Aquila AT01 Technical specifications
Aviation by Excellence AG
AIRPLANE FLIGHT MANUAL
AQUILA AT01
LBA Approved in Normal Category based on JAR-VLA.
This Airplane Flight Manual must be carried on board of the aircraft at all times and be kept
within the reach of the pilot during all flight operations. The amendment history and revision
status of each section of the Airplane Flight Manual are provided in the list of effective pages
and in the list of revisions.
This aircraft must be operated in compliance with the procedures and operating limits specified
herein.
SERIAL NO.: AQUILA AT01-
REGIST. NO.:
Revision A.01 was approved by the Luftfahrt-Bundesamt (LBA) on 30/08/2002 within the scope
of the type-certification. All revisions of section 2, 3, 4 and 5 beyond the scope of documentary
changes are subject to EASA-approval.
Doc. No. FM-AT01-1010-100E
First Issued: 05/06/2002
Cover Page Issue No.: A.18
Aviation AIRPLANE FLIGHT MANUAL
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INTRODUCTION
With the AQUILA AT01 you acquired a very efficient training and utility aircraft, which can
be operated very easily and exhibit excellent handling qualities.
Reliable operation, handling and maintenance guarantee always trouble-free flights and
continued airworthiness.
For that, we recommend to read this Airplane Flight Manual thoroughly and adhere to the
operating instructions and recommendations given herein.
Furthermore, we recommend attending a type training course held by AQUILA company
trained personnel to obtain a "feeling" for the optimal operation of the aircraft within a
shorter period of time.
NOTE
All limitations, procedures and performance data contained in this handbook are EASA-/
LBA-approved and mandatory. Not paying attention to the procedures and limits of the
handbook can lead to a loss of liability by the manufacturer.
THE HANDBOOK
The Airplane Flight Manual has been prepared using the recommendations of JAR-VLA
Appendix H (issue 26/4/90) “Specimen Flight Manual for a Very Light Aeroplane”.
The handbook is presented in loose-leaf form to ease the substitution of revisions and is
sized in A5-format for convenient storage in the airplane. Tab dividers throughout the
handbook allow quick reference to each section. Tables of Contents are located at the
beginning of each section to aid locating specific data within that section.
All rights reserved.
Reproduction or disclosure to third parties of this document or any part thereof is not
permitted, except with the prior and express written permission of the AQUILA Aviation by
Excellence AG.
Copyright © by Aviation by Excellence AG
Schönhagen, Germany
Aviation AIRPLANE FLIGHT MANUAL
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TABLE OF CONTENTS
SECTION
GENERAL 1
OPERATING LIMITATIONS (an approved section) 2
EMERGENCY PROCEDURES (an approved section) 3
NORMAL PROCEDURES (an approved section) 4
PERFORMANCE (an partly approved section) 5
WEIGHT AND BALANCE 6
DESCRIPTION OF THE AIRCRAFT AND ITS SYSTEMS 7
HANDLING, SERVICE AND MAINTENANCE 8
SUPPLEMENTS 9
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LIST OF EFFECTIVE PAGES
Section approved Issue
No.
Page Date
0 A.18 0-1 to 0-8 29/11/2010
1 A.12 1-1 to 1-12 17/09/2008
2 X A.12 2-1 to 2-20 17/09/2008
3 X A.12 3-1 to 3-16 17/09/2008
4 X A.18 4-1 to 4-20 29.11.2010
5 (X)* A.12 5-1 to 5-23 17/09/2008
6 A.12 6-1 to 6-14 17/09/2008
7 A.14 7-1 to 7-32 03/09/2009
8 A.12 8-1 to 8-8 17/09/2008
9 A.17 9-1 to 9-3 07/10/2010
- partly approved
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LIST OF REVISIONS
All implementations of revisions to this manual, except individual weight and balance
data, should be entered in the record of revisions on the next page. Revisions must either
be approved by the EASA or, in the case of documentary changes in accordance with
Part 21A.263©(4), by the Design Organisation of AQUILA Aviation by Excellence AG.
Additions and revisions to the text in an existing section will be identified by a vertical
black line adjacent to the applicable revised area. A new issue code appears in the footer
of the pages of the revised section.
The operation of the AQUILA AT01 is only permitted with an Airplane Flight Manual in the
current effective status carried on board.
Please refer to our web page www.aquila-aviation.de whenever the revision status of
your Airplane Flight Manual is in question.
Issue
No.
Description of Revisions Revised
Section(s)
Approval by
AQUILA*/EASA
Date/Signature
A.01 First Issue Alle 30/08/2002
A.02 Installation of Garmin Avionic 0,2,9 13/05/2003
A.03 Editorial corrections 0,4,5,7 16/05/2003
A.04 Supplements for Bendix King equipment 0,9 09/07/2003
A.05 External Power, Supplement for Pointer
ELT 0,7,9 09/10/2003
A.06 Winterization Kit 0,2,9 10/03/2004
A.07 KANNAD 406 AF, ELT 0,9 23/06/2005
A.08 Supplements for Garmin Avionic 0,1,4,9 30/06/2005
A.09 Supplement for Bendix King KT 73 0,9 08/07/2005
A.10 Supplement for ARTEX ME406, ELT 0,9 07/03/2008
A.11 Introduction of new Emergency Proc. And
various AFM-Supplements 0,3,9 28/08/2008 (EASA)
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Issue
No.
Description of Revisions Revised
Section(s)
Approval by
AQUILA*/EASA
Date/Signature
A.12 Documentary changes All 28.11.2008
A.13 Supplement Garrecht Mode-S
Transponder 0,9 19/03/2009
A.14 Supplement for Day/Night-VFR-
Operation 0,7,9 03/09/09
(25.03.2010 EASA)
A.15 Supplement ASPEN EFD 1000 PFD/MFD 0,9 07/12/2009
A.16 Supplement GARMIN G500-System 0,9 22.07.2010
A.17 Changes in supplement for GARMIN
G500-sytem 0,9 07.10.2010
(15.11.2010 EASA)
A.18 Normal procedure – Actions introduced by
SB-AT01-020 0,4 29.11.2010
(14.01.2011 EASA)
APPROVAL*
Issue A.18 of the Airplane Flight Manual is approved within the approval of Major-Change
AT01-00438 Rev.A02 by EASA.
14. Jan. 2011 10033370
Date EASA-approval
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RECORD OF REVISIONS
When a new revision to the Airplane Flight Manual is issued, the corresponding sections
have to be removed and replaced by the pages of the revised sections.
Only entire sections will be changed and have to be replaced. Each time, when the
incorporation of a revision is accomplished, an endorsement has to be made in the record
of revisions shown below.
Issue No. Revised
Sections Date of Issue Date of
insertion: Inserted by:
A.01 All 05/06/2002 --- ---
A.02 0,2,9 20/11/2002
A.03 0,4,5,7 15/04/2003
A.04 0,9 19/05/2003
A.05 0,7,9 30/09/2003
A.06 0,2,9 10/02/2004
A.07 0,9 30/07/2004
A.08 0,1,4,9 30/06/2005
A.09 0,9 05/07/2005
A.10 0,9 05/03/2006
A.11 0,3,9 30/11/2007
A.12 All 17/09/2008
A.13 0,9 19/03/2009
A.14 0,7,9 03/09/2009
A.15 0,9 07/12/2009
A.16 0,9 22/7/2010
A.17 0,9 07/10/2010
A.18 0,4 29/11/2010
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Purchase of Technical Publications
To guarantee safe operation and correct maintenance of the aircraft AQUILA AT01, all
manuals and technical publications must be kept in the current effective status.
All manuals and technical publications relating to the aircraft AQUILA AT01 are available
from the companies listed below:
(a) AQUILA AT01 related Manuals and Publications
AQUILA Aviation by Excellence AG
Flugplatz
D-14959 SCHÖNHAGEN
Tel: +49 (0)33731 707-0
Fax: +49 (0)33731 707-11
E-Mail: [email protected]
Internet: http://www.aquila-aviation.de
(b) Engine ROTAX 912 S related Manuals and Publications
ROTAX®authorized distributor for ROTAX®Aircraft Engines of the applicable
distribution area.
For contact details of the local authorized distributor for ROTAX Aircraft Engines,
please refer to chapter 13 of the ROTAX®Operator’s Manual for 912 S Engines.
(c) Propeller MTV-21 related Manuals and Publications
mt-Propeller Entwicklung GmbH
Flugplatz Straubing- Wallmühle
D-94348 ATTING
Tel: +49 (0)9429 9409-0
Fax: +49 (0)9429 8432
Internet: www.mt-propeller.com
E-mail: [email protected]
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Aviation
AIRPLANE FLIGHT MANUAL
AQUILA AT01
Section 1
GENERAL
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SECTION 1
GENERAL
Page
1.1 INTRODUCTION 1-2
1.2 AIRCRAFT TYPE CERTIFICATION 1-2
1.3 WARNING, CAUTIONS AND NOTES 1-3
1.4 AIRCRAFT PRINCIPAL DIMENSIONS 1-4
1.4.1
1.4.2
1.4.3
1.4.4
1.4.5
Overall Dimensions
Wings
Horizontal Stabilizer / Elevator
Fuselage and Vertical Stabilizer / Rudder
Landing Gear
1-4
1-4
1-4
1-4
1-4
1.5 AQUILA AT01 – THREE VIEW DRAWING 1-5
1.6 ENGINE 1-6
1.7 PROPELLER 1-6
1.8 FUEL 1-6
1.9 ENGINE OIL AND COOLANT 1-7
1.9.1
1.9.2
Engine Oil
Engine Coolant
1-7
1-8
1.10 WEIGHTS 1-8
1.11 TERMINOLOGY AND ABBREVIATIONS 1-9
1.12 CONVERSION FACTORS 1-11
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