airplane unintent...

Page 47: ...pped in the direction of the non defective tire To increase the maneuverability during rolling the nose wheel should be brought to the ground as soon as possible after touch down 4 To ease the load on...

Page 48: ...ncreases for each 10 kts tail wind by 0 6 km 1968 tt The glide distance from 1000 tt altitude decreases for each 10 kts head wind by 0 7 km 2296 tt 3 3 9 Electrical Power Failure a GENERATOR WARNING L...

Page 49: ...1 RPM 1200 RPM 2 Landing Lights OFF 3 Position Lights OFF 4 Ammeter check 5 If the LoN caution light continues to be illuminated and the ammeter is in the left side field discontinue any planned flig...

Page 50: ...oggle switch flap stops are fail safe adapt approaching procedure to available flap position only UP available only TIO available raise approach speed by 5 kts throttle as required flat approach angle...

Page 51: ...QUELCH for a few moments use headsets if available Radio system operative transmitting not possible 1 2 Selected Frequency Microphone Problem cannot be resolved check if correct check if available use...

Page 52: ...In Cabin Check 4 5 II Walk Around Check 4 6 4 4 2 Before Starting Engine 4 10 4 4 3 Starting Engine 4 11 4 4 4 Before Taxiing 4 12 4 4 5 Taxiing 4 12 4 4 6 Before Take off 4 13 4 4 7 Take off 4 14 4...

Page 53: ...h Climb Speed during normal take off for 15 m 50 tt obstacle 58 67 108 Best Rate of Climb speed at sea level v flaps T O 65 75 120 Best Angle of Climb speed at sea level v flaps T O 58 67 108 V IAS LA...

Page 54: ...DV 20 Flight Manual Diamond AIRCRAFT Normal Procedures INTENTIONALLY LEFT BLANK Doc 4 01 20 E 20 Aug 1999 Page 4 3...

Page 55: ...DV 20 Flight Manual Diamond AIRCRAFT Normal Procedures INTENTIONALLY LEFT BLANK Doc 4 01 20 E 20 Aug 1999 Page 4 4...

Page 56: ...the control light for coolant quantity does not terminate illumination coolant in the dispatcher vessel on top of the engine has to be replenished The upper cowling has to be removed to gain access t...

Page 57: ...I 1 G 81 1 1 01 G CAUTION Normal Procedures Visual Inspection is defined as check for defects cracks delaminations excessive play insecure or improper mounting inspection of general condition verific...

Page 58: ...ng check suck on opening c Pitot Static Probe clean hole open d Wing Tip Balancing Mass visual inspection e Position Light visual inspection f Mooring Harness on Wing Tip release g Aileron visual insp...

Page 59: ...d Mooring Hamess on Wing Tip release e Wing Tip Balancing Mass visual inspection f Position Light visual inspection 6 Right Main Landing Gear a Landing Gear Strut visual inspection b Wheel Fairing vi...

Page 60: ...om the open oil tank a Oil check level by using dip stick NOTE Consumption of oil and coolant is very low under normal operating conditions Therefore topping up is necessary and senseful only if the q...

Page 61: ...Throttle free IDLE Prop Speed Control Lever free max RPM Carburetor Heat free OFF Friction Device of Throttle Quadrant Adjust Avionics Master Switch OFF Master Switch Battery ON Generator Warning Lig...

Page 62: ...Ensure people are clear of the propeller danger zone Ignition Key Throttle Oil Pressure CAUTION START maximum 1500 RPM within green range after maximum of 10 seconds If oil pressure is below 0 8 bar...

Page 63: ...tch Flight Instruments and Avionics Parking Brake CAUTION Normal Procedures ON as required check check extend and retract fully ON set release Warm up engine to a minimum oil temperature of 50 C 122 O...

Page 64: ...Quantity Indicator check 7 Wing Flaps TIO 8 Trim NEUTRAL 9 Controls free 10 Throttle 1700 RPM 11 Propeller Speed Control Lever Pull completely 3 times RPM drop 100 200 RPM 12 Ignition Switch L BOTH R...

Page 65: ...ing the brakes for directional control increases the take off roll distance Lift Nose wheel Climb Speed CAUTION 51 kts 65 kts VIAS 59 mph 75 mph For the shortest possible take off distance to clear a...

Page 66: ...th increasing altitude 6 4 4 9 CRUISE 1 2 3 0 4000 ft 4000 7000 ft 7000 10000 ft 10000 ft Trim Wing flaps Throttle kts 65 63 62 59 Propeller Speed Control Lever Flaps T O mph km h 75 120 73 117 71 115...

Page 67: ...PROACH Airspeed Wing Flaps Trim Throttle Prop Speed Control Lever Carburetor Heat Electric Fuel Pump Wing Flaps Approach Speed CAUTION 2260 RPM IDLE ON UP 117 kts l135 mph 217 km h max 81 kts 193 mph...

Page 68: ...N Throttle Parking Brake Electric Fuel Pump Avionics Master Switch Ignition Switch Master Switch Battery NOTE Normal Procedures max RPM FULL OFF T O set with caution 58 kts I 67 mph I 108 km h IDLE UP...

Page 69: ...d 4 4 16 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 characteristics of the airplane is negligi...

Page 70: ...titude 5 3 4 Figure 5 4 Stall Speeds 5 3 5 Figure 5 5 Wind Data 5 3 6 Figure 5 6 Take Off Distances 5 3 7 Figure 5 7 Climb Performance I Cruising Altitudes 5 3 8 Intentionally left blank 5 3 9 Figure...

Page 71: ...good maintenance condition Note that the range and flight duration data in each diagram includes a 30 minute fuel reserve for the indicated power level The fuel consumption during cruise is based on p...

Page 72: ...1 FIGURE 5 1 Airspeed Indicator System Calibration assuming zero instrument error 150 0 130 0 110 0 en j 90 0 70 0 50 0 30 0 I o o M UP 87 t k TfO LOG o o III o o V o o V V AS kts Example V AS 93 kts...

Page 73: ...8 17 22 6 18 0 20 4 5 4 85 95 105 Pressure Standard Altitude Temp RPM MP Fuel Flow RPM MP Fuel Flow RPM MP Fuel Flow ft m C O F 1 100 in Hg I h galJhr 1 100 in Hg Uh gallhr 100 in Hg IIh 0 0 15 59 22...

Page 74: ...low the maximum possible MP at the respective cruising altitude This measure reduces fuel consumption significantly while hardly affecting the cruising speed For an economical cruise it is recommendab...

Page 75: ...500 r 0 0 500 2 000 30 20 10 0 10 Tempe tur C Example 20 Performance E w w 0 0 J J I I 5 5 I I iii iii z z w w 0 0 16 000 5000 4 sao 14000 4000 12000 3500 10000 3000 8000 2500 6000 2000 1500 4000 100...

Page 76: ...BankAngle Flaps oa 30 I ee 45 lAS CAS lAS CAS lAS CAS UP 79 92 85 99 94 109 TIC 72 83 77 89 85 98 LOG 70 81 75 87 83 96 Stall speeds in kts FI 1ps l Ban tAngle F 0 30C A5 I lAS CAS lAS CAS lAS CAS UP...

Page 77: ...I 10 f Z l J Z o 5 o u o z 0 L1i r 5 In 10 f J 0 z 0 c u 170 160150 140 130 o 5 10 15 CROSSWIND COMPONENT kts I I I o 10 20kM h 30 Wind speed Angle between wind direction and flight direction Headwind...

Page 78: ...ce Take off distance to clear a 15 m 50 ft obstacle NOTE Obstacle Height 4000 ft 9 C 48 O F 650 kg 1433 Ibs 8 kts 220 m 720 ft 380 m 1250 ft Poor maintenance condition of the airplane deviation from t...

Page 79: ...with flaps in TIO position 65 kts I 75 mph I 120 kml h ft Min 20 10 0 10 20 30 OUTSIDE AIR TEMPERATURE RATE OF CLIMB Mis Example Pressure Altitude OAT Mass Weight Result Climb performance CAUTION 640...

Page 80: ...DV 20 Flight Manual Performance INTENTIONALLY LEFT BLANK Doc 4 01 20 E 20 Aug 1999...

Page 81: ...000 10 0QO 8000 OJ T5 6000 4000 OJ I 2000 Vl OJ 0 0 2000 170 180 190 200 210 220 230 I I I I I I I t K V K I 1 1 V 0 II 7 S I II A V I Y W I 95 100 105 110 115 120 125 20 10 0 10 20 30 Pressure altitu...

Page 82: ...lity Example Result Flight tiMe 30 Minute reserve 0 2 3 4 5 hrs If lJ 80 20 70 c 60 16 50 12 c 40 0 3 30 8 0 20 lJ 3 4 L 10 0 0 0 1 2 3 4 5 hrs Flight tif 1e no reserve Fuel capacity Power Setting Pre...

Page 83: ...x take off power J 1 oC J r C I I I o 500 1 1000 1500 2000 2500 I I I I I I I I I I I o 1000 2000 3000 4000 5000 6000 7000 8000 9000 10000 Ft Example Result Pressure Altitude Pressure altitude 3000 ft...

Page 84: ...a 15 m 50ft obstacle Landing roll distance approx 454 m 1490 ft approx 228 m 748 ft Performance For each 750 m 2500 ft additional height above MSL add 10 to the landing distance NOTE Poor maintenance...

Page 85: ...6 4 6 3 MASS WEIGHT AND BALANCE REPORT 6 5 Figure 6 2 Mass Weight Balance Report 6 6 6 4 FLIGHT MASS WEIGHT AND CENTER OF GRAVITY 6 7 Figure 6 3 Mass Weight Balance Diagram 6 8 Figure 6 4 Permissible...

Page 86: ...ight and the center of gravity are recorded in a weighing report as illustrated in figure 6 1 and in the Mass Weight Balance Report figure 6 2 In case of equipment changes the new mass weight and CG p...

Page 87: ...edge of the wing from the root rib to the ground to determine the reference datum RD From this plain the distances x X i left and x re right are measured to the wheel axes and recorded in the weighing...

Page 88: ...eighing Conditions Support Front G Rear G21i Rear G e Including Brake Fluid Lubricant Coolant and Unusable Fuel 1 5 kg 13 31 Ibs Gross Tare kg Ibs kg Ibs X Net Mass kg Ibs Empty Mass Weight GL CG Posi...

Page 89: ...installed equipment as well as each repair affecting the empty mass weight the CG position of the empty mass weight or the empty mass weight moment must be entered in the Mass Weight and Balance Repor...

Page 90: ...f equipment DV 20 KATANA 100 Serial No IReg IPage No Date Entry No Changes of Mass Weight Actual Description Addition Subtraction Empty Mass Weight of part or Mass Arm Moment Mass Arm Moment Mass Arm...

Page 91: ...e empty mass weight and the empty mass weight moment of the airplane should be taken from the weighing report or from the mass weight balance report and entered into the form Calculation of Loading Co...

Page 92: ...77 Li1ers 20 34 US gal I 10 1 40 k I 60 Liter 15 85 US gal e 40 Liters 10 57 US gal I t o Example Result 10 20 30 40 LOAD MOMENT kgm Pilot and Passenger 172 kg 380 Ibs Fuel 0 75 kglliter 38 kg 6 26 I...

Page 93: ...A u 6 t Y j 700 650 600 60 I I I 4 J i I i i Er HO 160 180 200 220 240 260 PERMISSIBLE FLiGHT MASS WEIGHT MOMENT kgm DV 20 Example of page 6 10 CD Changes during Flight due to the fuel consumption 280...

Page 94: ...Lever Arm 0 143 m 5 63 in 380 2112 3 Baggage Lever Arm 0 824 m 32 44 in H H 4 Total Mass Weight and Total 692 173 000 Moment with empty fuel tank 1526 15000 sum of 1 3 5 Usable Fuel Load 38 31 996 0...

Page 95: ...Weight and lever arm of the equipment items are shown in the columns Mass and lArml The data corresponds to one equipment item if not specially marked e g for the ACL Power Supply each power supply ha...

Page 96: ...V COMM Transceiver 2 24 0 420 Bendix King KX155 4 94 16 54 A6 NAV Receiver 0 85 0 420 Becker NR3301 2 1 87 J 16 54 A7 NAV Indicator 0 45 0 390 Becker IN3360 0 99 15 35 A8 NAV Indicator 0 80 0 390 Beck...

Page 97: ...ATC2000 2 R 2 65 24 41 A 18 Transponder Controller 0 26 0 420 Becker CU2000 2 0 57 16 54 A 19 Transponder Antenna 0 09 0 400 Bendix King KA60 0 20 15 75 A20 DME 1 08 0 420 Bendix King KN62A 2 38 16 5...

Page 98: ...7 E6 Landing Light 0 23 1 480 HaAC 16035 0 51 58 27 E7 Cockpit Speaker 0 37 0 580 HaAC 16003 0 82 22 83 E8 Boom Microphone 0 34 0 530 Becker 1 PM 004 0 75 20 87 E9 Boom Microphone 0 20 0 530 Comunica...

Page 99: ...HOAC 16159 0 20 15 35 16 Cylinder Head Temp Indicator 0 14 0 390 HOAC 16160 0 31 15 35 17 RPM Indicator 0 38 0 390 HOAC 16301 0 84 15 35 18 Altimeter 0 39 0 390 United 5934 AM 3 0 86 15 35 18A Altimet...

Page 100: ...390 R C Allen RCA82 11 1 26 15 35 I 19 Directional Gyro 1 11 0 390 R C Allen RCA15AK 2 2 45 15 35 120 Directional Gyro 1 36 0 390 AIM 205 1A 3 0 15 35 121 Attitude Gyro 1 10 0 390 R C Allen RCA26AK 4...

Page 101: ...s in T1 Engine Rotax 912 S3 dry 61 00 1 186 With electr Starter 134 46 69 carburetors internal generator ignition unit and oil tank T2 Propeller GovernorWoodward 1 40 3 09 1 250 A210786 49 21 T3 Prope...

Page 102: ...ug 120 47 Z8 Shoulder Harness 0 80 0 400 left autoflug 12B 26 1 76 15 75 right autoflug 12B 26 Z9 Seat Cushion standard 1 70 0 143 left HOAC 18102 3 75 5 63 right HOAC 18101 Z 10 Seat Cushion leather...

Page 103: ...PLANE AND ITS SYSTEMS INTRODUCTION AIRFRAME FLIGHT CONTROLS INSTRUMENT PANEL LANDING GEAR SYSTEM SEATS AND SAFETY BELTS BAGGAGE COMPARTMENT CANOPY POWERPLANT FUEL SYSTEM ELECTRICAL SYSTEM PITOT AND ST...

Page 104: ...sandwich construction and contain a CFRP spar The ailerons 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...

Page 105: ...the top position of the switch is used during cruise flight When the switch is moved to a different position the flaps move automatically until the selected position is reached follow up system The cr...

Page 106: ...ack T grip located in the front of the control stick Forward Adjustment Push both pedals forward with your feet while pulling the black T grip Backward adjustment Pull pedals backward to desired posit...

Page 107: ...nllly IncJl IOt c Ee PO a Th AI C lrtlur 01 Heal Proptllar Spetu ConlfOi LO lor instruments marked with are optional The flight instruments are installed on the pilot s side of the instrument panel Ca...

Page 108: ...taken into account see Chapter 5 Wheel Brakes Hydraulically operated disc brakes act on the wheels of the main landing gear The wheel brakes are operated individually using the toe brake pedals eithe...

Page 109: ...ops on the A bolts under the seats Every seat is equipped with four point safety belt The locking of the safety belt occurs by inserting the belt ends into the belt lock The belt is opened by rotating...

Page 110: ...4 cylinder 4 stroke engine horizontally opposed liquid cooled cylinder heads air cooled cylinders Propeller drive via integrated reduction gear crankshaft RPM in parentheses Displacement Max TIO Powe...

Page 111: ...tum valve At temperature rise of the coolant the excess pressure valve opens and coolant will flow via a hose to the equalizing reservoir at atmospheric pressure When cooling down coolant will be suck...

Page 112: ...r console throttle quadrant to the right of the throttle Pulling the lever backwards causes a reduction in RPM The governor keeps the selected RPM constant regardless of airspeed or throttle setting I...

Page 113: ...nical Flfel Pump Fuel Quantity Indicator I o electrical line Tank Filler Vent Line GND Firewall Fuel Quaniity Sensor I I Firewall Breach Finger Filter Tank Drain Filter of electr Fuel Shut off Valve F...

Page 114: ...tainless steel wire bride coated teflon hoses are used for all fuel lines A fuel pressure sensor is installed on top of the cross shaped fitting As soon as the fuel pressure drops below 0 1 bar 1 45 p...

Page 115: ...hole lid in the center of the fuselage bottom Tank Drain To drain the tank sump activate the spring loaded drain by pushing the brass tube in with a drain container The brass tube protrudes approx 30...

Page 116: ...TAATI C SWITCH caSOIO O t SW ITCH T PAA Or IHGH O SWITCH POwer supply 2 The battery is connected to the master bus via the master circuit breaker 50 Amps The generator which is integrated in the engin...

Page 117: ...light illuminates when the airplane VOltage drops below 12 5V The color is amber This indicates that the situation should be noted but no immediate action is necessary Generator Warning Light The gene...

Page 118: ...resistance of a sensor changes with the measurable variable which causes the power to the instrument and consequently the needle deflection to change Oil pressure indicator cylinder head temperature i...

Page 119: ...from a hole in the leading edge of the left wing to the horn The hole is marked by a red circle around 7 14 AVIONICS The center of the instrument panel contains the radio and navigation equipment The...

Page 120: ...LTERATIONS OR REPAIRS GROUND HANDLING I ROAD TRANSPORT 8 4 1 Towing 8 4 2 Parking 8 4 3 Mooring 8 4 4 Jacking 8 4 5 Alignment 8 4 6 Road Transport CLEANING AND CARE 8 5 1 Painted Exterior Surfaces 8 5...

Page 121: ...intenance Manual 8 3 AIRPLANE ALTERATIONS OR REPAIRS It is essential that the responsible airworthiness authority be contacted prior to any alterations on the airplane to ensure that airworthiness of...

Page 122: ...the airplane to the ground Also on each end of the wings an eyelet can be installed and used as tie down points 8 4 4 JACKING The DV 20 KATANA 100 can be jacked at the two jackpoints located on the l...

Page 123: ...fuselage should move 2 Wings For transportation both wings must be removed from the fuselage To avoid any damage the wings are stored in upright position on the leading edge with the root rib area po...

Page 124: ...y with a mild detergent An automotive paint cleaner can be used for stubborn spots For best results clean the aeroplane after the day s flying is ended so that the dirt will not become engrained Oil s...

Page 125: ...OR SURFACES SEATS AND CARPETS The interior should be cleaned using a vacuum cleaner All loose items pens bags etc should be properly stored and secured All instruments can be cleaned using a soft dry...

Page 126: ...0 Flight Manual Diamond AIRCRAFT CHAPTER 9 SUPPLEMENTS At this time the following Supplement is available Supplement NO 5 Operation with a Winterization Kit Doc 4 01 20 E 20 Aug 1999 Supplements Page...

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