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ページを印刷する2.12 Further Limitations
2.12.1 O
PERATING
DG Flugzeugbau GmbH
Type: LS8-xx
Airspeed Limits:
Winch launch/Auto tow
Aero tow
In rough air
Never exceed (VNE)
Max. Take-off Mass *) 15 42
Max. Take-off Mass *): 18 59
*) including water ballast
Aerobatic manoeuvres not approved
Weight Limitations
Maximum Cockpit Load ....max.______kg/lbs
Minimum Cockpit Load
with tail battery, tail tank full min.
with tail battery, tail tank empty min. ______kg/lbs
without tail battery, tail tank full min
without tail battery, tail tank empty min._____kg/lbs
Lighter pilots must compensate lack of weight as
suggested in Flight Manual
MINIMUM COCKPIT LOAD:
with tail battery, tail tank full
with tail battery, tail tank empty
without tail battery, tail tank full
without tail battery, tail tank empty min. ________
m
ft
Up to 2000 ( 6500) - 280 174
Up to 3000 ( 9800) - 266 165
Up to 4000 (13100) - 253 157
Up to 6000 (19700) - 227 141
Up to 8000 (26200) - 202 126
Up to 10000 (32800) - 179 111
Up to 12000 (39400) - 156
Edition: June 2016 Revision 5
Flight Manual LS8-s and LS8-sb
P
L
LACARDS FOR
IMITATIONS
Serial No.:_______
Data Placard
km/h
Kt MPH.
140
76
195
105 121
195
105 121
280
151 174
m
ft
kg
525 1157
575 1267
______kg/lbs
min. ________
min. ________
min. ________
km/h mph
Kt.
151
144
137
122
109
97
97
84
TN 8024
xx= variant
-s or –sb
at right hand cockpit wall
87
lbs
_____kg/lbs
under instrument panel
kg / lbs
cover
Maximum baggage weight 5 kg (11 lbs)
(Soft items only)
at baggage compartment
near airspeed indicator, if not marked
on ASI
Limitations
EASA appr.
2-12