Airplane Factory SLING 4
Pilot Operating Handbook
Page | 2-6
DC-POH-001-X-C-3
Revision : 1.3
2.5
Crosswind and wind limitation (demonstrated)
Maximum demonstrated cross wind component
for take-off and landing:
15 kt.
2.6
Service ceiling
Service ceiling:
14 000 ft.
2.7
Load factors
Maximum positive limit load factor:
+3.8 g.
Maximum negative limit load factor:
-1.9 g.
Maximum positive load factor with flaps:
+2 g.
Maximum negative load factor with flaps:
0 g.
2.8
Weights
Maximum take-off weight:
920 kg (2028.25 lb).
Maximum landing weight:
920 kg (2028.25 lb).
Maximum luggage weight:
35 kg (77.16 lb).
Summary of Contents for SLING 4
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