AEROMOT AMT 200S SUPER XIMANGO S User manual

200-25
MAINTENANCE
MANUAL
AMT 200S

MAINTENANCEMANUAL
AMT 200S SECTION:1
MM - 200-25
SECTION 1 - DESCRIPTIONS, SYSTEMS, RIGGINGS AND PLACARDS
1. Motorglider Characteristics
1.1 Basic Dimensions
Wing span 57.32 ft (17.47 m)
Wing span with winglets (optional) 57.97 ft (17.67 m)
Wing span (wings folded) 33.30 ft (10.15 m)
Length 26.50 ft (8.08 m)
Maximum height 6.33 ft (1.93 m)
1.2 Wings
Wing surface (area) 201.29 Sqft (18.70 m2)
Dihedral 2° 30'
Profile Naca 643618
Angle of incidence 2°
Wing torsion -2°
1.3 Ailerons
Percent to wing chord (depth) 30%
Aileron span 10.24 ft (3.12 m)
Aileron surface (area) 7.32 Sqft (0.68 m2)
1.4 Airbrakes
Position at 45% of wing chord
Airbrake span 4.76 ft (1.45 m)
Type Schempp hirth on upper wing
surface
1.5 Horizontal Stabilizer
Horiz. stabilizer span 12.07 ft (3.68 m)
Horiz. stabilizer surface (area) 31.21 Sqft (2.90 m2)
Elevator surface 10.23 Sqft (0.95 m2)
Horiz. stabilizer - angle of incidence -1°
Page 1.1
August 10, 2004 - Rev. 8

MAINTENANCEMANUAL
AMT 200S SECTION:1
MM - 200-25
1.6 Vertical Empennage
Vertical empennage surface (area) 22.93 Sqft (2.13m2)
Rudder surface (area) 7.42 Sqft (0.69m2)
1.7 Landing Gear
Conventional: Two main gears with a tail wheel coupled at the rudder. For ground operation
the tail wheel disengages automaticaly when the minimum curve radius is reached.
Main landing gear shock absorber: Pressure 130 psi ( 9,14 kg/cm2) >0°C
Pressure 145 psi (10,19 kg/cm2) <0°C
Main wheel tire: 330 x 130 (5.00-4) pressure 45 psi (3.2 kg/cm2)
Tail wheel tire: 210 x 65 CR17 pressure 36.2 psi (2.5 kg/cm2)
Main landing gear track: 9.18 ft (2.80 m)
Distance between front and rear landing gear axes: 16.51 ft (5.35 m)
1.8 Power Plant
ROTAX 912 S4 or 912 S2 Engine:
-Maximum take-off power: 73.5 kw (99 HP) at 5800 RPM for 5 min
-Maximum continuous power: 69 kw (93 HP) at 5500 RPM
-Fuel - AVGAS 100 LL Octanes
-Carburetor - BING type 64/32
-Magneto - ROTAX DOUBLE - ELECTRONIC
-Alternator -DUCATI, 13.5 - 14.2 V/ 250 W
-Starter - ROTAX 12V/0.8 HP
-Oil lubricant - See recommended lubricants on page 5.21 of this manual
-Oil capacity - 0.79 U.S gallons (3,0 litres)
-Coolant capacity - 0.75 U.S gallons (2,8 litres);
Note:
Do not use general aviation engine oil (detergent or not)
Page 1.2
July 17, 2007 - Rev. 11

MAINTENANCEMANUAL
AMT 200S SECTION:1
MM - 200-25
1.9 Propeller
Hoffmann - model HO-V62R-1/170FA
2 blades, wood core covered with fiber glass
Three pitch positions: Minimum pitch, cruise pitch and feathered pitch
Change from minimum pitch to cruise pitch - 3800 RPM
Change from cruise pitch to minimum pitch - 2200 RPM
1.10 Cockpit
-Two places - side by side
-One piece canopy - longitudinal opening (slides backward)
-The canopy can be jettisoned at low airspeeds but the pilot must unlock it and pushit away
from the aircraft.
1.11 Seat Belts
Each seat is equipped with adjustable seat belts, which are attached to the fuselage by five
points.
Page 1.3
August 10, 2004 - Rev. 8

MAINTENANCEMANUAL
AMT 200S SECTION:1
MM - 200-25
1.12 Air Pressure Ports
1. Dynamic air pressure port
2. Static air pressure port
3. Total energy
Page 1.4
August 10, 2004 - Rev. 8

MAINTENANCEMANUAL
AMT 200S SECTION:1
MM - 200-25
Page 1.5
August 10, 2004 - Rev. 8
1.13 Vent holes and drains

MAINTENANCEMANUAL
AMT 200S SECTION:1
MM - 200-25
2. Electrical Diagram
Page 1.6
August 10, 2004 - Rev. 8
BATTERY DIAGRAM
(Motorgliders s/n 200.119, 200.122, 200.123, 200.124, 200.126 and 200.127)
BATTERY DIAGRAM
(Motorgliders s/n 200.128 to 200.132)
MAIN
SOARING
PP5A10
PP4A10
PP1B10
BLACK
RED
BUS BAR
GROUND
MAIN/SOARING
PP8A20N
PP1C10
PP7A20
SOARING K2
PP6A20
MASTER
ENGINE GROUND
PP3A4N
AIRCRAFT END
PP3B10N
PP2A4N
PP1D10
K1
SHUNT
PP1A4
ENGINE RELAY
20A
SOARING BUS
BAR
PP18A22
PP17A22
2A
2A
30A
CHT
11
MAIN BUS
BAR
AM METER/CHT
55
88
44
BATTERY
PP5A10
MAIN/SOARING
PP8A20N
AIRCRAFT
GROUND
BUS BAR
ENGINE
PP2A4N
PP3A4N PP1D10
PP7A20
MASTER
PP6A20
SOARING
PP1C10
SHUNT
PP1B10
K2
SOARING
MAIN
PP1A4
2A
ENGINE RELAY
BLACK
RED PP18A22
PP17A22
CHT
SOARING
20A
PP4A10
MAIN
30A
AMMETER/CHT
44
88
55
11
-
HOUR METER
2A
FUSE
LINE
MAIN BUS
BAR
E9A22
E10A22
-
HOUR METER
2A
SPARE
BUS BAR
SOARING
SWITCH
PRESSURE
E8A22
E7A22 E6A22
BATTERY
SHUNT
K1
2A

MAINTENANCEMANUAL
AMT 200S SECTION:1
MM - 200-25
Page 1.7
July 17, 2007 - Rev. 11
BATTERY DIAGRAM
(Motorglider s/n 200.133 and on)
BATTERY DIAGRAM
Optional Configuration
FIRE ALL
GROUND
BUS BAR
PP2A4N
PP15A16N
BATTERY CHARGER PLUG
PP3A4N
STARTER RELAY PP1A4
PP1A4 TO STARTER RELAY
PP1D10
PP6A20PP8A20N
PP14A16
ON
OFF
MASTER
S ITCH
PP1C10
PP1B10
K2
MAIN
2A
BLACK
RED PP18A22
PP17A22
CHT
PP4A10
MAIN
BUS
30A
AMMETER/CHT
4
8
5
1
+
-
HOUR METER
2A
FUSE
LINE
MAIN BUS
BAR
S ITCH
OIL PRESSURE
E8A22
E7A22 E6A22
BAT TERY
SHUNT
K1
2A
E9A22
E10A22
+
-
HOUR METER
2A
10A
FIRE ALL
GROUND
BUS BAR
PP2A4N
PP15A16N
BATTERY CHARGER PLUG
PP3A4N
STARTER RELAY PP1A4
PP1A4
T
O
S
T
A
R
T
E
R
R
E
L
A
Y
PP1D10
P
P
6
A
2
0
PP8A20N
PP14A16
ON
OFF
MASTER
S ITCH
P
P
1
C
1
0
P
P
1
B
1
0
K
2
M
A
I
N
2
A
BLAC
K
RED
P
P
4
A
1
0
M
A
I
N
B
U
S
3
0
A
+
-
H
O
U
R
M
E
T
E
R
2
A
F
U
S
E
L
I
N
E
M
A
I
N
B
U
S
B
A
R
S
I
T
C
H
O
I
L
P
R
E
S
S
U
R
E
E
8
A
2
2
E
7
A
2
2
E
6
A
2
2
BATTERY
SHUNT
K
1
2
A
E
9
A
2
2
E
1
0
A
2
2
+
-
H
O
U
R
M
E
T
E
R
2
A
10A

MAINTENANCEMANUAL
AMT 200S SECTION:1
MM - 200-25
Page 1.8
July 17, 2007 - Rev. 11
ALTERNATOR DIAGRAM
(Motorgliders s/n 200.119, 200.122, 200.123, 200.124, 200.126 and 200.127)
G
G
B
C
R
25V
22.000 uf ALTERNATOR
E7A22
KK3A20 30A
ALTERNATOR
HOUR METER
MAIN
BUS
BAR
PP11A20
K4
MAGNETO B
MAGNETO A
KK3 A20
JK4A18
JK3A18
PP1A4
BATTERY
KK1A4
K3
IGNITION B
IGNITION A
JK2A18
JK1A1 8
KK5A22
KK 2A20
STARTER
STARTER
5A
M
STARTER
MAI N BUS B AR
LA NDING GEAR
ALARM
KK6A20N
STARTER AND MAGNETO DIAGRAM
(Motorgliders s/n 200.119, 200.122 and on)

MAINTENANCEMANUAL
AMT 200S SECTION:1
MM - 200-25
Page 1.9
July 17, 2007 - Rev. 11
PP12A20N
G
G
B
CC
R
VOLTAGE REGULADOR
FUSE LINE
PP13A20
22.000 uf
25V
PP10A10
PP11A20
ALTERNATOR
K4
PP9A10 30A
ALTERNATOR
MAIN BUS
BAR
5A
22.000 uf
K4
ALTERNATOR
ALTERNATOR DIAGRAM
(Motorglider s/n 200.128 and on)
FLIGHT INSTRUMENT DIAGRAM
(Motorgliders s/n 200.119, 200.122 to 200.132)
F7A22
F14A22
F1A22
DIR EC.
GY RO
F8A22
ATT
INDICATOR
F1 3A22
F2A22
TURN BANK
2A
ATT
SOARING BUS
2A
GD
T&B
2A
MAIN B US BA R
F3A22N
PIL OT
F12A22N
COPILOT
TURN BANK
F11A22 F10A 22
2A
T&B
GY RO
DIR EC. F 4A22
F3A22
2A
GD
F6A22N
PIL OT
F15A22N
COPILOT
F8A22N
PILOT
F18A22N
COPILOT
INDICATOR
ATT
F1 7A22
F16A22
2A

MAINTENANCEMANUAL
AMT 200S SECTION:1
MM - 200-25
Page 1.10
July 17, 2007 - Rev. 11
F7A22
F14A22
F1A22
DIR EC
.
GY RO
(O PTIONAL)
F8A22
ATT
INDICATOR
(OPTIONAL )
F1 3A22
F2A22
TURN BANK
(OPTIONAL )
2A
ATT
2A
GD
T&B
2A
MAIN B US BA R
F3A22N
PIL OT
F12A22N
COPILOT
TURN BANK
(OPTIONAL )
F11A22 F10A 22
2A
T&B
DIR EC.
GY RO
(OPTIONAL )
F4A22
F3A22
2A
GD
F6A22N
PIL OT
F15A22N
COPILOT
F8A22N
PILOT
F18A22N
COPILOT
ATT
INDICATOR
(OPTIONAL )
F1 7A22
F16A22
2A
FLIGHT INSTRUMENT DIAGRAM
(Motorgliders s/n 200.133 and on)

MAINTENANCEMANUAL
AMT 200S SECTION:1
MM - 200-25
WARNING SYSTEM DIAGRAM
(LANDING GEAR, AIRBRAKE, STARTER ENGAGED, LOW BATTERY)
(Motorgliders s/n 200.119, 200.122 to 200.132)
4
5
6
GW3A22
6
4
5
3 3
2 2
1 1
GW3C22
GW2D22N
GW5B22
NO
C
NC
LEFT GEAR
MICRO SWITCH CONNECTOR
LEFT WING
MICRO SWITCH
RIGHT GEAR
NC
C
NO
GW5C22
GW2E22N
GW1C22
33
22
11
CONNECTOR
6
4
5
RIGHT WING
GW1A22
AIR BRAKE
MICRO SWITCH
NC
C
NO
GW6A22
GW2B22N
GW2A22N
GW2C22N
MICRO SWITCH
NC
NO
C
GW5A22
GW4A22
GEAR UP
GW5D22
GW12A22
GW1B22
GEAR LIGHT
2A
GW1B22
GW3B22
SOARING
BUS
GW4B22
RIGHT GEAR
LEFT GEAR
DOWN DOWN
35
4
1
GW10A22
GW11A22N
TEST
RETRACTED OR
IN TRANSIT
10
12
PW2A22
KK4A22
12
13
PW3A22N
KK5A22
STARTER
STARTER
ENGAGED
LOW
BATTERY
2
CANCEL
GW9A22
GW7B22
BUS
SOARING
2A
GEAR WARN
LOW BATT
2A
GW7C22
PW4A22N
GW7A22
PW1A22
3
9
11
Page 1.11
July 17, 2007 - Rev. 11

MAINTENANCEMANUAL
AMT 200S SECTION:1
MM - 200-25
Page 1.12
July 17, 2007 - Rev. 11
WARNING SYSTEM DIAGRAM
(LANDING GEAR, AIRBRAKE, STARTER ENGAGED, LOW BATTERY, COOLANT LEVEL)
(Motorgliders s/n 200.133 and on)
GEAR LIGHT
4
5
6
GW3A22
6
4
5
3
2
1
GW3C 22
GW2D22N
GW5B22
NO
C
NC
LEFT GEAR
MICRO SWITCH CONNECTOR
LEFT WING
MICRO SWITCH
RIGHT GEAR
NC
C
NO
GW5C22
GW2E22N
GW1C22
3
2
1
CONNECTOR
6
4
5
RIGHT WING
GW1A22
AIR B RAKE
MICRO SWITC H
NC
C
NO
GW6A22
GW2B22N
GW2A22N
GW2C22N
MICRO SWITC H
NC
NO
C
GW5A22
GW4A22
GEAR UP
GW5D22
GW12A22
GW1B22
GEAR LIGHT
2A
GW1B22
GW3B22
GW4B22
RIGHT GEAR
LEFT GEAR
DOWN DOWN
35
4
1
GW10A22
GW11A22N
TEST
RETRACTED OR
IN TRAN SIT
10
12
PW2A22
KK4A22
12
13
PW3A22N
KK5A22
STARTER
STARTER
ENGAGED
LOW
BATTERY
2
CANCEL
GW9A22
GW7B22
GW7C22
PW4A22N
GW17A22
GW7C22
GN16A22
GW 13A 22 GW 15A 22
GW1 A22N
SENSOR
COOLANT LEVEL
LOW BATT
GEAR WARN
GW7A22
PW1A22
3
9
2A
2A
2A
11
15
7
14
M
A
I
N
B
U
S
W
A
R
N
I
N
G
S
Y
S
T
E
M
U
N
I
T
W
A
R
N
I
N
G
S
Y
S
T
E
M
U
N
I
T

MAINTENANCEMANUAL
AMT 200S SECTION:1
MM - 200-25
Page 1.13
July 17, 2007 - Rev. 11
OIL TEMPERATURE / PRESSURE DIAGRAM - Standard configuration
4
5
3
1
OIL TEMP. SENDER
OIL PRES SURE
SENDER
OIL TEMP./
PRESSURE
INDICATOR
GND
BATTERY
MAIN
BUS
E A22N
E2A22
E3A22
E1A22
E4A22N
2A
5A
RV1A1RV1A1
2A
F5A22
2A
F3A22
2A
F1A22
3A
SN1A20
2A
ALTITUDE ENCODER
TRANSPONDER
VHF/COMM
ATT INDICATOR (OPTIONAL)
INTERCOM (OPTIONAL)
TURN AND BANK (OPTIONAL)
VHF/COMM B
A
RVZA1 N
TRANSPONDER B
A
SN2A20N
ALTITUDE
ENCODER
B
A
BLACK
JN3A22
AVIONICS DIAGRAM - Standard configuration
OIL TEMPERATURE / PRESSURE AND RPM INDICATION
Optional Configuration

MAINTENANCEMANUAL
AMT 200S SECTION:1
MM - 200-25
Page 1.14
July 17, 2007 - Rev. 11
Q5A22
D 15B
D 15B
Q4C22
Q4E22
Q5B22
Q6B22
Q7E22N
Q7E22N
Q4A22
Q7B22N
Q7A22N
Q6A22
FUEL
LEVEL
INDICATOR
2A
FUEL INDICATOR
3
5
1
1
2
3
1
2
3
RED
YELLOW
BLACK
RED
YELLOW
BLACK
SENDER
RIGHT
SENDER
LEFT
1
2
3
1
2
3
5A
PM2B20
PM2B20N
PM1A20
PM2A20N
AUX. POWER
LEFT AUX. POWER
RIGHT AUX. POWER
5A
Q1A1Q2A1
Q3A1 N
FUEL PUMP
FUEL PUMP
AVIONICS DIAGRAM - Standard configuration
FUEL LEVEL DIAGRAM - Standard configuration
FUEL LEVEL DIAGRAM
Optional Configuration

MAINTENANCEMANUAL
AMT 200S SECTION:1
MM - 200-25
Page 1.15
July 17, 2007 - Rev. 11
4
4
55
4
4
4
1
2
6
3
4
2
6
2
5
4
5
4
4
3. Ground Connecting Straps
Ground Connecting Straps Table
STRAP
1
2
3
4
5
6
IPCREFERENCE
IPCFIGURE 05
IPCFIGURE 13
IPCFIGURE 15
IPCFIGURE 16
IPCFIGURE 18
IPCFIGURE 20
PAGE
2.16
2.44/2.45/2.46/2.47/2.48
2.58
2.62
2.68
2.74
ITEM
2-3-43-66
18-26-44-90
19-26
3-26-33-60
11-27
66

MAINTENANCEMANUAL
AMT 200S SECTION:1
MM - 200-25
4. Fuel System
Each wing has one aluminum fuel tank located between the leading edge and the main gear
wheel well. The tanks are independent and the fuel level is indicated by a fuel quantity transmitter.
There is a three-position selector valve to select the tank in use and cut off the fuel.
Find the fuel system components below.
1- Tank cap and vent (breather)
2- Drain valves
3- Left fuel tank 11.89 U.S gallons (45 liters)
4- Right fuel tank11.89 U.S gallons (45 liters)
5- Fuel tubes and connections
6- Electric fuel pump
7- Carburetor
8- Mechanic fuel pump
9- Fuel filter
10- Three position fuel selector valve
Page 1.16
August 10, 2004 - Rev. 8
TOTAL
11.89 US gallons (45 litres)
11.89 US gallons (45 litres)
23.78 US gallons (90 litres)
USABLE
11.62 US gallons (44 litres)
11.62 US gallons (44 litres)
23.24 US gallons (88 litres)
Left Wing Tank
Right Wing Tank
Total Capacity

MAINTENANCEMANUAL
AMT 200S SECTION:1
MM - 200-25
Fuel System
Page 1.17
August 10, 2004 - Rev. 8
CARBURETOR
VENT AND
DRAIN TUBE
FIREWALL
FUEL RETURNING LINE
TO FUEL TANKS
3
2
2
4
6
10
9
8
7
5
7
5
5
5
5
5
5
5
5

MAINTENANCEMANUAL
AMT 200S SECTION:1
MM - 200-25
5. Brake System
5.1 Find below the basic components of the brake system.
1- Fluid reservoir
2- Master cylinders
3- Tubes
4- Fittings
5- Flexible tubes
6- Brake cylinder
7- Bleeder valve
5.2 Only use approved brake fluids: Aeroshell Fluid 41 or Esso HD 400.
5.3 Measure brake lining thickness (minimum 0.100 inches).
5.4 Follow the procedure below to bleed the brake lines if required.
- Push the brake pedals three times and keep the pedals pressed;
- Open the bleeder to remove all air bubbles from the brake lines;
- Close the bleeder when all air is removed;
- Examine brake pressure again by pressing the pedals.
5.5 Follow the same procedure for the other pedals.
Page 1.18
August 10, 2004 - Rev. 8

MAINTENANCEMANUAL
AMT 200S SECTION:1
MM - 200-25
Brake System
Page 1.19
August 10, 2004 - Rev. 8