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Diamond Aircraft DV 20 E, Flight Manual

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DV 20 E AFM

Performance

Doc. No. 4.01.25-E

Rev. 2

22-Mar-2022

Page 5 - 15

Gradient

ROC fpm

TAS KTAS

 

 

 

 

[%]

.

[

]

[

]

0 98

5.3.7  CLIMB PERFORMANCE - CRUISE CLIMB

Conditions:

- Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAX

- Propeller speed lever . . . . . . . . . . . . . . . . . . 5500 RPM

- Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CRUISE

- Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75  KIAS

The climb performance tables show the rate of climb. The gradient of climb can be

calculated using the following formula: 

Summary of Contents for DV 20 E

Page 1: ...rial Number ________ Registration ________ Doc No 4 01 25 E Date of Issue 15 Dec 2015 This Airplane Flight Manual has been approved by EASA under Approval No 10056462 DIAMOND AIRCRAFT INDUSTRIES GMBH N A OTTO STR 5 A 2700 WIENER NEUSTADT AUSTRIA Page 0 0 ...

Page 2: ...DV 20 E AFM Introduction Page 0 0a Rev 2 22 Mar 2022 Doc 4 01 25 E Intentionally left blank ...

Page 3: ...t must familiarize himself with the complete contents of this Airplane Flight Manual In the event that you have obtained your DIAMOND DV 20 E second hand please let us know your address so that we can supply you with the publications necessary for the safe operation of your airplane This document is protected by copyright All associated rights in particular those of translation reprinting radio tr...

Page 4: ...and side of the revised page with the revision number and date appearing at the bottom of the page If pages are revised which contain information valid for your particular serial number modification level of the airplane weighing data Equipment Inventory List of Supplements then this information must be transferred to the new pages in hand writing Temporary Revisions if applicable are inserted beh...

Page 5: ...ted Signature 1 MÄM 20 413 All All except cover page 15 Dec 2016 Revision 1 of the AFM Doc No 4 01 25 E is approved by EASA under Approval No 10061118 28 Feb 2017 2 MÄM 20 456 20 459 20 460 OÄM 20 245 20 271 All All except cover page 22 Mar 2022 Revision 2 of the AFM Doc No 4 01 25 E is approved under the authority of DOA No EASA 21J 052 06 Apr 2022 ...

Page 6: ...0 5 22 Mar 2022 0 6 22 Mar 2022 0 7 22 Mar 2022 0 8 22 Mar 2022 0 9 22 Mar 2022 0 10 22 Mar 2022 Ch Page Date 1 1 1 22 Mar 2022 1 2 22 Mar 2022 1 3 22 Mar 2022 1 4 22 Mar 2022 1 5 22 Mar 2022 1 6 22 Mar 2022 1 7 22 Mar 2022 1 8 22 Mar 2022 1 9 22 Mar 2022 1 10 22 Mar 2022 1 11 22 Mar 2022 1 12 22 Mar 2022 1 13 22 Mar 2022 1 14 22 Mar 2022 1 15 22 Mar 2022 1 16 22 Mar 2022 1 17 22 Mar 2022 1 18 22 ...

Page 7: ... 22 Mar 2022 appr 2 22 22 Mar 2022 appr 2 23 22 Mar 2022 appr 2 24 22 Mar 2022 appr 2 25 22 Mar 2022 appr 2 26 22 Mar 2022 Ch Page Date 3 appr 3 1 22 Mar 2022 appr 3 2 22 Mar 2022 appr 3 3 22 Mar 2022 appr 3 4 22 Mar 2022 appr 3 5 22 Mar 2022 appr 3 6 22 Mar 2022 appr 3 7 22 Mar 2022 appr 3 8 22 Mar 2022 appr 3 9 22 Mar 2022 appr 3 10 22 Mar 2022 appr 3 11 22 Mar 2022 appr 3 12 22 Mar 2022 appr 3 ...

Page 8: ... 3 40 22 Mar 2022 Ch Page Date 4 appr 4 1 22 Mar 2022 appr 4 2 22 Mar 2022 appr 4 3 22 Mar 2022 appr 4 4 22 Mar 2022 appr 4 5 22 Mar 2022 appr 4 6 22 Mar 2022 appr 4 7 22 Mar 2022 appr 4 8 22 Mar 2022 appr 4 9 22 Mar 2022 appr 4 10 22 Mar 2022 appr 4 11 22 Mar 2022 appr 4 12 22 Mar 2022 appr 4 13 22 Mar 2022 appr 4 14 22 Mar 2022 appr 4 15 22 Mar 2022 appr 4 16 22 Mar 2022 appr 4 17 22 Mar 2022 ap...

Page 9: ...ar 2022 5 15 22 Mar 2022 5 16 22 Mar 2022 5 17 22 Mar 2022 5 18 22 Mar 2022 5 19 22 Mar 2022 appr 5 20 22 Mar 2022 appr 5 21 22 Mar 2022 appr 5 22 22 Mar 2022 appr 5 23 22 Mar 2022 5 24 22 Mar 2022 5 25 22 Mar 2022 appr 5 26 22 Mar 2022 Ch Page Date 6 6 1 22 Mar 2022 6 2 22 Mar 2022 6 3 22 Mar 2022 6 4 22 Mar 2022 6 5 22 Mar 2022 6 6 22 Mar 2022 6 7 22 Mar 2022 6 8 22 Mar 2022 6 9 22 Mar 2022 6 10...

Page 10: ...2 Mar 2022 7 19 22 Mar 2022 7 20 22 Mar 2022 7 21 22 Mar 2022 7 22 22 Mar 2022 7 23 22 Mar 2022 7 24 22 Mar 2022 7 25 22 Mar 2022 7 26 22 Mar 2022 7 27 22 Mar 2022 Ch Page Date 7 7 28 22 Mar 2022 7 29 22 Mar 2022 7 30 22 Mar 2022 7 31 22 Mar 2022 7 32 22 Mar 2022 7 33 22 Mar 2022 7 34 22 Mar 2022 7 35 22 Mar 2022 7 36 22 Mar 2022 7 37 22 Mar 2022 7 38 22 Mar 2022 7 39 22 Mar 2022 7 40 22 Mar 2022 ...

Page 11: ...e 8 8 1 22 Mar 2022 8 2 22 Mar 2022 8 3 22 Mar 2022 8 4 22 Mar 2022 8 5 22 Mar 2022 8 6 22 Mar 2022 8 7 22 Mar 2022 8 8 22 Mar 2022 8 9 22 Mar 2022 8 10 22 Mar 2022 8 11 22 Mar 2022 8 12 22 Mar 2022 8 13 22 Mar 2022 8 14 22 Mar 2022 Ch Page Date 9 9 1 22 Mar 2022 9 2 22 Mar 2022 ...

Page 12: ...an approved chapter 2 EMERGENCY PROCEDURES an approved chapter 3 OPERATING PROCEDURES a non approved chapter 4 PERFORMANCE a partly approved chapter 5 MASS AND BALANCE EQUIPMENT LIST a non approved chapter 6 DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS a non approved chapter 7 AIRPLANE HANDLING CARE AND MAINTENANCE a non approved chapter 8 SUPPLEMENTS 9 ...

Page 13: ...SIS 1 3 1 3 WARNINGS CAUTIONS AND NOTES 1 3 1 4 DIMENSIONS 1 4 1 5 THREE VIEW DRAWING 1 6 1 6 DEFINITIONS AND ABBREVIATIONS 1 7 1 7 UNITS OF MEASUREMENT 1 13 1 7 1 CONVERSION FACTORS 1 13 1 7 2 CONVERSION CHART LITERS US GALLONS 1 15 1 8 SOURCE DOCUMENTATION 1 16 1 8 1 ENGINE 1 16 1 8 2 PROPELLER 1 17 1 8 3 AVIONICS SYSTEM 1 17 ...

Page 14: ... in the manufacturer s opinion could be of value to the pilot Equipment and modification level design details of the airplane may vary from serial number to serial number Therefore some of the information contained in this manual is applicable depending on the respective equipment and modification level The exact equipment of your serial number is recorded in the Equipment Inventory in Section 6 5...

Page 15: ...statements in the Airplane Flight Manual concerning the safety or operation of the airplane are highlighted by being prefixed by one of the following terms WARNING means that the non observation of the corresponding procedure leads to an immediate or important degradation in flight safety CAUTION means that the non observation of the corresponding procedure leads to a minor or to a more or less lo...

Page 16: ...are approximate Overall Dimensions Span 10 87 m 35 ft 8 in Length 7 15 m 23 ft 5 in Height 2 10 m 6 ft 11 in Wing Airfoil Wortmann FX 63 137 20 HOAC Wing Area 11 60 m 125 sq ft Mean aerodynamic chord 1 09 m 3 ft 7 in Aspect ratio 10 0 Dihedral 4 Leading edge sweep 0 5 Aileron Area total left right 0 65 m 7 sq ft ...

Page 17: ... Horizontal Tail Area 1 83 m2 18 7 sq ft Elevator area 0 50 m 5 4 sq ft Angle of incidence 4 relative to longitudinal axis of airplane Landing Gear Track 1 86 m 6 ft 1 in Wheelbase 1 68 m 5 ft 6 in Nose wheel 5 00 4 Main wheel 5 0 5 for details refer to the Airplane Maintenance Manual Doc No 4 02 25 latest revision ...

Page 18: ...General DV 20 E AFM Page 1 6 Rev 2 22 Mar 2022 Doc No 4 01 25 E 1 5 THREE VIEW DRAWING ...

Page 19: ...itude and temperature vA Maneuvering Speed Full or abrupt controlsurface movement is not permissible above this speed vFE Maximum Flaps Extended Speed This speed must not be exceeded with the given flap setting vNE Never Exceed Speed in smooth air This speed must not be exceeded in any operation vC Maximum Cruising Speed This speed may be exceeded only in smooth air and then only with caution vR R...

Page 20: ...n sea level is 15 C 59 F air pressure at MSL is 1013 25 hPa 29 92 inHg the temperature gradient up to the altitude at which the temperature reaches 56 5 C 69 7 F is 0 0065 C m 0 00357 F ft and above this 0 C m 0 F ft MSL Mean Sea Level OAT Outside Air Temperature QNH Theoretical atmospheric pressure at MSL calculated from the elevation of the measuring point above MSL and the actual atmospheric pr...

Page 21: ...rs are regarded as zero Wind The wind speeds which are shown as variables in the diagrams and tables in this manual should be regarded as headwind or tailwind components of the measured wind c Flight Performance and Flight Planning AGL Above Ground Level Demonstrated Crosswind Component The speed of the crosswind component at which adequate maneuverability for take off and landing has been demonst...

Page 22: ...s must be operated DP Datum Plane an imaginary vertical plane from which all horizontal distances for center of gravity calculations are measured Empty Mass The mass of the airplane including unusable fuel all operating fluids and the maximum quantity of oil Maximum Take off Mass The maximum permissible mass for take off Maximum Landing Mass The highest mass for landing conditions at the maximum d...

Page 23: ... propeller MAT Manifold air temperature f Designation of the Circuit Breakers on the Instrument Panel ICS Intercom System COM1 COM Radio No 1 GPS NAV1 Global Positioning System and NAV Receiver No 1 COM2 COM Radio No 2 XPDR Transponder AH Artificial Horizon AV MASTER Avionic Master FLAPS Flap System TRIM Trim system FUEL QTY AMP Fuel quantity indicator Ammeter EMU Engine Montoring Unit LANDING Lan...

Page 24: ...Control ALT External Alternator g Equipment ELT Emergency Locator Transmitter h Design Change Advisories MÄM Mandatory Design Change Advisory OÄM Optional Design Change Advisory VÄM Variant Design Change Advisory i Miscellaneous ATC Air Traffic Control CFRP Carbon Fiber Reinforced Plastic EASA European Aviation Safety Agency EPU External Power Unit GFRP Glass Fiber Reinforced Plastic GPS Global Po...

Page 25: ...l 0 9464 qts Speed km h kilometers per hour m s meters per second kts knots mph miles per hour fpm feet per minute km h 1 852 kts km h 1 609 mph m s x 196 85 fpm fpm 196 85 m s Speed of rotation RPM revolutions per minute Mass kg kilograms lb pounds kg x 2 2046 lb Force weight N newtons lbf pounds force N x 0 2248 lbf Pressure hPa hecto pascals mbar millibars bar bars inHg inches of mercury psi po...

Page 26: ...FM Dimension SI Units US Units Conversion Page 1 14 Rev 2 22 Mar 2022 Doc No 4 01 25 E Intensity of electric current A ampères Electric charge battery capacity Ah ampère hours Electric potential V volts Time sec seconds ...

Page 27: ...NVERSION CHART LITERS US GALLONS Liters US Gallons US Gallons Liters 10 2 6 2 7 6 15 4 0 4 15 1 20 5 3 6 22 7 25 6 6 8 30 3 30 7 9 10 37 9 35 9 2 12 45 4 40 10 6 14 53 0 45 11 9 16 60 6 50 13 2 18 68 1 60 15 9 20 75 7 70 18 5 22 83 3 80 21 1 24 90 9 90 23 8 26 98 4 100 26 4 ...

Page 28: ...terature that were used as sources for the Airplane Flight Manual and indicates the respective publisher However only the information given in the Airplane Flight Manual is valid 1 8 1 ENGINE Address BRP POWERTRAIN GMBH CO KG Rotaxstr 11 4623 Gunskirchen AUSTRIA Internet www flyrotax com Documents Operator s Manual OM 912 i latest revision ...

Page 29: ...er de Documents E 124 Operation and Installation Manual Hydraulically controlled variable pitch propeller MTV 5 6 9 11 12 14 15 16 21 22 25 1 8 3 AVIONICS SYSTEM Address Garmin International Inc 1200 East 151st Street Olathe Kansas 66062 USA Phone 1 913 3978200 Fax 1 913 3978282 Website www garmin com Documents G500 Cockpit Reference Guide P N 190 01102 03 latest revision G500 Pilot s Guide P N 19...

Page 30: ...General DV 20 E AFM Page 1 18 Rev 2 22 Mar 2022 Doc No 4 01 25 E Intentionally left blank ...

Page 31: ... ADVISORY ALERTS 2 9 2 7 MASS WEIGHT 2 10 2 8 CENTER OF GRAVITY 2 11 2 9 APPROVED MANEUVERS 2 12 2 10 MANEUVERING LOAD FACTORS 2 13 2 11 OPERATING ALTITUDE 2 14 2 12 FLIGHT CREW 2 14 2 13 KINDS OF OPERATION 2 14 2 14 FUEL 2 17 2 15 LIMITATION PLACARDS 2 18 2 16 OTHER LIMITATIONS 2 22 2 16 1 BATTERY CHARGE 2 22 2 16 2 DOOR LOCKING DEVICE 2 22 2 16 3 ELECTRONIC EQUIPMENT 2 22 2 16 4 GARMIN G500 AVIO...

Page 32: ...neFlight Manualprovidesoperatinglimitations instrument markings and placards necessary for the safe operation of the airplane its powerplant standard systems and standard equipment The limitations included in this Chapter are approved WARNING Operation of the airplane outside of the approved operating limitations is not permissible ...

Page 33: ... full or abrupt control surface movement above this speed vFE Max flaps extended speed LDG 78 KIAS Do not exceed these speeds with the given flap setting T O 100 KIAS vNO Max structural cruising speed 121 KIAS Do not exceed this speed except in smooth air and then only with caution vNE Never exceed speed in smooth air 164 KIAS Do not exceed this speed in any operation ...

Page 34: ...1 25 E 2 3 AIRSPEED INDICATOR MARKINGS Marking KIAS Significance White arc 35 78 KIAS Operating range with flaps fully extended Green arc 42 121 KIAS Normal operating range Yellow arc 121 164 KIAS Caution range Only in smooth air Red radial 164 KIAS Maximum speed for all operations vNE ...

Page 35: ...r 72 kW b Propeller Manufacturer mt Propeller Propeller designation MTV 21 A 175 05 Propeller diameter 175 cm Prop pitch angle 61 cm 14 5 low pitch 30 high pitch c Governor mt Propeller P 850 12 hydraulic governor d RPM limitations Maximum take off 5800 RPM max 5 min Maximum continuous 5500 RPM Minimum idle 1400 RPM e Oil pressure absolute Minimum 0 8 bar below 3500 RPM Maximum 7 0 bar for a short...

Page 36: ... air temperature Maximum 60 C i Coolant temperature Maximum 120 C NOTE A short cooling run should be performed before shutdown at higher coolant and oil temperatures to prevent vapor lock in the cylinder heads j Exhaust Gas Temperature Maximum 950 C k Fuel pressure relative to airbox pressure Minimum 2 8 bar Maximum 3 2 bar l Oil quantity without oil cooler Minimum 3 0 l Maximum 3 4 l Maximum oil ...

Page 37: ...fication which are NOT suitable See Rotax Service Instruction SI 912i 001 latest edition The use of multi grade oils is recommended At the selection of suitable lubricants refer to the additional information in the Rotax Service Instruction SI 912i 001 latest edition n Coolant Water Conventional coolant e g BASF Glysantine Protect Plus G48 Mixing Ratio 1 1 by volume CAUTION If the coolant level is...

Page 38: ...e Red arc bar upper prohibited range RPM 0 to 1400 RPM 1400 to 1800 RPM 1800 to 5500 RPM 5500 to 5800 RPM above 5800 RPM Oil pressure below 0 8 bar 0 8 to 2 0 bar 2 0 to 5 0 bar 5 0 to 7 0 bar above 7 0 bar Oil temp below 50 C 50 to 120 C 120 to 130 C above 130 C Coolant temp below 50 C 50 to 110 C 110 to 120 C above 120 C Fuel qty below 9 liters 9 to 93 liters EGT 65 to 900 C 900 to 950 C above 9...

Page 39: ...g Cause VOLTAGE The airframe receives no electric power from the engine due to generator failure START Engine starter is engaged CANOPY The canopy is not closed and locked LANE A B FAIL ECU Lane A B has detected a fault Caution alerts amber Meaning Cause EMU The start power relay is activated by the Engine Monitoring Unit or the BATTERY BACKUP Switch is ON ...

Page 40: ...Mass Weight Maximum take off mass 800 kg 1764 lb Minimum flight mass 580 kg 1279 lb Max load in baggage compartment only permissible with baggage harness 20 kg 44 lb WARNING Exceeding the mass limits will lead to overstressing of the airplane as well as to degradation of flight characteristics and flight performance ...

Page 41: ...en the fuselage tube is aligned horizontally the datum plane is vertical The reference datum RD for the center of gravity CG calculation is tangent to the leading edge of the wing at the root rib Center of Gravity Limitations The center of gravity CG position for flight conditions must be between the following limits Most forward flight CG 0 240 m 9 45 in aft of datum plane Most rearward flight CG...

Page 42: ...ed Maneuvers 1 All normal flight maneuvers 2 Stalling with the exception of dynamic stalling and 3 Lazy Eights Chandelles as well as steep turns and similar maneuvers in which an angle of bank of not more than 60 is attained CAUTION Aerobatics spinning and flight maneuvers with more than 60 of bank are not permitted CAUTION Intentional negative g maneuvers are not permitted ...

Page 43: ...ions The load factor limits for the engine must also be observed Refer to the corresponding Operator s Manual for the engine at vA at vNE with flaps in APP or LDG position Positive 4 4 4 4 2 0 Negative 2 2 1 53 0 0 WARNING Exceeding the maximum structural load factors will lead to overstressing of the airplane CAUTION Intentional negative g maneuvers are not permitted ...

Page 44: ...oved daytime flights according to Visual Flight Rules VFR withtheappropriateequipment nightflightsaccordingtoVisualFlightRules NVFR take off and landing on paved surfaces take off and landing on grass surfaces Flights into known or forecast thunderstorms are prohibited Flights into known or forecast icing conditions are prohibited Minimum Operational Equipment Serviceable The following table lists...

Page 45: ...ht navigation instruments Airspeed indicator on G500 or backup Altimeter on G500 or backup Magnetic compass 1 Headset used by pilot in command Vertical speed indicator VSI on G500 Attitude gyro artificial horizon on G500 or backup Turn bank indicator on G500 Directional gyro on G500 VHF radio COM VOR receiver Transponder XPDR mode A and mode C GPS receiver Engine instruments Fuel qty Oil press Oil...

Page 46: ...nt lighting Flashlight Other operational minimum equipment Stall warning system Alternate means for fuel quantity indication see Section 7 9 Safety belts for each occupied seat Airplane Flight Manual Safety Hammer Pitot heating system NOTE A list of approved equipment can be found in Chapter 6 Engine Systems and Equipment All engine systems and equipment must be functional prior to airplane take o...

Page 47: ... with AKI Anti Knock Index instead of RON specification following AKI value has to be observed min AKI 91 NOTE Use only uncontaminated fuel from reliable sources NOTE Use only fuel suitable for the respective climatic zone NOTE AVGAS 100LL places greater stress on the valve seats due to its high lead content and forms increased deposits in the combustion chamber and lead sediments in the oil syste...

Page 48: ...o 4 02 25 Chapter 11 The following limitation placards are in the forward view of the pilot Maneuvering speed vA 111 KIAS This airplane is classified a very light airplane and approved for day and night VFR in non icing conditions All aerobatic maneuvers including spinning are prohibited See Flight Manual for other limitations At the Fuel Quantity Indicator On the Right Hand Side of the Instrument...

Page 49: ...ating Limitations Doc No 4 01 25 E Rev 2 22 Mar 2022 EASA approved Page 2 19 FLAP SPEEDS FLAPS CRUISE T O LDG V LDG 78 KTS FE V T O 100 KTS FE FUEL PULL OFF Next to the Flap Selector Switch On the Fuel Shut off Control ...

Page 50: ...OSE OPEN TO LIFT CANOPY OPEN BOTH SIDES OPEN CLOSE TO LIFT CANOPY OPEN BOTH SIDES RESCUE HAMMER CLOSE OPEN OPEN CLOSE TO LIFT CANOPY OPEN BOTH SIDES OPEN TO LIFT CANOPY OPEN BOTH SIDES OPEN Next to the Canopy Handles Inside LH RH Next to the Canopy Handle Outside LH RH On the Co pilot s Backrest ...

Page 51: ...t Plus 4 10W 40 or see Airplane Flight Manual Super EN 228 AVGAS 100 LL or see AFM 93 l 24 5 US gal usable 84 l 22 2 US gal MAX BAGGAGE 20 kg 44 lb On the Sparbridge Between Pilot s and Co pilot s Seat In the Baggage Compartment In the Upper Cowling on the Door for the Oil Filler Neck Next to the Fuel Filler Neck ...

Page 52: ...ot be blocked by the key lock during operation of the airplane 2 16 3 ELECTRONIC EQUIPMENT The use and switching on of electronic equipment other than that which is part of the equipment of the airplane is not permitted as it could lead to interference with the airplane s avionics Examples of undesirable items of equipment are Mobile phones Remote radio controls Video screens employing CRTs Minidi...

Page 53: ...44 Magnetometer 2 01 In addition to the main components of the G500 Garmin GTN 650 GPS navigator is interfaced to the G500 The GPS system connected to the G500 must utilize the following or later approved software versions Component Identification Software version GTN 650 GPS WAAS 5 0 Nav 6 02 3 The AHRS used in the G500 is limited in its operational area Operations are prohibited north of 72 degr...

Page 54: ...ese regions but this will not affect the GPS track 4 The GDU 620 Navigation Angle can be set to either True or Magnetic on the AUX page The Navigation Angle defines whether the GDU 620 headings are referenced to True or Magnetic North The Navigation Angle set in the GDU 620 must match that which is set on the GNS navigator interfaced to the unit 2 16 5 SMOKING Smoking in the airplane is not permit...

Page 55: ...URE LIMITS CAUTION For airplanes with other than white undersides parking the airplane over a light colored or reflective surface in conditions of bright sunlight particularly at high OAT is not recommended Temperature limit of the structure for the operation of the airplane Maximum T O temperature 54 C 129 F ...

Page 56: ...Operating Limitations DV 20 E AFM Page 2 26 Rev 2 22 Mar 2022 EASA approved Doc No 4 01 25 E Intentionally left blank ...

Page 57: ...LURE AFTER LIFT OFF 3 6 3 2 4 ENGINE FAILURE IN FLIGHT 3 7 3 2 5 WARNING FLASHING ON THE EMU DISPLAY 3 11 3 3 ENGINE RESTART IN FLIGHT 3 12 3 3 1 RESTARTING THE ENGINE WITH WINDMILLING PROPELLER 3 12 3 3 2 RESTARTING THE ENGINE WITH STATIONARY PROPELLER 3 14 3 4 GLIDING 3 16 3 5 EMERGENCY LANDINGS 3 17 3 5 1 EMERGENCY LANDING WITH ENGINE OFF 3 17 3 5 2 PRECAUTIONARYLANDINGWITHENGINEPOWERAVAILABLE ...

Page 58: ...NG TAKE OFF 3 27 3 8 3 SMOKE AND FIRE IN FLIGHT 3 28 3 9 AVIONIC SYSTEM FAILURES 3 31 3 9 1 AVIONICS SYSTEM FAILURE 3 31 3 9 2 G500 FAILURES 3 32 3 10 RECOVERY FROM UNINTENTIONAL SPIN 3 34 3 11 OTHER EMERGENCIES 3 35 3 11 1 UNINTENTIONAL FLIGHT INTO ICING CONDITION 3 35 3 11 2 FLAP SYSTEM FAILURE 3 36 3 11 3 TRIM SYSTEM FAILURE 3 37 3 11 4 LANDING GEAR SYSTEM FAILURES 3 38 3 11 5 SUSPICION OF CARB...

Page 59: ...es and cover them in this Airplane Flight Manual a thorough understanding of the airplane by the pilot is in addition to his knowledge and experience an essential factor in the solution of any problems which may arise WARNING In each emergency control over the flight attitude and the preparation of a possible emergency landing have priority over attempts to solve the current problem first fly the ...

Page 60: ...de angle 800 kg 1762 lbs Flaps CRUISE 73 Precautionary landing with power and wing flaps in landing position 56 Emergency landing with engine off Flaps CRUISE 63 Flaps T O 56 Flaps LDG 56 3 1 3 SELECTING EMERGENCY FREQUENCY In an in flight emergency pressing and holding the Volume button on the GTN650 for 2 seconds will tune the emergency frequency of 121 500 MHz If the display is available it wil...

Page 61: ...le and START warning light ON 1 START button release immediately 2 Throttle IDLE 3 ENGINE MASTER OFF 4 ELECTRIC MASTER OFF 5 Terminate flight preparation END OF CHECKLIST b Loss of Oil Pressure 1 Stop the engine immediately 2 ENGINE MASTER OFF 3 ELECTRIC MASTER OFF 4 Terminate flight preparation END OF CHECKLIST c Exceeding the Maximum Manifold Temperature 1 Alternate Air Check closed 2 Throttle I...

Page 62: ...irspeed 60 KIAS 2 Throttle FULL 3 Propeller speed lever max RPM 4 Alternate air ON 5 LANE selector switch AUTO 6 Emergency fuel pump ON WARNING If adequate engine performance cannot be restored immediately prepare for an emergency landing If possible land straight ahead avoiding obstacles Do not attempt to turn back to the airfield Shortly before emergency landing 7 Fuel shut off valve pull OFF 8 ...

Page 63: ...NGS END OF CHECKLIST 3 2 4 ENGINE FAILURE IN FLIGHT a Engine Running Rough 1 Alternate air ON 2 Emergency fuel pump ON 3 Ammeter check 4 LANE A B FAIL lights check 5 Fuel pressure check 6 Oil pressure check 7 Oil temperature check 8 Throttle at present position No Improvement 9 Throttle reduce to minimum required power 10 Land at the nearest suitable airfield END OF CHECKLIST ...

Page 64: ...dance with 3 3 ENGINE RESTART IN FLIGHT can be attempted END OF CHECKLIST c Loss of Oil Pressure 1 Oil temperature check Oil temperature in green range 2 Land at the nearest suitable airfield END OF CHECKLIST Oil temperature outside green range upper limit 2 Throttle reduce to minimum required power 3 Land as soon as possible Prepare for an engine failure and emergency landing in accordance with 3...

Page 65: ...ST e Low Fuel Pressure 1 Emergency fuel pump ON 2 Land at the nearest suitable airfield Prepare for an engine failure and emergency landing in accordance with 3 5 EMERGENCY LANDINGS END OF CHECKLIST f Exceeding the Maximum Fuel Pressure 1 Emergency fuel pump OFF If fuel pressure remains too high 2 Land at the nearest suitable airfield Prepare for an engine failure and emergency landing in accordan...

Page 66: ...og book END OF CHECKLIST h Exceeding the Maximum Coolant Oil or Exhaust Gas Temperature 1 Throttle reduce to minimum required power 2 Land at nearest suitable airfield After Flight 3 Record maximum over temperature and duration in log book END OF CHECKLIST i Exceeding the Maximum Manifold Temperature NOTE If the maximum manifold temperature is exceeded expect reduced performance 1 Alternate Air Ch...

Page 67: ... DISPLAY 1 Check which engine parameters are in the red warning range NOTE MoredetailedinformationisavailableontheappropriateINFO page by pressing the INFO button on the EMU 2 MCR button Press 3 Refer to the appropriate emergency procedure 4 Continuously monitor the engine parameters in the red warning range END OF CHECKLIST ...

Page 68: ...ll forward max RPM 4 Fuel shut off valve check OPEN 5 Alternate Air OPEN 6 ENGINE MASTER check ON 7 LANE selector switch AUTO 8 BATTERY BACKUP Switch OFF 9 Emergency fuel pump ON 10 Throttle 2 cm 3 4 in forward if windmilling RPM too low for restart NOTE The RPM may be raised by pushing the airplane into a descent and accelerating to approx 121 KIAS A loss of 1300 ft 400 m altitude must be taken i...

Page 69: ... restart perform an emergency landing in accordance with 3 5 EMERGENCY LANDINGS 16 START Warning light check OFF After successful restart 17 Throttle increase to required power 18 Oil pressure check 19 AVIONIC MASTER ON if required 20 Oil temperature check If the LANE A B FAIL lights are not illuminated or flashing 21 BATTERY BACKUP Switch OFF EMU Caution light OFF 22 Ammeter check positive curren...

Page 70: ...2 cm 3 4 in forward 10 Starter button PRESS until 1500 RPM is reached Max 10s START warning light ON NOTE The engine may also be re started by increasing the airspeed by pushing the airplane into a descent and accelerating to approx 121 KIAS A loss of 1300 ft 400 m altitude must be taken into account WARNING If the engine performance cannot be restored immediately the airplane must be landed as so...

Page 71: ...TER ON if required 14 Oil temperature check If the LANE A B FAIL lights are not illuminated or flashing 15 BATTERY BACKUP Switch OFF EMU Caution light OFF 16 Ammeter check positive current WARNING If the current is negative Generator 2 has failed Proceed with Section 3 7 3 GENERATOR FAILURE END OF CHECKLIST ...

Page 72: ...22 Mar 2022 EASA approved Doc No 4 01 25 E 3 4 GLIDING 1 Wing flaps CRUISE 2 Airspeed at 800 kg 1764 lb 73 KIAS NOTE The glide ratio is 11 1 i e for 1000 ft 305 m of altitude the airplane can move forward 11 000 feet or 1 8 NM 3 3 km END OF CHECKLIST ...

Page 73: ...flaps in LDG position 56 KIAS flaps in T O position 56 KIAS flaps in CRUISE position 63 KIAS 3 Fuel shut off valve CLOSED 4 ENGINE MASTER OFF 5 BATTERY BACKUP Switch OFF 6 Safety belts secured 7 Radio transmit giving location and intentions Shortly before landing when reaching the landing area is ensured 8 Wing flaps LDG 9 ELECTRIC MASTER OFF 10 Touch down at lowest practical speed END OF CHECKLIS...

Page 74: ...landing on an upward slope should be sought 2 Consider wind 3 Approach If possible fly along a short cut rectangular circuit On the downwind leg of the circuit the landing area should be inspected for obstacles from a suitable height The degree of offset at each part of the circuit will allow the wind speed and direction to be assessed 4 Safety belts secured 5 Radio advice ATC Final Approach 6 Thr...

Page 75: ...FM Emergency Procedures Doc No 4 01 25 E Rev 2 22 Mar 2022 EASA approved Page 3 19 After Touch down 13 Brake as required 14 Fuel shut off valve CLOSED 15 ENGINE MASTER OFF 16 ELECTRIC MASTER OFF END OF CHECKLIST ...

Page 76: ...white instead of values in the data field Erroneous indications may be determined by comparing a display with other displays and other system information 1 Set power based on throttle lever position engine noise and speed 2 Monitor other indications to determine the health of the engine 3 Use known power lever settings 4 Use other system information such as annunciator messages fuel quantity and c...

Page 77: ...MALFUNCTIONS a LANE A B FAIL Light Illuminated or Flashing Inflight Land on the next suitable airfield NOTE If a LANE A B FAIL light is illuminated the engine is operated in power mode with increased fuel consumption up to 26 1 liter h END OF CHECKLIST On Ground Return to park position END OF CHECKLIST ...

Page 78: ... Speed Lever increase above 1500 RPM 2 BATTERY BACKUP Switch check OFF If the EMU Caution Light is still illuminated 3 Terminate flight preparation Inflight NOTE The EMU Caution light is illuminated during restart when the BATTERY BACKUP Switch is ON 4 BATTERY BACKUP Switch check desired position 5 Land on the next suitable airfield END OF CHECKLIST ...

Page 79: ...LECTRIC MASTER check ON If problem persists 3 Land at the nearest suitable airfield END OF CHECKLIST 3 7 2 LOW VOLTAGE WARNING LIGHT ILLUMINATED a Low VOLTAGE Indication on Ground 1 Propeller RPM increase RPM until VOLTAGE warning light extinguishes If low VOLTAGE warning light is still illuminated and the ammeter is indicating to the left of centre discharge Terminate flight preparation END OF CH...

Page 80: ... GEN circuit breaker check if tripped reset 2 Pitot heat OFF 3 Lights OFF 4 All non flight essential electrical consumers OFF If the low VOLTAGE warning light is still illuminated Proceed in accordance with 3 7 3 GENERATOR FAILURE 5 Critical electrical consumers progressively back ON monitoring ammeter for charging END OF CHECKLIST ...

Page 81: ...electrical consumers especially lights and pitot heat OFF 2 Land on the next suitable airfield CAUTION If any generator fails the airframe electrical system is automatically cut off from the generator The battery is the remaining source for the airframe electrical system for a minimum of 30 minutes NOTE In case of failure of the remaining generator expect imminent engine stoppage For re start proc...

Page 82: ...ound 1 Fuel Shut off Valve CLOSED 2 Throttle FULL 3 CABIN HEAT CLOSED 4 ENGINE MASTER OFF 5 ELECTRIC MASTER OFF 6 Evacuate airplane immediately END OF CHECKLIST b Electrical Fire with Smoke on the Ground 1 ELECTRIC MASTER OFF If engine is running 2 Throttle IDLE 3 Fuel Shut off Valve CLOSED 4 ENGINE MASTER OFF 5 Canopy open 6 Fire Extinguisher deploy as required END OF CHECKLIST ...

Page 83: ...g the airplane to a stop 3 After stopping proceed as in 3 8 1 SMOKE AND FIRE ON GROUND END OF CHECKLIST b Not Sufficient Runway Available for Straight Ahead Landing 1 Look for suitable landing site 2 Airspeed 60 KIAS 3 Flaps T O 4 Fuel shut off valve CLOSED 5 Throttle FULL 6 CABIN HEAT CLOSED 7 ENGINE MASTER OFF 8 ELECTRIC MASTER OFF 9 Perform emergency landing in accordance with 3 5 EMERGENCY LAN...

Page 84: ... position If a suitable landing area is available and can be safely reached airspeed can be increased to attempt to extinguish the fire Do not exceed airspeeds given as structural limitations 4 Throttle FULL 5 Cabin heat CLOSED 6 Emergency fuel pump check OFF 8 ENGINE MASTER OFF 7 ELECTRIC MASTER OFF 9 Perform emergency landing with engine off in accordance with 3 5 1 EMERGENCY LANDING WITH ENGINE...

Page 85: ...ated by opening the cabin air and the emergency windows WARNING Never open the canopy in flight 4 AVIONIC MASTER OFF 5 Electrically powered equipment OFF NOTE Restore electrical power systematically allowing time to monitor the system ammeter between reconnection of loads Watch carefully for smoke In case the fire is extinguished and electric power is required for continuation of the flight 6 ELEC...

Page 86: ... ELECTRIC MASTER OFF 2 Cabin air OPEN 3 Cabin heat CLOSED 4 Fire extinguisher discharge as required 5 Land at the nearest suitable airfield CAUTION If the fire extinguisher is used the cabin must be ventilated by opening the cabin air and the emergency windows WARNING Never open the canopy in flight END OF CHECKLIST ...

Page 87: ...circuit breaker trips again Land at the nearest suitable airfield 2 AVIONIC MASTER check 3 AVIONIC MASTER toggle If avionic system remains off line 4 Avionic Master circuit breaker pull 5 Land at the nearest suitable airfield END OF CHECKLIST b Radio System Operative No Reception 1 Microphone Key check for stuck Microphone Key on transceiver display 2 Headphones check deactivate SQUELCH for a few ...

Page 88: ...f available switch to COMM FAILURE code if required by the situation and permitted by applicable national regulations END OF CHECKLIST 3 9 2 G500 FAILURES a Red X A red X through any display field indicates that display field is not receiving valid data b Attitude Fail ATTITUDE FAIL The display system is not receiving attitude reference information from the AHRS accompanied by the removal of sky g...

Page 89: ...eceiving altitude input from the air data computer accompanied by a red X through the altimeter display Revert to the standby altimeter e Vert Speed Fail VERT SPEED FAIL The display system is not receiving vertical speed input from the air data computer accompanied by a red X through the vertical speed display Determine vertical speed based on the change of altitude information f HDG HDG The displ...

Page 90: ...DLE 2 Rudder full deflection against direction of spin 3 Control stick ease forward 4 Rudder neutral after rotation has stopped 5 Wing flaps CRUISE 6 Elevator pull carefully to recover smoothly from the dive 7 Return the airplane from a descending into a normal flight attitude Do not exceed the never exceed speed vNE 164 KIAS END OF CHECKLIST ...

Page 91: ...altitude or turning back 2 Continue to move control surfaces to maintain their moveability 3 Alternate air ON 4 Propeller speed lever increase RPM in order to prevent ice build up on the propeller blades 5 Cabin heat OPEN DEFROST 6 PITOT HEAT ON if installed CAUTION In case of icing on the leading edge of the wing the stall speed will increase and flight characteristics may degrade END OF CHECKLIS...

Page 92: ...e sector if flap extended Re check all positions of the flap switch Modified Approach Procedure Depending on the Available Flap Setting only CRUISE available Approach airspeed raise by at least 7 kts Throttle as required Land at a flat approach angle only T O available Approach airspeed normal Throttle as required Land at a flat approach angle only LDG available Perform normal landing END OF CHECK...

Page 93: ...s available for elevator but expect higher forces on control stick 3 Land at the nearest suitable airfield END OF CHECKLIST b Runaway of Trim 1 Control stick Grip stick and maintain control of airplane 2 TRIM circuit breaker pull circuit breaker 3 Rocker switch check if depressed If reason for runaway condition is obvious and has been resolved reset engage circuit breaker NOTE Full travel of the e...

Page 94: ...ECTRIC MASTER OFF END OF CHECKLIST b Landing with Defective Tire on Main Landing Gear 1 Final approach with wing flaps in landing position 2 Land airplane on the side of runway opposite to the side with the defective tire to compensate for change in direction which is to be expected during final rolling 3 Land with wing slightly tipped in the direction of the non defective tire To increase the man...

Page 95: ...al The occurrence of CO in the cabin is possible only due to a defect If a smell similar to exhaust gases is noticed in the cabin the following measures should be taken 1 Cabin heat defrost OFF 2 Ventilation open 3 Emergency windows open END OF CHECKLIST 3 11 6 INSTRUMENT PANEL LIGHTING FAILURE 1 Rocker switch map light ON 2 Dimming control turn fully clockwise 3 Lighting circuit breaker reset if ...

Page 96: ...LLUMINATED WARNING Do not try to open any canopy latch in flight This can result in inadvertent opening of the canopy and subsequent loss of control 1 Canopy latches LH RH Both pushed forward If the CANOPY light is still illuminated 1 Airspeed reduce below 85 KIAS 2 Land at next suitable airfield END OF CHECKLIST ...

Page 97: ...3 4 3 2 PRE FLIGHT INSPECTION 4 5 4 3 3 BEFORE STARTING ENGINE 4 12 4 3 4 STARTING ENGINE 4 13 4 3 5 BEFORE TAXIING 4 15 4 3 6 TAXIING 4 15 4 3 7 BEFORE TAKE OFF 4 16 4 3 8 TAKE OFF 4 18 4 3 9 CLIMB 4 19 4 3 10 CRUISE 4 19 4 3 11 DESCENT 4 20 4 3 12 APPROACH LANDING 4 21 4 3 13 GO AROUND 4 22 4 3 14 AFTER LANDING 4 22 4 3 15 SHUT DOWN 4 23 4 3 16 FLIGHT IN RAIN 4 23 4 3 17 CAUTION FLASHING ON THE ...

Page 98: ...d KIAS Climb speed during normal take off for 50 ft 15 m obstacle T O 60 Airspeed for best rate of climb vY T O 66 CRUISE 75 Airspeed for best angle of climb vX T O 60 Final approach speed LDG 56 T O 56 CRUISE 63 Max Structural cruising speed vNO Do not exceed this speed except in smooth air and then only with caution CRUISE 121 Max Maneuvering speed vA CRUISE 111 Max Flap speed vFE T O 100 LDG 78...

Page 99: ... 2 Inspection of the locking bolts for proper movement with no backlash 3 Check tire inflation Main wheels 2 3 bar 33 PSI Nose Wheel 1 8 bar 26 PSI 4 Check the spinner and its attachment including screws 5 Engine Master Check OFF 6 Electric Master Check OFF 7 Open the two inspection covers on the cowling 8 Check coolant level in expansion tank NOTE The inspection window must be covered with coolan...

Page 100: ...he direction of rotation 11 Check free travel of the throttle valve between stops 12 Inspect exhaust system for damage signs of leakage and poor condition NOTE Use lower cowling outlet for inspecting the exhaust muffler and lower parts of the engine 13 Inspect general condition of the engine and its installation through the inspection holes Look especially for signs of mechanical and thermal damag...

Page 101: ...p to date 3 Flight control lock removed 4 Flight controls check free and correct movement up to full deflection 5 Alternate air free OFF 6 Cabin heat free 7 Both brake pedals push 8 Parking brake SET release brake pedals 9 Throttle free IDLE 10 Propeller speed lever free HIGH 11 ELECTRIC MASTER ON 12 Annunciation lights EMU VOLTAGE START and CANOPY check 13 Fuel quantity sufficient 14 Engine instr...

Page 102: ...rim and flap indicator lights operational and dimmable 21 Exterior lights operational as required 22 ELECTRIC MASTER OFF 23 BATTERY BACKUP Switch check OFF seal installed 24 Foreign object inspection done 25 Emergency locator transmitter ELT ARM 26 Fire extinguisher check 27 Safety hammer check 28 Baggage stowed baggage net attached 29 Canopy clean undamaged END OF CHECKLIST ...

Page 103: ...V 20 E AFM Normal Operating Procedures Doc No 4 01 25 E Rev 2 22 Mar 2022 EASA approved Page 4 7 II Walk around Check Visual Inspection 5d f 5c 5b 5a 6 7a 7b j 1 3b c e 3a 3d 3f 4 2i 2a 2b 2g h 2d f 2c e ...

Page 104: ...ain Landing Gear a Landing gear strut visual inspection b Wheel fairing visual inspection c Tire wheel brake visual inspection d Wheel chocks remove e EPU cable if installed check removed 2 Left Wing a Entire wing visual inspection b Stall warning check suck on opening c Pitot static probe clean holes open d Tie down remove e Taxi and landing lights visual inspection f Wing tip position lights and...

Page 105: ...ure above the limit e Fuel quantity visual inspection fuel dipstick f Antennas visual inspection g Maintenance drain check closed not leaking 4 Empennage a Stabilizers and control surfaces visual inspection b Tie down remove c Trim tab on rudder visual inspection 5 Right Wing a Entire wing visual inspection b Wing flap including inspection panel visual inspection c Aileron including inspection pan...

Page 106: ...tank and slowly turn the propeller by hand several times in normal direction to pump oil from the engine into the oil tank maintaining compression pressure for a few seconds each time the process is completed when air reaches the oil tank a gurgling noise can be heard from the open oil tank CAUTION Do not turn the propeller against the normal direction of operation NOTE For normal operation the oi...

Page 107: ... completely covered by coolant Coolant overflow bottle check level b Cowling visual inspection c Air intakes free d Propeller visual inspection ground clearance minimum approx 25 cm 10 in e Propeller blades check for damage f Spinner visual inspection g Nose gear visual inspection towbar removed h Nose wheel fairing visual inspection i Nose tire and wheel visual inspection j Wheel chocks remove EN...

Page 108: ...ibited to enter or exit the airplane 1 Preflight inspection performed 2 Pedals adjusted locked 3 Passenger briefing performed 4 Safety belts all fastened 5 Parking brake set 6 Controls free movement 7 Fuel shut off valve check push OFF 8 Alternate Air OFF 9 Throttle IDLE 10 Propeller speed lever max RPM 11 Friction device of throttle quadrant adjust 12 AVIONIC MASTER OFF 13 ELECTRIC MASTER ON 14 L...

Page 109: ...SELECTOR switch AUTO 4 ENGINE MASTER ON noise of pump audible 5 LANE A B FAIL lights check both ON extinguished after 3 s 6 EMU caution lamp check ON 7 Fuel pressure check 2 8 to 3 2 bar 8 Fuel pump test switch press for minimum 5 s fuel pump noise must clearly change when switching fuel pressure must be between 2 8 and 3 2 bar 9 Throttle set 2 cm 3 4 in forward 10 Propeller speed lever full forwa...

Page 110: ...wn engine immediately max 10 seconds delay NOTE Oil pressure may advance to the yellow arc until oil temperature reaches normal operating temperatures 18 Engine instrument check for error messages 19 If 3 bar oil pressure is reached increase of engine speed is permitted 20 Throttle lever set to 2500 RPM for minimum 5 s 21 Low VOLTAGE warning light check OFF 22 EMU caution light check OFF 23 Ammete...

Page 111: ...F CHECKLIST 4 3 6 TAXIING 1 Brake check 2 Direction control check 3 Flight instruments and avionics check 4 Compass check CAUTION When taxiing on a poor surface select the lowest possible RPM to avoid damage to the propeller from stones or similar items CAUTION Avoid prolonged permanent braking while taxiing Prolonged permanent braking while taxiing will overheat the brakes and may cause loss of b...

Page 112: ...icator check 7 Engine and electric instruments within green range 8 Trim NEUTRAL 9 Wing flaps T O 10 Controls free 11 Propeller speed lever full forward max RPM 12 Throttle 4000 RPM 13 Propeller speed lever cycle 3 times Approx RPM drop 1000 RPM NOTE During the lane check not all sensor values are displayed on the engine instrument 14 LANE SELECTOR switch AUTO 15 LANE SELECTOR switch LANE A LANE B...

Page 113: ...xtinguished after 3 s 20 Alternate air ON RPM drop max 50 RPM 21 Throttle IDLE 22 Alternate air OFF 23 Circuit breakers check pressed IN 24 Emergency fuel pump check OFF 25 Fuel pump test switch Press for min 5s fuel pressure must remain between 2 8 and 3 2 bar 26 Emergency fuel pump ON 27 Throttle Full throttle for maximum 5 sec check propeller RPM 5600 200 RPM 28 Ammeter positive current 29 Park...

Page 114: ... RPM 5600 200 RPM 10 Elevator at beginning of rolling NEUTRAL 11 Directional control maintain with rudder NOTE In crosswind conditions directional control can be enhanced by differential braking Note that using the brakes for directional control increases the take off roll distance 12 Rotate 49 KIAS 13 Climb speed 60 KIAS After reaching safe height 14 Propeller speed lever max 5500 RPM 15 Emergenc...

Page 115: ...laps airspeed T O with 66 KIAS or CRUISE with 75 KIAS 5 Trim adjust END OF CHECKLIST 4 3 10 CRUISE 1 Throttle as required 2 Propeller speed lever 4300 5500 RPM 3 Wing flaps CRUISE 4 Trim as required 5 Engine instruments check NOTE During flight below the approach speed of 56 KIAS It is recommended to keep the canopy windows closed and to ventilate the cockpit via the air vents as necessary END OF ...

Page 116: ...A approved Doc No 4 01 25 E 4 3 11 DESCENT 1 Flight instruments and avionics adjust 2 Throttle as required 3 Propeller speed lever 4600 5000 RPM NOTE To achieve a fast descent Throttle IDLE Propeller speed lever 5500 RPM Wing flaps CRUISE Airspeed 121 KIAS END OF CHECKLIST ...

Page 117: ...d 4 ENGINE MASTER check ON 5 LANE SELECTOR switch check AUTO 7 Throttle as required 8 Airspeed check 100 KIAS max 9 Wing flaps T O 10 Trim as required 11 Propeller speed lever max RPM 12 Airspeed check 78 KIAS max 13 Wing flaps LDG 14 Approach speed 56 KIAS CAUTION For strong headwind crosswind danger of wind shear or turbulence a higher approach speed should be selected END OF CHECKLIST ...

Page 118: ...roved Doc No 4 01 25 E 4 3 13 GO AROUND 1 Propeller speed lever max RPM 2 Throttle FULL 3 Wing flaps T O 4 Airspeed 56 KIAS END OF CHECKLIST 4 3 14 AFTER LANDING 1 Throttle as required 2 Wing flaps CRUISE 3 Exterior lights as required 4 Emergency fuel pump OFF END OF CHECKLIST ...

Page 119: ...r 2 minutes 6 AVIONIC MASTER OFF 7 ENGINE MASTER OFF 8 Instrument panel lighting OFF 9 Emergency fuel pump Check OFF 10 ELECTRIC MASTER OFF 11 Tie downs and wheel chocks as required END OF CHECKLIST 4 3 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 negligible...

Page 120: ...essing the INFO button on the EMU 2 MCR button Press 3 Set appropriate action as desired 4 Continuously monitor the engine parameters in the amber caution range END OF CHECKLIST 4 3 18 VIEW DETAILED ENGINE PARAMETERS ON INFO PAGES OF THE EMU 1 INFO Button on the EMU Press 2 Select desired page Press 88 or 99 Button 3 Return to main page Press RET Button NOTE After approximately 5 seconds without a...

Page 121: ... 3 5 3 1 AIRSPEED CALIBRATION 5 3 5 3 2 INTERNATIONAL STANDARD ATMOSPHERE 5 4 5 3 3 STALLING SPEEDS 5 5 5 3 4 WIND COMPONENTS 5 6 5 3 5 TAKE OFF DISTANCE 5 7 5 3 6 CLIMB PERFORMANCE TAKE OFF CLIMB 5 12 5 3 7 CLIMB PERFORMANCE CRUISE CLIMB 5 15 5 3 8 CRUISE PERFORMANCE 5 18 5 3 9 LANDING DISTANCES 5 20 5 3 10 GO AROUND CLIMB PERFORMANCE 5 24 5 3 11 APPROVED NOISE DATA 5 26 5 3 12 COOLING PERFORMANC...

Page 122: ...s of the International Standard Atmosphere ISA 15 EC 59 F and 1013 25 hPa 29 92 inHg at sea level The performance diagrams and tables do not take into account variations in pilot experience or a poorly maintained airplane The performances given can be achieved if the procedures in this manual are followed and the airplane is maintained in good condition 5 2 USE OF THE PERFORMANCE TABLES AND DIAGRA...

Page 123: ...1 AIRSPEED CALIBRATION Airspeed Indicator Calibration Indicated Airspeed KIAS Calibrated Airspeed KCAS Flaps CRUISE Flaps T O Flaps LDG 40 48 45 53 52 50 58 57 55 55 62 61 59 60 66 65 64 65 70 69 68 70 75 73 72 75 79 77 76 80 83 81 79 90 92 89 100 101 96 110 110 120 120 130 129 140 138 150 147 160 156 164 159 ...

Page 124: ...Performance DV 20 E AFM Page 5 4 Rev 2 22 Mar 2022 Doc No 4 01 25 E 5 3 2 INTERNATIONAL STANDARD ATMOSPHERE ...

Page 125: ...s at Various Flight Masses Airspeeds most forward CG power off Bank Angle 0 30 45 60 KIAS KCAS KIAS KCAS KIAS KCAS KIAS KCAS CRUISE 42 52 47 56 55 62 69 74 T O 38 48 44 52 50 57 64 68 LDG 35 45 40 48 49 54 60 64 NOTE KIAS values may not be accurate at stall NOTE Maximum altitude loss during recovery is less than 300 ft ...

Page 126: ... 110 120 130 160 180 0 10 20 16 30 40 Crosswind Component kts 10 20 10 20 30 40 Headwind Component kts Flight Direction Maximum demonstrated Crosswind Component 5 3 4 WIND COMPONENTS Example Flight direction 360 Wind 32 30 kts Result Crosswind component 16 kts Max demonstrated crosswind component 20 kts ...

Page 127: ... take off distance for the noted condition Headwind Decrease by 10 for each 12 kt 6 2 m s headwind Tailwind Increase by 10 for each 3 kt 1 5 m s tailwind Grass runway 10 cm 4 in long Increase the ground roll by 25 Grass runway longer than 10 cm 4 in Increase the ground roll by 40 If brakes are not held while applying power distances apply where full power setting is complete WARNING For a safe tak...

Page 128: ... approved Doc No 4 01 25 E WARNING Poor maintenance condition of the airplane deviation from the given procedures uneven runway as well as unfavorable external factors rain unfavorable wind conditions including cross wind will increase the take off distance ...

Page 129: ...80 640 730 880 1020 579 3000 914 Ground Roll 300 340 380 430 520 610 331 15 m 50 ft 580 640 720 840 90 1170 633 4000 1219 Ground Roll 340 380 420 500 590 710 364 15 m 50 ft 640 730 810 950 1150 1360 706 5000 1524 Ground Roll 380 430 480 580 690 402 15 m 50 ft 730 820 920 1100 1320 772 6000 1829 Ground Roll 440 490 560 670 810 451 15 m 50 ft 840 950 1080 1300 1570 868 7000 2134 Ground Roll 500 570 ...

Page 130: ...440 490 540 610 720 870 493 3000 914 Ground Roll 260 290 330 380 450 530 286 15 m 50 ft 490 550 610 690 830 970 538 4000 1219 Ground Roll 300 330 370 430 510 610 314 15 m 50 ft 550 610 690 800 960 1130 591 5000 1524 Ground Roll 330 370 420 500 590 346 15 m 50 ft 610 700 770 920 1090 649 6000 1829 Ground Roll 380 430 480 580 700 390 15 m 50 ft 710 790 890 1060 1280 723 7000 2134 Ground Roll 440 490...

Page 131: ...50 ft 380 420 450 510 610 720 420 3000 914 Ground Roll 230 250 280 320 380 450 244 15 m 50 ft 410 460 510 580 690 810 449 4000 1219 Ground Roll 250 280 310 360 430 510 268 15 m 50 ft 450 510 570 660 780 910 495 5000 1524 Ground Roll 280 310 350 420 500 295 15 m 50 ft 510 570 630 750 900 548 6000 1829 Ground Roll 320 360 410 490 590 329 15 m 50 ft 580 650 730 880 1030 593 7000 2134 Ground Roll 370 ...

Page 132: ...OFF CLIMB Conditions Throttle MAX Propeller speed lever 5500 RPM Flaps T O Airspeed vY 66 KIAS The climb performance tables show the rate of climb The gradient of climb can be calculated using the following formula NOTE Rate of climb at MTOM 800 kg 1764 lb with a power setting of 100 at MSL and ISA conditions 660 ft min 3 4 m s with flaps T O ...

Page 133: ... 420 680 555 4000 1219 610 560 510 460 410 370 330 280 473 6000 1829 510 460 410 360 310 270 230 392 8000 2438 410 360 310 260 220 170 140 311 10000 3048 310 260 210 160 120 80 231 12000 3658 210 160 110 70 30 152 13000 3962 160 110 70 30 114 700 1543 SL 1030 970 920 860 810 760 710 670 837 2000 610 920 860 810 750 700 650 600 560 748 4000 1219 810 750 700 640 590 540 500 450 659 6000 1829 700 640...

Page 134: ... Mar 2022 EASA approved Doc No 4 01 25 E 600 1323 SL 1310 1250 1180 1120 1070 1010 960 900 1095 2000 610 1190 1130 1060 1000 940 890 830 780 996 4000 1219 1070 1000 940 880 820 770 710 660 896 6000 1829 940 880 810 760 700 650 600 796 8000 2438 810 750 690 640 580 530 480 697 10000 3048 690 630 570 520 470 420 600 12000 3658 570 510 460 410 360 320 505 13000 3962 510 460 400 360 310 270 459 For th...

Page 135: ...radient ROC fpm TAS KTAS 0 98 5 3 7 CLIMB PERFORMANCE CRUISE CLIMB Conditions Throttle MAX Propeller speed lever 5500 RPM Flaps CRUISE Airspeed 75 KIAS The climb performance tables show the rate of climb The gradient of climb can be calculated using the following formula ...

Page 136: ... 360 570 4000 1219 640 570 510 460 400 350 300 250 473 6000 1829 520 450 390 340 290 240 190 377 8000 2438 390 330 280 220 170 130 80 283 10000 3048 280 220 170 110 70 20 191 12000 3658 160 110 60 101 13000 3962 110 50 57 700 1543 SL 1130 1060 1000 930 870 810 750 690 898 2000 610 1000 930 860 800 740 680 620 570 791 4000 1219 870 800 730 670 610 550 500 440 685 6000 1829 730 660 600 540 480 430 3...

Page 137: ...ev 2 22 Mar 2022 Page 5 17 600 1323 SL 1460 1380 1300 1230 1160 1090 1020 960 1193 2000 610 1310 1230 1150 1080 1010 940 880 820 1073 4000 1219 1160 1080 1010 930 870 800 740 690 954 6000 1829 1010 930 860 790 730 670 610 837 8000 2438 860 790 720 650 590 530 480 722 10000 3048 710 650 580 520 460 510 611 12000 3658 580 510 450 390 340 290 504 13000 3962 510 450 390 330 280 230 452 For the rate of...

Page 138: ...pter 5 3 2 INTERNATIONAL STANDARD ATMOSPHERE NOTE Except for WOT operation the engine is running in the ECO mode with fuel flow as indicated in the following table In case where the POWER mode is activated at other throttle settings e g during an ECU malfunction the fuel flow is increased up to 26 1 l h This should be considered in the range calculation for the flight to the alternate airfield ...

Page 139: ...1 8 13 7 103 22 6 13 7 104 23 3 13 7 105 24 1 13 7 106 4300 20 4 11 1 89 21 1 11 1 90 21 8 11 1 91 22 5 11 1 92 23 3 11 1 92 6000 1829 5500 WOT 26 1 121 WOT 26 1 120 WOT 26 1 118 WOT 26 1 117 WOT 26 1 115 5000 23 2 16 5 111 4800 20 5 13 7 104 21 3 13 7 105 22 13 7 106 22 7 13 7 107 23 5 13 7 108 4300 19 9 11 1 90 20 7 11 1 91 21 4 11 1 92 22 1 11 1 93 22 8 11 1 94 8000 2438 5500 WOT 26 1 119 WOT 2...

Page 140: ...vel Approach speed vREF 56 KIAS WARNING For a safe landing the available runway length must be at least equal to the landing distance over a 50 ft 15 m obstacle WARNING Poor maintenance condition of the airplane deviation from the given procedures uneven runway as well as unfavorable external factors rain unfavorable wind conditions including cross wind will increase the landing distance ...

Page 141: ...ft 520 530 550 570 630 680 531 3000 914 Ground Roll 220 230 240 250 280 300 223 15 m 50 ft 530 550 560 600 650 710 543 4000 1219 Ground Roll 230 240 240 260 290 320 230 15 m 50 ft 550 570 580 620 680 740 557 5000 1524 Ground Roll 240 240 250 280 310 237 15 m 50 ft 570 580 600 650 710 570 6000 1829 Ground Roll 250 250 260 290 320 244 15 m 50 ft 580 600 620 680 740 585 7000 2134 Ground Roll 260 260 ...

Page 142: ...ft 480 500 510 530 580 630 492 3000 914 Ground Roll 190 200 210 220 240 270 196 15 m 50 ft 500 510 520 550 600 660 503 4000 1219 Ground Roll 200 210 210 230 250 280 201 15 m 50 ft 510 520 540 570 630 690 516 5000 1524 Ground Roll 210 210 220 240 270 208 15 m 50 ft 520 540 550 600 660 527 6000 1829 Ground Roll 220 220 230 260 280 214 15 m 50 ft 540 550 570 620 690 541 7000 2134 Ground Roll 220 230 ...

Page 143: ...ft 440 460 470 490 530 580 453 3000 914 Ground Roll 170 170 180 190 210 230 167 15 m 50 ft 460 470 480 510 560 600 464 4000 1219 Ground Roll 170 180 180 200 220 240 173 15 m 50 ft 470 480 500 530 580 630 474 5000 1524 Ground Roll 180 180 190 210 230 178 15 m 50 ft 480 500 510 550 600 485 6000 1829 Ground Roll 180 190 200 220 240 183 15 m 50 ft 500 510 520 570 630 497 7000 2134 Ground Roll 190 200 ...

Page 144: ... PERFORMANCE Conditions Throttle MAX Propeller speed lever HIGH Flaps LDG Airspeed vREF 56 KIAS The climb performance charts show the rate of climb The gradient and angle of climb can be calculated using the following formula NOTE The angles of climb at MSL and ISA condition are 4 5 for Maximum Take Off Mass 800 kg 1764 lb ...

Page 145: ...0 210 135 60 110 8000 2438 135 55 10000 3048 700 1543 SL 1060 980 905 830 755 680 610 540 790 2000 610 910 830 750 670 595 520 450 380 663 4000 1219 755 670 590 510 435 360 290 220 533 6000 1829 590 505 425 345 270 195 125 400 8000 2438 425 340 260 180 105 35 265 10000 3048 255 170 90 130 600 1323 SL 1490 1400 1315 1230 1150 1070 990 915 1190 2000 610 1320 1230 1145 1060 975 895 815 740 1050 4000 ...

Page 146: ...EASA approved Doc No 4 01 25 E 5 3 11 APPROVED NOISE DATA Max Flight Mass 800 kg 1764 lb ICAO Annex 16 Chapter X App 6 71 4 dB A 5 3 12 COOLING PERFORMANCE Cooling performance in accordance with CS VLA 1041 to 1047 has been demonstrated up to 47 C 117 F ...

Page 147: ...ge 6 1 INTRODUCTION 6 2 6 2 DATUM PLANE 6 3 6 3 MASS AND BALANCE REPORT 6 4 6 4 FLIGHT MASS AND CENTER OF GRAVITY 6 6 6 4 1 MOMENT ARMS 6 8 6 4 2 LOADING DIAGRAM 6 9 6 4 3 CALCULATION OF LOADING CONDITION 6 10 6 4 4 PERMISSIBLE CENTER OF GRAVITY RANGE 6 12 6 5 EQUIPMENT LIST AND EQUIPMENT INVENTORY 6 13 ...

Page 148: ...ing the flight mass CG position is described in this chapter Additionally a comprehensive list of the equipment approved for this airplane exists Equipment List The set of items marked as installed constitutes the Equipment Inventory Before the airplane is delivered the empty mass and the corresponding CG position are determined and entered in Section 6 3 MASS AND BALANCE REPORT NOTE Following equ...

Page 149: ...to the airplane s longitudinal axis and in front of the airplane as seen from the direction of flight The airplane s longitudinal axis is parallel with the upper surface of a 1000 56 wedge which is placed on top of the rear fuselage in front of the vertical stabilizer When the upper surface of the wedge is aligned horizontally the Datum Plane is vertical The Datum Plane is located at the most forw...

Page 150: ...e empty mass or the empty mass CG must be recorded in the Mass and Balance Report For the calculation of flight mass and corresponding CG position or moment the current empty mass and the corresponding CG position or moment in accordance with the Mass and Balance Report must always be used Condition of the airplane for establishing the empty mass Equipment as per Equipment Inventory see Section 6 ...

Page 151: ... 6 5 MASS AND BALANCE REPORT Page No Current empty mass Mo ment Mo ment Arm Mass Registration Changes in mass Subtraction Mo ment Mo ment Arm Mass Serial No Addition Mo ment Mo ment Arm Mass DV 20 E Description of part or Modification Upon delivery Entry No OUT IN Date ...

Page 152: ... tables and diagrams are required 6 4 1 MOMENT ARMS 6 4 2 LOADING DIAGRAM 6 4 3 CALCULATION OF LOADING CONDITION 6 4 4 PERMISSIBLE CENTER OF GRAVITY RANGE The diagrams should be used as follows 1 Take the empty mass and the empty mass moment of your airplane from the Mass and Balance Report and enter the figures in the appropriate boxes under the column marked Your DV 20 E in Table 6 4 3 CALCULATI...

Page 153: ...e masses and moments in the respective columns The CG position is calculated by dividing the total moment by the total mass using row 4 for the condition with empty fuel tank and row 6 for the pre take off condition The resulting CG position must be inside the limits As an illustration the total mass and the CG position are entered on Diagram 6 4 4 PERMISSIBLE CENTER OF GRAVITY RANGE This checks g...

Page 154: ... and Balance DV 20 E AFM Page 6 8 Rev 2 22 Mar 2022 Doc No 4 01 25 E 6 4 1 MOMENT ARMS The most important lever arms aft of the Datum Plane Item Lever Arm m in Pilot Co pilot 0 14 5 6 Fuel Baggage 0 82 32 4 ...

Page 155: ...DV 20 E AFM Mass and Balance Doc No 4 01 25 E Rev 2 22 Mar 2022 Page 6 9 6 4 2 LOADING DIAGRAM ...

Page 156: ...l mass to obtain the CG positions In our example empty tank 167 5 kgm 686 kg 0 244 m 14 569 in lb 1512 lb 9 64 in full tank 201 9 kgm 728 kg 0 277 m 17 582 in lb 1605 lb 10 95 in 3 Locate the values in the diagram in Section 6 4 4 PERMISSIBLE CENTER OF GRAVITY RANGE If the CG positions and related masses fall into the permitted area the loading condition is allowable Our example shows allowable lo...

Page 157: ... Copilot seat Lever arm 0 14 m 5 6 in 163 359 22 8 2010 3 Baggage Lever arm 0 82 m 32 4 in 0 0 0 0 4 Total mass total moment with empty fuel tank Total of 1 3 686 1512 167 5 14569 5 Usable fuel 0 72 kg liter 6 01 lb US gal Lever arm 0 82 m 32 4 in 42 93 34 4 3013 6 Total mass total moment with fuel Total of 4 and 5 728 1605 201 9 17582 The CGs shown in the following diagrams are those from the exa...

Page 158: ...osition m 0 22 0 24 0 26 0 28 Flight Mass lb Center of Gravity Position in 750 800 900 850 0 30 0 32 0 34 0 36 0 38 6 4 4 PERMISSIBLE CENTER OF GRAVITY RANGE The flight CG position must be within the following limits Most forward flight CG 0 240 m 9 45 in aft of datum plane Most rearward flight CG 0 370 m 14 57 in aft of datum plane ...

Page 159: ...ist below NOTE The equipment listed below cannot be installed in any arbitrary combination The airplane manufacturer must be contacted before removing or installing equipment with the exception of replacing a unit by an identical unit The items of equipment installed in your particular airplane are indicated in the appropriate column The set of items marked as installed constitutes the Equipment I...

Page 160: ...Aircraft 0 132 0 060 21 4 0 54 EQUIPMENT Safety belt pilot 504856 403 Amsafe Safety belt co pilot 504856 404 Amsafe ELT unit ME 406 453 6603 Artex 1 984 0 900 32 4 0 82 SAFETY EQUIPMENT Fire extinguisher A620T Amarex 2 315 1 050 26 4 0 67 First aid kit Safety Hammer VH620BR Lifeaxe 0 441 0 200 26 4 0 67 FLIGHT CONTROLS Flaps control module 22 2753 00 00 Diamond Aircraft 0 120 0 050 20 5 0 52 HYDRA...

Page 161: ...6 01 0770346 00 Whelen 0 280 0 127 0 0 0 0 LED Landing Light D21 3347 13 00 Diamond Aircraft 0 300 0 136 0 0 0 0 COMMUNICATION NAVIGATION Audio panel Marker ICS GMA 340 011 00401 10 Garmin 1 200 0 600 21 5 0 54 COMM NAV GPS 1 GTN 650 011 02256 00 Garmin 5 500 2 480 21 5 0 54 COMM 2 GTR 225A 011 02807 00 Garmin 2 360 1 070 21 5 0 54 Backup altimeter 5934PD 3 United Instruments 0 496 0 225 20 5 0 52...

Page 162: ...efer to DAI Service Bulletin MSB 20E 002 latest revision BRP Powertrain Fusebox 881320 BRP Powertrain 4 321 1 960 29 5 0 750 ENGINE FUEL PUMPS Fuel pump unit 889696 BRP Powertrain 3 527 1 600 29 5 0 750 ENGINE INDICATING Engine management unit EMU EMU 912 iS Evo Stock Flight Systems 1 764 0 800 20 5 0 52 EMU software Refer to DAI Service Bulletin MSB 20E 002 latest revision Stock Flight Systems EN...

Page 163: ...rer S N installed lb kg in m Doc No 4 01 25 E Rev 2 22 Mar 2022 Page 6 17 FUEL TANK SYSTEM Fuel probe 22 2840 02 00 Diamond Aircraft 0 350 0 160 32 3 0 820 AIRPLANE FLIGHT MANUAL Doc No 4 01 25 E Diamond Aircraft Place _______________________ Date ___________________________ Signature ______________________________ ...

Page 164: ...DV 20 E AFM Mass and Balance Doc No 4 01 25 E Rev 2 22 Mar 2022 Page 6 18 Intentionally left blank ...

Page 165: ... 5 LANDING GEAR 7 17 7 6 SEATS AND SAFETY HARNESSES 7 19 7 7 CANOPY AND CABIN INTERIOR 7 20 7 8 POWER PLANT 7 23 7 8 1 ENGINES GENERAL 7 23 7 8 2 PROPELLER 7 24 7 8 3 OPERATING CONTROLS 7 25 7 8 4 ENGINE INSTRUMENTS 7 27 7 8 5 FUEL SYSTEM 7 32 7 8 6 COOLING SYSTEM 7 36 7 8 7 OIL SYSTEM 7 38 7 9 ELECTRICAL SYSTEM 7 39 7 9 1 GENERAL 7 41 7 9 2 ENGINE MANAGEMENT SYSTEM EMS 7 43 7 10 PITOT STATIC SYST...

Page 166: ...ription DV 20 E AFM Page 7 2 Rev 2 22 Mar 2022 Doc No 4 01 25 E 7 12 1 GENERAL 7 48 7 12 2 GDU 620 DISPLAY 7 48 7 12 3 GRS 77 AHRS 7 49 7 12 4 GDC 74A ADC 7 49 7 12 5 GMU 44 MAGNETOMETER 7 49 7 12 6 GTN 650 GPS 7 49 ...

Page 167: ...escription Doc No 4 01 15 E Rev 2 22 Mar 2022 Page 7 3 7 1 INTRODUCTION Chapter 7 contains a description of the airplane and its systems together with operating instructions For details about optional equipment see Chapter 9 ...

Page 168: ...uselage connection is made with three bolts each The A and B bolts are fixed to the fuselage s root rib The A bolt is placed in front of the spar bridge the B bolt is near the trailing edge on each side of the fuselage The two main bolts are placed in the middle of the spar bridge structure They are accessible behind the seats and are inserted from the front side A spring loaded hook locks both bo...

Page 169: ... The indicator need only be checked if the OAT exceeds 38 C 100 F The indicator is accessed by lifting the flap between the two seatback cushions The indicator is visible through the cut out in the seat shell backs see Figure 2 At temperatures below the 54 C 129 F limit the indicator appears all red with a faint indication of 55 C At temperatures exceeding the 54 C 129 F limit the indicator displa...

Page 170: ...CFRP composite sandwich Hinges There are 4 hinges which are attached to the wing with a bolt and a sheet metal bracket Operation Each aileron is connected with an aileron control horn to the push rods of the aileron control system A rod end bearing is screwed into a steel push rod and locked by means of a jam nut which has locking varnish applied to it Damage to this varnish can indicate a twistin...

Page 171: ...system A rod end bearing is screwed into a steel push rod and locked by means of a jam nut which has locking varnish applied to it Damage to this varnish can indicate a twisting and thus a change to the adjustment The connection between the rod end bearing and the control horn is a bolt the nut of which is likewise sealed with locking varnish Each flap control horn is attached to the flap part wit...

Page 172: ...sitions The electrical flap drive has an automatic circuit breaker which can also be operated manually Flap Position Indicator The current flap position is indicated by means of three lights beside the flap selector switch When the upper light green is illuminated the flaps are in the Cruise position CRUISE when the center light white is illuminated the flaps are in Take Off position T O when the ...

Page 173: ...as well as the connection to the pushrod can be visually inspected at the upper end of the rudder Rudder Construction GFRP sandwich Hinges Upper hinge One bolt Lower hinge Bearing bracket including rudder stops held by 4 screws to the rear web of the vertical stabilizer The mating part on the rudder is a bracket which is attached to the rudder by 2 bolts The bolts and nuts are accessible for visua...

Page 174: ...nd can be tripped manually to disable the system Push switch to the front nose down Push switch to the rear nose up Pedal Adjustment NOTE The pedals must only be adjusted on the ground The pedals for rudder and brakes are unlocked by pulling the T grip located in front of the rudder pedal sledge tubes NOTE Pull the T grip straight back Do not pull upwards Forward adjustment Push both pedals forwar...

Page 175: ...ith each airplane and should be installed whenever the airplane is parked See Figure 7 3 Installation and Removal of the Control Lock CAUTION Failure to install the flight control lock whenever the airplane is parked may result in control system damage due to gusts or turbulence Figure 7 3 Installation and Removal of the Control Lock ...

Page 176: ...pose the control stick tube and push the control stick forward against the control lock e Loop the straps around the control stick as shown and push forward on the control stick f Clip the straps into the left and right buckle receptacles located under the instrument panel g Adjust the straps as required Straps should be tight to secure the controls properly h To remove push the control stick forw...

Page 177: ...o 4 01 15 E Rev 2 22 Mar 2022 Page 7 13 7 4 INSTRUMENT PANEL Figure 7 4 Instrument Panel NOTE The figure above shows the typical installation position for the equipment The actual installation may vary due to the approved equipment version ...

Page 178: ...Airplane Description DV 20 E AFM Page 7 14 Rev 2 22 Mar 2022 Doc No 4 01 25 E Figure 7 5 Circuit Breaker Panel ...

Page 179: ...DV 20 E AFM Airplane Description Doc No 4 01 15 E Rev 2 22 Mar 2022 Page 7 15 Figure 7 6 Circuit Breaker Panel if OÄM 20 245 b is installed ...

Page 180: ...mergency compass 24 Instrument Light Dimmer 10 Engine Monitoring Unit 25 Light switches 11 Hourmeter 26 LANE A B FAIL caution lights 12 Circuit breakers 27 Start button 13 Ammeter 28 Engine Master switch 14 Accessory power plug 29 Lane Selector switch 15 Fuel quantity indicator 30 Designations and abbreviations used to identify the circuit breakers are explained in Section 1 5 DEFINITIONS AND ABBR...

Page 181: ...on the wheels of the main landing gear The wheel brakes are individually operated by means of toe pedals Parking Brake The lever is located on the small center console under the instrument panel and is in the upper position when the brakes are released To operate the parking brake pull the lever downwards until it catches Brake pressure is built up by multiple operation of the toe brake pedals and...

Page 182: ...Airplane Description DV 20 E AFM Page 7 18 Rev 2 22 Mar 2022 Doc No 4 01 25 E Figure 7 7 Brake System Schematic Diagram ...

Page 183: ...g controls Covers on the control sticks prevent loose objects from falling into the area of the controls The seats have removable furnishings The seats are fitted with four point safety harnesses To put on the safety belt slip the arms through the belts and buckle the left and right belts Adjust the length of the lap belts so that the buckle is centered around your waist The shoulder belts are adj...

Page 184: ...t down During engine operation it is prohibited to enter or exit the airplane Closing the Canopy Close the canopy by pulling down the canopy frame see Figure 7 8 Latching the canopy is accomplished by moving the two latching handles on the left and right side of the frame to the CLOSE position Opening the Canopy To open the canopy move the two latching handles on the left and right side of the fra...

Page 185: ... the Canopy from Outside Move both the LH and RH external latching handles in the aft up direction to the CLOSE position Opening the Canopy from Outside Move both the LH and RH external latching handles in the Fwd Down direction to the OPEN position and lift the canopy Figure 7 8 Canopy ...

Page 186: ... all cabin heat to Floor Cabin Air The air inlet for the ventilation system is located on the fuselage shell next to the pilots and copilots feet The air is distributed to the cabin via 2 nozzles 2 on the instrument panel LH RH side The jet direction of each cone can be changed easily and the jet intensity can be regulated by rotation of the nozzle The two sliding windows in the canopy can be open...

Page 187: ...ation are displayed on the engine instrument The engine can only be operated with the ENGINE MASTER switch ON The electrical system of the engine is separated from the electrical system of the airframe For engine start both electric systems are automatically connected by the start power relay until Generator 1 produces sufficient power to sustain the engine For restart in flight the electric syste...

Page 188: ...led Otherwise the engine is operated inthe fuelefficient ECO mode The engine instrument EMU 912iS evo indicates the current mode of operation 7 8 2 PROPELLER A mt propeller MTV 21 A 175 05 hydraulically regulated 2 blade constant speed propeller is installed The propeller has wood composite blades with fiber reinforced plastic coating and stainless steel edge cladding in the region of the propelle...

Page 189: ... rear are defined in relation to the direction of flight This throttle lever is used to set the desired manifold pressure Lever forward MAX wide open throttle Lever to rear IDLE Idle The separate ECU controls injected fuel quantity and ignition according to the desired engine throttle valve position selected with the throttle lever Propeller Speed Lever Central lever with blue handle Lever forward...

Page 190: ...over speeding and excessively rapid RPM changes The light wooden propeller blades produce more rapid RPM changes than metal blades CAUTION Following failure of the governor or a serious drop in oil pressure the RPM should be adjusted using the throttle Every effort should be made not to exceed 5800 RPM ELECTRIC MASTER The ELECTRIC MASTER switch has two positions OFF disconnecting battery power ON ...

Page 191: ...center console To open the alternate air source the lever is pulled to the rear The alternate air source is closed with the lever in the forward position BATTERY BACKUP Switch The guarded and secured BATTERY BACKUP Switch connects the engine and airframe electric system for restart after engine failure 7 8 4 ENGINE INSTRUMENTS The engine instruments are displayed on the EMU 912 iS evo and a separa...

Page 192: ...ashing the lane is still working and the engine control function has not been switched to the other lane When the LANE A B FAIL light is illuminatedpermanently thelanesenginecontrolfunction is switched over the other lane The engine is now operated in the power modus with increased fuel consumption Full engine power is still available NOTE The engine manufacturer allows limited operation with one ...

Page 193: ...s on the MAIN page Engine parameters with operating limitations and caution ranges that are displayed as alphanumeric values are color coded with green amber and red On the INFO page more detailed information is provided including color coded bars and drag indicators The drag indicators are reset by pressing the ZERO button The brightness of the display can be adjusted by rotating the MCR button ...

Page 194: ... Oil pressure bar Oil temperature C EGT Exhaust gas temperature C CT Coolant temperature C FUEL Fuel pressure bar Fuel consumption rate l h ECV ECU voltage V MAT Manifold air temperature C MODE Engine operation mode POWER ECO WARNING Engine parameter s in the red range CAUTION Engine parameter s in the amber range MCR Master Caution Reset INFO INFO Subpage ...

Page 195: ...DV 20 E AFM Airplane Description Doc No 4 01 15 E Rev 2 22 Mar 2022 Page 7 31 Figure 7 10 EMU Display INFO Page RET Return to main page 88 Page down 99 Page Up ZERO Reset drag indicators ...

Page 196: ... stud is located on the lower side of the fuselage near the trailing edge of the left hand wing The airplane must be grounded prior to any fueling operation The tank vent line runs from the filler neck through the fuselage bottom skin to the exterior of the airplane The vent line is the translucent plastic hose adjacent to the left wing root The vent line must be clear for proper fuel system opera...

Page 197: ...the fuselage adjacent to the fuel tank drain Fuel Pumps The fuel pump unit contains two serially installed electric fuel pumps One is the main pump which works continuously as long as the engine master is switched ON During landing and take off or in case of low fuel pressure the second fuel pump can be activated with the emergency fuel pump switch A vapour separator is located downstream of the f...

Page 198: ... of the firewall and is controlled by a handle on the right side center pedestal To activate the fuel shut off valve lift the handle release lock and pull the handle out In the open position the knob is in In the closed position the knob is out Fuel pressure is measured between the shut off valve and the fine filter The fine filter has a bypass with a check valve in case the filter becomes clogged...

Page 199: ...el level during the preflight check Electric fuel gauges may malfunction Check fuel quantity with the fuel dipstick before each flight To check the fuel level a Insert the graduated end of the fuel dipstick into the tank through the fuel filler opening until the dipstick touches the bottom b Withdraw the dipstick from the fuel tank c Read the fuel quantity The dipstick is calibrated in increments ...

Page 200: ...nspection hole in the right hand side of the upper cowling provides access to the overflow bottle The coolant level must be between the MIN and MAX marking The expansion tank is closed by a pressure cap with pressure relief valve and return valve As the coolant heats up and expands the pressure relief valve opens and the coolant flows via a hose to the overflow bottle at atmospheric pressure As it...

Page 201: ...DV 20 E AFM Airplane Description Doc No 4 01 15 E Rev 2 22 Mar 2022 Page 7 37 Figure 7 13 Overflow Bottle ...

Page 202: ...essure regulator and oil pressure sensor The oil pump transports the oil from the oil tank through a radiator and the oil filter to the lubrication points of the engine see Figure 7 14 Surplus oil accumulates at the bottom of the crankcase and is forced back to the oil tank by the piston blow by gases 1 Pressure regulator 4 Oil cooler 2 Oil pump 5 Oil filter 3 Oil tank 6 Venting tube Figure 7 14 O...

Page 203: ...DV 20 E AFM Airplane Description Doc No 4 01 15 E Rev 2 22 Mar 2022 Page 7 39 7 9 ELECTRICAL SYSTEM Figure 7 15 Electric System Schematic ...

Page 204: ...Airplane Description DV 20 E AFM Page 7 40 Rev 2 22 Mar 2022 Doc No 4 01 25 E Figure 7 16 Electrical System Schematic if OÄM 20 245 b is installed ...

Page 205: ...eexplainedinSection 1 5 DEFINITIONS AND ABBREVIATIONS Ammeter The ammeter shows the intensity of the current with which the battery is being charged positive range or discharged negative range Landing and Taxi Lights Landing and taxi lights are built into the LH wing and are each operated by means of a switch LANDING TAXI located on the row of switches on the instrument panel Position and Strobe L...

Page 206: ...e LH section of the instrument panel the internal lighting of the instruments is switched on and its brightness is adjusted Pitot Heating The Pitot probe which provides measurement for the Pitot static system is electrically heated The heating is activated with a switch PITOT HEAT located on the row of switches on the instrument panel ...

Page 207: ...t for start the engine no external power supply The EMS primarily comprises High voltage ignition components connectors spark plugs ignition cables double ignition coils ECU ECU actuators OUTPUT 4 double ignition coils Lamps Fuel injection 2 per cylinder CAN data for an indicating instrument ECU signals INPUT Sensors EMS power supply Regulator rectifier Generator FUSE BOX all power supply componen...

Page 208: ...once the engine has reached its idle speed NOTE Until the idle speed is reached the EMS requires an external 12 V supply from the onboard system of the airplane ECU The ECU is a digital engine control unit which contains the LANE A and the LANE B in a single housing In principle each LANE represents an independent computer In the AUTO both LANE select switch ON setting the ECU decides which LANE t...

Page 209: ...er the propeller The alternator is driven by a V belt from the propeller drive The alternator is connected to the electrical system via the ALT circuit breaker The regulator of the alternator is protected by the ALT CONTROL circuit breaker A failure of the external alternator is indicated by an alternator warning light AWL installed on top of the instrument panel on the LH side 7 10 PITOT STATIC S...

Page 210: ... static pressure probe should be protected whenever the airplane is parked to prevent contamination and subsequent malfunction of the airplane systems relying on its proper functioning NOTE Use only the factory supplied pitot static probe cover with the Remove before Flight flag attached ...

Page 211: ...der as the speed approaches the stall speed The horn is activated by air from a suction hose that connects to a hole in the leading edge of the left wing The hole has a red circle around it The stall warning hole should be plugged whenever the aircraft is parked to prevent contamination and subsequent malfunction of the stall warning system NOTE Use only the factory supplied stall warning plug wit...

Page 212: ...presents primary flight instrumentation and navigation It also provides a moving map to the pilot through large format displays 7 12 2 GDU 620 DISPLAY This displays the real time true airspeed calculations and selectable winds aloft data as well as airplane ground speed GPS active waypoint distance towaypoint desired actual track and more In normal operating mode the Primary Flight Display PFD pre...

Page 213: ...ure altitude airspeed vertical speed and OAT information to the G500 system The GDC 74A provides data to the GDU 620 and GRS 77 using ARINC 429 digital interfaces The GDC 74A also communicates maintenance and configuration information to the GDU 620 using an RS 232 interface 7 12 5 GMU 44 MAGNETOMETER The GMU 44 magnetometer senses magnetic field information Data is sent to the GRS 77 AHRS for pro...

Page 214: ...Airplane Description DV 20 E AFM Page 7 50 Rev 2 22 Mar 2022 Doc No 4 01 25 E Intentionally left blank ...

Page 215: ...IONS OR REPAIRS 8 3 8 4 SERVICING 8 3 8 4 1 REFUELING 8 3 8 4 2 ENGINE OIL LEVEL CHECK 8 4 8 4 3 TIRE INFLATION PRESSURE CHECK 8 4 8 5 GROUND HANDLING ROAD TRANSPORT 8 5 8 5 1 GROUND HANDLING 8 5 8 5 2 PARKING 8 7 8 5 3 MOORING 8 9 8 5 4 JACKING 8 10 8 6 CLEANING AND CARE 8 11 8 6 1 PAINTED SURFACES 8 11 8 6 2 CANOPY 8 12 8 6 3 PROPELLER 8 12 8 6 4 ENGINE 8 12 8 6 5 INTERIOR SURFACES 8 12 8 7 GROU...

Page 216: ...nspection must be performed every year The respective inspection checklists are prescribed in the Airplane Maintenance Manual Chapter 05 For maintenanceworkonengineandpropeller the currently effective Operator s Manuals Service Instructions Service Letters and Service Bulletins of BRP Powertrain and mt Propeller must be followed For airframe inspections the currently effective checklists manuals S...

Page 217: ... Fuel burns violently and can cause injury to persons and damage to the airplane WARNING Do not get fuel on your skin Fuel can cause skin disease WARNING Connect the airplane and the fuel supply vehicle to electrical ground before refueling If you do not ground the airplane static electricity can cause fire during refueling WARNING Make sure that a suitable fire extinguisher is available at all ti...

Page 218: ...hicle 8 4 2 ENGINE OIL LEVEL CHECK 1 Open the inspection door on the top cowling 2 Remove the filler cap 3 Turn the propeller until a gurgling sound is heard 4 Remove the dip stick 5 Read the oil level from the dip stick 6 If necessary add engine oil 8 Install the dip stick and the filler cap 9 Close the inspection door 8 4 3 TIRE INFLATION PRESSURE CHECK 1 Remove dust cap from valve stem by turni...

Page 219: ...f the aircraft is towed forward without using the tow bar the nose wheel will follow the movement of the airplane It is recommended that the tow bar be used to pull the aircraft forward Towing the aircraft can be assisted by pulling on the propeller at the root just next to the propeller spinner If any additional assistance is required the aircraft may only be pushed on the trailing edge of the wi...

Page 220: ...wheel Moving Backward By following a simple procedure it is very easy to move the airplane backwards CAUTION Do not push or lift on the spinner Do not push on control surfaces 1 Push down with one hand on the aft section of the fuselage near the vertical stabilizer to lift the nose wheel 2 Push back on the leading edge of the horizontal stabilizer close to its center 3 Using this technique the air...

Page 221: ...ed For extended and unattended parking as well as in unpredictable wind conditions the airplane must be anchored to the ground or placed in a hangar Parking in a hangar is recommended When parking the airplane the flight controls lock must be installed and pitot static probe cover and stall warning plug should be fitted refer to Chapter 7 Aircraft Description When adjusting the rudder pedals to in...

Page 222: ... lock must be removed before flight The control surfaces gust lock is installed as follows 1 Move the rudder pedals fully rearward Pull straight back on the T grip do not pull up 2 Engage the control surfaces gust lock with the pedals 3 Engage the stick wrap straps around stick once 4 Attach the locks and tighten the straps For removal reverse the sequence NOTE It is recommended to cover the canop...

Page 223: ...5 3 MOORING Near the lower end of the tail fin of the airplane there is a hole which can be used to tie down the airplane to the ground Also on each wing near the wing tip an eyelet with a metric M8 thread can be installed and used as tie down points Figure 8 2 Mooring Points Locations ...

Page 224: ...M Page 8 10 Rev 2 22 Mar 2022 Doc No 4 01 25 E 8 5 4 JACKING The airplane can be jacked at the two jackpoints located on the lower side of the center wing s LH and RH root ribs as well as at the tail fin Figure 8 3 Jacking Point Locations ...

Page 225: ...gainst moisture and dampness It is also recommended not to store the airplane outside for long periods of time Dirt insects etc can be removed with water alone and if necessary with a mild detergent An automotive paint cleaner can be used for stubborn spots For best results clean the airplane after the day s flying is ended so that the dirt will not become ingrained Oil stains exhaust stains etc o...

Page 226: ...eservatives The penetration of moisture into the wooden core must be avoided by all means Should doubts arise an appropriately rated inspector must be consulted 8 6 4 ENGINE Engine cleaning is part of the scheduled inspections 8 6 5 INTERIOR SURFACES The interior should be cleaned using a vacuum cleaner All loose items pens bags etc should be removed or properly stored and secured All instruments ...

Page 227: ...any snow from the airplane using a soft brush 2 Put the airplane in a heated hangar or spray deicing fluid onto ice covered surfaces using a suitable spray bottle 3 Use a soft piece of cloth to wipe the airplane dry Approved deicing fluids are Manufacturer Name Kilfrost TKS 80 Aeroshell Compound 07 AL 5 DTD 406B ...

Page 228: ...Handling Care Maintenance DV 20 E AFM Page 8 14 Rev 2 22 Mar 2022 Doc No 4 01 25 E Intentionally left blank ...

Page 229: ...DV 20 E AFM Supplements Doc No 4 01 25 E Rev 2 22 Mar 2022 Page 9 1 CHAPTER 9 SUPPLEMENTS Page 9 1 INTRODUCTION 9 2 9 2 LIST OF SUPPLEMENTS 9 2 ...

Page 230: ...e applied in addition to the procedures given in the main part of the Airplane Flight Manual All approved supplements are listed in the List of Supplements in this Chapter The Airplane Flight Manual contains exactly those Supplements which correspond to the installed equipment according to the Equipment Inventory of Section 6 5 9 2 LIST OF SUPPLEMENTS Airplane S N Registration Date Sup No Title Re...

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