Remos GX eLITE Owner's manual

Pilot Operating Handbook
Airplane Registration Number ______________________
Airplane Serial Number ______________________
REMOS Order No. 104175, dated May 2015

G3-8 MA FM 3200 - R02
Introduction
Introduction i
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 vjg" HCCÓu" ygdukvg0" Hqt" vjku" cktrncpg" vjg" hqnnqykpi"
standards have been used:
number
revision
purpose
ASTM F2245
13b
Design and Performance
ASTM F2245
13b
Required Equipment
ASTM F2245
13b
Aircraft Operating Instructions
ASTM F2972
14g1
Quality Assurance
ASTM F2295
06
Continued Airworthiness
ASTM F2483
12
Maintenance Manual
ASTM F2746
12
Pilot Operating Handbook
This table is applicable only for newly delivered aircraft. It is not
applicable in case the POH has been updated for existing aircraft.
Manufacturer: REMOS AG
Franzfelde 31
D-17309 Pasewalk
GERMANY
Phone: [phone]
Fax: [phone]
Internet: www.remos.com

G3-8 MA FM 3200 - R02
Introduction
Introduction ii
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 ÎMain Part
sect.
description
document-no.
revision
up to SN 428
SN 429 or higher or with
NOT-014 implemented
0
Introduction
G3-8 MA FM 3200
01
02
1
General Information
G3-8 MA FM 1201
05
06
2
Operating Limitations
G3-8 MA FM 3202
01
02
3
Emergency Procedures
G3-8 MA FM 1203
05
06
4
Normal Procedures
G3-8 MA FM 1204
05
06
5
Performance
G3-8 MA FM 1205
05
06
6
Weight and Balance
G3-8 MA FM 1206
05
05
7
Systems
G3-8 MA FM 3207
02
02
8
Handling and Servicing
G3-8 MA FM 1208
05
06
Pilot Operating Handbook ÎSupplement
9
Flight Training
G3-8 MA FM 1209
04
06
10
Glider Towing
G3-8 MA FM 1210
05
06
11
Banner Towing
G3-8 MA FM 1211
01
03
12
Continued Airworthiness
G3-8 MA FM 1212
01
02

G3-8 MA FM 3200 - R02
Introduction
Introduction iii
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
ocpwhcevwtgtÓu"jqogrcig0
no.
page
concern
date
sign

G3-8 MA FM 3200 - R02
Introduction
Introduction iv
Views
Wingspan 30.6 ft
Height 7,.5 ft
Overall Length 21.3 ft

G3-8 MA FM 1201 - R06
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
Performance
1-4
1.7
Engine
1-4
1.8
Fuel
1-5
1.9
Oil
1-5
1.10
Propeller
1-6
1.11
ICAO Designator
1-6
1.12
Noise Certification
1-6

G3-8 MA FM 1201 - R06
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
nqecn"fgcngt"qt"fktgevn{"htqo"vjg"ocpwhcevwtgtÓu"jqogrcig0
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 1201 - R06
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
30 ft 6 in
length
21 ft 3 in
height
7 ft 5 in
wing area
118 sq ft
MTOW
1,320 lb
wing loading
11 lb/sq ft

G3-8 MA FM 1201 - R06
1 General Information
General Information 1 - 4
1.6 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 3,00 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= 51 kIAS (*)
rate of climb at VY
840 ft/min @ VY= 60 kIAS (*)
stall speed clean
44 kIAS
stall speed flaps 40 deg
42 kIAS
[*] Sensenich or Neuform propeller, range and endurance incl. 30min reserve
1.7 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
slipper clutch
optional
coolant
BASF Glysantin Protect Plus/G48
mixing ratio
1:1 (Glysantin : water)

G3-8 MA FM 1201 - R06
1 General Information
General Information 1 - 5
1.8 Fuel
usable fuel quantity
21 US gallons
total fuel quantity
22 US gallons
fuel qualities
AVGAS, MOGAS or min. AKI 91,
ideally free of ethanol
NOTE
Please refer to REMOS notification NOT-001 and
ROTAX SI-912-016/SI-914-019 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.
1.9 Oil
engine oil
synthetic or semi-synthetic
oil rating
API-SG or higher
engine oil capacity
min. 2.1 qts
max. 3.1 qts
recommended oil
AeroShell Sport PLUS 4 10W-40
NOTE
Please refer to REMOS notification NOT-001 and
ROTAX SI-912-016/SI-914-019 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.

G3-8 MA FM 1201 - R06
1 General Information
General Information 1 - 6
1.10 Propeller
manufacturer
type and number of blades
1. FIii. Tonini
2. Woodcomp
3. Sensenich
4. Neuform
1. GT-169,5/164
2-blade, wood
2. SR38+1
2-blade, wood
3. 2A0R5R70EN
2-blade, composite
4. CR3-65-47-101,6
3-blade, composite
1.11 ICAO Designator
ICAO Designator: GX (as per ICAO Doc. 8643)
1.12 Noise Certification
According to noise requirements for Ultralight aircraft (LS-UL) dated
August 1996, the REMOS GX is certified to a noise level of
60 dB (A).

G3-8 MA FM 3202 - R02
2 Operating Limitations
Operating Limitations 2 - 1
Table of Contents
sect.
description
page
2.1
Reference Airspeeds
2-2
2.2
Stalling Speeds at Maximum Takeoff Weight
2-3
2.3
Flap Extended Speed Range
2-3
2.4
Maximum Maneuvering Speed
2-3
2.5
Never Exceed Speed
2-4
2.6
Maximum Wind Velocity for Tie-Down
2-4
2.7
Crosswind and Wind Limitations
2-4
2.8
Maximum Parachute Deploy Airspeed
2-5
2.9
Service Ceiling
2-5
2.10
Load Factors
2-5
2.11
Maximum Structure Temperature
2-5
2.12
Prohibited Maneuvers
2-5
2.13
Approved Flight Maneuvers
2-6
2.14
Engine
2-6
2.15
Fuel
2-7
2.16
Oil
2-7
2.17
Weight and Balance
2-8
2.18
Crew
2-8
2.19
Flight Conditions and Minimum Equipment List
2-9
2.20
Airspeed Indicator Range and Markings
2-10
2.21
Placards and Markings
2-11

G3-8 MA FM 3202 - R02
2 Operating Limitations
Operating Limitations 2 - 2
2.1 Reference Airspeeds
speed
IAS
description
VNE
never exceed speed
134
kts
airspeed which shall never
be exceeded
VNO
maximum speed
in turbulence
107
kts
airspeed which shall not be
exceeded in gusty weather
VA
maneuvering speed
88
kts
maximum airspeed for all
permissible maneuvers
VFE
max. speed with
flaps fully extended
78
kts
airspeed which may never be
exceeded with flaps down
VAPP
approach airspeed
60
kts
recommended airspeed for
approach at gross weight
VX
airspeed for best
angle of climb
51
kts
airspeed for the steepest climb
with flaps up
VY
airspeed for best
rate of climb
60
kts
airspeed for the greatest altitude
gain in the shortest time, flaps up
VS1
stall speed with
flaps retracted (0°)
44
kts
stall speed at gross weight
with flaps up
VS0
stall speed with
flaps extended (40°)
42
kts
stall speed at gross weight
with flaps down

G3-8 MA FM 3202 - R02
2 Operating Limitations
Operating Limitations 2 - 3
2.2 Stalling Speeds at Maximum Takeoff Weight
stall speed with flaps extended VS0 = 42 kts
stall speed with flaps retracted VS1 = 44 kts
2.3 Flap Extended Speed Range
Flaps may be operated and the aircraft may be flown at airspeeds
higher than VFE as long as flap deflection is limited. Following
restrictions apply as a function of airspeed:
VFE
[ deg ]
[ kts ]
10
133
15
113
20
99
30
86
40
78
With flaps set to any deflection the safe load factor is limited to 2.
2.4 Maximum Maneuvering Speed
maximum maneuvering speed VA= 88 kts
At maneuvering speed one control, i.e. either aileron, or elevator or
rudder control, may deflected until its stop once. Above VA
permissible deflection is reduced, until at never exceed speed VNE
only one third of the deflection is permitted.

G3-8 MA FM 3202 - R02
2 Operating Limitations
Operating Limitations 2 - 4
2.5 Never Exceed Speed
never exceed speed VNE = 134 kts
Due do the reduced density of air at altitude, true airspeed is higher
than calibrated or indicated airspeed. Therefore VNE is limited to
134 kts true airspeed in order to prevent flutter. With increasing
altitude VNE is limited to lower values than indicated by redline
according to the following table.
altitude
IAS
[ ft ]
[ kts ]
0
135
5,000
128
10,000
119
15,000
110
At never exceed speed VNE only one third of the maximum control
deflection (aileron, elevator, rudder) is permitted.
2.6 Maximum Wind Velocity for Tie-Down
max. wind velocity for tie-down in the open VR= 38 kts
2.7 Crosswind and Wind Limitations
maximum demonstrated cross wind
component for take-off and landing 15 knots
The maximum demonstrated crosswind component is not a
limitation. The pilot may exceed this demonstrated crosswind
component on his or her own discretion. In case the pilot operates
the aircraft in crosswind components higher than demonstrated he or
she shall be aware of the fact that this flight regime has not been
tested. A general wind limitation is not defined for the REMOS GX.

G3-8 MA FM 3202 - R02
2 Operating Limitations
Operating Limitations 2 - 5
2.8 Maximum Parachute Deploy Airspeed
maximum parachute deploy airspeed 120 kts
2.9 Service Ceiling
service ceiling 15,000 ft
2.10 Load Factors
safe load factors +4.0 g / -2.0 g
With flaps set to any deflection the safe load factor is limited to 2.
2.11 Maximum Structure Temperature
max. certified structure temperature 130°F = 54°C
2.12 Prohibited Maneuvers
Flight maneuvers not permitted
‚aerobatics
‚spins
‚flight in icing conditions

G3-8 MA FM 3202 - R02
2 Operating Limitations
Operating Limitations 2 - 6
2.13 Approved Flight Maneuvers
The following maneuvers are permitted
‚all non-aerobatic maneuvers,
including stalls and departure stalls
‚flight with the doors off
2.14 Engine
manufacturer
Bombardier-Rotax
engine type
912 UL-S2 or 912-S2
max. power
take-off
73.5 kW / 100 HP
max. cont.
69.0 kW / 95 HP
max. engine speed
take-off
5,800 rpm
continuous
5,500 rpm
gear ratio
2.43 : 1
slipper clutch
optional
coolant
BASF Glysantin Protect Plus/G48
coolant or CHT temp
min
not defined
max
135°C = 275°F
120°C = 248°F with SB-011 complied
mixing ratio
1:1 (Glysantin : water)
NOTE
Please refer to REMOS notification NOT-001 and
ROTAX SI-912-016/SI-914-019 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.

G3-8 MA FM 3202 - R02
2 Operating Limitations
Operating Limitations 2 - 7
2.15 Fuel
usable fuel quantity
21 US gallons
total fuel quantity
22 US gallons
fuel qualities
AVGAS, MOGAS or min. AKI 91,
ideally free of ethanol
fuel pressure
min.
0,15 bar = 2.2 psi
max.
0,50 bar = 7.3 psi
NOTE
Please refer to REMOS notification NOT-001 and
ROTAX SI-912-016/SI-914-019 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.
2.16 Oil
engine oil
synthetic or semi-synthetic
oil rating
API-SG or higher
engine oil capacity
min. 2.1 qts
max. 3.1 qts
recommended oil
AeroShell Sport PLUS 4 10W-40
NOTE
Please refer to REMOS notification NOT-001 and
ROTAX SI-912-016/SI-914-019 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.

G3-8 MA FM 3202 - R02
2 Operating Limitations
Operating Limitations 2 - 8
2.17 Weight and Balance
front limit of C.G.
9.6 in
(245 mm)
rear limit of C.G.
16.3 in
(415 mm)
maximum take-off weight (MTOW)
1,320 lb
(600 kg)
typical empty weight
710 lb
(322 kg)
max. baggage in baggage compartment
66 lb
(30 kg)
max. baggage in each bin
4.4 lb
(2 kg)
max. fuel
126 lb
(57 kg)
2.18 Crew
The REMOS GX is certified to be operated with a minimum of 1
occupant (the pilot in command) and a maximum of 2 occupants.
If not otherwise defined by regulations or by the owner/operator, the
pilot in command is normally seated on the left.

G3-8 MA FM 3202 - R02
2 Operating Limitations
Operating Limitations 2 - 9
2.19 Flight Conditions and Minimum Equipment List
operation
minimum equipment
Day-VFR
as per D-VFR Minimum Equipment List
Night-VFR
not approved
IFR in IMC
not approved
IFR in VMC
not approved
Aerobatics
not approved
D-VFR minimum equipment list
‚engine ROTAX 912 UL-S
‚silencer
‚airbox
‚propeller as defined in chapter 2
‚carburetor heating system
‚compass with compass card
‚altimeter
‚airspeed indicator
‚safety belts
‚ELT
‚electrical system including circuit breakers
‚master and engine kill (ignition) switch
‚engine instruments (e.g. Dynon FlightDEK D-180)