STEMME S6 Maintenance Manual

MAINTENANCE MANUAL
STEMME TSA-M
MAINTENANCE MANUAL
STEMME TSA-M
Permitted Range of Empty Mass CG-Location
Figure 203
08-10-00
Page 207
Permitted Range of Empty Mass CG-Location
300 320 340 360 380 400 420 440 460 480 500 520 540 560 580 600
630 640 650 660 670 680 690 700 710 720 730 740 750 760 770 780
Empty Mass [kg]
Permitted Range of Empty Mass CG-Location aft of
RP [mm]
Nose Heavy Area
Permitted Range of CG-
Location
Tail Heavy Area
Foremost CG-
Location
Rearmost CG- Location for min. Load of 40 kg 100kg 80kg 60kg 50kg
08-10-00
Page 206
Weight and Balance Report
Nov 18/11
Nov 18/11
EFFECTIVITY
Model S6
EFFECTIVITY
Model S6
1. Determining of Empty Weight Center of Gravity
1.1 After Weighing:
( )
e
frl
S
m
bmamm
x
×-×+
=
[mm / in.]
Þ
S
x
=
( + ) ×
-
×
=
mm / in.
***
1.2 After Changes, without weighing:
Following changes have been made on the powered glider:
Install. /
Removal
Item
Weight (
+
/
-
)
m = [kg / lbs]***
Mome nt 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.
new
addoldold
newS
m
Mxm
x
+×
=
,
[mm / in.]
Þ
newS
x
,
=
×
+
=
mm / in.
** *
2. Definition of load
Empty Weight: kg / lbs***
empty weight CG aft of datum:
mm / in. ***
Minimum Load Required on seat (otherwise ballast)****: kg / lbs***
Maximum Load (Max AUW - 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 Figure 2 03, page 207
Site, Date Stamp Sign Job Leader
Inspector Statement: All measu red data are within the allowable ranges and correspond to the production and
maintenance instru ctions of the type.
Site, Date Stamp Sign Inspec tor

STEMME S6 Specifications

General

Brand	STEMME
Model	S6
Category	Aircrafts
Language	English