Remos G-3 /600 Owner's manual

Edition 4 / Rev. 03 USA
including Flight Training Supplement

02
REMOS
3
600
02
REMOS G-3 /600 - Pilot Operating Handbook
Light Sport Aircraft REMOS G-3 /600 with ROTAX 912S Engine.
REMOS Aircraft GmbH
Franzfelde 31 D-17309 Pasewalk
Germany
Tel.:
Fax:
e-mail:
Internet:
(+49) 03973/225519-0
(+49) 03973/225519-99
[email protected]
www.remos.com
Important:
Serial No.:
Manufacturer:
Engine-Type:
Year of Construction: Serial No. Engine:
Call Sign:
Propeller-Type:
Serial No. Propeller:
Date Signature / Dealer Stamp
The REMOS G-3 /600 was manufactured in accordance with the Light Sport Aircraft
airworthiness standards and does not conform to standard category airworthiness
requirements.
REMOS
3
600

REMOS
3
600
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3
600
03
Remarks and Alterations
Applied Modifications
Please make a notation below, if any changes have been made to this manual or to the
plane. This manual is an important documentation for pilots in command to ensure a
safe operation of the aircraft. Therefore it is recommended to keep this Operating
Handbook updated with the newest information available. You can get the latest
upgrades of this manual from your dealer or directly from the manufacturer´s homepage.
Pos. Page Description Date Sign

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3
600
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600
04
Remarks and Alterations
Applied Modifications (continued)
Pos. Page Description Date Sign

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3
600
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3
600
05
Remarks and Alterations
Applied Modifications
Pos. Page Description Date Sign

02
REMOS
3
600
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3
600
06
Table of Contents
General information about this handbook
This Flight Operation Handbook is divided into several chapters. These chapters can be
identified quickly by the use of the colored markings on the top corners of each side. The
structure of this handbook complies to the Light Sport Aircraft airworthiness standards.
Contents
General Information
Introduction
Certification
Quick Reference
Technical Specifications
Airplane and Systems Descriptions
Engine overview
Engine
Propeller, Gearbox
Fuel and fuel capacity
Engine oil, coolant
Operating weights and loading
Cockpit and basic equipment
Center panel controls and circuit breakers
Engine control gauges (Rotax Flydat)
Additional gauges (basic equipment)
1
1.1
1.2
1.3
1.4
2
2.1
2.2
2.3
2.4
2.5
2.6
2.7
2.8
2.9
2.10
Page
12
12
12
13
Page
14
15
15
15
16
16
17
18
19
20

REMOS
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600
Table of Contents
3
3.1
3.2
3.3
3.4
3.5
3.6
3.7
Operating Limitations
Airspeed limits
Crosswind and wind limitations
Service ceiling
Load factors
Prohibited maneuvers
Center of gravity range
Permissible flight maneuvers
Page
21
22
22
22
22
23
23
REMOS
3
600
07
4
4.1
4.2
4.3
4.4
4.5
4.6
4.7
Weight and Balance Information
Installed equipment list
Weight and balance form
Center of gravity (CG) range and determination
CG-calculation
CG-calculation example
CG-diagram
Aircraft specific weights
Page
24
24
25
26
27
28
29
5
5.1
5.2
5.3
5.4
5.5
Performance
Takeoff and landing distances
Rate of climb
Takeoff distance effected by external circumstances
Takeoff distance effected by pressure altitude
Cruise speeds, RPM, fuel consumption and range
Page
30
30
31
31
32

32
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600
R
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600
08
Table of Contents
6
6.1
6.2
6.3
6.4
6.5
6.6
6.7
6.8
6.9
6.10
6.11
6.12
6.13
Emergency Procedures
Door emergency eject
Recovering from stall
Rescue system
Operating the rescue system (optional equipment)
Illustrated rescue system installation
Engine failure / Loss of power before takeoff
Engine failure after takeoff
Engine failure in flight
Emergency landing procedure
Minimum gliding ratios
In-flight engine fire procedures
Emergency landing on water
Recover from unintended spin
Page
33
33
34
34
35
36
36
37
37
37
38
38
38
Normal Procedures
Preflight check
Engine starting
Taxiing
Normal takeoff
Best angle of climb speed (VX)
Best rate of climb speed (VY)
Cruise
Approach
Normal Landing
Short field takeoff
7
7.1
7.2
7.3
7.4
7.5
7.6
7.7
7.8
7.9
7.10
Page
39
40
42
42
43
43
43
44
44
44

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43 09
REMOS
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600
Table of Contents
8
8.1
8.2
8.3
8.4
8.5
8.6
8.7
8.8
8.9
8.10
8.11
8.12
8.13
8.14
8.15
8.16
8.17
8.18
8.19
8.20
8.21
Aircraft Ground Handling and Servicing
Servicing fuel, oil and coolant
Towing and tie-down instructions
100/200 hr service / 12 month inspection
300 hr service
Cleaning and care
Folding wing system
Preparation for assembling and disassembling
Connecting folded wings to fuselage
Installing horizontal stabilizer
Final check after assembling
Disassembling the aircraft
Airframe servicing
Main gear servicing
Nose gear servicing
Hydraulic brakes
Disassembling and assembling wheels
Wheels and tires
Changing engine oil
Exhaust system servicing
Propeller servicing
Airbox system and air cleaner element
Page
47
47
48
49
49
50
50
51
52
52
52
53
53
54
54
55
56
56
57
58
58
7
7.11
7.12
Normal Procedures
Aborted landing procedures
Low airspeed and stall
Page
44
45

09
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10
Table of Contents
9
9.1
9.2
9.3
9.4
9.5
Required Placards and Markings
Airspeed indicator range markings
Operating limitations on instrument panel
Passenger warning
No intentional spins
Miscellaneous placards and markings
Page
59
60
60
60
61
10
10.1
10.2
Page
64
77
Supplementary Information
Flight training supplement
Towing glider

11
Views
Wingspan 32.3 ft (9800mm)
Overall Length 21.4 ft (6470mm)
Height 5.5 ft (2280mm)
The REMOS G-3 /600 is designed as full composite carbon fiber & fiberglass aircraft. You
will find detailed information on the following pages.

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3
600
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600
12
1 General Information
1.1 Introduction
This Operation Handbook is designed to help enable a safe and successful completion
of each flight with the REMOS G-3 /600. It provides you with all necessary information
for regular maintenance and operation of the aircraft. Therefore we recommend that the
pilot keeps this Operating Handbook upgraded with the newest information available.
You can get the newest version of this Handbook from your local dealer or directly from
the manufacturer´s homepage.
1.2 Certification
The REMOS G-3 /600 complies to the rules of the Light Sport Aircraft airworthiness
standards and does not conform to standard category airworthiness requirements.
1.3 Quick Reference
Type: Full composite carbon fiber / fiberglass aircraft with two seats.
Design: High wing design with struts, front mounted engine and propeller, traditional
stabilizer concept, differential ailerons aerodynamically compensated.
Electrically operated flaps (0° to 40°), electric elevator trim, three-wheel
landing gear with steerable nosewheel. Fiberglass main gear with hydraulic
disc brakes.

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13
General Information1
Technical Specifications1.4
Wingspan
Length
Height
Wing area
Wing load *
Wing width
* at 1320 lb maximum takeoff weight
32.3
21.4
5.5
131.0
10.08
4.06
ft
ft
ft
ft2
lb/ft2
ft
Design:
Engine:
Propeller:
The cabin is equipped with two seats side by side and will be entered and
exited by doors on the left and right side of the fuselage.
Main components are built in halfshells from composite fiber material, which
are bonded together (carbon fiber, Kevlar and glass fiber).
Rotax 912 ULS
2-blade fixed pitch (wood), 2-blade ground adjustable (carbon)

14
Engine overview2.1
To ensure maximum durability and performance of your Rotax engine, it is essential to
use the lubricants and maintain the values described in this chapter.
Components
REMOS prop-spacer
Gearbox including
clutch
Oil cooler
Water cooler
REMOS stainless steel
exhaust system
Carburetor heating
REMOS-Airbox
Carburetor
Battery
Voltage regulator
Ceramic-firewall
REMOS engine mount
Coolant expansion tank
1.
2.
3.
4.
5.
6.
7.
8.
9.
10.
11.
12.
13.
1
2
3
4
5
6
7
8
8
911
12
13
10
Airplane Systems and Descriptions2

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600
15
Engine2.2
Engine manufacturer:
Engine type:
Max. power:
Max. rpm:
Max. cylinder head temperature:
Max. fuel pressure:
Max. oil temperature:
Min. oil temperature:
.
* Manufacturer specification till overhaul / TBO = 1500 hrs.
Values are subject to change without notice, please refer to
the latest issues of the appropriate manufacturer manuals.
ROTAX
912 ULS*
73.6 kW / 100 hp
69.9 kW / 95 hp
5800 rpm.
5500 rpm.
275°F (135°C)
5.7 psi (0.4 Bar)
266°F (130°C)
120°F (50°C)
Permissible fuel qualities:
Useable fuel capacity:
Total fuel capacity:
Premium Unleaded Auto Fuel,
100 LL Aviation Fuel
21 gallons
22 gallons
Propeller manufacturer:
Propeller type / no. of blades:
Gearbox manufacturer:
Gearbox ratio : Propeller:
Clutch:
F. IIi Tonini / Sensenich
GT-169,5-164, 2-blade wood / 2A0-R5R70-EN
ROTAX
2.43 : 1
yes
at take-off:
permanent:
at take-off:
permanent:
Airplane and Systems Descriptions2
Propeller, Gearbox2.3
Fuel and fuel capacity2.4

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600
16
Engine oil,coolant2.5
* No aircraft engine oils, refer to Rotax operation instructions.
** Empty weight with basic equipment like described within
the Pilot Operating Hanbook, without rescue System.
Values are subject to change without notice, please refer to
the latest issues of the appropriate manufacturer manuals.
Engine oil:
Engine oil capacity:
Recommended oil:
Recommended cooling fluid:
Coolant capacity:
(mixture antifreeze/water 1:1)
Automobile engine oils*
0.75 gallons (2.8 litre)
Shell Advance 10W 40
semi-synthetic
BASF Glysantin, green
0.65 gallons (2.5 liters)
Airplane and Systems Descriptions2
Operating weights and loading2.6
Maximum permissible take-off weight (W):
Minimum useful load (WU):
Maximum empty weight (WE):
Minimum empty weight:**
Minimum flying weight:
Occupants (at minimum empty weight):
Baggage:
Fuel (max):
1320 lb
430 lb
890 lb
626 lb
740 lb
513 lb
66 lb
126 lb
(600 kg)
(195 kg)
(405 kg)
(280 kg)
(336 kg)
(233 kg)
(30 kg)
(57 kg)

17
Airplane and Systems Descriptions
2.7 Cockpit and basic equipment Remark:
Instruments and switches This illustration shows the
basic equipment only.
123
456
7
10
8
11
9
13
14
16
17
21 23
24 26
22
25
27
18
15
19 20
12
Airspeed indicator
Reserved for att. gyro
Altimeter
Slip indicator
Reserved for dir. gyro
Vertical speed indicator
Compass
Flydat (refer to page 19)
Opt. oil cooler flap control
1.
2.
3.
4.
5.
6.
7.
8.
9.
Optional throttle
Reserved for GPS
Reserved for XPDR
Reserved for radio
Reserved for Intercom
Reserved for Manifoldtemp.
Fuel quantity gauge
Reserved for add. gauges
Reserved for RS-232 con.
10.
11.
12.
13.
14.
15.
16.
17.
18.
Throttle lever
Charge indicator light
Master switch
Ignition key / magneto check
Avionics master switch
Circuit breakers
22.
23.
24.
25.
26.
27.
Trim/Flap control switch
Device switches
Trim and Flap indicators
19.
20.
21.
2

02
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600
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600
18
2.8 Center panel controls and circuit breakers
The most important switches for operation of the aircraft are placed on the center panel.
The illustration below shows the basic equipped aircraft.
Illustration below:
Circuit breakers
and related devices
(if fitted).
Trim control switch
Flap control switch. Flaps are extended continuously
while pushing down the switch. Flaps are automatically
retracted when switched to the upper position. Flap
position is indicated on the gauge beneath.
All switches in upper position = on
ACL switch (anti collision light)
Electric fuel pump
Position lights
Instrument/avionics illumination (if installed)
Landing light (optional)
Not used
Circuit breakers for master & avionics circuits
Master switch (all electric systems on or off)
Caution! Do not switch off with engine running, because
serious damage to avionics components could occur!
Avionics master switch (all devices connected to the
avionics bus, fuse 7-12, on or off)
1.
2.
3.
4.
5.
6.
7.
8.
9.
10.
11.
Airplane Systems and Description2
12345678 9
10 11
Main Fuses:
(Master Switch)
Avionics-Fuses:
(Avionics Switch)
Master Fuse
Clock, Temp. Gauge Memory
Fuel Pump, Position Lights, ACL
Landing- Instr. Lights, Volt-, Fuel Gauge, Eng. Gauges
Trim, Flap Drive
Starter Relay, Adjustable Prop, Constant Speed
GPS, 12V Receptacle
Flight Computer, Directional Gyro
EFIS/PFD, Attitude Gyro
EFIS/MFD, Turn Indicator
Transponder, Blind encoder
Radio, Intercom
1
2
3
4
5
6
7
8
9
10
11
12
25 A
3 (6) A
10 A
10 A
10 A
10 A
10 A
10 A
10 A
10 A
10 A
10 A
Charge Fuse:
(engine comp.)
30 A

19
The Rotax Flydat
provides the following
engine gauges:
Illustration below:
An special placard on the
panel shows the limits for
rpm, oil- and water
temperature, oil pressure
and exhaust temperature.
For further information
please refer to the Rotax
user manual.
Engine speed gauge
Operation hour gauge
Exhaust temperature gauge
Water temperature gauge
Oil temperature gauge
Oil pressure gauge
RPM 5800/6000
Warngrenze/
Alarmgrenze
EGT 880/900
EGT 880/900
CHT 150/160 OIL-T 140/150
OIL-P max. 5,0/7,0
min. 2,0/0,8
Indicates whether left
or right side exhaust
temp. is displayed
Cylinder head /
water temperature
° F/°C
Exhaust temperature
rearward cylinders
° F/°C
Operation hours.
multiply displayed
value by 0.1
Engine speed
rpm
Exhaust temperature
forward cylinders
° F/°C
Oil pressure
Displayed value must be
multiplied by 0.1
Oil temperature
° F/°C
Airplane Systems and Description2
Engine control gauges (Rotax Flydat)2.9
RPM 5800/6000
Warning-Limit/
Alert-Limit
EGT 1600/1650˚F
EGT 1600/1650˚F
CHT 300/320˚F OIL-T 280/300˚F
OIL-P max. 72/100
min. 29/12

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02
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20
2.10 Additional gauges
Manifold/outside temperature gauge (optional)
This digital temperature gauge enables a precise measurement of manifold and outside
temperature. An alert function indicates when carburetor heating is recommended. Alert
temperature threshold is adjustable.
Electrical fuel quantity gauge (basic equipment)
For a comfortable fuel quantity reading an electrical fuel gauge
is provided with the basic equipment of your REMOS G-3 /600,
additional to the fuel level sight gauge. If the needle indicates
"zero", there are 0.5 gallons left in the fuel tank. For flight safety
it is strongly recommended to double check the reading on the
level sight gauge.
For detailed information please refer to the sepearate
operators manual.
Choose between carburetor/
manifold temperature and
outside temperature (see left).
Adjust alert temperature.
Reset button
Choose temperature to be
displayed (manifold/outside).
Alert tell tale, to indicate that
true temperature is below
alert temperature setting.
Recommended: 55˚F.
Instruction placard
1.
2.
3.
4.
5.
6.
Airplane Systems and Description2
123
45
6
IN
Out
Manifold/Outside-Temp.
Manifold temperature
Outside temperature
=
=