Aerospool WT9 Dynamic LSA Ciub S Technical specifications

AE4ObL
SPOL
S
RO.
LflvIITED
COMPANY
AEROSPOOL
PRIEVIDZA
Airfield
Prievidza
971
03
PRIEVIDZA
Slovak
Republic
Fax:
+42
46
51
83
250
Tel.:
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4651
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200
aerosø[email protected]
wwwaerospool.sk
FLIGUT
MANUAL
FOR
THE
LIGHT
SPORT AIRPLANE
WT9
Dynamic
LSA
Ciub
$
MTOW
550kg
Type:
WT9
Dynamic
LSA
Model: Ciub
S
Seiial
No:
DY
- 361/2010
LSA
Registiation:
L
k)
—
flate
of Issue:
01.
12.
2009
Signature:
Authority:
Stamp:
OrinaI
date
ofapproval:
This
airplane
is to
be
operated
in compliance
with
information
and
limitations
contained
herein.

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WT-9
Dynamic
Ciub
S FLIGHT MANUAL
I
Section
0
Page
0-1
I
)
D
D
0.1.
RECORD
OF
REVISION
Any
revisjon
of
the
present
manuat,
except
actual weight
data,
must
be
recorded
in the
foltowing
tabte
and
in
case
of
approved Sections
endorsed
by
the
responsible
airworthiness
authority.
The new
or
amended
text
in
the revised
pages will
be
indicated
by a
black
verticat
line
in
the
right
hand
margin,
and
the
Revision
No.
and
the
date
wiIl
be
shown
on the bottom
left
side
ofthe
page.
Rev.
Affected Affected
flate
flate
Approval
flate
Signature
No. Section Pages
inserted
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,
15.01.07 15.01.07
4-1-3,
4-12,
5-4,
7-2,
7-11,12
57
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
70
1,2
01.12.08
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30.05.11
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t
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Date:
12.09.2011, Rev.:
10

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WT-9
Dynamic Ciub
S FLIGHT
MANUAL Section
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I
WT9
Dynamie
LSA
Ciub S
FLIGHT
MANUAL
I
Section
0
Page
0-4
0.3
TABLE
OF CONTENTS
GENERAL
LIM
ITATIONS
EMERGENCY
PROCEDURES
NORMAL PROCEDURES
PERFORMANCE
WEIGHT
AND
BALANCE
I
EQUIPMENT
LIST
AIRCRAFT
AND
SYSTEMS
DESCRIPTION
AIRCRAFT
HANDLING,
SERVICING
AND
MAINTENANCE
SUPPLEMENTS
Date:
01.12.09,
Rev.:0
I
Section
1
2
3
4
5
6
7
8
9

0
0
0

WT9 Dynamic
LSA Ciub
S
J
FLIGHT
MANUAL
Section
1
Page 1-1
I
SECTION
i
GENERAL
Page
1.1
Introduction
1-1
1.2
Certification
basis
1-1
1.3
Warnings,
cautïons
and
notes
1-1
1.4
Desciiptive
data
1-2
1.5
Air
plane
views
1-3
1.1
Introduction
The
airplane
Flight
Manual
has
been
prepared
to provide
pilots
and
instructors
with
information
for
the
safe and
efficient operation
ofthis
airplane.
This
manual
contains
supplementaiy
data
supplied
by the
airplane manufacturer.
1.2
Certification
basis
F-2245
Standard
Specification
for
Design
and
Performance
of
a Light Sport
Airplane.
1.3
Warnings,
cautions and
notes
The
following
definitions
apply
to
wamings,
cautions
and
notes
used
in the
flight
manual.
WARNING
Means
that the
non-observation
ofthe
corresponding procedure
leads
to
an immediate
or important degradation
ofthe
fliglit
safety.
CAUTION
Means that
the
non-observation ofthe
corresponding
procedure
leads
to a
minor
or to
a more
or
less long
term
degradation
ofthe
flight
safety.
NOTE
Draws
the
attention
to any
special
item,
not directly
related
to
safety
but
which
is
important
or unusual.
Date:
01.12.09,
Rev.:
0
I

WI-9 Dynamic Ciub S FLIGHT MANUAL Section 1 Page 1-2
I
1.4 Descriptive data
1.4.1 Airplane description
WT-9 Dynamic Ciub S is Iow-wing monoplane with
fixed landing gear. The airftame
consists ofa sandwich shells from advanced composite material. There are two places
in the cockpit, side by side type. This aircraft is intended for sporting,
recreation
and
tourist flying in accordance with VFR.
WT-9 Dynamic Ciub
S
has been
approved by
the DaeC in the Category of
Airworthiness Normal
As the power plant this aircraft uses the 4 cylimder, 4 stroke ROTAX engines,
912 S2.
Propelers: This plane is fated with
3
bladed in-flight electricaly adjustable propeller
and the following type and model is approved: Woodcomp $R 2000 D.
1.4.2 Technical
data
Wing
span 9,00
m
Wingarea 10,3m2
tD
Wing
aspect
ratio 7,82
Length 6,4
m
Height 2,0 m
Aerodynamic mean chord
(MAC
)
1,185
m
Control surfaces
Aileron span 1,25
m
Alleron area 0,273 m2
Flap span 2,2$ m
flap area 0,75 m2
Horizontal tail span 2,40 m
Horizontal tail area 1,6$ m2
Vertical tall span 1,022 m
Vertical tall area
1,02
m2
0
Landing gear
Wheel spacing 1,49 m
Wheel base 2,27 m
Main wheel diameter 0,35 m
Nose wheel diameter 0,32 m
Weights
Empty weight kg
Maximurn take-off weight 472,5 kg
Useful bad kg
fuel
tanks
capacity litres
The
ROTAX 912 S2(
73
kW) has
a
maximum
rpm
limitation on take off
of 5800
1/min. The Woodcomp SR 2000 D. Propeller diameter is 1,7 m.
Date: 12.09.2011, Rev.: 10

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WT9 Dynamic
LSA
Ciub
$
FLIGHT
MANUAL
I
Section
2
Page
2-1
2.1
Introduction
2.2
Airspeed
SECTION
2
LIMITATIONS
2.3
Airspeed
indicator
markings
2.4
Power
plant
2.5
Power
plant
instrument
markings
2.6
Miscellaneous
instrument
markings
2.7
Weight
2.8
Centre
ofgravity
2.9
Approved
manoeuvres
2.10
Manoeuviing
bad
factors
2.11
Flight
crew
2.12
Kinds
ofoperation
2.13
fuel,
oil
2.14
Maximum
passenger
seating
2.15
Other
limitations
2.16
Limitations
placards
Page
2-1
2-1
2-2
2-2
2-3
2-4
2-5
2-5
2-5
2-6
2-6
2-6
2-6
2-7
2-7
2-7
2.1
Introducfion
Section
2
includes
operating
limitations,
instrument
markings,
and
basic
placards
necessaiy
for
safe
operation
of
the
airplane,
its
engine,
standard systems
and
______
equipment.
Ihe
limitations
included
in
this
section
and
in
Section
9
have
beeri
approved
by
the
aviation
authority.
2.2
Airspeed
Airspeed
limitations
and
their
operational significance
are
shown
below:
Speed lAS
Remarks
kmlh
MPH
knots
VNE
Never
Exceed
speed
280
174 150
Do
not
exceed this
speed in
any
operation
VNO
Normal
Operating Limit
250
156 135
Do
not
exceed
this
speed
except in
speed
smooth
air,
and
then only
with
caution
V Rough
Air
speed
230
143 124 Do
not exceed
this
speed
except in
smooth
air.
Air
movements
in
lee-wave
rotors,
thunderclouds,
visible
whwlwind,
or
over
mountain crests
are
to
be
understood
as
rough
air
Date: 01.12.09,
Rev.:
0
,,Appr”

I
WT9
Dynamic
LSA Ciub
S
FLIGHT
MANUAL
I
Section
2
Page
2-2
i
Speed
km!h
lAS
MPH knots
Remarks
VA
Manoeuvring
speed
165
103 88
Do not
make
full or
abrupt
control
movernent
above
this
speed,
because
under
certam
conditions
the
aircraft
may
be
ovcrstressed
by full control
movement
VFE
Maximum
flap
Extended
140
88
75
Do not
exceed
these
speeds
with
the
speed
given
flap
setting.
2.3
Air
speed
indicator
markings
Airspeed
indicator
markings
and
their
colour-code
significance
are
shown
betow:
Mai king
lAS
value
or
range
Significance
km/h
MPH
knots
Positive
Flap
Operating
Range.
(
Lower
limit
is
maximum
weight
1.1
Vso
in
landing
White
arc
65 —
140
40
- 88
- ‘
configuration.
Upper
limit
is
maximum
speed
permissible
with
flaps extended
positive.)
Normal
Operating
Range.
(
Lower
limit
is
70
—
230
43 - 143
37
- 124
maximum
weight
1.1
VSI
at
most forward
c.g.
Gieen
aic
with
flaps
. Upper
limit is
VRA.
YelIow
arc
230
— 280
143 - 174
124
- 150
Manoeuvres
must
be
conducted
with
caution
and only
in smooth
air.
Yellow
triangle
100
62
53
Minimum
Approach
speed
Yellow
line
165
103
88
VA
Manoevring
speed
Red
line
280 174 150
Maximum
speed
for
all
operations.
0
Engine
Manufacturer:
ROTAX-Bombardier,
Gunskirchen,
Austria
Engine
Models:
ROTAX
912
ULS
Maximum
Power -
Take-off:
Continuous:
Maxirnum
Engine
Speed
—
Take-off:
Continuo
us:
Maximum
Cylinder
Head
Temperature:
Maximum
Oil Temperature:
130
0
C
Oil
Pressure: Minimum:
0,8
bar
(12
psi)
Maximum:
7
bar
(102
psi)
Minimum:
0,15 bar
(
2.2
psi)
Maximum:
0,4
bar
(5.8
psi)
the
foIlowing
fuels
can
be
used:
min. RON
95
0
2.4
Powerplant
73,5
kW/100F]P
69kW/93,$FW
5800
1/min
(
5 min)
5500
1/min
1350
C
0
0
fuel
Pressure:
Fuel Grade:
Date: 01.12.09,
Rev.: 0
,,Appr”
I
ww

I
WT9
Dynamic
LSA
Ciub
S
FLIGHT
MANUAL
Section
2
Page
2-3
I
- EN
22$
Super
(Unleaded
Automotive Gasohne RON
95)
-
EN 22$
Super plus
(Unleaded Automotive Gasoline
RON
9$)
- AVGAS
100
LL
(Due
to
the
higher
lead
content
in
AVGAS,
the
wear
ofthe
valve
seats,
the
deposits
in
combustion
chamber
and lead
sediments
in the
lubrication
system
will
increase.
Therefore,
use
AVGAS
only
ifyou
encounter
problems
with
vapour
lock
or
ifthe
other
fuel
types
are
not
avai
lable)
- Fuel
E10
(unleaded gasolme
blended
with
10%
ethanol
- engine
oil
ofa
registered
brand
with
gear
additives. Use only
oil
with
AP1
ciassification
,,SF”
or
,,SG”
-
high
performance
4-stroke motor
cycle
oils
are
recommended
-
If
using
aircrafi engine
oil,
then only blended
one.
3,0
litre
2,0
litre
max.
0,1
l!h
WARNING
Never
use
AVGAS,
LB 95
with fully
synthetic
engine
oils.
II
Propeller
Manufacturer:
Propeller
Model:
Propeller
Diameter:
Propeller
Blade Angle
DUC-
Helices,
Lentilly,
France
DUC
Swirl,
3
blade
on
ground
adjustable
propeller
1,7 m
24°
Additional data
can
be
found
in
Section
7,
Subpart
7.9,
in
the
Operator
Manual
for
engine
ROTAX
912
ULS
and
in the
User
Guide
for
propeller
DUC
Swirl.
According
to
customer
requirement round
one—purpose
needle
instruments
are fitted
in
the instrument
panel.
Date:
05.02.2010, Rev.:
i
I
,,Appr”
Oil
Grade:
Oil
capacity:
Minimum:
Oil
consumption:
2.5
Powerplant
instrument
markings

WT9
Dynamic
LSA
Ciub
S FLIGHT
MANUAL
Section
2
Page
2-4
Powerplant
instrument
markings
and
their colour
code
significance
are
shown
below:
2.6
Miscellaneous
instrument
markings
0
0
According
to
option
of
the
customer
miscellaneous
instrument
can
be
mounted. The
following
miscellaneous
instrument
markings
and
their colour code significance
are
shown
below:
Red
Line
Green
Arc YeIlow
Red
Line
Instrument
Unit
Minimum
Normal Ait
Maximum
Limit
Operating
Caution
Limit
Range
Boost-pressure
in
ilg
11,8
11,8-28
28-29,5
29,5
gauge
(EMS
D-1000)
Ehau
°c
250
300-800
250-300
880
temperature
(EMS
D-1000) 800-880
Fuel
flow
meter
LPH
(EMSD-1000)
upto 25
25
Fuet
reserve
litre Red light
annunciator
will
be
illunilitated
witli
the
indicator remaining
fuel
of 7
litre
in
each fuel tank
Red
Line
Green
Arc
YeJlow
Red
Line
Instrument
Unit
Minimum
Normal
Arc
Madmum
(indication
within
Limit
Operating
Caution
Limit
EMS
D-1000)
Range
Tachometer
rpm
i
400
i
$00
—5
500
5500—5800
5
800
Oil
temperature
50
90
— 110
50
—
130
indicator
11
—
Cylinder-head
50
—
90
temperature
°C
50
90—110
110—135
135
indicator
Fuel-pressure
bai’
0,15
0,4
indicator
Oil-pressure
bai•
0,8
2—
5 0,8
- 2
7
indicator
5—7
Fuel
indicator
htre
0
0
Date:
01.12.09,
Rev.: 0
,,Appr”

I
WT-9
Dynamic
Ciub
S
FLIGHT
MANUAL
I
Section
2
Page
2-5
Empty
weight
kg
Maximum
take-offweight
472,5
kg
Maximum
land
ing
weight
472,5
kg
Useful
bad
kg
Maximurn
fuel
weight
kg
Maximum weight
in
Baggage
Compartment
10 kg
WARNING
Maintain
maximum take
off
weight
472,5
kg
Depending
on
different
countries
rules
2.8
Centre
of gravity
Position
ofC.G.:
Empty
airplane
12
± 2% MAC
Position
ofC.G.
in
flight
20
+ 30%
MAC
Rear
centre
of gravity
limit
is
valid
for
en-route weight
at maximum
crew
weight.
forward
centre
ofgravity
limit
is
valid
for
minimum pilot
weight
70 kg and
minimum
capacity
ofthe
fuel
tanks.
Example
to check
the
centre
ofgravity
position
is
in
Sect.
6.
2.9
Approved manoeuvres
WT-9
Dynamic
Ciub
S is
certified
in the
Normal
Category.
The
folbowing
manoeuvres
are
permited:
— Steep
tums
with
the
angle
of
bank
up
to
600
- appropriate
entry
speed
is
140
kmlh.
— Lazy
eighths
-
appropriate
entry
speed
is 140
km/h.
—
Combat
turns
-
appropriate
entry
speed
is
200
kmlh.
WARNING
Aerobatic
manoeuvres
and
intentional
spins
are
prohibited!
Date:
12.09.2011, Rev.:
10
,Appr”
I
2.7
Weight

I
WT9 Dynamie
LSA
Ciub
S
FLIGHT
MANUAL
Section
2
Page
2-6
I
2.10
Manoeuviing
bad
factois
2.11
Flightcrew
Ihe
minimum
flight
crew
with which
the
airplane
is allowed
to
fly
is one
pibot
sitting
in
the left
pilot
seat.
The
passenger
or
another pilot
may occupy
the
right seat
in
the
cockpit.
2.12
Kinds
ofoperation
The aircraft
WT9
Dynamic LSA
Ciub
S
is approved
to
perform
flights in
accordance
with
VFR
day only.
Aerobatic manoeuvres
and
intentional
spins
are prohibited!
0
WARNING
JFR
flights
and flights
in
icing
conditions
are
prohibited.
for
flight
operations
the
following
minimum equipment
must
be
installed:
-
Magnetic
compass
-
Sensitive barometric
altimeter
- Airspeed indicator
-
Pibot’s
Safety
beits
2.13
Fuel
The following
fuels and
oils can
be used
for
ihe
aircrafi WT9
Dynamic
LSA
Ciub
S
see
chapter
2.4
Powerplant
and the
Operator’s
Manual
for
engine
ROTAX
912
ULS.
I
Date:
01.12.09, Rev.: 0
I
Aiwr”
Manoeuvre
speed
Speed
Load factors
km/h
MPH
knots
VA-
Manoeuvring
speed
165
103
8$
+
VNE
Never
exceed speed
280
174
iso
+
4
V.
— Manoeuvring
speed
165
103 $8
-2
VNE_
Never
exceed
speed
280
174 150
-2
VFE—
Maximum
Flap
Extended
140
$8
75
+
2
speed
0
0
0

WT-9
Dynamic
CIub
S
FLIGHT
MANUAL
Section
2
Page 2-7
I
_______________________________
Lefttank(1)
Righttank(l)
The
total
quantity
of
fuel
in
the tank
Unusable
fuel
in the tank
The
total
usable
quantity
of fuel in
the tank
2.14
Maximum
passenger
seating
The maximum
number
ofpassenger
aboard
is
one
passenger
sitting
in
the right
seat in
the
cockpit.
2.15
Other
limitations
The maximum
demonstrated
crosswind
vetocity
for
take-offand
tanding
is
12,4
m/s
(24
knots).
NO
SMOKING
on
board
the ultralight
aircraft.
Maximum
towing
cable
bad
is
3.000
N. If the
strength
oftow
cable
is more
than
3000
N
a
weak
link
must
by
used.
Maximum
weight
oftowed
glider
is
750 kg.
Maximum
weight
oftotving
aircraft
by
I pilot occupation
is 440
kg.
2.16
Limitations
placards
Airspeed
lAS
km/h
MPH knots
Never
Exceed
speed
VNE
280
174 150
Normal
Operating
Limit
speed
VNO
250
156 135
Rough Air
speed
VRA
230
143
124
Manoeuvring
speed
VA
165 103 88
Maximum Flap Extended
speed
VFE
140
88 75
Aerobatics,
intentional
spins
and
stalis
are prohibited!
I
IFR
flights
and
flights
in
icing
conditions
are prohibited!
I
Date:
12.09.2011,
Rev.:
10
,,Appr”
I

[
WT9 Dynamic
LSA
Ciub
S
FLIGHT
MANUAL
Section
2
Page
2-8
I
Maximurn
allowed
filling
of
the
fueJ
tanks
in
litres
Baggage
I
Crew
weight
(kg)
weight
(kg)
160
170
180 190
200
210 220 230 240
0
full
99
85
71 57
43
29
15
1
5
full
92 78
64
50
36
22
8
0
JO
99
85
71
57
43
29
15
i
0
Maximum
Baggage
weight
10
kg
-c
I
Date: 01.12.09,
Rev.:
0
j
,,Appr”