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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Instrument Panel see Figure 7.
Aircraft Flight Manual | Diamond Aircraft
Covers on the control sticks prevent loose objects from entering the control area. Fuel System A Push down with one hand on the aft section of the fuselage near loh vertical stabilizer, to lift the nose wheel.
The CG range which an airplane with a given weight must be operated within. This increase of 50 kg lbs imposes no significant change to the control and stability of the aircraft.
Power Supply A 12 V battery is connected to the master bus diqmond the battery circuit breaker 50 Amps. The navigational instruments are located on the right hand side of the instrument panel.
For every feet of altitude the aircraft can move forward 11, feet or 1. Leading edge of wing at root rib. On the upper engine cowling behind the propeller spinner.
Diamond DA20-C1 Manual
Check Avionics Master Circuit If popped, press and monitor status, Breaker If it pops again, land at the nearest suitable airport. On the instrument panel above the GPS.
Climb up to pattern altitude. Minimum Equipment, Flight and Navigation Instruments International Standard Dlamond at which air is identified as a dry gas. Electrical Powered Equipment The individual consumers e. Comments to this Manuals Your Name. The soft keys can be used to select the appropriate soft key function.
DAC1 This manual must be carried in the aircraft at all times! NOTE Steps 5, 6, 7, 8, 9, and 10 are to be performed without delay between steps. Wind Components Maximum demonstrated crosswind component: Small Inner Knob Selects a specific page within a page group.
For this reason it is highly recommended that diamonr airplane, especially the riamond edge of the wings are kept clean at all times.
Fuel Filter Bowl Drain It also contains supplemental data supplied by the airplane manufacturer which can be useful to the pilot.
Page Figure 1. The soft key labels shown depend on the soft key level or page being displayed. The outlet baffles are attached to the lower cowling with screws. Safe handling of an airplane increases and ensures your safety and provides you with many hours of enjoyment. Cabin Heat The cabin heat and defrost system, directs ram air through the exhaust heat dizmond into the cabin heat valve.
Diamond Aircraft :: Basic Manual
Mooring The tail skid of the airplane has a tie down hole which can be used to moor airplane. Jacking The DAC1 can be jacked at the two jack points located on the lower side of the fuselage’s root ribs and at the tail fin. Powerplant The DAC1 may be equipped with an optional altitude compensating fuel pump.
Calibrated airspeed; Indicated speed corrected for installation and instrument errors. Voltage supplied to the EPU receptacle should be volts nominal. The new or amended text will be indicated by a bold black vertical line in the left hand margin of a revised page.
Included in this module are two panel illumination lights and one map light. Empty Weight use the data for your Road Transport When transporting the airplane on the road, it is recommended that you use an open trailer. DAC1 pob manuals and publications. Refer to Chapter 9, Supplements, for details of optional systems and equipment. It is determined by dividing the total moment sum of the individual moments by the total weight.
The DAC1 may be equipped with an optional altitude compensating fuel pump.
Got it, continue to print. NOTE To achieve a fast descent Cruising Altitude in standard conditions: Individual supplements address each optional equipment installation. The static pressure is measured by the same probe.