SC-POH-1-1-17
Revision: -
Date of issue: 2011-09-01
SECTION 2
LIMITATIONS
S
S
p
p
o
o
r
r
t
t
C
C
r
r
u
u
i
i
s
s
e
e
r
r
2-3
NOTE
Altitude losses shown in the table present max. values determined on the basis of
flight tests using average piloting skill.
2.3 Flap extended speed range - V
S0
to V
FE
Flap operating range ....................................................
31 - 75 KIAS
2.4 Manoeuvring speed - V
A
Manoeuvring speed
at 1,320 lb
........................................
88 KIAS
Manoeuvring speed
at 900 lb
...........................................
70 KIAS
2.5 Maximum structural cruising speed – V
NO
Maximum structural cruising speed ..................................
108 KIAS
2.6 Never exceed speed - V
NE
Never exceed speed .........................................................
138 KIAS
2.7 Service ceiling
Service ceiling ..................................................................
14,378 ft
2.8 Load factors
Maximum positive limit load factor ..........................................
+ 4 g
Maximum negative limit load factor .........................................
- 2 g
2.9 Approved manoeuvres
The
S
S
p
p
o
o
r
r
t
t
C
C
r
r
u
u
i
i
s
s
e
e
r
r
is approved for normal and below listed manoeuvres:
x
Steep turns not exceeding
60°
bank
x
Lazy eights
x
Chandelles
x
Stalls (except whip stalls)
