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  9. LET L-23 Super Blanik Technical specifications

LET L-23 Super Blanik Technical specifications

LET
, 686
04
KUNOVICE, CZECH REPUBLIC
SAILPLANE FLIGHT MANUAL
Seria
l
Nos.eligible
: 938101,
and
subse
quend
:-r•:.:Ji:~~-~
..
.;~,:;;...
...
:
.,..:
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..
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.
-:.
. . t 0
:·
B.2
3
~
SUPER
.
-
BLANIK
·
·-.-.:~t
.:
..
:;.:~
:
~
:.:!.·
,•,"'
.-:
.;
·.
.
Model :
Serial No
.:
~.~:
9-783
'
0(
(
~·'
-.
..
·~
.,.
....
,;.
..
,
'\
Registration :
Document No
.:
Do-
L23 . 1012.5
Date of Issue : December 1, 1993
ThissailplaneFli
ght
Manualis
FAA
Approved foru.s.-registeredsailplanes
inaccordancewithprovision
of
14CFR Part
21
.29,and as reguired
by
FAA
TypeCertificateDataSheet
No
.G60EU.
Approved
by
TheCivilAviationInspectorateofTheCzechRepublicinPrague.
Signature :
~
Authority :
CA
l,
Prague
Stamp:
~
~
-
~~
,
~
.
Originaldateo approval:December6,1993
This
S~Hp
lane
FlightManual
mu
st
be
curied
in
the
sailplane
at
alltimes.
This
sa
ilp
lane
is
to
be
operated
in
c
ompl
i
an
ce with
information
and
limi
t
aliol)s
cont
ained
herein
.
~
686
04
KUNOVICE
CZECH REPUBUC
L
23
SUPER
•
BLA
N
IK
SAI
LPLA
.NE
FLIGH
T
MANUAL
O.
l.
RECORD
OF
REVISIONS
Oo
• L
23
. 1012.5
Any
re
v
ision
or
amendment
of
the
present
Manual
w
ill
be
issued
in
the
form
of
Bulletins.
approved
by
the
Civil
Aviation
Authority
of
the
Czech
Republic.
supplement
of
wh
i
ch
will
contain
new
(revised)
pages.
User's
duty
is
to
mak-e a
note
about
revrsions
in
the
Record
of
revrsions
and
to
replace
existing
pages
wi
th
revised
and
effect
i
ve
ones
.
Revised
or
amend
!ld
parts
oi
the
text
will
be
i
ndicated
by
a
ver
t
ical
line
in
the
left
hand
margin
and
the
revision
No
.
and
the
date
will
be
shown
on
the
bottom
left
hand
oi
the
page
.
Rev
. I
AlfeCJ:ed
j
.>lf
ected
pages
j 'Jate I Bl)lletln i
Date
of
Oate
inse.ned
and
No. !Section I i ;
No
. i
BUIIeli
n : signature
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686
04
KUNOV1
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CZECH REPUBUC
fle.f.
""-eel
No
.
Sec;on
.
Dec 1/93
L
23
SUPER ·
BLANIK
S
AILPLANE
FLIGHT
M
ANUAL
Ntoctedpagos
Oal
o
8ull<!lin
Ooao
ol
No
.
Welin
apProval
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. -
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686
04
KUNOVICE
CZECH
AEPUSUC
SAILPLA
NE'
FLIGHT
MANUAL
Oo
• L
23
. 1012.5
0.2.
LIST
OF
EFFECTIVE
PAGES
Pages
identified
as
"
Appr
.·
provide
information
reguired
10
be
furnishe
·d
by
the
Federal
Aviarion
Aegularions
.
.
Date
j Section '
Se<:tlon
I
Page
. .
Page
! Date
!
I !
Jan
t3i99 •
0 1 • I Apcr.
tS
Dec
1/93
i 2 : .
0«:
t
i93
I Appr. 16
Dec
11'93
.
i 3
Jan
t3i99
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1193
! 4 i
Jan
13i99 ! Appr.
18
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t/93
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ppr
.
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Dec
t/93
I l
I Appr. 20
Oec
1/93
I Apor.
21
i Dec
t/93
I ! ! Appr. ?2 . Dec 1/93
I I l i
1 i 1
Oct30/96
5 Appr. 1
Dec
t/93
' 2
Dec
1
;9
3 ! .>.ppr. 2
Dec
1193
! l I
l 3
Oct
30i
96
I Appr.3 :
Oec
1/93
4 i Oct 30196 I .>.ppr. • Dec t/93
! 5 Oct 30196 !
I i i
2 ! Appr. t l
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t/93 6 1
Dec
t/93
I Appr. 2 ;
Dec
ti93 i 2 !
Dec
ti93
! ApJli
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I
0«:
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3 : Dec t/93
:. i Dec
i/93
I Appr. 4
0«:
1/93 I 4 !
I Appr. 5 IDec20/9S 5 ' Dec 20/9S
Appr
.6
Dec 1/93 I 6 i Dec
20/9S
Appr. 1
0«:
1/93 I 7· I Dec 20/!lS
Appr. 8
0«:
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•
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0«:
1/93 !
Appr.
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Dct30/96
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Oct30
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96
3 • Appr. t Oct 30/96 7 I I •
Sep
20/96
'Appr. 2 Oct30196 2 .
Dec
t
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Appr. 3 Oct 30/96 3 '
Dec
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Appr
.4
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30/96 4 \
Oct30/96
Appr. 5 I
Oct30
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96
5 I Oct30196
I 6
Oct
30196.
I
'
4 I Appr, 1
0«:
1
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8 1
Dec
1193
Appr. 2
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1/93
I Appr. 3
Dec
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Appr. • I
0«:
1/93 i
I
ApP<
. S I
Oct
30196
I9 I 1 •
Jan
131'99
.
' Oct30196
I Appr. 6 2
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13199
! Appr. 7
Oct30/96
3 • Jan13199
Appr. 8 J
Dec
t/93
i
APP<
· 9
0«:
1/93 .
.
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.
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0«:
1/93 I .
___
_ _
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. Appr.
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l
Dec
1193
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Appr.
12
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1193
I l
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Dec
1/90 I
App<
.
14
i
Dec
1/93 I
Jan
131
99
® 0 - 3
~
686
04 KU
NOVI
CE
CZECH
REPUBUC
L
23
SU
PER
-B
LANIK
SAILPLANE
FLI
GHT
MANUAL
Do
• L
23
. 1012.5
0.3.
TABLE
OF
CONTENTS
Section
Ge
ner
al
( a
non-approved
section
) 1
Limitation
s
(an
approv
ed
se
·
ction
) 2
Emergency
procedures
(an
approved
section
) 3
Normal
procedures
(an
app
roved
section
) 4
Pe
r!orman
ce
(a
partly
approved
sec
ti
on
) 5
Weight
a
nd
ba
l
ance
( a
non-appro
v
ed
section
) 6
Sailplane
and
s
ystems
description
( a
non-approved
section
) 7
S
ailplan
e
handling,
ca
re
and
maintenanc
e ( a
non-approved
section
) 8
Sp
pplem
en
ts (a
partly
approved
section
) 9
Jan 13/99 @
0·4
~
686
04
KUNOVlCE
CZECH
REPU6UC
Oct30!96@
L23
SUPER
-
B
L.A
r~:K
SAILPLANE
FLIGHT
MANUAL
Do
-L 23. 1012..5
SECTION
1
General
CONTENTS
1.1
Introduction
1.2
Certifica
t
ion
basis
1.3
Warnings,
cautions
and
notes
1.4
Descriptive
data
1.5. 1
Three-view
drawing
-
to
ser.
No.
xx
8320
1.5
.2
Three
-view
drawing
-from
ser
.
No.96
8401
1
-,
~
68604 K
UNOV1CE
CZEQH REPUBLIC
L 23 SUPER -
BLANIK
SA
ILPLANE
FLIGHT
MANUAL
Oo-
L 23. 1012.5
1
.1
I
NTRODU
CTIO
N
The
sailplane
flight
manual
has
been
pr
epared
to
provide
pilots
with
information
for
t
he
safe
and
eHicient
op
e
ration
of
the
L
23
SU
PER-
BLANIK
sailplane
.
Tills
manual
inc
ludes
t
he
mater
ial
required
to
be
furn
i
shed
to
the
pilot
by
JAR • 22.
II
also
contains
su
pplemental
da
ta
supplied
by
the
sailplane
man
uf
actu
rer
.
1.2
CERTIFICATION
BASIS
This
typ
e
of
sailplan
e
has
been
approved
by
the
Ci
vil
Aviation
I
nspec
t
orate
of
the
Cz
ech
Republic
in
accordance
whh
JAR
-
22.
C
hange
4
Iss
ued
Ap
ril
1, 1980
including
Amendment
22
/86/1
Elf
.
Oct.
22. 1
986
and
AC
21.17
-2.
1.3.
WARNINGS.
CAUTIO
NS
AHP
NOTES
T
he
f
ollo
w
ing
delinit
i
ons
apply
to
wa
rnings,
cau
t
ions
a
nd no
tes
used
in
t
he
Flight
M
anual
.
WARNING
:
CAUTIO
N:
No
te
:
Dec
1/93
M
EA
NS
THAT
THE
NON
·0
8SERVATtON
OF
THE
CO
RRESPONDING
PRO
CEDU
RE
LEADS
TO
AN
IMMEDIATE
OR
IMPORTANT
DEGRADATION
OF
THE
FLIGHT
SAFETY
means
that
the
non-observation
of
the
corresponding
procedure
leads
to
a
min
or
or
to
a
more
·
or
less
long
term
degradation
of
the
flight
safety
.
draws
the
atte
ntion
on
any
-s
pec
ia
l
item
not
direc
tly
related
to
safety
but
w
hich
Is
impor
tant
or
unusual
.
1
-2
~
68604 KUNOVICE
CZECH REPUBUC
SAILPLANE
FLIGH
T M
ANUAL
Oo
• L
23
. 1012.5
1.4
OESCB
!
PT
!VE
QATA
The
L
23
SUPER
·
BLANiK
sailp
lane
is
a
cantilever.
high
-wi
ng,
tw
o-
soo
t
gl
ider
of
all
-
me
t
al
struc
tu
re
. W
ing
tip
extens
ions
are
op
t
ional.
Basic
dj
mensions
W
ing
span
• •
...
• .
..•.•
....
.
.•....
53
. 15
It
(16
.2
m)
(w
i
th
the
inst
alled
w
ing
tip
extensions)
.
....
59
.
71
It
(t8.
2
m)
N
ote
:
II
th
e
wing
t
ip
with
suppor
t
ing
w
heel
is
installed
wing
span
is .
Le
ngth
He
igh
t
.
53
.
:35
It
(16
.
26
m)
.
27
.
89
fl(8.5
m)
. 6.
23
11(1
.9
m)
Wing
area
. . . . • . • • • • • •
..•
. . . . . .
206
.13
sq
lt(19
.15
sq
.
m)
(w
it
h
the
inst
alled
w
ing
tip
extensions)
. •
...
215
.27
sq
fi(20
.
00sq
.
m)
Aspec
t
ratio
..
. .
..
••....
..•
.
•••.•.
13.7
(with
the
installed
wing
tip
extensions)
..
.
..
16.6
Me
an
ae
r
odynamic
chord
.
....
.•
. . .
....
4.'
11
tt(1.253
m)
1 • 3
~
686
04
KUNOVI
CE
CZECH
AEPUBUC
L
23
S
UP
ER ·
BLA
N
IK
SAILP
LAN
E
FLI
GHT MA
NU
AL
Do
-l 23. 1012.5
1.5.1
D1
R
EE
·V
I
EW
O
RA
WING
(Dimensions
in
nvn)
• vaf
od
tO
ser
. No.
XX
8320
Feb 1
5197
@
·•
r·
.,
~
-----
--
--
0
0
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-
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-
I~
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~
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•
--
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t -4
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68604 KUNOVI
CE
CZECH RE
PUBUC
L
23
SUPER -
BLANIK
S
AILPLANE
FLIGHT
MANUA
L
Do-L
23. 1
012
.5
1.5
.2
THBE
E •
VlEW
DRAWING (Dimensions
in
mm
) . valid l
rom
se<
. No. 968401
;:.,
t I
~
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::
r
~
r-+-
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\\
51
0
« 0
M N
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=
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-
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v
.
~
F
eb
15197 @ 1 • 5
~
686 04 KUNOVICE
CZEC
H
REPUB
LIC
L
23
S
UPER
• BLANIK
SAILPLANE
FLIGHT
MANUAL
SEC
TI
O N 2
Limitations
CO
N
TE
N
TS
2. 1
Introduction
2.2
Airspeed
2.3
Airspeed
Indicator
mark
ings
2.4
Weight
2.5
Centr
e
of
gravity
2.6
Approved
manoeuvres
2.7 M
anoeu
v
ring
load
fa
ctors
2.8
Flig
.
ti
t
crew
2.9
Kinds
of
operation
2.
10
M
inim
um
equipmen
t
2.11
Aeroto
w
and
w
inch-
launch
ing
2.12
Other
limitations
2.
13
Limitation
placards
Do-L
23
.
10
1
2.5
2-
1
~
l23
SU
P
ER-
BL
AN
IK
686 04KUNOVICE
CZECH REPUBUC
SAilP
LANE
FLIGHT
MAN
UA
L Oo -L
23.
1
0'1.2
.5
2.1
I
NIROOUC
T!ON
Section
2
includes
operating
limitations
and
basic
placards
necessary
lor
sale
operation
of
the
sailplane
.
its
standard
systems
a
nd
standard
equipmen
t.
The
limitations
in
this
sect
i
on
are
FAA
approved
by
the
CAl,
Czech
Republic
.
The
values
in
parentheses
are
valid
only
when
using
wing
tip
extensions
.
2 .2 AIR
SPE
ED
Speed
km/h lAS Remarks
VNE
Never
exceed
speed
up
230
Do
not
ex
ceed
t
his
speed
in
any
to
a
pressure
altitude of
operation
and
do
not
use
more
lhan
4200
m 1!3
of
control
deflection
VRA
Rough
air
speed 160
Do
not
exceed
this
speed
except in
smooth
air.
and
then
only
with
caution.
Examples
of
rough
air are
lee-wave
ro
t
or
thunderclouds
etc
.
VA
Manoeuvring
speed
150
Do
not
make
full
or
abrupt
control
movement
above
this
speed
.
because
under
ce<tain
conditions
•
t
he
sailplane
may
be
overstressed
by
full
control
movement
Vw
Maximum
winch-
120
Do
not
exceed
this
speed
during
launching
speed
winch-
or
autotow-launching
VT
M
aximum
aeroto
w
ing
150
Oo
not
exceed
this
speed
during
speed
aerotowing
VlO
Maximum
landing
ge
ar
230
Do
not
ex1end
or
retract
the landing
opetating
speed
gear
above this
speed
Note:
VNE
alrsp!led
limits
above
4200
m
Pressure
Altitude
are
redu-
ced
as
follo
w
s:
Pressure Altitude m •
4200
6000
7500
9000
10500
VNE
km/h
-
iAS
-··
--
-
230
- ·-
230
··
-- ·
ns-
-- -
200
-
--,
as
·-
(230)
(210)
(195)
(180)
(165)
•-
Altimeter
Setting
at
1013.25 hPa.
Appr. @
Feb15/97
2-2
r:s
l
23
SUPER -
BLA
NIK
686 04 KUNOVICE
CZECH REPUBUC
SAilP
LA
NE
F
LIGHT
MAN
U
AL
Oo · L 23. 1012.5
2.3
AIRS
P
EED
I
NQICAT
OR MA
RKIN
GS
M
arking
lkm/h
lAS (value -
ran
ge)
Signi
l
icance
Green
arc
66.
160
Normal
Operating
Range
.
.
(Lower
lim
it
is
max
imum weight
1.1
vst
at
mos
t f
orward
e.g.
Up
per
limit
is
rough
a
ir
speed)
Yellow arc 160 . 230 M
anoeuvres
must
be
conducted
with
caution
and
only in
smooth
air.
Red
line
230
Ma
ximum
speed
lor
all
operation
s
Yellow
tr
ian
gle 75
Approach
speed
at
ma
x
imum
coo
·> wei
ghl.
N
ote
: ye.ltow
triangle
(90•)
valld:fr~m
·
,.ser
.
No
·
97
~402
2.4 W
EIG
HT
LI
MI
TS
Max
lm
um
.
take
-
oil
and
landing
weigh
t:
• w
ith
two
occupan
ts
.•.•.•
-
with
one
pilo
t
.•.
.
•••
Empty
weight
wi
th
standard
equipment
.•
..
and
th
e
cor
respond
i
ng
cen
tre
'
510
kg
420
kg
310
kg
:!:
2
%(3
15
kg=
2%)
of
gravity
position
• • . • • . . • . • • • 67.30
:!:
1%
MAC(6
8.
30:!:
2%
MA
C)
M
aximum
weight
of
all
non
lifting
parts
353
kg
(348
kg)
N
ote:
Aw-
@>
Feb
15197
Refer
to
weight
and
Balance
(
Se
ction
6
.0
)
to
determine
actual
empty
we
ight
I
e.g
.
as
est
a
blished
by
t
he
installed
equipment
and
manufacturing
tolerances.
• 4
-.
- -
--
-
--
--
-
( Con
l)
2·3
~
686
04 KUNOV1CE
CZECH AEPUBUC
L
23
SUPER
-
BLANIK
SA
ILPLAN
E
FLIGHT
MANUA
L
Pilot's
weight
{including
parachute)
:
-
minimum
pilot's
weight
{solo
) . . . . .
..
70
kg
Do - l
23
. 1012.5
It
is
necessary
to
use
lront
seat
removable
ballast
of
15
kg
when
llown
solo
by
a
pilot
(includ
i
ng
parachute)
we
i
ghing
tess
t
han
70
kg
in
the
lront
cockpit.
Note
:
Installation
of
the
front
seat
ballast
is
described
in
Section
7,
paragraph
7.2
of
this
Flight
M
anual.
-
maximum
pilot's
weight
(
solo
)
..
0 0
110
kg
M
aximum
useful
to
ad
(occupants.
baggage.
optional
equipment)
. .
..•.•
200
kg
(195
kg)
Maximum
baggage
compartment
load
...
10
kg
2 - 4
~
68604 KUNOVICE
CZECH REPUBLIC S
AIL
PLA
NE FLIGHT MAN
UAL
Do-
L 23. 1012.5
2.5
CE
N
TRE
O F
GRA
VITY
Cenlre
of
gravity
range
- f
ront
limit
...
.•...
23%
M
AC
i.e.
4.
397
in
(
11
2
mm)
aft
of
reference
dalum
-
rear
limit
. _ • . _
•.
•
•.•..•
.
••
.•..
.•
40%
M
AC
i.e
.
12
.
783
in
(325
mm)
af
t
of
reference
datum
Wing
tip
extensions
installa
t
ion
moves
the
center
of
gravi
ty
of
the
empty
sailplane
1%
M
AC
(0
.493
in
e 1
2.53
mm)
to
the
back
.
The
reference
datum
is
located
93
.6
in(2
.
37
m)
aft
of
the
sailplane
no
se.
2.6
APPROVED
MAN
OEU
vRES
(U
TILIT
Y CA
TEGORY)
Sailplane
is
certified
in
the
Utility
Category
.
W
ith
the
installed
w
ing
tip
extensions
all
aerobatic
manoeuvres
are
proh
i
bited
.
M
anoeuvre
Airspeeds
•
km/h
lAS
Pr
ocedures
SOLO
DUAL
ENTRY RECOVERY
Loop
160 180 X
Section
4.4.6 item 1.
Stall
turn
170 180 X
Section
4.4.6 i
tem
2.
Lazy
Eight
180 180 X
Section
4.4.6
item
3.
Spin 60
60
X
Section
4.4.6 item 4.
1
60
160
X
Chandelle(
climbing)
180 180 X
Section
4.4.6
item
5.
Steep
turn
170 180 X
Section
4.4.6
item
6.
Appr. @
Feb
15197
2 • 5
~
686
04
KUNOVICE
CZECH REPUBLIC SAILPLANE FLIGHT MANUAL
2 .7 .
MANOEUV
R
ING
LOAD
FACTORS
6
0 s
u
~
.,
4
..
0
..J
3
/
~
~
....
...
,
"
I
. i I i I I
,....
weigh~
510
kg
;-.._
I '
Do
- L 23. 1012.5
0
-...
so
100 150
200
1SOS
peed k
m/hiAS
"'
I
I
".
I
· I
[\.
...--
v
eloN
510kg
·2
I I I I I
FIG. 2 · I
2.8
FLIG
HT
CR
EW
Min
imum
·
one
pilot
. M
aximum
number
ol
occupants
is
two.
If
the
sai
lplane
is
10
be
llown
solo
.
the
pilot
must
be
sitting
in
the
front
se
at
and
his
we
ight
(i
ncluding
parachute)
must
be
70
kg
at
least.
II
the
pilot's
we
ight
is
less
than
70
kg,
it
is
necessary
to
use
the
cushio
n wi
th
1S
kg
ballast.
WARNING
:
TH
E REAR
SEAT
MUST
BE SECURED
AGAINST
FOLDING
AND
SAFETY
HA
RNESSES ON
THE
REAR
SEAT
MUST
BE
CONNECTED
,
DRAWN
TOGETHER
AND
SECUR
ED
.
2 .9
KINDS
OF
OP
E
RATION
T
he
sailp
la
ne
is
appr
oved
lor
Day
VFR
operations.
Cloud
·
flying
is
permitted
w
here
operational
regulations
permit
,
and
t
he
min
i
mum
reguired
egu
i
pment
is
Ins
talled
and
operable
.
(Conl)
Appr. @
Feb
15197
2-6
..
~
I:
I
~
686
04
K
UN
OVtCE
CZECH
REPUBLIC SAILPLANE F
LIGHT
MAN
UAL
2.11 AE
BO
TOW A
ND
WIN
CH
l A
UN
CHI
NG
A
ero
tqw
Oo • L 23.
10
12.5
•
the
maximum
cable
strength
or
cable
safety
device
(w
eak
link)
strength
is 65
00
N .
•
max
i
mum
per
missible
speed
Vr%
150
km/h
lAS
·
th
e
minimum
cable
length
lor
aero
t
owlng
is
15
m.
recommended
length
is
30 •
40
m.
W
inch-launching
• !
he
m
aximu
m
cable
stre
n
gth
or
cab
le
safety d
ev
•
ce
( w
eak
li
nk )
is 6
50
0 N .
•
ma
x
imum
permissible
speed
Vw =
120
km/h
lAS
2.1
20I
HER
l!MIIAT!ON
S
A. Max
imum
crosswind
componen
t
..
•maximum
de
monstrated crosswind
com
crone
nt
lor
sale approach. l
ancflt1g
and
aerotow launching
is
8 m/s lora
ng
le
90
.
Max
imum demonstratedcrosswind component lorwinch-launch
ing
:
c
..
c:
0
0.
e
0
u
'0
c:
1
0
0
·
FIG
.
2·
2
- - __
....
--
-
---·-
--
--
--
·- -
--
---
B.
Max
imu
m
demons
t
ra
ted
operatin
g
altitude
• 4
200
m
(Con
t. )
Appr. @
Feb
1519
7
~
L23
SUPER-
BLANIK
68604 KUNOVICE
CZECH REPUBUC
SA
ILPLAN
E
FLIGHT
MANU
AL
Oo - L
23
.
1012
.5
C.
Ma
ximum
Tire
Pressure
37
psi.
D.
Continued
Airworthiness
Life L.
imits:
The
fnilial
sailplane
service life
is
specified
to
sooo
fl
i
ght
hours
and
30000
landings
under
th
e fo
llo
wi
ng
oper
ating
conditions
:
-
Max.
4.83 take-offs per 1 flight
hour;
-
The
winch launching -aerotow take-
off
ratio
is
5 : 1;
-Crew:
35
% double, 65% single;
-Elementary tra
ining
-to-advanced t
ra
inin
g and
to
performance
soar
i
ng
ra
t
io
is 4
0%
: 60%, whereby t
he
aeroba
tics share is 2%
of
the
total
operation.
Sailplane
life
La
versus
operation
w
ith
wi
ng
-tip e
xte
nsions
is
La
~
6000 -25.x
(w
here x is
ope
ration
with
wing
tip
extens
i
ons
•n
percents
of
t
he
,
total
operation
time)
Appr.
Dec
1
/93
2 - 9
~
6e6
04
KUNOVICE
CZECH
REPUBUC
..., 4-
<J
vv
r
._.-.
-
----·•••
..
SAI
LPLANE
FLIGHT
M
ANUAL
2.
13
LIM
IIAT
IOHS
PL
ACA
R
DS
Do·
L 23. 1
012
.5
The
fo
ll
owing
op
_
erating
limllations
are
empha
s
ized
on
the
limilation
placards
in
both
cockpits
:
a)
front
cockpit
SEAT
SACK
PED
AL
ADJUS
TM
ENT
. .
-.l'll.OTS
WOOHT
•OA
S«.O
RICf
S:
•
wmtOUT
IAU.AST n ••
•
WI'TH
t .
..
&AUASt " kt
.
"''
..-s
15
kg
----,
j)
..
)
•
AIR VENT F
RONT
L
IFT
OFF
para
3.2.1
To
ser. No. xx 8320
C
ENT
RE
OF
GRAV
I
TY
RANGE
. F
RO
NT LI
MI
T •
23
%
M.A
C
REAR
LIM
IT . • 4
0%
M
AC
b)
both
f
ront
and
rear
co
ckpits
c....,P )
c
~
)
AIR BRAKES
(
~
)
(
~
)
lANDING
GEAR
(
s-
)
JElTISONIUFT
OFF
(REAR
SEAT
ONLY)
see para3.2.1
To ser. No. xx 8320
(
~
J)
FRONT
CANOPY.
JElTISON
see
para
3.2..
1
(
~
)
WHEEl
BRAKE
To
ser.
No
. xx 8320
[X]
-
---
(
~
-----
(
~
1)
__
-a
A
:
A~·e-
--------
cANOPv
UFT
OFF
CANOPY
JElTISON
( REAR
SEAT
ONLV )
From ser
No
96
8401
see para 3.2.2
· · Fromser. No. 96
8401
Appr.
@)
Feb
15197
2.
10

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