Aquila AT01 Caractéristiques techniques

Aviation GmbH

AIRPLANE FLIGHT MANUAL

AQUILA AT01

LBA Approved in Normal Category based on JAR-VLA.

This Airplane Flight Manual must be carried on board 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.: B.04

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INTRODUCTION

With the AQUILA AT01 you have acquired a very efficient training and utility aircraft,

which can be operated very easily and which exhibits excellent handling qualities.

Reliable operation, handling and maintenance guarantee trouble-free flights and

continued airworthiness.

To ensure this, we recommend that you 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 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. Failing to pay 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 the location of 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

GmbH.

Schönhagen, Germany

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TABLE OF CONTENTS

SECTION

GENERAL 1

OPERATING LIMITATIONS (approved section) 2

EMERGENCY PROCEDURES (approved section) 3

NORMAL PROCEDURES (approved section) 4

PERFORMANCE (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 B.04 0-1 to 0-8 13/04/2015

1 B.01 1-1 to 1-12 12/07/2012

2 X B.01 2-1 to 2-20 12/07/2012

3 X B.01 3-1 to 3-16 12/07/2012

4 X B.04 4-1 to 4-20 13/04/2015

5 (X)* B.01 5-1 to 5-23 12/07/2012

6 B.01 6-1 to 6-14 12/07/2012

7 B.04 7-1 to 7-32 13/04/2015

8 B.01 8-1 to 8-8 12/07/2012

9 B.04 9-1 to 9-3 13/04/2015

•- 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 into 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(c)(4), by the Design Organization of AQUILA Aviation GmbH.

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 on board the aircraft.

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)

A.19 Documentary changes 0,9 14/09/2011

A.20 Supplement ASPEN PFD and GARMIN

G500 for Day/Night-VFR-Operation

0,9 21/03/2012

(20.04.2012 EASA)

A.21 Supplement GARMIN GTN650, GMA 350 0, 9 21/05/2012

B.01 Editorial corrections All 12/07/2012

B.02 Supplement Trig TT22 0, 9 21/11/2012

B.03

Documentary changes, revised

supplement winter kit, supplements

Garrecht TRX 1500 and 2000

0, 9 04/03/2014

B.04 Documentary changes 0, 4, 7, 9 13/04/2015

Revision B.04 of AFM ref. FM-AT01-1010-100E is approved under the authority of

DOA ref. EASA.21J.025.

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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

A.19 0,9 14/09/2011

A.20 0,9 21/03/2012

A.21 0,9 21/05/2012

B.01 All 12/07/2012

B.02 0, 9 21/11/2012

B.03 0, 9 04/03/2014

B.04 0, 4, 7, 9 13/04/2015

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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 GmbH

OT Schönhagen

Flugplatz

D-14959 Trebbin

Tel: +49 (0)33731 707-0

Fax: +49 (0)33731 707-11

E-Mail: kontakt@aquila-aviation.de

Internet: http://www.aquila-aviation.de

http://www.facebook.com/aquilaa210

(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: sales@mt-propeller.com

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Aviation

AIRPLANE FLIGHT MANUAL

AQUILA AT01 Section 4

NORMAL PROCEDURES

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SECTION 4

NORMAL PROCEDURES

Page

4.1 INTRODUCTION 4-2

4.2 AIRSPEEDS FOR NORMAL OPERATION 4-3

4.3 RESERVED 4-5

4.4 PRE-FLIGHT INSPECTION 4-6

4.4.1

4.4.2

Daily Pre-flight Check

Check Before Every Flight

4-6

4-11

4.5 CHECKLISTS FOR NORMAL PROCEDURES 4-13

4.5.1

4.5.2

4.5.3

4.5.4

4.5.5

4.5.6

4.5.7

4.5.8

4.5.9

4.5.10

4.5.11

4.5.12

4.5.13

4.5.14

Before Engine Start-up

Engine Start-up

Before Taxiing

Taxiing

Before Take-off (at the Taxi Holding Position)

Take-off

Climb

Cruise

Descent

Landing

Balked Landing

After Landing

Engine Shutdown

Flight in Heavy Rain and/or with Strongly Soiled Wings

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4-13

4-14

4-15

4-16

4-17

4-18

4-19

4-20

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