STEMME S12 User Manual

DOCUMENT NUMBER:
L500-912.820 ISSUE JUL 20, 2016
AMENDMENT: 00
DATE: 
CHAPTERPAGE D5
MAINTENANCE MANUAL STEMME S12
Weight and balance report
Document Number
1001
-
12
-
S12
-
2
STEMME S12
Page 2 (of 2)
4. Determining of Empty Weight Center of Gravity
4.1. After Weighing:
x
mb
m
a
S
S
e
=
⋅
+
[mm / in.]***
⇒
S
x
=
x
+
=
mm / in.
***
4.2. After Changes, without Weighing:
Following changes have been made on the powered glider:
Install. /
Removal
Item
Weight (
+
/
-
)
m = [kg / lbs]***
Moment Arm (
+
/
-
)
x = [mm / in.]***
Moment (
+
/
-
)
M =[mm kg / in. lbs]***
Sum m
add
=
Sum M
add
=
-
NOTE: Count weight installed positive, weights removed negative.
Count moment arms aft of datum positive, in front of datum negative.
add
addoldold
newS
m
Mxm
x
+
⋅
=
,
[mm / in.]***
⇒
newS
x
,
=
x +
= mm / in.
***
5. Definition of load
Empty Weight:
kg / lbs***
Empty weight CG aft of datum:
mm / in. ***
Minimum Load Required on seat (full water ballast and luggage)
(otherwise
ballast)****
kg / lbs***
Minimum Load Required on seat (empty water ballast and luggage)
kg / lbs***
Maximum Load (MTOW - Empty Weight)
kg / lbs***
Max. Load in Cockpit (Cockpit load must be at least 10 kg / 22 lbs less than
maximum load!)
kg / lbs***
*** Units: cross out if not applicable
****According to Maintenance Manual, Section 6.3
Strausberg,
Site, Date Stamp Sign Job Leader
Inspector Statement: All measured data are within the allowable ranges and correspond to the production
and
maintenance instructions of the type.
Strausberg,
Site, Date Stamp Sign Inspector

STEMME S12 Specifications

General

Brand	STEMME
Model	S12
Category	Aircrafts
Language	English