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
Nov 18/11
08-10-00
Page 206
Nov 18/11
Weight and Balance Report
540
Permitted Range of Empty Mass CG-Location - Retractable L/G, 900 kg MTOW
Tail Heavy Area
500 520
Location aft of
110 kg 105 kg 100 kg
460 480
Permitted Range of Empty Mass CG-
90 kg 80 kg 75 kg 70 kg
420 440
RP [m]
-
60 kg
Rearmost CG- Location for min. Cockpit Load of 55 kg
400 420
-
Location
360 380
Nose Heavy Area
-
340
650 660 670 680 690 700 710 720 730 740 750 760 770 780
Empty Mass [kg]
-
Location Foremost CG
95 kg
85 kg
65 kg
Permitted Range of CG
EFFECTIVITY
Model S6-RT
EFFECTIVITY
Model S6-RT
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 o ut if not applicable
****According to Figure 203, 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