DAA1-VLA Aircraft Flight Manual. 8. 18/01/ Download. DA TR AFM Temporary Revision – Maximum CHT with SB installed. 09/11/ AIRPLANE FLIGHT MANUAL (english) – BASIC MANUAL. Doc. No. Description. Rev. Date. Downl. E. Airplane Flight Manual (AFM). 9. We ask that you carefully read this Airplane Flight Manual and to pay special attention to the permission of DIAMOND AIRCRAFT Austria is.
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Icing Unintentional Flight Into Icing Area Leave icing area through change of altitude or change of fa20 direction to reach area with higher outside air temp. Distance from the reference datum to the CG. Climb up to pattern altitude. For revision and subscription service please contact the following: No part of this manual may be reproduced or copied.
Flap System Failure Flap Position Indicator Failure visual check of the flap position select airspeed within the range of the white arc marked on the airspeed indicator check diwmond positions of the flap toggle switch flap stops are fail-safe modify approach and landing as follows: Fuel Pump Fuel Prime This database is updated on a day cycle.
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Internal Lighting Description 7. Voltage supplied to the EPU receptacle should be volts nominal. It is the pilot’s responsibility to adhere to the weight and balance limitations and to take into consideration the change of the center of gravity CG position due to fuel consumption.
Included in this module are two panel illumination lights and one map light. If equipped with altitude compensating fuel pump. Some DAC1 aircraft dda20 have a fuel vapor separator in the distribution manifold. Ad20 of Effective Pages revised. Operations are prohibited north of 72 degrees North and south of 70 degrees South latitudes and in the following four regions DAC1 This manual must be carried in the aircraft at all times! Around the stall warning hole in the left wing. Next to the fuel filler cap.
Empty Weight use the data for your airplane Towing Forward The airplane is most easily and safely maneuvered by hand with the tow-bar attached to the nose wheel.
It is essential that the responsible airworthiness authority be contacted prior to any alterations on the airplane to ensure that the airworthiness of the airplane is not affected.
Doc DAC1 April 06, Where additional performance data has been provided, beyond the basis for certification, it has not been reviewed or approved by Transport Canada.
On the upper engine cowling behind the propeller spinner. Cabin Heat The cabin heat and defrost system, directs ram air through the exhaust heat shroud into the cabin heat valve.
However, engine failure or other airplane related emergency situations will most dda20 never occur if the mandatory pre-flight check and maintenance are performed properly. The static pressure is measured by the same probe. Cruise The mixture control allows leaning of the fuel mixture to maximize fuel economy during cruise conditions.
NOTE The G cockpit reference guide and the G pilot’s guide contain detailed descriptions of the annunciator system and all warnings, cautions and advisories.
Voltmeter The voltmeter indicates the status of the electrical bus.
Diamond Aircraft :: Basic Manual
The pages superseded by the revision must be removed and destroyed. The affected pages of any revision must be inserted into the manual as well as the Record of Revisions upon receipt. On the right side of the aircraft above the EPU receptacle.
Normal Operation Checklist In dq20 to those items contained in Section 4, Normal Operating Procedures, Preflight Inspection, check the following items if this supplement is applicable to the aircraft you are operating: Refer to Page for index of supplements.
When 5 US gallons remain in the main tank the fuel system display is flashed an audible tone is heard and the EC displays the warning. There are no other changes to the fuel system. To print the manual completely, please, download it. Only portions of the flight manual affected by the installation are included in this supplement.
Scope and revision status can be found in the List of Effective Pages and in the Record of Revisions. Take-off Distance Figure 5.