STEMME S12 User Manual

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 dierence 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 dierence 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 ight manual (section 6.2), the
dierence between minimum load and actual load must be compensated by ballast.

STEMME S12 Specifications

General

Brand	STEMME
Model	S12
Category	Aircrafts
Language	English