Aquila AT01 Caractéristiques techniques

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

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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.

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.

Schönhagen, Germany

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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.

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

Dokument No.: Issue: Supersedes Issue: Date: Page:

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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

1.5 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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