DG-1000T - DG Flugzeugbau

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Flight manual DG-1000T 1) Control column The rear control stick is removable. First open the snap shackle at the trim release lever to disengage the trim cable. Pull out the stick after unscrewing the cap nut. 2) Release lever for the trim mechanism - green Operation see section 7.5 elevator control 3) Trim position indicator and trim preselection lever 4) Tow release knob - yellow 5) Rudder pedal adjustment knob – black (only in front cockpit) By pulling on the knob, the locking pin will be disengaged and the rudder pedals can be pulled back towards the pilot or pushed forward away from the pilot. 6) Front instrument panel After removing the side screws at the base 2 x M 6 and after removing the screws attaching the cover to the panel 6 x M 4, the cover can be removed towards the front. The panel remains in the aircraft. 7) Compass installation position 8) Radio installation position 9) Rear instrument panel After removing the side screws attaching the panel to the cover (4 x M 4) the panel can be hinged backwards into the cockpit (take out the control stick first!). Issued: July 2005 7.4 Flight manual DG-1000T 10) Undercarriage retraction - extension handle - black back = retracted, front = extended, The undercarriage is locked in the extended position by an overcentre locking arrangement and an additional safety catch. The handle is to be turned towards the cockpit wall, so that the locking catch will engage. In retracted position the landing gear is locked over centre. With TN1000/13 executed, standard from ser. no. 10-133 on: An additional landing gear positive locking device (notch and latch at the landing gear struts) secures the landing gear in the extended position. An additional catch in the front upper area of the landing gear box secures the landing gear in retracted position. 11) Airbrake handle - blue The wheel brake is operated at the end of the airbrake handle travel. Parking brake combined with an airbrake securing device (Piggotthook): Pull the airbrake handle back to actuate the wheelbrake and rotate the handle to the cockpit wall. A detent will engage in one of 4 notches to hold the system in this position. In case the airbrakes mistakenly haven’t been locked, a detent engages in one of several notches to avoid inadvertent deployment of the airbrakes. To open and to close the airbrakes the operating handle must be rotated into the cockpit so far that the detent passes the notches. 12) Constantly open de-misting air vents 13) Main air vent 14) Main air vent operating knob pushed to front = closed pulled = open 15) Swivel air vents 16) Canopy opening handle - white-red towards the nose = closed into cockpit = open Issued: February 2008 TN 1000/13 7.5
Flight manual DG-1000T 17) Canopy emergency release handle - red towards the nose = closed into cockpit = open For emergency release also handle 16 has to be operated! 18) Water ballast dump handles - silver lever on top of the handles = fintank Rotate backward to dump. The wing waterballast can only be dumped after dumping the fin waterballast upper handle = right wingtank lower handle = left wingtank forward = valve closed into the cockpit = valve open. The wing ballast can only be dumped after opening the fin tank 19) Push to talk button (Option) (placard only if installed in the instrument panel) 20) 12 V socket for charging the batteries and socket for headset (Option), front and rear cockpit.. 21) Adjustment strap for the rear seat shell (to be operated on the ground) 22) Selector switch for additional batteries (Option), up = internal battery centre position = off down = additional batteries 23) Control light for the trim ballast box in the fin: The control light in the front instrument panel starts blinking after each transaction Senden transmit intern off extern Trim-ballast box in the fin Min. load in the front seat kg kg box empty box filled with the weights. By counting the amount of blinks, the amount of ballast can be determined. For a heavy weight 2 blinks appear and 1 blink for a light weight, this means 10 blinks if the box is filled up completely. After a pause of 2-3 seconds the blinking will be repeated etc.. The blinking can be stopped by pressing on the control light. Pressing again on the control light reactivates the blinking feature. A switch will be operated by the locking pin of the ballast box cover. As long as the switch is not closed, the control light for the ballast box will blink with doubled speed without interruption. The blinking can’t be switched off by pressing on the control light. Issued: July 2005 7.6 Flight manual DG-1000T 24. DEI-NT with integrated ignition switch: Switching up the ignition (the toggle has to be pulled out for switching). raises the powerplant to its operating position automatically Switching off the ignition: First the powerplant will be retracted to the position for stopping the propeller from turning. the powerplant will remain in this position until the propeller stopped turning. Than the powerplant will be automatically retracted a further 5° and the propeller stopper moves forward in the propeller circle. You may turn the propeller into the position for retraction (ignition switched off) by pressing the starter button. As soon as the propeller is in the position for retraction (close to the stopper) the engine will retract by itself. Description of the DEI-NT see section 7.4. 25. Socket for data download from the DEI-NT 26. Main switch (key switch) Turn anticlockwise: off, Turn clockwise first position: In this position the 12V socket is live for charging the battery- Turn clockwise second position: on With this main switch the complete electric power supply will be cut off. After taking out the main switch key the motorglider can't be operated. 27. Manual retraction – extension switch for the powerplant man. Any operation of this switch switches off the automatic extension-retraction system (only with ignition switched off). Operation of the ignition switch reactivates the automatic system. up = extension down = retraction. Hold the switch until the extension procedure stops. Note: Extend the engine manually on the ground prior to take-off or for maintenance work. Manual retraction only to be used in the air if the automatics don't work. Make sure, that the propeller is vertical. 28. Fuel cock – red zu Brandhahn auf to the front = open closed fuel cock open to the rear = closed Close the fuel cock only in an emergency (see chapter 3) Issued: July 2005 7.7
Page 1 and 2: DG Flugzeugbau GmbH Otto-Lilienthal
Page 3 and 4: Flight manual DG-1000T 0.2 List of
Page 5 and 6: 0.3 Table of contents Flight manual
Page 7 and 8: Flight manual DG-1000T 1.4 Descript
Page 9 and 10: Flight manual DG-1000T 2.1 Introduc
Page 11 and 12: Flight manual DG-1000T Cylinderhead
Page 13 and 14: Flight manual DG-1000T 2.12 Kinds o
Page 15 and 16: 2.20 Other limitations Flight manua
Page 17 and 18: Flight manual DG-1000T 3.5 Spin Rec
Page 19 and 20: Flight manual DG-1000T 3.15 Loss of
Page 21 and 22: Flight manual DG-1000T 4. Rigging o
Page 23 and 24: Flight manual DG-1000T 4.3 Daily In
Page 25 and 26: 4.4 Pre-flight inspection Flight ma
Page 27 and 28: Flight manual DG-1000T 4.5.4.2 Stop
Page 29 and 30: Flight manual DG-1000T 4.5.7.2 Fin
Page 31 and 32: Spins Flight manual DG-1000T Cautio
Page 33 and 34: Flight manual DG-1000T Slow roll Af
Page 37 and 38: Flight manual DG-1000T 5.3.3 Flight
Page 39 and 40: 6 Mass (weight) and balance Flight
Page 41 and 42: Flight manual DG-1000T 6.8.4 Batter
Page 43 and 44: Flight manual DG-1000T 6.8.10 DG-10
Page 45: Flight manual DG-1000T 7.1 Introduc
Page 49 and 50: 7.4 DEI-NT Operation ignition switc
Page 51 and 52: Flight manual DG-1000T CAUTION: If
Page 53 and 54: Flight manual DG-1000T 7.7 Landing
Page 55 and 56: Flight manual DG-1000T 7.15 Pitot a
Page 59 and 60: Flight manual DG-1000T Plexiglas ca
Page 61 and 62: Section 2 Limitations subsections a
Page 63 and 64: Flight manual DG-1000T 4.5.12.3 Res
Page 65: 7.14 Electrical system Subsection a

DG-1000T - DG Flugzeugbau

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