Sonaca aircraft S201 Especificaciones técnicas

sonaca aircraft^

S201 AFM

SONACA GROUP

S201 AIRCRAFT FLIGHT MANUAL

Model: S201

m~K6€-

SONAIR-S2-D-MAN-006

14/10/2020

Sonaca Aircraft S.A.

Serial No:

Registration:

Document No. :

Date of Issue:

Approved by:

Signature:

Agency:

Stamp:

Original date of approval: 01/07/2019

N/A

This airplane must be operated in

compliance with information and limitations

contained herein. This pilot operating

handbook must be available on board of the

airplane at all times.

0-MANUAL ADMINISTRATION

sonaca aircraft

S201AFM

0.1-APPROVAL

SONACAGROUP

0MANUAL ADMINISTRATION

0.1 APPROVAL

The content of approved chapters is approved by EASA. All other content is

approved by Sonaca Aircraft S.A. under the authority of EASA DOA No.

EASA.21J.614 in accordance with Part 21.

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sonacaaircraft^ 0-MANUAL ADMINISTRATION

S201AFM

0.2 -RECORD OF REVISIONS

SONACA GROUP

0.2 RECORD OF REVISIONS

All revisions of this manual, with the exception of -

●Temporary Revisions,

●updates of the modiﬁcation level,

●updated mass and balance information,

●updates of the Equipment Inventory, and

●updates of the List of Supplements,

Must be recorded in the following table and in case of approved Sections

endorsed by the Agency.

The new or amended text in the revised pages will be indicated by ablack vertical

line in the left hand margin, and the Revision No. and the date will be shown on

the bottom left hand side of the page.

Approved by

Affected

Pages

Approval

Date

Rev. N° Affected

Section

All AllAEASA

0.2,1.8, 2.11.9,

2.11.10,3.10.3,

3.10.10, 7.5,

7.7.S.2

See table

below

Ri 14/10/2020 Sonaca Aircraft S.A.

^This revision of the AFM is applicable to aircraft MSN025-onwards only, and to previous aircraft retroﬁtted with

SB-SONAIR-S2-014 implementing the change of backup instrument from KI300 to GI275. Aircraft not equipped

with a GI275 mu s t use revi s ion Aof th is manua l .

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0-MANUAL ADMINISTRATION

S201 AFM

0 . 3 - L I S T O F E F F E C T I V E PA G E S

SONACAGROUP

0 . 3 L I S T O F E F F E C T I V E P A G E S

This section lists the pages of the manual, together with the revision

corresponding to each page and the approving organism.

Rev. Approved 2-4 AEASA 3-9 AEASA

Page N“ %2-5 AEASA 3-10 AEASA

0-0 AEASA 2-6 AEASA 3-11 AEASA

0-1 AEASA 2-7 AEASA 3-12 AEASA

0-2 BSonaca Aircraft 2-8 AEASA 3-13 AEASA

0-3 BSonaca Aircraft 2-9 AEASA 3-14 EASAA

0-4 BSonaca Aircraft 2-10 AEASA 3-15 AEASA

0-5 BSonaca Aircraft 2-11 AEASA 3-16 AEASA

1-1 AEASA 2-12 AEASA 3-17 EASAA

1-2 AEASA 2-13 AEASA 3-18 AEASA

1-3 AEASA 2-14 AEASA 3-19 AEASA

1-4 AEASA 2-15 AEASA 3-20 EASAA

1-5 AEASA 2-16 AEASA 3-21 AEASA

1-6 AEASA 2-17 AEASA 3-22 EASAA

1-7 AEASA 2-18 BSonaca Aircraft 3-23 AEASA

1-8 AEASA 2-19 AEASA 3-24 AEASA

1-9 AEASA 2-20 AEASA 3-25 AEASA

1-10 AEASA 2-21 B3-26 EASASonaca Aircraft A

1-11 AEASA 2-22 AEASA 3-27 AEASA

1-12 AEASA 2-23 AEASA 3-28 BSonaca Aircraft

1-13 AEASA 2-24 BSonaca Aircraft 3-29 AEASA

1-14 AEASA 2-25 EASA 3-30AAEASA

1-15 AEASA 2-26 AEASA 3-31 AEASA

1-16 AEASA 2-27 AEASA 3-32 AEASA

1-17 AEASA 2-28 AEASA 3-33 AEASA

1-18 AEASA 2-29 AEASA 3-34 AEASA

1-19 AEASA 2-30 AEASA 3-35 AEASA

1-20 AEASA 2-31 AEASA 3-36 AEASA

1-21 AEASA 3-1 AEASA 3-37 AEASA

1-22 AEASA 3-2 AEASA 3-38 EASAA

1-23 AEASA 3-3 AEASA 3-39 AEASA

1-24 AEASA 3-4 AEASA 3-40 EASAA

1-25 BSonaca Aircraft 3-5 AEASA 3-41 AEASA

2-1 AEASA 3-6 AEASA 3-42 BSonaca Aircraft

2-2 AEASA 3-7 AEASA 3-43 BSonaca Aircraft

2-3 AEASA 3-8 AEASA 3-44 BSonaca Aircraft

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0 . 3 - L I S T O F E F F E C T I V E PA G E S

SOWACA GROUP

7-68 AEASA 7-84 AEASA 8-5 AEASA

7-69 AEASA 7-85 AEASA 8-6 EASAA

7-70 AEASA 7-86 AEASA 8-7 AEASA

7-71 AEASA 7-87 AEASA 8-8 EASAA

7-72 AEASA 7-88 AEASA 8-9 AEASA

7-73 AEASA 7-89 AEASA 8-10 AEASA

7-74 AEASA 7-90 AEASA 8-11 AEASA

7-75 AEASA 7-91 AEASA 9-1 AEASA

7-76 AEASA 7-92 AEASA 9-2 AEASA

7-77 AEASA 7-93 AEASA 9-3 AEASA

7-78 AEASA 7-94 AEASA 9-4 EASAA

7-79 AEASA 7-95 AEASA 9-5 AEASA

7-80 AEASA 8-1 AEASA 9-6 AEASA

7-81 AEASA 8-2 AEASA 9-7 AEASA

7-82 AEASA 8-3 AEASA 9-8 AEASA

7-83 AEASA 8-4 EASAA9-9 AEASA

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0 . 4 - T A B L E O F C O N T E N T

SONACA GROUP

0 . 4 T A B L E O F C O N T E N T

0-1

0MANUAL ADMINISTRATION

1-11GENERAL INFORMATION

2-1

2LIMITATIONS

3-13EMERGENCY PROCEDURES

4-1

4NORMAL PROCEDURES

5-15PERFORMANCE

6-1

6WEIGHT AND BALANCE

7-17 A I R P L A N E A N D S Y S T E M S D E S C R I P T I O N

8 A I R P L A N E G R O U N D H A N D L I N G A N D S E R V I C I N G 8-1

9-19ADDITIONAL INFORMATION

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sonaca aircraft^ 1-GENERAL INFORMATION

S201 AFM

1 . 1 - T A B L E O F C O N T E N T

SOMACA GROUP

1GENERAL INFORMATION

1 . 1 T A B L E O F C O N T E N T

1 . 1 T A B L E O F C O N T E N T 1-1

1.2 INTRODUCTION 1-2

1.3 CERTIFICATION BASIS 1-4

1.4 WARNING, CAUTION AND NOTES 1-5

1.5 AIRCRAFT DESCRIPTION AND DIMENSIONS 1-6

1.6 DEFINITION AND ABBREVIATIONS 1-11

1 . 7 U N I T S O F M E A S U R E M E N T 1-20

1 . 8 S O U R C E D O C U M E N T A T I O N 1-23

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s1-GENERAL INFORMATION

sonaca aircraft

S201AFM

1.2 -INTRODUCTION

SONACAGROUP

1.2 INTRODUCTION

This Aeroplane Flight Manual has been prepared to provide pilots and instructors

with information for the safe and efﬁcient operation of the SONACA S201

aeroplane.

This manual includes the information required by CS-VLA to be furnished to the

pilot of the Sonaca S201. It also contains supplemental data supplied by Sonaca

Aircraft S.A., the aeroplane manufacturer.

The Sonaca S201 is atwo seat (side-by-side), single engine, tricycle ﬁxed

undercarriage, aluminium aircraft with aconventional low wing design.

The Sonaca S201 is certiﬁed based upon the EASA CS-VLA (Certiﬁcation Standard

Very Light Aircraft) standard, having amaximum Take Off Weight of 750 kg.

The Sonaca S201 is intended primarily for training and recreational ﬂying. It is

not intended for aerobatic operations.

The Sonaca S201 is approved for day and night VFR operation.

Minimum equipment required for day or night VFR are deﬁned in paragraph

7.13.

VFR ﬂights in rain are authorized.

The present document is also referenced as Pilot Operating Flandbook, or

Handbook, or Manual.

This revision of the AFM is applicable to aircraft MSN025-onwards and previous

aircraft retroﬁtted with SB-SONAIR-S2-014 implementing the change of backup

instrument from KI300 to GI27S only. Aircraft not equipped with aGI275 must

u s e r e v i s i o n A o f t h i s m a n u a l .

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s1-GENERAL INFORMATION

sonaca aircraft

S201 AFM

1.2 -INTRODUCTION

SONACA GROUP

NOTE

T H I S M A N U A L I S W R I T T E N F O R T H E S T A N D A R D R O T A X 9 1 4 F P O W E R E D

SONACA S201, AS MANUFACTURED ON THEIR PREMISES BY SONACA

AIRCRAFT S.A. DIFFERENCES APPLICABLE TO POSSIBLE OPTIONS, AS

INSTALLED OR APPROVED BY SONACA AIRCRAFT S.A., ARE INCLUDED IN

A P P L I C A B L E S U P P L E M E N T S O F T H I S H A N D B O O K S E C T I O N 9 .

AIRCRAFT WHICH DIFFER FROM THE PRODUCTION STANDARD, IN

WHATEVER WAY, ARE NOT ADDRESSED IN THIS MANUAL, EXCEPT TO THE

E X T E N T T H E S A I D A I R C R A F T C O R R E S P O N D S T O S O N A C A A I R C R A F T S . A .

APPROVED MODIFICATIONS

NOTE

THIS EDITION OF THIS MANUAL IS BASED ON EASA REQUIREMENTS.

D E F I N I T I O N S A R E A C C O R D I N G L Y C O N S I S T E N T W I T H E A S A R E G U L A T I O N S

ONLY.

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