SC-POH-1-1-17
Revision: -
Date of issue: 2011-09-01
SECTION 1
GENERAL INFORMATION
S
S
p
p
o
o
r
r
t
t
C
C
r
r
u
u
i
i
s
s
e
e
r
r
1-5
1.2 Summary of performances
Weights:
Max. takeoff and landing weight ....................
1,320 lb
Max. weight of fuel .........................................
180 lb
Max. baggage weight in rear fuselage ...........
40 lb
Max. baggage weight in each wing locker .....
22 lb
Wing loading ..................................................
10 lb/sq ft
Power loading ................................................
13.39 lb/hp
Speeds:
Maximum at sea level ....................................
119 KIAS
Cruise, 75% power at 3,000 ft .......................
93 KIAS
Range and endurance:
Range ............................................................
516 NM
Endurance .....................................................
5:25 h:mm
Conditions:
Usable fuel .............................................................. 29.85 US gal
75% power of engine .............................................. 5,000 RPM
Altitude .................................................................... 3,000 ft
Reserve .................................................................. 30 minutes
Empty weight (minimum equipment) ..............
842.3 lb
SC-POH-1-1-17
Revision: -
Date of issue: 2011-09-01
SECTION 1
GENERAL INFORMATION
S
S
p
p
o
o
r
r
t
t
C
C
r
r
u
u
i
i
s
s
e
e
r
r
1-5
1.2 Summary of performances
Weights:
Max. takeoff and landing weight ....................
1,320 lb
Max. weight of fuel .........................................
180 lb
Max. baggage weight in rear fuselage ...........
40 lb
Max. baggage weight in each wing locker .....
22 lb
Wing loading ..................................................
10 lb/sq ft
Power loading ................................................
13.39 lb/hp
Speeds:
Maximum at sea level ....................................
119 KIAS
Cruise, 75% power at 3,000 ft .......................
93 KIAS
Range and endurance:
Range ............................................................
516 NM
Endurance .....................................................
5:25 h:mm
Conditions:
Usable fuel .............................................................. 29.85 US gal
75% power of engine .............................................. 5,000 RPM
Altitude .................................................................... 3,000 ft
Reserve .................................................................. 30 minutes