Sinus 912 LSA Glider 550 MTOW
www.pipistrel.eu
REV. 3
Placards
This aircraft is approved to fly in v
isual meteorological conditions (VMC) only
and flights in instrumental meteorological conditions (IMC) are prohibited!
This aircr
aft is equipped
with a rocket powered ballistic rescue system.
PASSENGER WARNING
This aircraft was manufactured in accordance with Light Sport Aircraft airworthiness standards and does not
conform to standard category airworthiness requirements
NO STEP
3,5 l OIL
Refer to ROT
AX manual
NO STEP
80 %
ANTIFREEZE
+ 20 % W
ATER
ROCKET
GAS
EXHAUST
A
T
TENTION!
ROCKET
INSIDE
MAX 1.8 bar
MAX 26 psi
MAX 1.2 bar
MAX 18 psi
MAX 0.8 bar
MAX 12 psi
MAX 1.8 bar
MAX 26 psi
OPEN
CLOSED
D
R
R
A
E
I
T
N
A
V
W
A
/
L
L
V
E
E
U F
CL
N
O
E
S
P
E
O
DANGER
EXPL
OSIVE
EGRESS
EAW
MT
OW
CREW WT
LUGGAGE WT
lbs
1212 lbs
min.121 lbs
55 lbs
FUEL
QTY
30 l (7.9 USgal)
use automotive fuel
This aircr
aft is equipped
with a rocket powered ballistic rescue system.
EAW
MT
OW
CREW WT
LUGGAGE WT
kg
550 kg
min. 55 kg
25 kg
FUEL
QTY
30 l (7.9 USgal)
use automotive fuel
US
gal
Li
ter
US
gal
Li
ter
Sv50
Sv50
1
3
4
5
6
2
30
5
10
15
20
1
3
4
5
6
2
5
10
15
20
30
5
10
15
20
US
gal
Li
ter
US
gal
Li
ter
1
4
6
2
Sv30
Sv30
5
10
15
20
5
10
15
20
1
4
6
2
PULL FOR PARACHUTE
DEPLOYMENT
WARNING
ROCKET FOR PARACHUTE
DEPLOYMENT INSIDE
+18
+9
0
34-60 kts
38-70 kts
40-86 kts, then
-5
Respect limits
from POH!
VSO VS1 VFE VA VNO
34 kts 40 kts 70 kts 76 kts 76 kts
VNE
120 kts
Respect limits
from POH!
OPEN
CLOSED
R
L
R
MIC
L
OPEN
CLOSED
O
PE
N
CL
O
SE
D
O
PE
N
CL
O
SE
D
HEADSET
SEE AIRCRAFT FLIGHT MANUAL FOR BAGGAGE LIMITATIONS AND WEIGHT
AND BALANCE INFORMATION
2-8
Limitations