Remos REMOS GX nXES Owner's manual

REMOS GX nXES
Pilot Operating Handbook
Airplane Registration Number ______________________
Airplane Serial Number ______________________
REMOS Order No. 104178, dated December 2017

G3-8 MA FM 6200 –R03
Introduction
Introduction ii
Light Sport Aircraft REMOS GX
The REMOS GX was manufactured in accordance with the Light Sport
Aircraft airworthiness standards and does not conform to standard
category airworthiness requirements.
The standards to be used for certification are given by FAA and can
be obtained from the FAA’s website. For this airplane the following
standards have been used:
number
revision
purpose
ASTM F2245
16c
Design and Performance
ASTM F2245
16c
Required Equipment
ASTM F2245
16c
Aircraft Operating Instructions
ASTM F2972
15
Quality Assurance
ASTM F2295
06
Continued Airworthiness
ASTM F2483
12
Maintenance Manual
ASTM F2746
14
Pilot Operating Handbook
NOTE
This table is applicable only for newly delivered
aircraft. It is not applicable in case the POH has been
updated for existing aircraft.
NOTE
This POH may only be used for aircraft SN429 or
higher or with REMOS notification NOT-014
implemented.
Manufacturer: REMOS AG
Franzfelde 31
D-17309 Pasewalk
GERMANY
Phone: [phone]
Fax: [phone]
Internet: www.remos.com

G3-8 MA FM 6200 –R03
Introduction
Introduction iii
List of Content and Revisions
This POH consists of the following listed pages and sections. You will
find a marking indicating the revision and date of issue at the top
border of each page. Insert the latest changed pages.
Pilot Operating Handbook –Main Part
sect.
description
document-no.
revision
0
Introduction
G3-8 MA FM 6200
03
1
General Information
G3-8 MA FM 5201
01
2
Operating Limitations
G3-8 MA FM 1202
07
3
Emergency Procedures
G3-8 MA FM 1203
07
4
Normal Procedures
G3-8 MA FM 1204
07
5
Performance
G3-8 MA FM 5205
01
6
Weight and Balance
G3-8 MA FM 1206
06
7
Systems
G3-8 MA FM 5207
03
8
Handling and Servicing
G3-8 MA FM 1208
07
Pilot Operating Handbook –Supplement
sect.
description
document-no.
revision
9
Flight Training
G3-8 MA FM 1209
07
10
Glider Towing
G3-8 MA FM 1210
07
11
Banner Towing
G3-8 MA FM 1211
04
12
Continued Airworthiness
G3-8 MA FM 1212
03
13
Abbreviated Checklists
G3-8 MA FM 1213
01
NOTE
This POH may only be used for aircraft SN429 or
higher or with REMOS notification NOT-014
implemented.

G3-8 MA FM 6200 –R03
Introduction
Introduction iv
Remarks and Alterations
Please make a notation below if any changes have been made to this
manual or to the plane. This manual is an important document for the
pilot in command to ensure 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 updates of this
manual from your dealer or directly from the manufacturer’s
homepage.
no.
page
concern
date
sign

G3-8 MA FM 5201 - R01
1 General Information
General Information 1 - 1
Table of Contents
sect.
description
page
1.1
Introduction
1-2
1.2
Certification
1-2
1.3
Continued Airworthiness
1-2
1.4
Quick Reference
1-3
1.5
Technical Specifications
1-3
1.6
Views
1-4
1.7
Performance
1-5
1.8
Engine
1-5
1.9
Fuel
1-6
1.10
Oil
1-6
1.11
Propeller
1-7
1.12
ICAO Designator
1-7
1.13
Noise Certification
1-7

G3-8 MA FM 5201 - R01
1 General Information
General Information 1 - 2
1.1 Introduction
This Operating 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 keep
this Operating Handbook updated with the newest information
available. You can get the latest version of this Handbook from your
local dealer or directly from the manufacturer’s homepage.
NOTE
This POH may only be used for aircraft SN429 or higher
or with REMOS notification NOT-014 implemented.
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 Continued Airworthiness
Technical publications for continued airworthiness are released on
the REMOS website www.remos.com and they may be downloaded
free of charge.
Bombardier-Rotax releases technical publications on their website
www.flyrotax.com from which they may be downloaded free of
charge. Documentation update for avionics may be downloaded on
www.dynonavionics.com and www.garmin.com.
It is the responsibility of the owner/operator of the aircraft to keep the
aircraft and its documentation up to date and to comply with all
technical publications.

G3-8 MA FM 5201 - R01
1 General Information
General Information 1 - 3
1.4 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 nose wheel. Main gear with hydraulic
disc brakes. The cabin is equipped with two seats
side by side and can be entered and exited by doors
on the left and right side of the fuselage.
Layout: Main components are built in half shells from
composite fiber material, which are bonded together
(carbon fiber, Kevlar and glass fiber).
1.5 Technical Specifications
wingspan
9.32 m = 30 ft 6 in
length
6.48 m = 21 ft 3 in
height
2.28 m = 7 ft 5 in
wing area
10.98 m2= 118 sq ft
MTOW
600 kg = 1,320 lb
wing loading
55 kg/m2= 11 lb/sq ft

G3-8 MA FM 5201 - R01
1 General Information
General Information 1 - 4
1.6 Views
Wingspan 9.32 m = 30.6 ft
Height 2.28 m = 7,.5 ft
Overall Length 6.48 m = 21.3 ft

G3-8 MA FM 5201 - R01
1 General Information
General Information 1 - 5
1.7 Performance
This section shall give a summary of the performance of the
REMOS GX. Detailed performance data is given in section 5 of this
Pilot Operating Handbook.
top speed at 3,000 ft
115 kTAS @° 5.500 rpm (*)
cruise speed at 3,000 ft
102 kTAS @° 5.000 rpm (*)
range at 3,000 ft
347 nm @° 5,000 rpm (*)
endurance at 3,000 ft
3,4 h @° 5.000 rpm (*)
rate of climb at VX
780 ft/min @ VX= 50 kIAS (*)
rate of climb at VY
840 ft/min @ VY= 60 kIAS (*)
stall speed clean
44 kIAS
stall speed flaps 40 deg
42 kIAS
1.8 Engine
manufacturer
Bombardier-Rotax
engine type
912 UL-S2
max. power
take-off
73.6 kW / 100 HP
max. cont.
69.9 kW / 95 HP
max. engine speed
take-off
5,800 rpm
continuous
5,500 rpm
gear ratio
2.43 : 1
coolant
type
BASF Glysantin Protect Plus/G48
mixing ratio
see section 7

G3-8 MA FM 5201 - R01
1 General Information
General Information 1 - 6
1.9 Fuel
total fuel quantity
84 ltr = 22 US gallons
usable fuel quantity
80 ltr = 21 US gallons
fuel qualities
fuel released by latest revision of
ROTAX service instruction SI-912-
016, preferably free of ethanol.
NOTE
Please refer to REMOS notification NOT-001 and
ROTAX SI-912-016 for further information on suitable
engine fluids (fuel, oil, cooling liquid, additives, etc).
Have a frequent look on www.flyrotax.com and on
www.remos.com for the latest information.
1.10 Oil
engine oil
oil released by latest revision of
ROTAX service instruction SI-912-016
oil rating
RON 424
engine oil capacity
min. 2.0 ltr = 2.1 qts
max. 3.0 ltr = 3.1 qts
recommended oil
AeroShell Sport PLUS 4 10W-40
NOTE
Please refer to REMOS notification NOT-001 and
ROTAX SI-912-016 for further information on suitable
engine fluids (fuel, oil, cooling liquid, additives, etc).
Have a frequent look on www.flyrotax.com and on
www.remos.com for the latest information.