DOCUMENT NUMBER:
L500-912.820 ISSUE JUL 20, 2016
AMENDMENT: 00
DATE: --
CHAPTER-
PAGE 6-7
MAINTENANCE MANUAL STEMME S12
Figure 6.3.c
Range of Empty Weight CG as a function of Empty Weight and Minimum Load
for no tail-boom loading (empty water ballast and luggage compartment)
THE FOLLOWING WEIGHT LIMITS MAY NOT BE EXCEEDED UNDER NO CIRCUMSTANCES:
• Max. T/O weight 900 kg / 1984.16 lb,
• Max. weight of non-supporting parts (GNT) 610 kg / 1344.82 lb,
• Max. total load, which is cockpit-load plus fuel: 900 kg minus empty weight according to
valid »Weight and Balance Summary«,
• Max. cockpit-load, which is the sum of both cockpit occupants (incl. parachutes) plus
weight of baggage in baggage compartments: 202 kg / 445.33 lb, but not more than the
weight limit stated in the »Weight and Balance Report«,
• Max. 180 kg / 396.83 lb total for both occupants including parachutes,
• Max. weight per seat (pilot or copilot, incl. parachute) 110 kg / 243 242.51 lb,
• Max. baggage load in cockpit baggage compartments 22 kg / 48.5 lb, but maximum
is also the difference between max cockpit load and max weight of both occupants
(180 kg / 396.83 lb).
• Max. baggage load in tail-boom baggage compartments 20 kg / 44.09 lb, but maximum
is also the difference between max cockpit load and max weight of both occupants
(180 kg / 396.83 lb).
When loads are below minimum loads as stated in the flight manual (section »6.2«), the
difference between minimum load and actual load must be compensated by ballast.
Summary of Contents for S12
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Page 255: ...A FLIGHT CONTROLS PITCH CONTROL AND TRIM ...
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