Remos G 2008 Series Owner's manual

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ii
Rev. 01 – 07-01-2008
Aircraft Data
Light Sport Aircraft REMOS GX with Rotax 912 UL-S Engine
The REMOS GX was manufactured in accordance with the Light Sport Aircraft airworthiness standards
and does not conform to standard category airworthiness requirements.
Serial No.: Engine-Type:
Year of constr.: Serial No. Engine:
Call Sign: Propeller-Type:
Serial No. Propeller:
Manufacturer: REMOS Aircraft GmbH Flugzeugbau
Franzfelde 31
D-17309 Pasewalk
Phone: [phone]
Fax: [phone]
e-mail: [email protected]
Internet: www.remos.com Date: Signature/Dealer Stamp:

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Rev. 01 – 07-01-2008
List of Effective Pages
This POH consists of the following listed pages and sections. You will find a marking, indicating the
revison and date of issue at the top border of each page. Insert latest changed pages, destroy
superseded pages. Note: Changed pages are indicated by the marking “changed” on top of the page.
Total number of pages in this publication is: 116, consisting of the following:
Section/Page: Section No.: Change No.: Issued: Section/Page: Section No.: Change No.: Issued:
Title i Revision 01 07-01-2008
Aircraft Data ii Revision 01 07-01-2008
List of Effective Pages iii Revision 01 07-01-2008
Remarks and Alterations IV - V Revision 01 07-01-2008
Table of Contents Vi Revision 01 07-01-2008
Views Vii Revision 01 07-01-2008
General Information 1-1 thru 1-3 Revision 01 07-01-2008
Airplane and Systems Descriptions 2-1 thru 2-21 Revision 01 07-01-2008
Operating Limitations 3-1 thru 3-4 Revision 01 07-01-2008
Weight and Balance Information 4-1 thru 4-7 Revision 01 07-01-2008
Performance 5-1 thru 5-6 Revision 01 07-01-2008
Emergency Procedures 6-1 thru 6-7 Revision 01 07-01-2008
Normal Procedures 7-1 thru 7-9 Revision 01 07-01-2008
Aircraft Ground Handling and Servicing 8-1 thru 8-20 Revision 01 07-01-2008
Required Placards and Markings 9-1 thru 9-8 Revision 01 07-01-2008
Supplementary Information 10-1 Revision 01 07-01-2008
Flight Training Supplement 10.1-1 thru 10.1-9 Revision 01 07-01-2008
Towing Glider Supplement 10.2-1 thru 10.2-13 Revision 01 07-01-2008
Rear Page X Revision 01 07-01-2008

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Rev. 01 – 07-01-2008
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 Concern Date Signature

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Rev. 01 – 07-01-2008
Remarks and Alterations
Applied Modifications (continued)
Pos. Page Concern Date Signature

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Rev. 01 – 07-01-2008
Table of Contents
General Information about this Handbook
This Flight Operation Handbook is divided into several chapters. The structure of this handbook complies
to the Light Sport Aircraft airworthiness standards.
Section Description Page
1 General Information 1-1 thru 1-3
2 Airplane and Systems Descriptions 2-1 thru 2-21
3 Operating Limitations 3-1 thru 3-4
4 Weight and Balance Information 4-1 thru 4-7
5 Performance 5-1 thru 5-6
6 Emergency Procedures 6-1 thru 6-7
7 Normal Procedures 7-1 thru 7-9
8 Aircraft Ground Handling and Servicing 8-1 thru 8-20
9 Required Placards and Markings 9-1 thru 9-8
10 Supplementary Information 10-1
10.1 Flight Training Supplement 10.1-1 thru 10.1-9
10.2 Towing Glider Supplement 10.2-1 thru 10.2-13

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Rev. 01 – 07-01-2008
Views
The REMOS GX is designed as full composite carbon fiber aircraft.

General Information 1 - 1
Rev. 01 – 07-01-2008
1 General Information
Table of Contents
Paragr. Description Page
1.1 Introduction 1-2
1.2 Certification 1-2
1.3 Quick Reference 1-2
1.4 Technical Specifications 1-3

General Information 1 - 2
Rev. 01 – 07-01-2008
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 GX. 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 GX was manufactured in accordance with the Light Sport Aircraft airworthiness standards
and does not conform to standard category airworthiness requirements.
1.3 Quick Reference
Type: Full composite carbon fiber aircraft with two seats.
Design: High wing design with struts, front mounted engine and propeller, traditional stabilizer
concept, differential ailerons. Electrically operated flaps (0° to 40°), electric elevator trim,
three-wheel landing gear with steerable nosewheel. Main gear with hydraulic disc brakes.
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.

General Information 1 - 3
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1 General Information
Layout: Main components are built in halfshells from composite fiber material, which are bonded
together (carbon fiber, Kevlar and glass fiber).
Engine: Rotax 912 UL-S
Propeller: 2-blade ground adjustable (composite)
1.4 Technical Specifications
Specifications posted below are related with an MTOM of 1320 lb.
Wingspan 30.6 ft
Overall Length 21.3 ft
Height 7.5 ft
Wing area 118.0 ft²
Wing load 11.18 lb/ft²
Wing width 4.06 ft

Airplane and Systems Description 2 - 1
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2 Airplane and Systems Description
Table of Contents
Paragr. Description Page Paragr. Description Page
2.1 Engine 2-2 2.14 Center Console 2-13
2.2 Propeller, Gearbox 2-2 2.15 Avionics Equipment 2-14
2.3 Fuel and Fuel Capacity 2-2 2.16 Secondary Instrumentation… 2-17
2.4 Engine Oil, Coolant 2-3 2.17 Glass Cockpit – Left Hand Panel 2-18
2.5 Operating Weights and Loading 2-3 2.18 Dynon EFIS D-100 / HS-34 2-20
2.6 Cockpit Overview 2-4 2.19 Dynon EMS D-120 2-21
2.7 Basic Instrumentation 2-6
2.8 Rotax Flydat 2-7
2.9 Analog Engine Gauges 2-8
2.10 Control Panel 2-9
2.11 Electric Fuses 2-10
2.12 Cockpit Lighting 2-11
2.13 Dual Throttle, Oil Temp Control… 2-12

Airplane and Systems Description 2 - 2
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2 Airplane and Systems Description
2.1 Engine
Manufacturer: Bombardier-Rotax
Engine type: 912 UL-S *
Max. power: at take-off: 73,6 kW / 100 hp
permanent: 69,9 kW / 95 hp
Max. rpm: at take-off: 5,800 rpm.
permanent: 5,500 rpm.
Max. cylinder head temperature: 275°F (135°C)
Max. fuel pressure: 5.7 psi (0.4 Bar)
Max. oil temperature: 266°F (130° C)
Min. oil temperature: 120°F (50°C)
2.2 Propeller, Gearbox
Propeller Manufacturer: Sensenich
Propeller type / number of blades: 2A0-R5R70-EN, 2-blade, carbon **
Gearbox Manufacturer: Rotax
Gearbox ratio, Engine : Propeller: 2,43 : 1
Clutch: yes
2.3 Fuel and Fuel Capacity
Permissible fuel qualities: Premium Unleaded Auto Fuel,
100 LL Aviation Fuel
Useable fuel capacity: 21 gallons
Total fuel capacity: 22 gallons
* Manufacturer specification until overhaul / TBO = 1500 hrs.
** Refer to manufacturer specification for servicing information.
Values are subject to change without notice, please refer to the
latest issues of the appropriate manufacturer manuals.

Airplane and Systems Description 2 - 3
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2 Airplane and Systems Description
2.4 Engine Oil, Coolant
Engine oil: Automotive engine oils * 1
Engine oil capacity: 0.75 gallons (2.8 liters)
Recommended oil: Motorcycle oil of a registered brand with gear
additives 1
Recommended cooling fluid: Conventional coolant, ethylene glycol based 1
Coolant capacity: 0.65 gallons (2.5 liters)
Ratio: 1:1 (Concentrate : Water)
2.5 Operating Weights and Loading
Maximum take-off weight (MTOW): 1320 lb (600 kg)
Maximum useful load: 650 lb (295 kg)
Minimum empty weight: ** 670 lb (305 kg)
Minimum flying weight: 815 lb (370 kg)
Baggage: 66 lb (30 kg)
Fuel (max): 126 lb (57 kg)
* No Aircraft engine oils, refer to Rotax operation instructions
1Refer to Rotax SI-18-1997 / SI-912-016
**
Empty weight with basic equipment as described within the POH,
without rescue system.
Values are subject to change without notice, please refer to the
latest issues of the appropriate manufacturer manuals.

Airplane and Systems Description 2 - 4
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2 Airplane and Systems Description
2.6 Cockpit Overview
Cockpit example
The following pages will give you more
information about how to operate your
REMOS GX.
Note: Some of the illustrated devices or
options may not be available, due to
the regulations of the ASTM standard.
Please ask your local dealer for more
information.

Airplane and Systems Description 2 - 5
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2 Airplane and Systems Description

Airplane and Systems Description 2 - 6
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2 Airplane and Systems Description
2.7 Basic Instrumentation (“Explorer”)
The basic equipment of your REMOS GX consists of the following:
ASI, VSI, Altimeter, Slip Indicator, Magnetic Compass, Rotax FLYdat(rpm, operation hours indicator,
exhaust gas-, oil pressure-, oil temp.-, CHT temp.-gauges).
If you have chosen the „Cross-Country“ version, you will also find an artificial horizon, directional gyro,
turn and bank indicator. Please refer to the appropriate manuals for detailed information.

Airplane and Systems Description 2 - 7
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2 Airplane and Systems Description
2.8 Rotax FLYdat
The Rotax FLYdat represents an instrument, specially developed for the Rotax engine for indicating and
acquisition of engine operating data. The operating data is being permanentely compared with the
specific engine operating limit. If the signalled operating data exceeds the stored operating limit, the
FLYdat will create a warning.
The FLYdat features the following actual readings:
Engine speed, CHT-temperature, oil pressure and temperature, exhaust gas temperature and hours of
operation.
For maintainence and analysis of engine issues, the FLYdat picks up and stores the essential operating
data. To read out and reset the warning messages, the FLYdat can be connected to a PC, using the
included RS-232 serial cable.
A decal in the cockpit will show the appropriate engine limits.

Airplane and Systems Description 2 - 8
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2 Airplane and Systems Description
2.9 Analog Engine Gauges (customized only)
With the anlog engine gauges installed, there is no exhaust gas temperature and no hours of operation
recording available. It is strongly recommended to maintain the values below, to achieve the maximum
engine performance and endurance. Take special care to warm up the engine before take-off to at least
120°F (50°C).
Engine Gauges Oil Pressure Oil Temperature CHT Temperature rpm.
Minimum: 11.4 psi (0.8 Bar) 120°F (50° C) 120°F (50° C) 1,400 rpm.
Normal Range: 28.4-71.0 psi (2-5 Bar) 194-230°F (90-110° C) 167-230°F (75-110° C) 1,400–5,500 rpm.
Maximum: 99.4 psi (7.0 Bar) 266°F (130° C) 275°F (135° C) 5,800 rpm.
Note: Please refer to the latest version of the engine manufacturer operating manual for detailed information.

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2 Airplane and Systems Description
2.10 Control Panel
Most of the major controls and switches to operate the aircraft are combined on the central control panel.
All switches are labeled definitely.
The following functions are contained:
• Electric trim control lever (blue)
• Flap control lever (white)
• Anti Collision Light (ACL)
• Electric fuel pump
• Navigation lights (wing & tail)
• Instrument lighting
• Landing light
• Autopilot engage (optional)
• Trim position indicator (LED, left)
• Flap position indicator (LED, right)
• Throttle control with friction lock
• Charge tell tale for electric generator
• Master- and Avionic switches
• Ignition lock / magneto check

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2 Airplane and Systems Description
2.11 Electric Fuses
The electrical system of the Remos GX consists of a Master-Bus system, which allows installation of
additional equipment very easily. The Master-Bus is separated into Master and Avionics circuits, each
populated by 6 automatic circuit breakers. An additional charge fuse is loctated in front of the firewall,
beneath the battery bracket.
All the circuit breakers are labeled,
additionally the decal to the right
is applied inside the cockpit, to give
more detailed information.
In kind of a defect, the circuit breakers
may also be replaced by standard
automotive fuses.