Aerospool WT-9 Dynamic Technical specifications

LIMITED COMPANY
AEROSPOOL PRIEVIDZA
Airfield Prievidza
971 03 PRIEVIDZA
Sl vak Republic
Fax: [phone]
Tel.: [phone]
aer sp l@aer sp l.sk
www.aer sp l.sk
F L I G H T M A N U A L
FOR THE AEROPLANE
WT-9 Dynamic
Type: WT-9 Dynamic
Model:
erial No:
Registration:
Date of Issue:
Pages identified by „Appr“ are approved by the Civil Aviation Authority of the
ignature:
Authority:
tamp:
Original date of approval:
This aer plane has t be perated in c mpliance with inf rmati n and limitati ns c ntained
herein.

WT-9 Dynamic Club
FLIGHT MANUAL ection 0 Page 0-
1
0.1. RECORD OF REVI ION
Any revisi n f the present manual, except actual weight data, must be rec rded in the
f ll wing table and in case f appr ved Secti ns end rsed by the resp nsible
airw rthiness auth rity.
The new r amended text in the revised pages will be indicated by a black vertical line in
the right hand margin, and the Revisi n N . and the date will be sh wn n the b tt m
left side f the page.
Rev.
No.
Affected
ection
Affected
Pages Date
Approval Date Date
inserted ignature
1 2, 3 2-1,2, 3-3 08.12.03
08.12.03
2 3 3-2 22.09.04
22.09.04
3 7 2,7,8,9,10 01.10.06
01.10.06
4 2, 4, 5, 7 2-5,7,9,
4-1-3, 4-12,
5-4,
7-2, 7-11,12
15.01.07
15.01.07
5 7 7-12 17.08.10
17.08.10
5 1 1-4 21.02.07
21.02.07
6 7 7-5 28.11.07
28.11.07
7 0 1, 2 01.12.08
ZBWT9
10A/2008
- - 01.12.08
7 3 5, 6 01.12.08
ZBWT9
10A/2008
- - 01.12.08
8 0 1, 2 05.10.09
ZBWT9
11A/2009
- - 05.02.2010
8 2 1, 3, 6 05.10.09
ZBWT9
11A/2009
- - 05.02.2010
8 4 12 05.10.09
ZBWT9
11A/2009
- - 05.02.2010
Date:05.10.2009, Rev.: 8

WT-9 Dynamic Club FLIGHT MANUAL ection 0 Page 0-2
0.2 LI T OF EFFECTIVE PAGE
ection Page Date ection Page Date
0 0-1 05.10.2009 5 „Appr“ 5-1 01.12.2001
0-2 05.10.2009 „Appr“ 5-2 01.12.2001
0-3 01.12.2001 „Appr“ 5-3 01.12.2001
0-4 01.12.2001 „Appr“ 5-4 15.01.2007
„Appr“ 5-5 01.12.2001
1 1-1 01.12.2001
1-2 01.12.2001 6 6-1 01.12.2001
1-3 01.12.2001 6-2 01.12.2001
1-4 21.02.2007 6-3 01.12.2001
„Appr“ 6-4 01.12.2001
2 „Appr“ 2-1 05.10.2009
„Appr“ 2-2 08.12.2003 7 7-1 01.12.2001
„Appr“ 2-3 05.10.2009 7-2 15.01.2007
„Appr“ 2-4 01.12.2001 7-3 01.12.2001
„Appr“ 2-5 15.01.2007 7-4 01.12.2001
„Appr“ 2-6 05.10.2009 7-5 28.11.2007
„Appr“ 2-7 15.01.2007 7-6 01.12.2001
„Appr“ 2-8 01.12.2001 7-7 01.10.2006
7-8 01.10.2006
3 „Appr“ 3-1 01.12.2001 7-9 01.10.2006
„Appr“ 3-2 22.09.2004 7-10 01.10.2006
„Appr“ 3-3 08.12.2003 7-11 15.01.2007
„Appr“ 3-4 01.12.2001 7-12 15.01.2007
„Appr“ 3-5 01.12.2008
„Appr“ 3-6 01.12.2008 8 8-1 01.12.2001
8-2 01.12.2001
4 „Appr“ 4-1 15.01.2007 8-3 01.12.2001
„Appr“ 4-2 15.01.2007 8-4 01.12.2001
„Appr“ 4-3 15.01.2007 8-5 01.12.2001
„Appr“ 4-4 01.12.2001 8-6 01.12.2001
„Appr“ 4-5 01.12.2001
„Appr“ 4-6 01.12.2001 9 „Appr“ 9-1 01.12.2001
„Appr“ 4-7 01.12.2001 „Appr“ 9-2 01.12.2001
„Appr“ 4-8 01.12.2001
„Appr“ 4-9 01.12.2001
„Appr“ 4-10
01.12.2001
„Appr“ 4-11
01.12.2001
„Appr“ 4-12
05.10.2009
Date:05.10.2009, Rev.: 8

WT-9 Dynamic Club FLIGHT MANUAL ection 0 Page 0-3
ection Page Date ection Page Date
Date:01.12.01

WT-9 Dynamic Club FLIGHT MANUAL ection 0 Page 0-4
0.3 TABLE OF CONTENT
ection
GENERAL 1
LIMITATION 2
EMERGENCY PROCEDURE 3
NORMAL PROCEDURE 4
PERFORMANCE 5
WEIGHT AND BALANCE / EQUIPMENT LI T 6
AIRPLANE AND Y TEM DE CRIPTION 7
AIRPLANE HANDLING, ERVICING
AND MAINTENANCE 8
UPPLEMENT 9
Date:1.12.2001

WT-9 Dynamic Club FLIGHT MANUAL ection 1 Page 1-
1
ECTION 1
GENERAL
Page
1.1 Introduction 1-1
1.2 Certification basis 1-1
1.3 Warnings, cautions and notes 1-1
1.4 Descriptive data 1-2
1.5 Three – view drawing 1-3
1.1 Introduction
The aer plane Flight Manual has been prepared t pr vide pil ts and instruct rs with
inf rmati n f r the safe and efficient perati n f this aer plane.
This manual c ntains supplementary data supplied by the aer plane manufacturer.
1.2 Certification basis
This type f airplane has been appr ved in Germany by the Deutscher Aer Club e.V.
(DaeC) in acc rdance with the German Certificati n Regulati ns and Airw rthiness
Requirements f r ultra light airplane f the DaeC (BFU des DaeC, Ausgabe 10/95) and
the Type Certificate N . 61179 has been issued n 23.10.2001.
The Civil Aviati n Auth rities f Sl vak Republic f ll wing an applicati n by
AEROSPOOL, sp l. s r. . Prievidza and after studying the d cumentati n Predpis
MDPT SR L 8/A and LU č. P- ULL-1 SR has issued the Type Certificate f
Airw rthiness
N . V-80/2004 dated April 25
th
2005 f r Type WT-9 Dynamic
Categ ry f Airw rthiness : Normal
1.3 Warnings, cautions and notes
The f ll wing definiti ns apply t warnings, cauti ns and n tes used in the flight
manual.
WARNING
Means that the n n- bservati n f the c rresp nding pr cedure
leads t an immediate r imp rtant degradati n f the flight
safety.
CAUTION
Means that the n n- bservati n f the c rresp nding pr cedure
leads t a min r r t a m re r less l ng term degradati n f the
flight safety.
NOTE
Draws the attenti n t any special item, n t directly related t
safety but which is imp rtant r unusual.
Date: 1.12.2001

WT-9 Dynamic Club FLIGHT MANUAL ection 1 Page 1-2
1.4 Descriptive data
1.4.1 Airplane description
WT-9 Dynamic Club S is l w-wing m n plane with fixed landing gear. The airframe
c nsists f a sandwich shells fr m advanced c mp site material. There are tw places
in the c ckpit, side by side type. This airplane is intended f r sp rting, recreati n and
t urist flying in acc rdance with VFR.
WT-9 Dynamic Club S has been appr ved by the DaeC in the Categ ry f
Airw rthiness : N rmal
As the p wer plant this airplane uses the 4 cylimder, 4 str ke ROTAX engines, 912
ULS. Pr pelers: This plane is fitted with 2 blades hydraulic c nstant speed MTV-21-A
1.4.2 Technical data
Wing span.................................................…. 9,00 m
Wing area…................................................... 10,3 m
2
Wing aspect rati ............................................ 7,82
Length............................................................. 6,4 m
Height.........................................................… 2,0 m
Aer dynamic mean ch rd ( MAC )............… 1,185 m
Control surfaces
Ailer n span………........................................ 1,25 m
Ailer n area…................................................. 0,273 m
2
Flap span………............................................. 2,28 m
Flap area…….................................................. 0,75 m
2
H riz ntal tail span……………….……......... 2,40 m
H riz ntal tail area…………………............... 1,68 m
2
Vertical tail span………………...............….... 1,022 m
Vertical tail area……………….................….. 1,02 m
2
Landing gear
Wheel spacing.……………………............…. 1,49 m
Wheel base..................................................…. 2,27 m
Main wheel diameter……………................… 0,35 m
N se wheel diameter………………………… 0,32 m
Weights
Empty weight ……………………………….….... 334,1 kg
Maximum take- ff weight…….....................……. 472,5 kg
Useful l ad……….....................................……..... 138,4 kg
Fuel tanks capacity…………................................. 126 litres
The ROTAX 912 ULS (73 kW- 100HP) with a maximum rpm limitati n n take ff f
5800 1/min. The pr peller MTV-21-A diameter is 1,7 m
Date: 1.12.2001

WT-9 Dynamic Club FLIGHT MANUAL ection 1 Page 1-3
1.5. Aeroplane views
Date: 01.12.2001
Ph t 2
Ph t 1

WT-9 Dynamic Club FLIGHT MANUAL ection 1 Page 1-4
1.5.1 Three – view drawing
Date: 21.2.2007 / Rev.: 5

WT-9 Dynamic Club FLIGHT MANUAL ection 2 Page 2-1
ECTION 2
LIMITATION
Page
2.1 Introduction 2-1
2.2 Airspeed 2-1
2.3 Airspeed indicator markings 2-2
2.4 Power plant 2-2
2.5 Power plant instrument markings 2-3
2.6 Miscellaneous instrument markings 2-4
2.7 Weight 2-5
2.8 Centre of gravity 2-5
2.9 Approved manoeuvres 2-5
2.10 Manoeuvring load factors 2-6
2.11 Flight crew 2-6
2.12 Kinds of operation 2-6
2.13 Fuel, oil 2-6
2.14 Maximum passenger seating 2-7
2.15 Other limitations 2-7
2.16 Limitations placards 2-7
2.1 Introduction
Secti n 2 includes perating limitati ns, instrument markings, and basic placards
necessary f r safe perati n f the aer plane, its engine, standard systems and standard
equipment. The limitati ns included in this secti n have been appr ved by the Civil
Aviati n Auth rity f the Sl vak Republic.
2.2 Airspeed
Airspeed limitati ns and their perati nal significance are sh wn bel w:
peed IA Remarks
km/h MPH knots
V
NE
Never Exceed speed 280 174 150 D n t exceed this speed in any
perati n
V
NO
N rmal Operating Limit
speed 250 156 135 D n t exceed this speed except in
sm th air, and then nly with cauti n
V
RA
R ugh Air speed 225 140 121
D n t exceed this speed except in
sm th air. Air m vements in lee-wave
r t rs, thundercl uds, visible whirlwind,
r ver m untain crests are t be
underst d as r ugh air
Date: 05.10.2009, Rev.: 8 „Appr“