Pipistrel Taurus ELECTRO G2 Technical specifications

Flight manual and
Maintenance manual
applies to Taurus ELECTRO G2
WARNING!
This booklet MUST be present inside the cockpit at all times!
Should you be selling the aircraft make sure this manual is handed over to the new owner.
REV. 0
(9 March, 2011)
This is the original manual of Pipistrel d.o.o. Ajdovščina
Should third-party translations to other languages contain any discreptancies,
Pipistrel d.o.o. Ajdovščina denies all responsibility.

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Taurus model:
Factory serial number:
Date of manufacture:
Aircraft empty weight (kg):
Available crew weight (no front ballast):
Available crew weight (9 kg front ballast):
Available luggage weight:
List of equipment included in aircraft empty weight:
Date and place of issue: Ajdovščina,
To log into the Owner’s section, receive updates and Service Bulletins, go to: www.pipistrel.si and log in
the top right corner of the page with:
Username: owner1
Password: ab2008
THANK YOU!

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Flight manual and
Maintenance manual for
Model: Taurus ELECTRO
Data Sheet:
Factory serial number:
Registration number:
Date of Issue: March, 2011
Pages signed under “Approval” in section Index of revisions and List of valid pages
(pages 4 and 5 of this manual) are approved by:
Authority: SLO.DOA.002
Signature:
Stamp:
Original date of Approval: March, 2011
This aircraft is to be operated in compliance with information and limitations contained herein.
The original English Language edition of this manual has been approved as operating instruction
according to “Pravilnik o ultralahkih letalnih napravah” of Republic of Slovenia.
Approval of translation has been done by best knowledge and judgement.
Pipistrel d.o.o. Ajdovščina, Goriška cesta 50a, SI- 5270 Ajdovščina, Slovenija
tel: [phone], fax: [phone], e-mail: [email protected]
www.pipistrel.si
Taurus ELECTRO

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Index of revisions
Enter and sign the list of revised pages in the manual into the spaces provided below. All revised pages
should be clearly designated in the upper right corner of the page, also, any changes in page content
should be clearly visible (e.g. marked with a bold black vertical line).
Name of
revision
Reason for
Revision:
Revision no.,
date: Description: Affected
pages:
Approval,
signature:
Original / Rev. 0
9 March, 2011 First original release. / Tomazic

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List of valid pages
This manual contains 96 original and revised pages listed below.
Pages State
(Revision) Approval:
Cover REV. 0
Page numbering REV. 0
Authority approval sheet 3REV. 0
Index of revisions 4REV. 0
List of valid pages 5REV. 0
Table of contents 7REV. 0
General 9 - 12 REV. 0
Limitations 13 - 20 REV. 0
Emergency procedures 21 - 28 REV. 0
Normal procedures 29 - 42 REV. 0
Performance 43 - 51 REV. 0
Weight and balance 53 - 59 REV. 0
Aircraft and systems on board 61 - 73 REV. 0
Handling and maintenance 75 - 84 REV. 0
Appendix 85 - 93 REV. 0
CAUTION!
This manual is valid only if it contains all of the original and revised pages listed above.

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Table of contents
General
Limitations
Emergency procedures
Normal procedures
Performance
Weight and balance
Aircraft and systems on board
Handling and maintenance
Appendix

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Introduction
Notes and remarks
Technical data
3-view drawing
General
General

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Introduction
This manual contains all information needed
for appropriate and safe use of Taurus Electro
IT IS MANDATORY TO CAREFULLY
STUDY THIS MANUAL PRIOR TO USE
OF AIRCRAFT
In case of aircraft damage or people injury
resulting form disobeying instructions in the
manual PIPISTREL d.o.o. Ajdovscina denies all
responsibility.
All text, design, layout and graphics are
owned by PIPISTREL d.o.o. Ajdovscina
Therefore this manual and any of its contents
may not be copied or distributed in any man-
ner (electronic, web or printed) without the
prior consent of PIPISTREL d.o.o. Ajdovscina
Notes and remarks
Safety definitions used in the manual:
WARNING! DISREGARDING THE FOLLOWING INSTRUCTIONS WILL LEAD TO SEVERE
DETERIORATION OF FLIGHT SAFETY AND HAZARDOUS SITUATIONS, INCLUDING SUCH
RESULTING IN INJURY AND LOSS OF LIFE.
CAUTION! DISREGARDING THE FOLLOWING INSTRUCTIONS WILL LEAD TO SERIOUS
DETERIORATION OF FLIGHT SAFETY.
Technical data
PROPORTIONS ELECTRO
wing span 14.97 m
length 7.30 m
height (propeller extended) 2.7 m
wing area 12.26 m2
vertical tail area 0.86 m2
horizontal stabilizer and elevator area 1.275 m2
aspect ratio 18.30
positive flap deflection (down) 5°, 9 °, 18 °
negative flap deflection (up) -5°
centre of gravity (% of MAC) 23% - 45%
General