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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All airplane components must be stored on a cushioned surface and secured to avoid any movement during transport. Each change of the installed Electrical Powered Equipment The individual consumers e. Normal Operation Checklist In addition 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: On the upper engine cowling behind the propeller spinner.

Aircraft Flight Manual | Diamond Aircraft

The affected pages of any revision must be inserted into the manual as well as the Record of Revisions upon receipt. Page Figure 1. Where additional performance data has been provided, beyond the basis for certification, it has not been reviewed or approved by Transport Canada. An own-ship position icon will be displayed on these charts. Flight Instruments The flight instruments are installed on the pilot’s side of the doamond panel. All loose items pens, bags etc.

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Covers on the control sticks prevent loose objects from entering the control area. The engine has high pressure wet sump lubrication. The amp meter monitors generator load which will indicate low amps when the generator is off or has malfunctioned.


Length or Altitude 1 [ft. 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 all positions of the flap toggle switch flap stops are fail-safe modify approach and landing as follows: Fuel Pump Fuel Prime International Standard Atmosphere at which air is identified as a dry gas.

This Supplement to the AFM is provided to acquaint the pilot with the limitations as well as normal, abnormal and emergency operating procedures of the Garmin G With this system it is not necessary to manually lean the mixture with altitude. Mode Annunciation window — displays mode in use.

The DAC1 may be equipped with an optional altitude compensating fuel pump. The switches for the lights are located on the instrument panel.


Small Inner Knob Selects a specific page within a page group. On the upper left corner of the instrument panel. Switches on the instrument panel below the GDU display On the flap controller Power setting below the instrument panel Garmin G Integrated Display System.

The navigational instruments are located on the right hand side of the instrument panel. Radio, Fuel Diamobd, Position Lights, etc. The pages superseded by the revision must be removed and destroyed.

Regulate warm up RPM to maintain pressure below psi limit.


Stall speeds in kts Figure 5. For every feet of altitude the aircraft can move forward 11, feet or 1. Additional for aircraft equipped with altitude compensating fuel system Electrical System Voltage is displayed both analog and digitally.

The suspension of the nose wheel is provided by an elastomer spring. For this reason you should take the time to familiarize yourself with your new airplane. Copies of the manual can be obtained through. Fuel Filter Bowl Drain Change in center of gravity is due to fuel consumption Diampnd 6. Voltmeter The voltmeter indicates the status of the electrical bus.

If equipped with an outside handle. Throttle Lever Fuel Quantity Ind. The followin g diagrams, Figure 6. The maximum speed of the crosswind component at which the manoeuvrability of the airplane during take-off and landing has been demonstrated during type certification test flights.

For this reason it is highly recommended that the airplane, especially the leading xa20 of the wings are kept clean at all times. The oil is pumped by a mechanical, fiamond driven pump. No part pph this manual may be reproduced or copied. 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. Center of Gravity Limits: December 19, REV