Related Manuals for Glaser-Dirks DG-800 A
Summary of Contents for Glaser-Dirks DG-800 A
- Page 2 Flight manual DG-800 A 0.1 Record of revisions Any revision of the present manual, except actual weighing data, must be recorded in the following table and in case of approved sections endorsed by the responsible airworthiness authority. The new or amended text in the revised page will be indicated by a black vertical line in the right hand margin, and the Revision No.
- Page 3 Flight manual DG-800 A 0.2 List of effective pages Section page issued replaced replaced Sept. 93 see manual amendments " " Sept. 93 Sept. 93 Febr. 94 Sept. 93 " " " App. " Oct. 95 " " " "...
- Page 4 Flight manual DG-800 A 0.2 List of effective pages (cont.) Section page issued replaced replaced App. 4.10 Sept. 93 " 4.11 " March 97 " . 4.12 " " 4.13 " " 4.14 " " 4.15 " " 4.16 "...
- Page 5 Flight manual DG-800 A 0.2 List of effective pages (cont.) Section page issued replaced replaced Sept. 93 " " Oct. 95 " " June 99 Dec. 00 " " March 97 Oct. 04 " " 7.10 " 7.11 " Oct. 04 7.12...
- Page 36 Flight manual DG-800 4.2.3.4 Storage of the pump system (see a) To increase the lifetime of the pump it is better not to empty the pump, but to store the pump filled with fuel. Therefore remove hose A by disengaging the coupling . The couplings C + D are closing the fuel lines to the pump when disengaged.
- Page 37 Flight manual DG-800 4.2.5 Rigging and derigging the wing tip extensions (Option) 1. Insert the wing tip extensions into the wing. Press in the locking pin with your finger. Insert the wing tip as far as the flaperon connector starts to slide into the flaperon slot.
- Page 64 Flight manual DG-800 5.2.3 Take off performance The data is valid for take off from dry level hard surface, no wind and proper condition of engine, propeller and aircraft. The take off procedure is to be executed according to 4.5.2. = take off roll = take off distance to 15 m (50 ft.) altitude = temperature on ground...
- Page 86 Flight manual DG-800 29) Throttle handle with integrated starter button Throttle The starter button is only activated when the engine is extended and the ignition switch is in the "on" position. Starter As soon as an engine speed of 1200 RPM is exceeded, the starter will be switched off.
- Page 90 Flight manual DG-800 44) Outside air temperature OAT indication (Option). Switch No. 43 to the left: OAT in °C is displayed on the right display. Note: If the option is not installed and you press switch No. 43 to the left nothing will be displayed on the right display.
- Page 95 Flight manual DG-800 7.11. Powerplant 7.11.1 Engine Rotax 505 Manufacturer: Bombardier Rotax at Gunskirchen, Austria Type: aircooled 2-cylinder twostroke engine with dual electronic ignition. Take off power: 43 PS (31 KW) at 6200 RPM Reduction: 2 : 1 by toothed drive belt 7.11.2 Propeller MT 136 R 75 - 1 B Manufacturer...
- Page 104 Flight manual DG-800 8.8 cont. 5. Fuel leaks out of the carburettors see 4 A 6. Loss of electrical power see flight manual sect. 3.10. 7. Ignition problems No spark: - on 1 spark plug of one ignition circuit: Spark plug, ignition cable or electronic box defective. - on both spark plugs of one ignition circuit: Too low starting r.p.m.;...
- Page 105 Flight manual DG-800 Section 9 Supplements Introduction List of inserted supplements Winglets at the 18m wingtips Emergency bail-out aid NOAH Issued: June 2002 TN 873/18...
- Page 106 Flight manual DG-800 Introduction This section contains the appropriate supplements necessary to safety and efficiently operate the sailplane when equipped with various optional systems and equipment not provided with the standard sailplane. List of inserted supplements Date of Document No. Title of the inserted supplement insertion July 1997 Winglets at the 18m wingtips...
- Page 107 Flight manual DG-800 Winglets at the 18m wingtips Section 1 Introduction In the following text the changes to those sections of the flight manual which are effected by the installation of winglets at the 18m wingtips will be given Brief description In addition to the wing configurations described in sections 1 up to 8 of the flight manual winglets at the 18m wingtips are approved.
- Page 108 Flight manual DG-800 Emergency bail-out aid NOAH Section 1 Introduction In the following text the changes to those sections of the flight manual which are effected by the installation of winglets at the 18m wingtips will be given Brief description NOAH is a system to facilitate the bail-out of the cockpit in an emergency.
- Page 109 Flight manual DG-800 Section 3 Use of NOAH in case of an emergency bail out: Note: We recommend strongly the use of an automatic parachute. Only with an automatic parachute will the bail out procedure be nearly automatic and precious time and altitude can be saved.
- Page 110 Flight manual DG-800 Section 7 The NOAH actuation handle is located at the right hand side abeam the control stick, it is marked black and yellow. NOAH A sticker is wrapped around the actuation handle and the guiding airbag tube for the actuation cable. The sticker serves as an additional means to guard against inadvertent operation.