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DG Flugzeugbau DG-1000M Flight Manual

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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.
Affected
No.
Pages/section
1
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
2
0.2, 0.4 ÷ 0.6, 2.5,
2.6, 4.33, 7.19, 7.30
Issued: July 2014
Copyright DG Flugzeugbau GmbH - any copy or publishing prohibited
Flight Manual DG-1000M
Description
Manual revision
TN1000/22
Manual revision
TN1000/23
TN1000/23
Issue
EASA
Date
Approval
Date
October
10. Dec.
2012
2012
July
7 August
2014
2014
Inserted
Date
Signature
0.2

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Summary of Contents for DG Flugzeugbau DG-1000M

  • Page 1 6.9 ÷ 6.15, 7.2, 7.6, 7.9, 7.12, 7.25 ÷ 7.28, 7.30, 8.3 0.2, 0.4 ÷ 0.6, 2.5, Manual revision July 7 August 2.6, 4.33, 7.19, 7.30 TN1000/23 2014 2014 Issued: July 2014 TN1000/23 Copyright DG Flugzeugbau GmbH - any copy or publishing prohibited...
  • Page 2 " October 2010 " October 2010 October 2012 " October 2010 " October 2010 " October 2010 " October 2010 " October 2010 " October 2010 Issued: July 2014 TN1000/23 Copyright DG Flugzeugbau GmbH - any copy or publishing prohibited...
  • Page 3 October 2012 EASA-app. October 2010 October 2012 October 2010 October 2012 October 2010 October 2012 5.10 October 2010 October 2012 5.11 October 2012 5.12 October 2012 Issued: July 2014 TN1000/23 Copyright DG Flugzeugbau GmbH - any copy or publishing prohibited...
  • Page 4 7.25 October 2010 October 2012 7.26 October 2010 7.27 October 2010 October 2012 7.28 October 2010 October 2012 7.29 October 2010 7.30 October 2010 October 2012 July 2014 Issued: July 2014 TN1000/23 Copyright DG Flugzeugbau GmbH - any copy or publishing prohibited...
  • Page 5 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 for not exceeding the max. permissible RPM of the propeller. Propeller: Diameter 1.6 m (5.25 ft)
  • Page 6 FC or FD or higher quality. Mixing ratio 1:50. Note: The SOLO company recommends the following oil types: CASTROL Actevo 2T or CASTROL Super TwoStroke.. Issued: July 2014 TN1000/23 EASA app. 2.6 Copyright DG Flugzeugbau GmbH - any copy or publishing prohibited...
  • Page 7 Flight Manual DG-1000M 4.6 Flight with the engine removed from the aircraft The DG-1000M can be flown without the engine when the engine is sent for a major overhaul, or removed to decrease the aircraft empty weight for competition flying or for aerobatics.
  • Page 8 Case a) Retract the powerplant again manually, then try to extend the engine again. Case b) Partially retract the engine manually and then try to extend the powerplant manually up to its operating position. Issued: July 2014 TN1000/23 7.19 Copyright DG Flugzeugbau GmbH - any copy or publishing prohibited...
  • Page 9 To use headsets with standard microphones one V-adapter 10E109 must be installed per headset. In gliding mode the standard microphones of the headsets will not be switched off. Issued: July 2014 TN1000/23 7.30 Copyright DG Flugzeugbau GmbH - any copy or publishing prohibited...