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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP Pilot´s Operating Handbook Supplement for the DR400/120D DR400/140B DR400/180R DR400/200R DR400/RP Equipped with TAE 125 Installation TYPE ........ DR 400 MODEL No....... SERIAL No....... REGISTER No....This supplement must be attached to the EASA approved Pilot´s Operating Handbook of the DR400/120D, DR400/140B, DR400/180R, DR400/200R or DR400/RP when the TAE 125-01 or TAE 125-02-99 installation has been installed in accordance with EASA.A.S.01380 or...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP Page - ii Issue 3 - July 2014...
Date: March 16 ,2012 Office of Airworthiness Change of TC holder Initial issue C.E.A.P.R July EASA STC 10014219 Numbering of CEAPR 2014 transfer documents The parts of the text which changed are marked with a vertical line on the margin of the page.
Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP LIST OF EFFECTIVE SECTIONS Section Issue/ Revision Date July 2014 July 2014 July 2014 July 2014 July 2014 July 2014 July 2014 July 2014 Page - iv Issue 3 - July 2014...
Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP TABLE OF CONTENTS APPROVAL ....................iii LOG OF REVISIONS ................iii LIST OF EFFECTIVE SECTIONS ............iii ABBREVIATIONS ..................xi SECTION 0 GENERAL CONVENTIONS IN THIS HANDBOOK ..........0-1 FOR DR400 AIRCRAFT FROM SERIAL NUMBER 2500 AND UP ..0-1 UPDATE AND REVISION OF THE MANUAL ........
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP SECTION 2 LIMITATIONS APPROVED OPERATION ..............2-1 MAXIMUM ALTITUDE................2-1 FLIGHT LOAD FACTOR LIMITS AT MAXIMUM WEIGHT ....2-2 MAXIMUM AUTHORIZED WEIGHTS ..........2-2 WEIGHT AND BALANCE ..............2-2 LOAD PLANNING ................. 2-3 ENGINE OPERATING LIMITS .............. 2-3 ENGINE INSTRUMENT MARKINGS ...........
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP SECTION 3 EMERGENCY PROCEDURES ENGINE FAILURE OR LOSS OF POWER ........... 3-2 During takeoff roll ................... 3-2 Immediately after takeoff ............... 3-2 During flight .................... 3-3 LANDING WITHOUT ENGINE POWER ..........3-4 Restart after engine failure ..............3-5 FADEC malfunction in flight ..............
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP SECTION 4 NORMAL PROCEDURES NORMAL OPERATING SPEEDS ............4-1 Best rate of climb speed ................ 4-1 Maximum operating speed in turbulent air ..........4-1 Never Exceed speed ................4-1 Maximum speed ..................4-1 Landing speed, final approach .............. 4-1 PRE-FLIGHT INSPECTION ..............
Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP ABBREVIATIONS Thielert Aircraft Engines GmbH, developing manufacturing company of the Centurion 2.0 S engine, (since July 2013, Technify Motors GmbH). FADEC Full Authority Digital Engine Control CED 125 Compact Engine Display. Multifunctional instrument for indication of engine data of the TAE 125-01 and TAE 125-02- 99 engine.
Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP SECTION 0 GENERAL CONVENTION IN THIS HANDBOOK This manual contains the following convention and warnings. They should be strictly followed to rule out personal injury, property damage, and impairment to the aircraft´s operating safety or damage to it as a result of improper functioning.
Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP Due to the specific characteristic of the TAE 125 engine, all of the information from the original DR400 flight manual recognized by EASA are no longer valid with the reference to: carburetor and carburetor pre-heating, ...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP installation and is equipped with the following operating and display elements: Rocker Switch "Battery" The battery must be switched ON in normal operation. The circuit breaker below the Rocker Switch "Battery" disables the alternator. The alternator can be left ON always. Key Switch "Starter"...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP EXTERNAL POWER PLUG ELECT . PUMP LANDING LIGHT BAT T ERY BATTERY T AXI LIGHT NAVIGAT ION LIGHT ALT ERNAT OR S T ROBE ALTERNATOR LIGHT ENGINE MAS T ER GL OW PITOT HEAT (optional) PIT OT HEAT...
Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP FADEC-RESET In case of a FADEC-warning, one or both FADEC warning lamps are flashing. If then the "FADEC" Test Knob is pressed for at least 2 seconds: a) the active warning lamps will extinguish if it was a LOW category warning.
Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP ENGINE OIL Oil quantity between dipstick min and max indication: ....1 liter Total engine capacity including filters and coolers: ....6.7 liters Approved grades: ........Refer to Section 2 – Limitations CAUTION: Use the approved oil with exact declaration only! FUEL SYSTEM The fuel system of the TAE 125 installation includes a variant of the...
Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP If Diesel fuel is used, Diesel fuel according DIN EN 590 has to be used exclusively. Note: There differences national supplements to EN 590. Approved are Diesel fuels with the addition DIN EN 590. Fuel capacity Total usable Tank...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP ENGINE Engine-driven Excess from fuel pump Excess from fuel pump fuel injectors F U E L F IL T E R Fire-wall FADEC Fuel quantity Electric fuel pump, 10 12 14 Fuel Fuel ½ O F F F U E L with fuel filter...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP ENGINE Engine-driven Excess from fuel pump Excess from fuel pump fuel injectors F U E L F IL T E R Fire-wall FADEC Fuel quantity Electric fuel pump, 10 12 Fuel Fuel ½ F U E L with fuel filter low-level temperature...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP Figure 1-5 Instrument panel model #1 Note: The avionics instrument panel is shown as an example only. Issue 3 – July 2014 Page 1 - 11...
Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP Instrument panel model #1 Fonction Fonction Fonction Airspeed indicator Warning lights Fuel tank valve Lights test & Elevator trim control Gyro horizon day/night dimmer valve switch Instrument panel Elevator trim Altimeter light position indicator Safety switches: landing light, taxi Cabin heat /...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP Figure 1-6 Instrument panel model #2 Note: The avionics instrument panel is shown as an example only. Issue 3 – July 2014 Page 1 - 13...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP Instrument panel model #2 Fonction Fonction Fonction Lights test & Elevator trim Airspeed indicator day/night dimmer position indicator switch Cabin heat Instrument panel Gyro horizon windshield defrost light control Safety switches: landing light, taxi Altimeter light, strobe light, Cabin heat...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP Figure 1-7 Instrument panel model #3 Note: The avionics instrument panel is shown as an example only. Issue 3 – July 2014 Page 1 - 15...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP Instrument panel model #3 Fonction Fonction Fonction Airspeed indicator Glow light Clock / chronometer Gyro horizon FADEC test button Hourmeter CED-125 lighting Altimeter Circuit breakers knob CED test / warning Turn coordinator Fresh air vent switch off Electric throttle Avionics Master...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP Figure 1-8 Instrument panel model #4 Note: The avionics instrument panel is shown as an example only. Issue 3 – July 2014 Page 1 - 17...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP Instrument panel model #4 Fonction Fonction Fonction Cabin heat Airspeed indicator Glow light windshield defrost control Gyro horizon FADEC test button Clock / chronometer CED-125 lighting Altimeter Hourmeter knob CED test / warning Turn coordinator Circuit breakers switch off Electrical throttle...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP ”Three-display“ and “four-display“ instruments Example Of the Westach triple Example of the Westach quad indicator installed on models #1 indicator installed on model #3 and #2 Compact Engine Display CED-125 Figure 1-4 CED-125 detail Issue 3 –...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP HEATING AND VENTILATION Figure 1-5 Heating and Ventilation 1 Fresh Air Intake 2 Heat Exchanger 3 Warm Air Distribution Box 4 Warm Air Distribution Box 5 Forward / Aft Selection 6 Defrost / Heating Selection Box 7 Defrost Jet 8 Forward Heating 9 Aft Heating...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP Heating Control Settings Function Pulled Pushed Control 0 Heat ON/OFF - Button Lock Control 1 Heating ON/OFF FRONT WINDSHIELD Control 2 Defrost / Heating HEATING DEFROST Control 3 Front / Rear select. REAR FRONT Table 1-6 Heating Control Settings Figure 1-6 Heat Control Placard, Right Cabin Side Wall This STC installation has a fourth control (Control 0 in table above).
Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP FLIGHT LOAD FACTOR LIMITS AT MAXIMUM WEIGHT (2006 lb) 910 kg (category “U“): Flaps up ............n between -2.2 and +4.4 Flaps down ..................n = +2 (2161 lb) 980 kg (category "N"): Flaps up ............n between -1.9 and -3.8 Flaps down ...................
Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP LOAD PLANNING (Refer also to weight and balance chart, section 6) The weight of the engine oil, as well as the unusable fuel must be included in the empty weight of the aircraft. Weight kg (lb) m (in) 2 x 77...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP Engine operating limits for takeoff and continuous operation ▲ WARNING: It is not allowed to start the engine outside of these temperature limits. Note: operating limit temperature temperature limit below which the engine may be started, but not operated at the takeoff RPM.
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP Minimum fuel temperature limits in the fuel tanks: Minimum permissible fuel Minimum permissible fuel Fuel temperature in the fuel temperature in the fuel tank before takeoff tank during the flight Jet A-1, JET A, Fuel No.3 JP-8, - 30°C - 35°C...
Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP ENGINE INSTRUMENT MARKINGS The engine data of the TAE 125 installation to be monitored are integrated in the combined engine instrument CED-125. The ranges of the individual engine monitoring parameters are shown in the following table.
Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP PLACARDS JET A1 (ASTM 1655) DIESEL (EN590) litres 24.2 imp / 29 US Gal Figure 2-1 Near the Fuel Tank Caps: 110 liters JET/Diesel Fuel JET A1 (ASTM 1655) ONLY litres 11 imp / 13.2 US Gal Figure 2-2 Optional Extended Range Tank HUILE DR 400/135 CDI OIL DR 400/CDI...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP Figure 2-4 Near the CED FUEL ( LITER S ) F = 100 ¾ = 75 ½ = 50 ¼ = 25 E = 0 T EST / A C K Figure 2-5 Near their respective gauges or switches FUEL ENGINE FADEC...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP FUEL T(°C) FUEL QTY (litres) indicated MAIN T ANK OP T . T ANK Figure 2-8 If optional extended range fuel tank is installed, placard must be placed near to the fuel gauge. Figure 2-9 If optional extended range fuel tank is installed, placard must be placed near the fuel transfer control.
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP SECTION 3 EMERGENCY PROCEDURES INDEX OF CHECKLISTS ENGINE FAILURE OR LOSS OF POWER ........... 3-2 During takeoff roll ................... 3-2 Immediately after takeoff ............... 3-2 During flight .................... 3-3 LANDING WITHOUT ENGINE POWER ..........3-4 Restart after engine failure ..............
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP ENGINE FAILURE OR LOSS OF POWER During takeoff roll Thrust Lever ................IDLE Apply brakes and hold direction. Avoid obstructions. Engine Master switch ..............OFF Battery and ALT CB ..............OFF Fuel selector................OFF Emergency ground egress ..........
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP During flight Establish glide: Flaps retracted ..........(78 KIAS) 144 km/h (In these conditions, without wind, the aircraft covers approx. 8 times its height above ground). Locate suitable field. If altitude is sufficient to restart: Electric fuel pump ................
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP LANDING WITHOUT ENGINE POWER Look for a suitable landing area: Airspeed ........144 km/h (78 KIAS) flaps retracted 139 km/h (75 KIAS) flaps T/O Seat belts and harness ............. Tight Before landing: Electric pump ................OFF Fuel selector................
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP Restart after engine failure Note: If altitude permits and a restart is possible. Airspeed ......... Flaps retracted (78 KIAS) 144 km/h [max. 100 KIAS, min. 70 KIAS] Reliable restart altitude ......... Below 13 000 ft Battery and ALT CB ............
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP FADEC malfunction in flight Note: FADEC consists components that are independent of each other: FADEC A and FADEC B. In case of malfunctions in the active FADEC, it automatically switches to the other. a) One FADEC Lamp is flashing (1) Press FADEC-Test knob at least 2 seconds (2) FADEC Lamp extinguished (LOW category warning):...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP b) Both FADEC Lamps are flashing Note: The load display may not correspond to the current value. (1) Press FADEC-Test knob at least 2 seconds (refer to section 1 “FADEC Reset”) (2) FADEC Lamps extinguished (LOW): a) Continue flight normally, b) Inform service center after landing.
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP c) Abnormal engine behavior Note: FADEC system normally switches automatically between FADEC A and B in case of malfunction, order select "healthiest" component. If this automatic switching doesn't work, it is possible to manually force the system to switch to FADEC B only, and check for improvement in engine behavior.
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP ENGINE SHUT-DOWN IN FLIGHT Note: If it is necessary to shut down the engine in flight (for instance, abnormal engine behavior does not allow continued flight, fuel leak, fire, etc.): 1) Reduce speed ........Below (100 KIAS) 185 km/h 2) Engine master switch...............
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP FIRE Engine fire on the ground, during starting 1) Engine master switch .............. OFF 2) Fuel selector ................OFF 3) Electric fuel pump..............OFF 4) Battery + alternator switch ............OFF 5) Emergency ground egress ........... As required Extinguish the flames with a fire extinguisher, wool blankets or sand.
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP Electrical fire Note: case electrical fire (smell fumes indicating wire insulation burning): 1) All electrical equipment and c (after brief call) ....... OFF leave Alternator, Battery and Engine Master ON 2) Cabin ventilation ..............OFF 3) Cabin heat ................
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP ROUGH ENGINE OPERATION Oil pressure too low (< 2.3 bar in cruise or <1.2 bar at idle power) (1) Reduce power as quickly as possible (2) Check oil temperature: If the oil temperature is high or near operating limits, i) Land as soon as possible ii) Be prepared for an emergency landing...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP Oil temperature too high (1) Increase airspeed and reduce power as quickly as possible (2) Check oil pressure. If the oil pressure is lower than normal (<2.3 bar in cruise or <1.2 bar at idle), i) Land as soon as possible ii) Be prepared for an emergency landing iii) Expect engine failure...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP “Cool level” light illuminates 1) Increase airspeed and reduce the power 2) Cabin heat ................OFF 3) Monitor coolant temperature 4) Monitor oil temperature 5) If coolant temperature and/or oil temperature are rising into amber and towards red range: i) Land as soon as practical ii) Be prepared for an emergency landing...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP Propeller RPM too high Note: If propeller RPM above 2300 (red range): 1) Reduce power 2) Reduce airspeed below 100 KIAS (185 km/h) or as appropriate to prevent propeller overspeed 3) Set power as required to maintain altitude and land as soon as practical.
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP ICING ▲ WARNING: It is prohibited to fly in known icing conditions. Icing has a very strong negative effect on the aerodynamic characteristics of the aircraft. Stalling speed increases. Proceed as follows when inadvertently encountering icing: Pitot heat switch ............
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP ELECTRICAL POWER SUPPLY MALFUNCTION Note: The TAE 125 requires an electrical power source for its operation. If the alternator fails, the only power source will be provided by the battery. The time the engine can run on battery alone will depend on total electrical consumption supported by the battery, i.e.
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP If the “ALT“ light is lit or the ammeter shows battery discharge during normal engine operation for more than 5 minutes Alternator circuit breaker ..........Check ON CAUTION: FADEC supplied battery only until this point, the RPM can momentarily drop, when the alternator will be switched on.
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP INADVERTENT SPIN Should a spin occur, apply the following procedure: Power Lever ............... Idle (pull) Rudder ........Full opposite to direction of rotation Elevator ................. Neutral Ailerons ................Neutral Once the rotation is stopped, bring rudder to neutral position and recover within flight limitations.
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP SECTION 4 NORMAL PROCEDURES NORMAL OPERATING SPEEDS The speeds listed below are indicated airspeeds recommended for normal operation of the aircraft. These speeds are based on a standard aircraft, operated at max. take- off weight, in standard atmosphere and at sea level. They may vary from one aircraft to another depending on the equipment installed, the conditions of the aircraft and of the engine, the atmospheric conditions and the skills of the pilot.
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP PRE-FLIGHT INSPECTION To be performed before each flight. This inspection may be shortened for intermediate landings on route. Figure 4-1 Pre-flight inspection Issue 3 – July 2014 Page 4 - 2...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP Master engine switch ................OFF Avionics master switch (if equipped) ...........OFF Controls ................Free and correct Battery switch ..................ON ▲ WARNING: When turning on the battery switch, using an external power source, or pulling the propeller through by hand, treat the propeller as if the Engine Master switch was on.
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP a) Horizontal stabilizer ........Surface condition, hinge wear in tolerance b) Rudder ........Check hinge wear in tolerance a) Static vent ............ Clean, unobstructed a) Flap and aileron ....... Check condition and hinges b) Wing tip and navigation lights (optional) ... Check condition a) Stall warning ..........
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP a) Nose gear ......Check attachment and condition of fairing, normal shock absorber compression, tire inflated, tow bar removed b) Canopy cleanliness ............Check Left main landing gear ......Check attachment and condition of fairing, normal shock absorber compression, tire inflated b) Pitot .............
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP 11) Circuit breakers ................ON Note: electronic engine control needs electrical power source for its operation. For normal operation, battery switch and alternator circuit breaker have to be ON. Separate switching is only allowed for tests and in event of emergencies.
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP 13) Check ........... Oil pressure / Idle RPM 890 CAUTION: after seconds minimum pressure of 1 bar is not indicated, shut down the engine immediately! 14) “Engine“ resp. “CED“ Caution light ......Acknowledge 15) ALT light .................
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP WARM UP Cabin heat can be pulled to facilitate quicker coolant warming. Let the engine warm up about 2 minutes at idle Increase to not more than 1400 RPM until oil temperature minimum 50 °C, coolant temperature minimum 60 °C (All CED LEDs...............
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP (FADEC self-check: a) Thrust Lever ......... IDLE (both FADEC lamps should be OFF) b) FADEC test button ....... PRESS and HOLD button for entire test c) Both FADEC lamps ........ON, RPM increases Note: If the FADEC test does not start, verify if the thrust lever is in IDLE position.
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP ▲ WARNING: The whole test procedure has to be performed without any discrepancy. In case the engine shuts down or the FADEC lamps are flashing, takeoff is PROHIBITED. This applies even if the engine seems to run without failure after the test.
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP TAKEOFF Normal takeoff 1) Thrust lever ............FULL FORWARD 2) Takeoff RPM before rotation ......... 2300 RPM 3) Takeoff speed ..........106 km/h (57 KIAS) 4) Initial climb speed ........... 120 km/h (65 KIAS) 5) After obstacles clearance, Reduce angle of climb to reach ......
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP CLIMB Normal climb (flaps up) Best rate of climb: 145 km/h (78 KIAS) from 0 to 9 500 ft, 139 km/h (75 KIAS) up to 11 500 ft, 133 km/h (72 KIAS) above 11 500 ft. A climb at higher speed, when best rate is not required, will provide for more forward visibility.
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP DESCENT Power ....As required to maintain the desired descent path Pull cabin heat to keep the coolant warm if power setting is low. If coolant temperature in amber range and engine caution lamp illuminated, increase power to recover green coolant temperature range.
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP LANDING Short landing Flaps ............ (2nd notch) landing position Approach speed, with Thrust Lever setting .......... 115 km/h (62 KIAS) After touchdown, brake heavily keeping nose up with elevator and retracting the flaps. Overshoot procedure Thrust Lever ............Full power (push) Speed ..............
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP PARKING BRAKE USE Brake on Press on both pedals. Keep pressure on while pulling the parking brake control. Release the pressure on the pedals, the parking brake control must remain in pulled position. Pull the parking brake control. Press on both pedals, then release the pressure on the pedals.
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP SECTION 5 PERFORMANCE AIRSPEED INSTALLATION CALIBRATION No change STALL SPEEDS Engine idle km/h (kt) Weight 980 kg (2161 lb) Bank angle 0° 30° 60° Flaps up 99 (54) 106 (58) 140 (76) Flaps 1st notch, take off position 92 (50) 98 (53) 130 (70)
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP TAKEOFF PERFORMANCE At max. take-off weight 980 kg (2161 lb), without wind, flaps in takeoff position, engine full power Conditions No wind, flaps in takeoff position (1 notch), engine full power on brakes before release ...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP Take off distance [m] at 880 kg (1940 lb) Pressure ISA conditions ISA + 10°C ISA + 20°C Altitude to 50 ft to 50 ft to 50 ft [ft] To lift-off To lift-off To lift-off height height height...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP CLIMB PERFORMANCE At sea level Flaps takeoff Flaps retracted Best angle of climb 120 km/h (65 KIAS) 120 km/h (65 KIAS) Best rate of climb 141 km/h (76 KIAS) 144 km/h (78 KIAS) Table 5-4 Climb performance at sea level Rate of climb, flaps retracted, 980 kg (MTOW): Climb speeds: 78 kt from 0 to 9500 ft...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP Rate of climb, Flaps retracted, 880 kg Pressure Rate of climb [ft/min] at 880 kg (1940 lb) Altitude ISA+10°C ISA+20°C [ft] conditions 1000 1500 2000 2500 3000 3500 4000 4500 5000 5500 6000 6500 7000 7500 8000...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP Time to climb, flaps retracted, 980 kg Climb speeds: 78 kt from 0 to 9500 ft 75 kt up to 11500 ft 72 kt above. Pressure Time to climb [min] at 980 kg (2161 lb) (MTOW) Altitude ISA conditions ISA+10°C...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP Pressure Time to climb [min] at 980 kg (2161 lb) (MTOW) Altitude ISA conditions ISA+10°C ISA+20°C [ft] 12 500 24.2 24.5 25.8 13 000 26.0 26.3 27.5 13 500 27.9 28.2 29.5 14 000 30.1 30.4 31.6...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP Pressure Time to climb [min] at 880 kg (1940 lb) (MTOW) Altitude ISA conditions ISA+10°C ISA+20°C [ft] 9500 11.3 11.4 11.9 10 000 11.9 12.1 12.6 10 500 12.8 12.9 13.5 11 000 13.6 13.8 14.3 11 500...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP CRUISE PERFORMANCE At maximum takeoff weight 980 kg (2161 lb), in standard atmosphere. Range and endurance calculations take into account 45 min. reserve (at 55% load) at destination. Assumption is made that higher consumption for climb is compensated by a cruise descent.
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP Standard and ISA conditions Standard Tank Press. Auxiliary Tank Engine Alt. 109 Liters Fuel flow Load 159 Liters [ft] KCAS KTAS [l/h] Hours Hours 8000 21.2 8000 19.6 8000 18.1 8000 16.7 8000 15.3 8000 13.9 10.4...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP LANDING PERFORMANCE At max. takeoff weight 980 kg (2161 lb) Without wind, flaps in landing position, engine at idle. Concrete, flat and dry runway Altitude Temperature Weight 980 kg (2161 lb) Landing Distance Landing Distance (ground touch) from 15 m (50 ft) Ft (m)
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP SECTION 6 WEIGHT AND BALANCE The following nomograph is used to determine balance of the DR400. Remember that diesel and JET FUEL are heavier than AVGAS, and they carry more energy per volume. Because the fuel in the Robin series is in an aft location, fuel consumption shifts the CG forward.
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP USE OF WEIGHT AND BALANCE DIAGRAM 1. Calculate the weight of the fully loaded aircraft: Empty weight (from the Weight & Balance Data Sheet) + pilot and passengers weights + baggage weight + standard fuel (1 liter JET A-1 = 0.81 kg) Make sure that the total weight does not exceed 980 kg (2161 lb) in cat.
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP (lb) 980 (2161) Cat. N 910 (2006) Cat. U 720 (1587) 0.410 0.428 0.564 0.205 (in) (16.16) (16.85) (22.2) % of mac Figure 6-2 Use of Weight and Balance Diagram ▲ WARNING: For the calculation of the aircraft center of gravity, do not use the values of empty aircraft weight and moment indicated in the above example! Use the values indicated in the latest licensed weight...
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Supplement DR400/120D, DR400/140B, DR400/180R, DR400/200R, DR400/RP SECTION 7 SUPPLEMENTS TABLE OF CONTENTS No supplements Issue 3 – July 2014 Page 7 - 1...