Pilot Operating Handbook for LSA Edition for GXeLITE

f=ie:r*rss gx: Introduction_ 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. Serial No.: Built: Call Sign: Engine-Type: Serial No. Engine: Propeller-Type: Manufacturer: REMOS Aircraft GmbH Flugzeugbau Internet: www.remos.de

HEMS5 GX Introduction_ List of Content and List of Effective Pages 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.

HEMS5 GX Introduction_List of Revisions sect.

Introduction 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.

Introduction Views

General Information

General Information 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. The REMOS GX was manufactured in accordance with the Light Sport Aircraft airworthiness standards and does not conform to standard...

REMS5 GX 1 General Information1.4 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...

REMS5 GX 1 General Information1.6 Engine manufacturer Please refer to REMOS notification NOT-001 and ROTAX SI-912-016/SI-914-019 for further information on fuel containing ethanol and on suitable engine oils. Have a frequent look on www.rotax-engines.com and on www.remos.com for the latest information. General Information

ICAO Designator: GX (as per ICAO Doc. 8643) 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).

HEMS5 GX 2 Operating Limitations Table of Contents_ sect.

HEMS5 GX 2 Operating Limitations 2.1 Reference Airspeeds speed

2.2 Stalling Speeds at Maximum Takeoff Weight stall speed with flaps extended VS0 = 44 mph = 38 kts stall speed with flaps retracted VS1 = 51 mph = 44 kts 2.3 Flap Extended Speed Range For deflected flaps following speed restrictions apply as a function of airspeed: With flaps set to any deflection the safe load factor is limited to 2. 2.4 Maximum Maneuvering Speed maximum maneuvering speed VA = 108 mph = 94 kts

2.5 Never Exceed Speed never exceed speed VNE = 155 mph = 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 155 mph = 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. 2.6 Maximum Wind Velocity for Tie-Down max. wind velocity for tie-down in the open VR = 44 mph = 38 kts 2.7 Crosswind and Wind Limitations maximum demonstrated cross wind component for take-off and landing 15...

2.8 Maximum Parachute Deploy Airspeed maximum parachute deploy airspeed 138 mph = 120 kts 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 2.13 Permissible Flight Maneuvers The following maneuvers are permitted • all non-aerobatic maneuvers, including stalls and departure stalls • flight with the doors off

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 (Dynon FlightDEK D-180)

2.18 Airspeed Indicator Range and Markings

HEMS5 GX 2 Operating Limitations 2.19 Placards and Markings The required placards and markings are created with the following color codes. Information white lettering on a black black lettering on a white background - white framed background - black framed Information Safety white lettering on a black red lettering on a white background - red framed background - red framed Safety Warning white lettering on a red red lettering on a white background - white framed background - red framed

GXeLITE Rev. 01 2 Operating Limitations The following placards are mandatory and define operational limitations. They are located on the instrument panel. The list below does not define the layout but the content and intent of the placards. placards location right cockpit Airspeed Limitations Never Exceed Speed VhF 155 mph ))AS) Normal Operate Airspeed V'jii I23mptl (IAN) Max. Airspeed Flaps Extended V=E 81 mptt (IAS) Engine Limitations Rntax 912 Engine Speed 5300 FLPM Cyfimter Head Temperature 150*C Operating Limitations 2 - 11 center console center console