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Summary of Contents for Rans S-7LS Courier
- Page 1 S-7LS COURIER LIGHT SPORT AIRCRAFT PILOT OPERATING HANDBOOK Serial Number: Registration Number: March 3, 2005 COPYRIGHT © 2005 RANS DESIGNS KANSAS, USA...
- Page 2 Rans Inc. Model S-7LS COURIER Table of Contents TABLE OF CONTENTS SECTION GENERAL INFORMATION …………………………………… OPERATING LIMITATIONS……………………………………. WEIGHT AND BALANCE INFORMATION …………………… PERFORMANCE ………………………………………………… EMERGENCY PROCEDURES ………………………………… NORMAL PROCEDURES ……………………………………… AIRCRAFT GROUND HANDLING AND SERVICING … REQUIRED PLACARDS AND MARKINGS ………………….
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Page 3: Table Of Contents
Rans Inc. Section 1 Model S-7LS COURIER General Information SECTION 1 GENERAL INFORMATION TABLE OF CONTENTS Page Three View………………………………………………………………………………. 1-3 Introduction………………………………………………………………………………. 1-4 Airplane and Systems Descriptions…………………………………………………… 1-4 Airframe………………………………………………………………………… 1-4 Flight Controls…………………………………………………………………. 1-4 Trim Control System………………………………………………………….. Wing Flap System…………………………………………………………….. Landing Gear………………………………………………………………….. - Page 4 Rans Inc. Section 1 Model S-7LS COURIER General Information Operating Weights and Loadings ………………………………………………….. 1-16 Maximum Airplane Weights …………………………………………………. 1-16 Standard Airplane Weights …………………………………………………… 1-16 Cabin and Entry Dimensions ………………………………………………… 1-16 Specific Loadings……………………………………………………………… 1-16 Symbols, Abbreviations and Terminology …………………………………………… 1-16 General Airspeed Terminology and Symbols ………………………………...
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Page 5: Three View
Rans Inc. Section 1 Model S-7LS COURIER General Information THREE VIEW Revision - B May 8, 2007 1- 3... -
Page 6: Introduction
Rans Inc. Section 1 Model S-7LS COURIER General Information INTRODUCTION This handbook contains 8 sections. The pilot should study the entire handbook to familiarize himself with the limitations, performance and procedures applicable for this aircraft. Section 1 provides general information and system descriptions. -
Page 7: Trim Control System
Rans Inc. Section 1 Model S-7LS COURIER General Information Rudder pedals Brake pedals Throttle lever TRIM CONTROL SYSTEM The AC has an in flight elevator trim system. The movable trim tab is operated through a servomotor installed in the right elevator via a short pushrod. -
Page 8: Seat Belts And Shoulder Harness
Rans Inc. Section 1 Model S-7LS COURIER General Information SEAT BELTS AND SHOULDER HARNESSES The aircraft is equipped with a four-point pilot restraint system. At any time the pilot is seated in the aircraft with the intent of moving it, the pilot restraint system must be securely fastened. -
Page 9: Oil System
Rans Inc. Section 1 Model S-7LS COURIER General Information OIL SYSTEM The engine is equipped with a dry sump forced lubrication system with a main oil pump with integrated pressure regulator and oil pressure sensor. The oil pump sucks the oil from the oil tank via the oil cooler and forces it through the oil filter to the points of lubrication of the engine. -
Page 10: Carburetor Heat
Rans Inc. Section 1 Model S-7LS COURIER General Information CARBURATOR HEAT Each one of the two carburetors of the Rotax 912S engine has a separate pre heating system consisting of a heat exchanger, heat control unit and connecting duct hose. One control knob operates both systems. - Page 11 Rans Inc. Section 1 Model S-7LS COURIER General Information The instrument panel mounted control knob opens or closes the valves in both heat control units with a simple mixer simultaneously. The position of the valve determines if the engine runs on “cool” air coming through the air filter or on “hot” unfiltered air coming from the heat exchanger.
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Page 12: Propeller
Rans Inc. Section 1 Model S-7LS COURIER General Information PROPELLER The propeller is a fixed pitch Sensenich wood propeller. The maximum diameter is 72". The propeller has a polyurethane leading edge for protection and better service life. Always park the aircraft with propeller blades horizontal to preserve balance. - Page 13 Rans Inc. Section 1 Model S-7LS COURIER General Information Figure 1-4.Fuel system Airframe Revision - B May 8, 2007 1- 11...
- Page 14 Rans Inc. Section 1 Model S-7LS COURIER General Information In addition to the engine mounted (mechanical) fuel pump, there is an electric (back up) fuel pump mounted to the aft engine mount. These pumps are fed from a gascolator mounted on the firewall. This system incorporates an anti vapor lock feature at the fuel tee between the carburetors that feeds the vapor back to the gascolator at the firewall.
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Page 15: Brake System
Rans Inc. Section 1 Model S-7LS COURIER General Information Fuel Grade: unleaded automotive (ASTM D 4814) gasoline with minimum AKI (Anti Knock Index) of 91 (R+M)/2 – No alcohol permitted. Or AVGAS 100 LL For additional information refer to ROTAX Operators - and Maintenance Manual ►ATTENTION: If engine is mainly run on AVGAS... -
Page 16: Electrical System
Rans Inc. Section 1 Model S-7LS COURIER General Information ELECTRICAL SYSTEM The S-7LS electrical system is a 12-volt negative ground system. An integral AC generator mounted in the aft end of the engine powers it. It stores energy in a sealed maintenance free battery, located in the tail cone. - Page 17 Rans Inc. Section 1 Model S-7LS COURIER General Information SPINS PROHIBITED MUSIC IN OIL PRESS. OIL TEMP. PARKING BRAKE T.O. PULL SET EMRG. COM DOWN CABIN HEAT PULL ON CARB HEAT ENG. INSTR. TRIM STARTER REGULATOR REG. PULL ON OUTPUT INTERCOM TRANSPO.
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Page 18: Operating Weights And Loadings
Rans Inc. Section 1 Model S-7LS COURIER General Information OPERATING WEIGHTS AND LOADINGS MAXIMUM AIRPLANE WEIGHTS Ramp: 1235 lb. Takeoff: 1235 lb. Landing: 1235 lb. Weight in Baggage Compartment: 50 lb. STANDARD AIRPLANE WEIGHTS Standard Empty eight: 740 lb. Maximum Useful load: 495 lb. -
Page 19: Symbols, Abbreviations And Terminology
Rans Inc. Section 1 Model S-7LS COURIER General Information SYMBOLS, ABBREVIATIONS AND TERMINOLOGY The following definitions are of symbols, abbreviations and terminology used in this handbook and which may be of operational significance to the pilot. GENERAL AIRSPEED TERMINOLOGY AND SYMBOLS Calibrated Airspeed is indicated airspeed corrected for position and instrument error. -
Page 20: Meteorological Terminology
Rans Inc. Section 1 Model S-7LS COURIER General Information METEOROLOGICAL TERMINOLOGY Outside Air Temperature is the free air static temperature STANDARD TEMPERATURE Standard Temperature is 15 ° C at sea level and decreases approximately 2° C for each 1000 ft of altitude. -
Page 21: Weight And Balance Terminology
Rans Inc. Section 1 Model S-7LS COURIER General Information WEIGHT AND BALANCE TERMINOLOGY REFERENCE DATUM Reference Datum is an imaginary vertical plane from which all horizontal distances are measured. STATION A location along the airplane fuselage given in terms of distance from the reference datum. - Page 22 RANS Inc. Section 2 Model S-7LS COURIER Operating Limitations SECTION 2 OPERATING LIMITATIONS TABLE OF CONTENTS Page Introduction ……………………………………………………………………………… 2-2 Airspeed Limitations …………………………………………………………………… 2-2 Powerplant Limitations ………………………………………………………………… 2-3 Weight Limits …………………………………………………………………………… 2-4 Center of Gravity Limits ……………………………………………………………….. 2-4 Maneuver Limits ………………………………………………………………………… 2-4 Flight Load Factor Limits ……………………………………………………………….
- Page 23 RANS Inc. Section 2 Model S-7LS COURIER Operating Limitations INTRODUCTION Section 2 includes operating limitations, instrument markings, and basic placards necessary for the safe operation of the airplane, power plant and standard equipment. The Rotax 912 Operators Manual must be on board of the airplane.
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Page 24: Powerplant Limitations
RANS Inc. Section 2 Model S-7LS COURIER Operating Limitations POWER PLANT LIMITATIONS Number of Engines: Engine Manufacturer: Rotax Engine Model Number: 912 UL/S Horsepower rating and Engine speed (ISA): Maximum Takeoff (max off 5 min): 98.5 HP at 5800 RPM Max. -
Page 25: Weight Limits
The angle of bank should not exceed 60 ° and the pitch attitude may not exceed 30 °. Stalls except whip stalls are approved with slow deceleration. ► Acrobatic maneuvers, including spins are not approved in the RANS S-7LS aircraft. FLIGHT LOAD FACTOR LIMITS Flight Load Factors: Flaps Up: + 4.0 g, - 2.0g... -
Page 26: Kinds Of Operation Limits
Model S-7LS COURIER Operating Limitations KINDS OF OPERATION LIMITS The RANS S-7LS is limited to Day and Night VFR operations. Flight into known icing conditions is prohibited. This aircraft is limited to two occupants only. During solo flights the pilot must sit in the front seat. - Page 27 Rans Inc. Section 3 Model S-7LS COURIER Weight and Balance Information SECTION 3 WEIGHT AND BALANCE INFORMATION TABLE OF CONTENTS Page Introduction……………………………………………………………………………… 3-2 Installed Equipment List ……………………………………………………………… Airplane Weighing Procedures ………………………………………………………. 3-4 Weight and Balance……………………………………………………………………. 3-7 Revision - A March 3, 2005...
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Page 28: Introduction
Rans Inc. Section 3 Model S-7LS COURIER Weight and Balance Information INTRODUCTION This Section lists standard equipment installed, describes the procedures for establishing of basic empty weight and moment of the airplane. Procedures for calculating the weight and moment for various loadings are also provided. Sample forms are provided for reference. - Page 29 Rans Inc. Section 3 Model S-7LS COURIER Weight and Balance Information Tire Supplier: Specialty Tires of America Inc. Tire Part number: Aero Trainer 6.00x6; 6 Ply ; Type 3; AD4E4 Air Trac 8.00 X 6; 6 Ply; Type 3; AA1J4...
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Page 30: Airplane Weighing Procedures
Rans Inc. Section 3 Model S-7LS COURIER Weight and Balance Information Regulator Rectifier Supplier: Rotax Regulator Rectifier Part Number: 965 347 Starter Relay Supplier: Rotax Starter Relay Part Number: 992 819 FUEL SYSTEM: Gascolator Supplier: Aircraft Spruce Gascolator Part Number:... - Page 31 Rans Inc. Section 3 Model S-7LS COURIER Weight and Balance Information 5. Using weights from item 3 and measurements from item 4, the airplane basic empty weight and moment can be determined by completing Figure 3-1. (The airplane basic empty weight includes the unusable fuel amount of 1.25 gall.) •...
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Page 33: Weight And Balance
Rans Inc. Section 3 Model S-7LS COURIER Weight and Balance Information Weight and Balance The following will enable you to determine the weight and balance of your AC and to operate it within the prescribed center of gravity limitations. The S-7LS is a simple AC and so are the weight and balance calculations. - Page 39 Rans Inc. Section 4 Model S-7LS COURIER Performance SECTION 4 PERFORMANCE TABLE OF CONTENTS Page Introduction…………………………………………………………………………….. Airspeed Indicator Calibration………………………………………………………… 4-2 Temperature Conversion Chart………………………………………………………. 4-3 Wind Components……………………………………………………………………… 4-4 Stall Speeds…………………………………………………………………………….. 4-5 Takeoff Distance Short Field …………………………………………………………. 4-6 Maximum Rate of Climb……………………………………………………………….. 4-7 Cruise Performance……………………………………………………………………..
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Page 40: Introduction
Rans Inc. Section 4 Model S-7LS COURIER Performance INTRODUCTION SECTION 4 provides performance Information. The data assumes that the aircraft and engine are in good condition and that average piloting techniques are used. All performance data are given at forward CG- limit and gross weight if not stated otherwise. -
Page 41: Temperature Conversion Chart
Rans Inc. Section 4 Model S-7LS COURIER Performance TEMPERATURE CONVERSION CHART Figure 4-2. Temperature Conversion Chart Original Issue March 3, 2005 4- 3... -
Page 42: Wind Components
Rans Inc. Section 4 Model S-7LS COURIER Performance WIND COMPONENTS Note: Maximum demonstrated crosswind velocity (90 degree) is 12 knots. Figure 4-3. Cross Wind Component Chart Original Issue March 3, 2005 4- 4... -
Page 43: Stall Speeds
Rans Inc. Section 4 Model S-7LS COURIER Performance STALL SPEEDS CONDITIONS: Power Off NOTES 1. Maximum altitude loss during a stall recovery may be as much as 160 feet. 2. IAS (MPH) Values are approximate. 3. All values are in MPH 4. -
Page 45: Maximum Rate Of Climb
Rans Inc. Section 4 Model S-7LS COURIER Performance MAXIMUM RATE OF CLIMB CONDITIONS: Full Throttle Flaps Up Gross weight (1235 lb.) Forward CG NOTES: 1. Airspeeds are indicated airspeeds (IAS). 2. Service ceiling 12,500 ft. (MSL) Pressure Climb Standard R/C for STD... -
Page 47: Maximum Demonstrated Crosswind Velocity
Rans Inc. Section 4 Model S-7LS COURIER Performance MAXIMUM DEMONSTRATED CROSSWIND VELOCITY Takeoff 12 Knots (90 degree) Landing 12 Knots (90 degree) This is not considered limiting. DEMONSTRATED OPERATING TEMPERATURE Satisfactory engine cooling has been demonstrated for this airplane with an outside air temperature 23 º... - Page 48 Rans Inc. Section 5 Model S-7LS COURIER Emergency Procedures SECTION 5 EMERGENCY PROCEDURES TABLE OF CONTENTS Page Introduction…………………………………………………………………………….. Airspeeds for Emergency Operation…………………………………………………. 5-2 Engine Failure After Takeof………………………………………………….. 5-2 Maneuvering Speed…………………………………………………………… 5-2 Maximum Glide………………………………………………………………... 5-2 Precautionary Landing with Engine Power…………………………………. 5-2 Landing without Engine Power…………………………………………….
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Page 49: Introduction
Rans Inc. Section 5 Model S-7LS COURIER Emergency Procedures INTRODUCTION SECTION 5 provides checklists and amplified procedures for coping with emergencies that may occur. Emergencies caused by aircraft or powerplant malfunctions are rare if proper preflight inspections and maintenance are performed. Emergencies caused by extreme weather situations can be minimized or eliminated by good judgment and proper preflight planning. -
Page 50: Engine Failure During Flight
Rans Inc. Section 5 Model S-7LS COURIER Emergency Procedures Engine Failure During Flight Fly the Airplane! Airspeed - 64 MPH for best glide Select Emergency Landing Area - PROCEED To It. Attempt Engine RESTART. Ignition - Check ON. Choke - Check OFF. -
Page 51: Landing With A Defective Main Wheel Tire
Rans Inc. Section 5 Model S-7LS COURIER Emergency Procedures Place folded coat or cushion over face at touch down Airplane - Unlatch Seat Belts and EVACUATE through doors. Life Raft and Vests - INFLATE (If onboard). LANDING WITH A DEFECTIVE MAIN WHEEL TIRE... -
Page 52: Amplified Procedures
Rans Inc. Section 5 Model S-7LS COURIER Emergency Procedures If fire appears out and electrical power is necessary for continuance of flight: Circuit Breakers - CHECK for faulty circuit, do not reset faulty circuit Master Switch - ON. Radio/Electrical Switches - ON one at a time, with delay after each until short circuit is localized. -
Page 53: Forced Landings
Rans Inc. Section 5 Model S-7LS COURIER Emergency Procedures FORCED LANDINGS Select a suitable landing site and proceed to it. If all attempts to restart the engine fail and a forced landing is imminent, follow the checklist for Emergency Landing Without Power. -
Page 54: Carburetor Ice
Rans Inc. Section 5 Model S-7LS COURIER Emergency Procedures CARBURETOR ICE A sudden engine roughness or loss of rpm could be Carburetor Ice problems. Actuate the Carburetor Ice by pulling on the Carburetor Ice Control Knob. As soon as the engine roughness or suspected carburetor ice is gone turn off the Carburetor Heat. - Page 55 Rans Inc. Section 6 Model S-7LS COURIER Normal Procedures SECTION 6 NORMAL PROCEDURES TABLE OF CONTENTS Page Introduction………………………………………………………………………………. 6-3 Airspeeds For Normal Operations…………………………………………………….. 6-3 Operational Checklists…………………………………………………………………. 6-3 Preflight Inspection……………………………………………………………………… 6-3 Cabin……………………………………………………………………………. 6-5 Empennage…………………………………………………………………….. 6-5 Left Wing – Trailing Edge………………………………………………………. 6-5 Left Wing…………………………………………………………………………...
- Page 56 Rans Inc. Section 6 Model S-7LS COURIER Normal Procedures Takeoff………………………………………………………………………….. 6-13 Power Check and Takeoff Roll…………………………………….. 6-13 Flap Settings………………………………………………………… 6-14 Short Field Takeoff………………………………………………… 6-14 Crosswind Takeoff…………………………………………………. 6-14 Enroute Climb…………………………………………………………………………… 6-14 Cruise……………………………………………………………………………………. 6-14 Stalls…………………………………………………………………………………….. 6-15 Approach…………………………………………………………………………………. 6-15 Landing…………………………………………………………………………………. 6-15 Normal Landing………………………………………………………………..
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Page 57: Normal Procedures
Rans Inc. Section 6 Model S-7LS COURIER Normal Procedures INTRODUCTION SECTION 6 provides checklists and amplified (detailed) procedures for the conduct of normal operations. AIRSPEEDS FOR NORMAL OPERATION The following airspeeds are based on operations at a Maximum Gross Weight of 1235... - Page 58 Rans Inc. Section 6 Model S-7LS COURIER Normal Procedures operations. Always exercise due care and good judgment. It is also recommended to remove visible moisture (water) from at least wings and tail surfaces because of its negative effects on performance of the aircraft.
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Page 59: Cabin
Rans Inc. Section 6 Model S-7LS COURIER Normal Procedures 1 Cabin Airplane Flight Manual – AVAILABLE IN CABIN Parking brake – SET Ignition switch -OFF Master switch -OFF Avionics Master - OFF Circuit Breakers - CHECK IN Fuel Selector Valve - ON Fuel Quantity Indicator –CHECK QUANTITY... -
Page 60: Left Wing
Rans Inc. Section 6 Model S-7LS COURIER Normal Procedures 4 Left Wing Wing tip – CHECK security Pitot tube – CHECK security Leading edge – CHECK condition, dents, nicks Wing Tie Down - DISCONNECT Forward lift strut and jury strut- CHECK security, dents, nicks Fuel quantity –... -
Page 61: 7 Right Wing- Trailing Edge
Rans Inc. Section 6 Model S-7LS COURIER Normal Procedures 7 Right wing- Trailing Edge Aileron – CHECK freedom of movement and security Flap – CHECK security Rear strut and jury strut attach – CHECK security, dents, nicks Fuel quick drain valve on bottom of wing; - DRAIN at least a cupful of fuel (using sampler cup) to check for water, sediment and proper fuel grade before first flight of day and after each refueling. -
Page 62: Taxiing
Rans Inc. Section 6 Model S-7LS COURIER Normal Procedures TAXIING Brakes - CHECK. Control deflection as required for wind BEFORE TAKEOFF Cabin Doors - CLOSED OR SECURED. Parking Brake - SET. Flight Controls - FREE and Correct. Flight Instruments - SET. -
Page 63: Enroute Climb
Rans Inc. Section 6 Model S-7LS COURIER Normal Procedures (10) Flaps - RETRACT slowly after reaching 60 MPH. ENROUTE CLIMB NORMAL CLIMB Airspeed – 70-80 MPH. NOTE: If a maximum performance climb is necessary, use speeds shown in the maximum rate of climb table in Section 5. -
Page 64: Short Field Landing
Rans Inc. Section 6 Model S-7LS COURIER Normal Procedures SHORT FIELD LANDING Airspeed (approach) – 66-70 MPH (flaps UP). Flaps (on final) – FULL (below 69 MPH) Airspeed - MAINTAIN 59 MPH . Power - REDUCE to idle as obstacle is cleared... -
Page 65: Amplified Procedures
If you have any reservations, DO-NOT-FLY! ALWAYS do your own preflight. Refer to Figure 6-1. Starting at the nose, work around the Rans S-7LS aircraft in a clockwise manner as illustrated. NOTE: This suggested outline for a preflight inspection generally covers the critical areas that MUST be checked prior to each flight. - Page 66 Rans Inc. Section 6 Model S-7LS COURIER Normal Procedures NOTE: For more specific information regarding powerplant operation, refer to the Rotax Operator's Manual. The manual contains IMPORTANT safety, maintenance, and operating information. TAXING (Ground Handling) The S-7LS is a tail wheel aircraft. Concentrate on taxiing till the moment you tied the aircraft down.
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Page 67: Before Takeoff
Rans Inc. Section 6 Model S-7LS COURIER Normal Procedures When taxing in strong crosswinds a little extra throttle will help the aircraft turn due to the increased airflow over the rudder. Caution should be used not to use excessive throttle, sudden throttle movements or excessive braking. -
Page 68: Flap Settings
Rans Inc. Section 6 Model S-7LS COURIER Normal Procedures If the takeoff is being made over loose impediments, advance the throttle slowly. This will allow the aircraft to be well into the takeoff roll before high propeller RPM's are reached, and decreases the possibility of propeller damage. The rate the throttle is advanced must be dictated by the available runway and obstructions in the departure path. -
Page 69: Stalls
Rans Inc. Section 6 Model S-7LS COURIER Normal Procedures STALLS The stall characteristics of the S-7LS aircraft are conventional. Use slow deceleration. The position and feel of the flight controls can be used as an indication of an impending stall. The control stick will be aft of its normal flight position and the aircraft will feel "mushy". -
Page 70: Hot Weather Operation
Rans Inc. Section 6 Model S-7LS COURIER Normal Procedures SECURING THE AIRCRAFT If the aircraft must be left unattended outdoors, always secure it with tie-downs. The type of tie-downs used is a matter of personal choice. A good "rule-of-thumb" is to ensure that what you secure the aircraft to (and with) will restrain at least 1235 lbs at each tie-down location. - Page 71 Rans Inc. Section 7 Model S-7LS COURIER Aircraft Ground Handling and Servicing SECTION 7 AIRCRAFT GROUND HANDLING AND SERVICING TABLE OF CONTENTS Page Ground Handling ………………………………………………………………………. 7-2 Towing and Tie- Down Instructions ………………………………………………… Servicing with Fuel ……………………………………………………………………. Servicing with Oil ………………………………………………………………………. 7-3 Servicing with coolant ………………………………………………………………….
- Page 72 Rans Inc. Section 7 Model S-7LS COURIER Aircraft Ground Handling and Servicing GROUND HANDLING On the ground the aircraft is most easily maneuvered by hand using the handles on the leading edge of the horizontal stabilizer. The aircraft has a 360 degree full swivel tail wheel, which is connected to the rudder by a centering cam.
- Page 73 Rans Inc. Section 7 Model S-7LS COURIER Aircraft Ground Handling and Servicing SERVICING WITH OIL The engine oil is contained inside the oil bottle which is mounted firewall forward. Oil quantity is 3 qts. Reference Section 1 for a description of the system and approved oil grades.
- Page 74 Rans Inc. Section 7 Model S-7LS COURIER Aircraft Ground Handling and Servicing WINDSHIELD AND WINDOWS The windshield and windows are made from lexan. Do not bring in contact with fuel. Fuel will harm these surfaces almost immediately. If fuel is spilled accidentally wipe off with lots of water.
- Page 75 Rans Inc. Section 8 Model S-7LS COURIER Required Placards and Markings SECTION 8 REQUIRED PLACARDS AND MARKINGS TABLE OF CONTENTS Page Airspeed Indicator Markings ………………………………………………………….. 8-2 Powerplant Instrument Markings ……………………………………………………... 8-2 Placards ………………………………………………………………………………….. 8-3 REVISION - A May 8, 2007...
- Page 76 Rans Inc. Section 8 Model S-7LS COURIER Required Placards and Markings AIRSPEED INDICATOR MARKINGS Airspeed indicator markings and their color code meanings are shown in Table 8-1. Marking IAS Value or Meaning Range(mph) White Arc 45 - 69 Full Flap Operating Range. Lower limit is maximum weight stalling speed in landing configuration.
- Page 77 PLACARDS The following labels and placards contain important information needed for proper operation of the RANS S-7LS aircraft and must be displayed in the location described in this section. All placards are available through Rans Inc. Refer to your parts manual.
- Page 78 Rans Inc. Section 8 Model S-7LS COURIER Required Placards and Markings On front face of CHT gauge Besides ELT remote control on instrument panel All range markings on instrument front face as shown Passenger Warning on lower left side of instrument panel.
- Page 81 Rans Inc. Section 9 Model S-7LS COURIER Supplementary Information SECTION 9 SUPPLEMENTARY INFORMATION TABLE OF CONTENTS Page Familiarization Flight Procedures ……………………………………………………... 9-3 Pilot Operating Advisories………………………………………………………………. 9-4 Revision - A May 8, 2007 9- 1...
- Page 82 Rans Inc. Section 9 Model S-7LS COURIER Supplementary Information FAMILIARIZATION FLIGHT PROCEDURES The pilot should familiarize himself thoroughly with this Manual, ROTAX Engine Operators Manual, applicable Aviation Regulations and the aircraft itself, before any solo flight is attempted. Scope and detail of a familiarization flight will depend on level of experience and currency of the pilot.
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