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Flight Manual DG-1000M

 

Issued: July 2014  

TN1000/23 

Copyright DG Flugzeugbau GmbH - any copy or publishing prohibited

 

0.2

 

0

 

Revisions 

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 under lying document for the 
revision and the date will be shown on the bottom of the page. 

 

Rev. 
No. 

Affected 
Pages/section 

Description Issue 

Date 

EASA 
Approval 
Date 

Inserted 
Date 
Signature

Title, 0.1, 0.2, 
0.4÷0.7, 1.5, 2.5, 2.7, 
2.10, 2.11, 2.13, 
2.14, 3.2, 4.7, 4.9 
÷4.11, 4.14, 4.15, 
4.21, 4.24, 4.29, 
4.33, 5.1, 5.4 ÷ 5.12, 
6.1 ÷ 6.3, 6.5, 6.7, 
6.9 ÷ 6.15, 7.2, 7.6, 
7.9, 7.12, 7.25 ÷ 
7.28, 7.30, 8.3 

Manual revision 
TN1000/22 

October 
2012 

10. Dec. 

2012 

 

0.2, 0.4 ÷ 0.6, 2.5, 
2.6, 4.33, 7.19, 7.30 

Manual revision 
TN1000/23 

July 
2014 

7 August 

2014 

 

 

Summary of Contents for DG-1000M

Page 1: ...age will be indicated by a black vertical line in the right hand margin and the under lying document for the revision and the date will be shown on the bottom of the page Rev No Affected Pages section...

Page 2: ...ctober 2010 October 2012 1 6 October 2010 2 EASA app 2 1 October 2010 2 2 October 2010 2 3 October 2010 2 4 October 2010 2 5 October 2010 October 2012 July 2014 2 6 October 2010 July 2014 2 7 October...

Page 3: ...ctober 2012 4 16 October 2010 4 17 October 2010 4 18 October 2010 4 19 October 2010 4 20 October 2010 4 21 October 2010 October 2012 4 22 October 2010 4 23 October 2010 4 24 October 2010 October 2012...

Page 4: ...2 6 13 October 2012 6 14 October 2012 6 15 October 2012 7 7 1 October 2010 7 2 October 2010 October 2012 7 3 October 2010 7 4 October 2010 7 5 October 2010 7 6 October 2010 October 2012 7 7 October 20...

Page 5: ...ignition If you reduce the engine speed the ignition will be activated again Note The max engine RPM given by the engine manufacturer is 6700 RPM This max RPM is reduced for operation in the DG 1000M...

Page 6: ...s Limitation data for the non useable amount of fuel printed above the display red 1 L When a fuel quantity of approx 4 Litres is reached a full screen warning Low Fuel appears when this warning has b...

Page 7: ...Carry out a C G calculation according to section 6 9 The in flight C G will be moved forward by approx 75 mm 3 in depending on the flight mass and empty mass C G This C G shift is acceptable as the f...

Page 8: ...retracted e g on the trailer after derigging after 60 seconds With landing gear extended e g in the hangar after 5 minutes In both cases time counts after the last operation of any item of the electri...

Page 9: ...0 12 V min 12 Ah mass 5 5 kg 12 1 lbs is permitted The battery fuse is installed at the battery type G fuse G 250 V 5 x 20 4 A fast The wiring for this battery is in parallel to the battery in the bag...

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