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Rotax CESSNA 150 Manual

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Airplane Flight Manual
CESSNA 150
Series F150L
Engine: ROTAX 912 S3
Propeller: Hoffmann HO-V352F/170FQ+10
160
SDF Nr.
Revision 1
April 2001
OK-RTX
Blue Skies Aviation Oy
Lentotie 89
17130 Vesivehmaa
E-Mail: info@blueskies.fi
Internet: http://www.blueskies.fi www.rotax-cessna.com

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Summary of Contents for Rotax CESSNA 150

  • Page 1 Airplane Flight Manual CESSNA 150 Series F150L Engine: ROTAX 912 S3 Propeller: Hoffmann HO-V352F/170FQ+10 SDF Nr. Revision 1 April 2001 OK-RTX Blue Skies Aviation Oy Lentotie 89 17130 Vesivehmaa E-Mail: info@blueskies.fi Internet: http://www.blueskies.fi www.rotax-cessna.com...
  • Page 2 This manual describes the operation and performance of the Cessna () 150 () model with the conversion NS402S with ROTAX 912S3 and HOFFMANN HO-V352F / 170FQ + 10 propeller. The flight manual applies to all models and was created using the original AFM of the Cessna (F) 150M series.

  • Page 3: Summary Of Revisions

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Edition 1 - A SUMMARY OF REVISIONS Change Changed pages Reason change recognized LBA – Remarks Date endorsement 0-3, 0-4 09.07.02/Sp 2-2b Operating limits f.
  • Page 4 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Edition 1- A TYPE SPECIFIC AFM PAGES Series SERIES-SPECIFIC PAGES (F)150F 1-6a, 2-2a, 2-5a, 2-7a, 5-6a, 7-2a, 7-3a, 7-4a, 7-5a, 7-6a, 8-2a, 8-3a...
  • Page 5 Airplane Flight Manual Cessna F150L Nr. 160 Converted with conversion kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 GENERAL NOTE In addition to the instructions for use, this manual also includes a list of maintenance and periodic inspections and performance data.
  • Page 6 Airplane Flight Manual Cessna F150L Nr. 160 Converted with conversion kit NS402S with ROTAX 912 S3 Page: and HOFFMANN HO-V352F/170FQ+10 Revision 1 Fig. 1 - 1...

  • Page 7: General Dimensions

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with conversion kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 DESCRIPTION AND DIMENSIONS GENERAL DIMENSIONS Wingspan: 10.16 m Maximum length: 7.5 m Maximum height: 2.63 m WING Wing profile: NACA 2412 Wing area: 14.9 m2...
  • Page 8 Airplane Flight Manual Cessna F150L Nr. 160 Converted with conversion kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 ELEVATOR TRIM Movement up: 10 ° ± 1 ° Movement down: 20 ° ± 1 ° RUDDER AND FIN Fin area: 0.83 m2...

  • Page 9: Carburetor Heat

    Converted with conversion kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 COOLANT Approximately 2.5 ltr.for mixing and frost prevention see ROTAX– operating handbook CARBURETOR HEAT Manual operation PROPELLER Designation: HOFFMANN HO-V352F / 170FQ + 10 Type:...
  • Page 10 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 1-6b NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 INSTRUMENT PANEL ()(A)150K-L turn Coordinator 16 Ammeter 33 Circuit breakers airspeed indicator 17 Right fuel gauge 34 Rheostat for instruments...
  • Page 11 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 Fuel system description Fig. 1 - 2...

  • Page 12: Fuel System

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 FUEL SYSTEM The fuel is supplied to the engine from two tanks, one located in each wing. From these tanks,...
  • Page 13 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 Electrical system Abb. 1 - 4...

  • Page 14: Electrical System

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 1-10 NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 ELECTRICAL SYSTEM The airplane is equipped with a 14-volt, direct current electrical system with one internal generator (Generator 1) and one externally mounted generator (Generator 2) (see Abb. 1 - 4).

  • Page 15: Circuit Breakers And Fuses

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 1-11 NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 GENERATOR – CONTROLIGHT The red generator indicator lights are indicators of too low a charging current. These warning lights indicate to the pilot an error in the power supply by the respective generator.

  • Page 16: Wing Flap System

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 1-12 NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 INTERIOR LIGHTNING The instrument panel and the operator panel are illuminated by floodlights and optionally by built-in lights. Two concentrically arranged control knobs labeled "FLIGHT LIGHT" and "INSTRUM.

  • Page 17: Parking Brake

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 1-13 NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 Heated fresh air and outside air are blended in a cabin manifold just aft of the firewall by adjustment of the heat and air controls;...

  • Page 18: Seat Belt And Shoulder Harness

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 1-14 NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 A child's seat is available for installation in the rear of the cabin. The seat back is secured to the cabin sidewalls, and the seat bottom is attached to brackets on the floor.
  • Page 19 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 1-15 NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 Note Pressure altitude should not be confused with indicated altitude. To obtain pressure altitude, momentarily set the barometric scale on the altimeter to 1013 mb and read pressure altitude on the altimeter.
  • Page 20 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 revision 1 LIMITATIONS INTRODUCTION This section sets out the operating limitations, instrument markings and placards required for the safe operation of the aircraft, engine and standard equipment and equipment.

  • Page 21: Airspeed Limitations

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 2-2a NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 AIRSPEED LIMITATIONS Airspeed limitations in flight operations are presented in the table below All Models (F)150F, (F)150G, (F)150H, (F)150J, (F)150K, (F)150L...

  • Page 22: Engine Instrument Markings

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 POWERRPLANT LIMITATIONS ENGINE Manufacturer BOMBARDIER-ROTAX GmbH Engine model ROTAX 912S3 Engine operating limits for take-off: 73.5 kW (100PS)/ 2385 Rpm...

  • Page 23: Maximum Weights

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 MAXIMUM WEIGHTS maximum take-off weight: 726 kg Maximum landing weight: 726 kg maximum weight in baggage compartment: • Baggage area 1 (or passenger in child seat), Station 127 to 193cm 54 kg, note the sign below •...
  • Page 24 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 2-5a NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 APPROVED FLIGHT MANEUVRES (Models (F)150F, (F)150G, (F)150H, (F)150J, (F)150K, (F)150L) This airplane is certified as a utility category and is designed for limited aerobatics. In acquision of various certificates such as professional pilot, IFR and instructor ratings.

  • Page 25: Flight Load Factors

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 FLIGHT LOAD FACTORS Flaps up + 4.4g, -0.5g (5 Seconds. Limited by engine) Flaps down +3,5 g (No negative loads approved)
  • Page 26 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 2-7a NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 PLACARDS The following information must be displayed in the form of composite or individual placards IN THE FULL VIEW OF THE PILOT (Models (F)150F, (F)150G, (F)150H, (F)150J, (F)150K, (F)150L) (The DAY-NIGHT-, VFR- and IFR-flight ”entry shown on the example below, will wary as the...
  • Page 27 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Edition 1 IN THE PAGGAGE COMPARTMENT Maximum paggage and/or auxiliary passenger For additional loading instructions see weight and balance data. IN THE VICINITY OF FUEL SHUT OFF VALVE(STANDARD TANKS) Fuel 22,5 gal = 85 ltr.
  • Page 28 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Edition 1 ON THE INSTUMENT PANEL NEAR OVER VOLTAGE WARNING LIGHT over voltage ON COOLANT TANK OR ON COVER 2.5 ltr. - coolant...
  • Page 29 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Edition 1 EMERGENCY PROCEDURES ENGINE FAILURES ENGINE FAILURE DURING TAKE OFF RUN (WITH ADEQUATE RUNWAY AHEAD) - ABORTING THE TAKE OFF - Throttle ........
  • Page 30 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Edition 1 After landing Throttle ........IDLE Fuel shut off valve ......OFF Main switch ........OFF 10) Magneto switch ......Off ENGINE STOPPED Airspeed (IAS) ......
  • Page 31 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Edition 1 RELIGTING THE ENGINE WITH PROPELLER WINDMILLING as long as the airspeed is not below 62 mph (54kts) the propeller continues on wind milling Airspeed (IAS) ......
  • Page 32 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Edition 1 Maximum gliding distance Airspeed 70 mph (60) IAS Propeller wind milling Wing flaps UP, zero wind FIRES ENGINE FIRE ON GROUND DURING STARTING Improper starting techniques in cold weather conditions can lead to kick back and ignition of the accumulated fuel in intake manifold.

  • Page 33: Engine Fire During Flight

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Edition 1 ENGINE FIRE DURING FLIGHT Although engine fires are extremely rare in flight, the following measures should be taken if such fire occur: Fuel shut off valve ...........

  • Page 34: Landing With A Flat Main Tire

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Edition 1 If the fire seems to be extinguished and electric power is needed to continue the flight: Main switch ............. On Circuit breakers ..........

  • Page 35: Forced Landings

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Edition 1 FORCED LANDINGS PRECAUTIONARY LANDING WITH ENGINE POWER Before commencing a landing off airport you should overfly the desired landing area at low but safe altitude to check the terrain for obstacles and conditions.
  • Page 36 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Edition 1 DITCHING Prepare for ditching by securing or jettison heavy objects in the luggage compartment. To protect the faces of the occupants, obtain folded coats or cushion ready at hand. Send "Mayday"...

  • Page 37: Spiral Dive

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Edition 1 11) Approach at 75-85 mph (65 bis 75 Kts) depending upon the amount of ice accumulation 12) Perform a landing in level attitude.

  • Page 38: Electrical Power Supply Malfunctions

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 3-10 NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Edition 1 Changes in the equipment of the aircraft or the aircraft weight and center of gravity due to subsequently installed equipment or cabin occupancy may lead to a change in the behavior of the aircraft, especially during prolonged spins.

  • Page 39: Rough Engine Operation Or Loss Of Power

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 3-11 NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Edition 1 If the overvoltage conditions remains Circuit breaker „Gen. Feld 1“ ..... Push Circuit breaker „Gen. Feld 2“ ..... Pull 50A-Circuit breaker „Generator 2“...

  • Page 40: Low Oil Pressure

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 3-12 NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Edition 1 IGNITION MODULE FAULT A sudden engine roughness or misfiring is usually evidence of ignition module problems. Switching from BOTH to either L or R ignition switch position will identify which system is malfunctioning.

  • Page 41: Exterior Check

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 EXTERIOR CHECK External inspection Note Visually check airplane for general condition during walk-around inspection. In cold weather, remove even small accumulations of frost, ice or snow from wing, tail and control surfaces.
  • Page 42 Warning: check or refill only when the engine is cold. Check the engine oil level with dipstick (see. also, ROTAX 912 () user’s manu- al). Before checking the oil level, run the engine for 1 min. At idle speed or turn the propeller by hand a few turns to pump the engine oil completely out of the crank- case.

  • Page 43: Before Engine Start

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: Revision 1 – Change A HOFFMANN HO-V352F/170FQ+10 10) Check the venturi for obstruction.. Check main wheel for correct pressure. Before first flight of the day and after each refueling, use sampler cup and drain small quantity of fuel tank sum quick drain valve to check for water, sediment and proper fuel grade..

  • Page 44: Before Taxi

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 BEFORE TAXI electrical switches ........as needed Engine instruments ........check Flaps(indication and Function) ..... check (Flaps down and then again up) Avionics(Switch) ..........

  • Page 45: Normal Climb

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 SHORT FIEL TAKE OFF Flaps ............... 10° carburetor heat ..........cold (forward) Brakes ............apply Propeller control ..........max. RPM Throttle ............

  • Page 46: Normal Landing

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 NORMAL LANDING Touch down ........ main wheels first Landing roll ........lower nose wheel gently Brakes ......... minimum required AFTER LANDING Wing flaps ........

  • Page 47: Operating Details

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 OPERATING DETAILS STARTING THE ENGINE Usually a warm engine is started with throttle control in for approx. 2 cm. without choke. A cold...
  • Page 48 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 Taxing diagram Strong quartering tail winds require caution. Avoid sudden bursts of the throttle and sharp braking when the airplane is in this attitude. Use the steerable nose wheel and rudder to...
  • Page 49 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 CHECKING THE IGNITION MODULES Checking the ignition modules should be done at an engine speed of 1700 rpm, prop control on high setting (forward).

  • Page 50: Cruise Climb

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 4-10 NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 WING FLAP SETTINGS Normal take-offs are accomplished with wing flaps retracted. Using 10° wing flaps reduces the total distance over an obstacle by approximately 10%. This advantage is however lost in total climb gradient after 15 m obstacle has been cleared.
  • Page 51 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 4-11 NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 CRUISE FLIGHT Normal cruise is performed with an engine power between 55 and 75%. The required settings to achieve these performance figures at different altitudes and temperatures can be found or from the performance data in Section V.

  • Page 52: Short Field Landing

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 4-12 NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 SPINS Spins not approved for this airplane (see section 2). To stop an unintentional spin, see. Emergency section...

  • Page 53: Cold Weather Operations

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 4-13 NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 COLD WEATHER OPERATIONS Prior to starting with temperatures below freezing, it is advisable to pull the propeller through several times by hand to "break loose"...

  • Page 54: Use Of Performance Charts

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 PERFORMANCE INTRODUCTION Performance data charts on the following pages are presented so that you may know what to expect from the airplane under various conditions, and, to facilitate the planning of flights in detail and with reasonable accuracy.
  • Page 55 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 These distances are well within the available take-off field length. However, a correction for the effect of wind may be made based on Note 3 of the takeoff chart. The correction for a 12-knot headwind is: ...
  • Page 56 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 FOR ISA+16 THE RESULT IS THEREFORE   − − − − roll  −  roll roll roll ...

  • Page 57: Fuel Required

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 FUEL REQUIRED The total fuel requirement for the flight may be estimated using the performance information in figures Fig. 5 - 5 to Fig. 5 - 9 . For this sample problem it can be seen from Fig. 5 - 8 that a climb from 1500ft to 5500ft requires 4.1ltr.
  • Page 58 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 CONVERSION CHART PRESSURE ALTITUDE – DENSITY ALTITUDE Fig. 5 - 1 – Pressure altitude/Density altitude...

  • Page 59: Airspeed System Calibration

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 5-6b NS402S with ROTAX 912 S3 and Page: Revision 1 – Change A HOFFMANN HO-V352F/170FQ+10 AIRSPEED SYSTEM CALIBRATION Airspeed, IAS, indicated air speed deviates from the calibrated airspeed CAS as follows (mph)

  • Page 60: Takeoff Distance

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 TAKEOFF DISTANCE 4000 ft 8000 ft level Deviation Ground Total to Ground Total to Ground Total to clear from...

  • Page 61: Rate Of Climb

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 CLIMB RATE OF CLIMB Fig. 5 - 5 – Rate of climb Note: Flaps up, Full throttle...
  • Page 62 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 TIME TO CLIMB Fig. 5 - 6 – Time to climb...
  • Page 63 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 5-10 NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 DISTANCE TO FLY Fig. 5 - 7 –Distance travelled during climb...
  • Page 64 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 5-11 NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 FUEL USED TO ALTITUDE Fig. 5 - 8 – Fuel used during climb Note: 4 liter for starting the engine, taxi and warm up is reserved...

  • Page 65: Cruise Performance

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 5-12 NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 CRUISE PERFORMANCE Density alt 2000ft T = 11°C Endurance, hours Range, NM Standard Longrange Standard Longrange Tanks Tanks...
  • Page 66 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 5-13 NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 LANDING DISTANCE OVER 15 M OBSTACLE Engine at idle power, flaps 40°, hard surface, wind calm SL and 15° C.

  • Page 67: Fuel Strainer

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 MAINTENANCE INSTRUCTION – HANDLING ON GROUND SERVICING On the following pages, under the header "MAINTENANCE INSTRUCTIONS", the consuma- bles, quantities and specifications of common service items (such as fuel, oil, etc.) are listed to provide you with this information at all times and without delay.
  • Page 68 Fill with engine oil (without additives). This work must be performed in accordance with the ROTAX 912 Series Service Manual () (). When using AVGAS, the engine oil change is required every 50 hours of operation.

  • Page 69: Care Of The Airplane

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 The oil change must be carried out at least once a year, even if less than 100 flight hours have been flown during this period.

  • Page 70: Windshield - Windows

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 Proper tie-down procedure is the best precaution against damage to the parked airplane by gusty or strong winds. Tie down the airplane securely, proceed as follows:: Set the parking brake and install the control wheel lock.

  • Page 71: Painted Surfaces

    Airplane Flight Manual CessnaF150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 PAINTED SURFACES The painted exterior surfaces of your Cessna have a durable, long lasting finish and, under normal conditions, require no polishing or buffing. Approximately 15 days are requires for paint to cure completely;...
  • Page 72 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 Oily spots may be cleaned with household removers, used sparingly. Before using any solvent, read the instructions on the container and test it on obscure place on the fabric to be cleaned.

  • Page 73: Mass And Balance

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 7 MASS AND BALANCE...
  • Page 74 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 7-2c NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 DETERMING CENTER OF GRAVITY Before each flight the pilot must ensure that the airplane is loaded correctly. The Fig. 7c - 3...
  • Page 75 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 7-3c NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 LOADING ARRAGEMENT Abb. 7c - 1 – Loading arrangement...
  • Page 76 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 7-4c NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 BAGGAGE AREA LOADING AND TIE-DOWN BAGGARE AREA MAXIMUM LOADS Fig. 7c - 2 – Baggage area loading and tie down A cargo tie-down net is provided to secure baggage in the baggage area.
  • Page 77 Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 7-5c NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 LOADING EXAMPLE Example airplane Your airplane (example) Weight Moment/1000 Weight Moment/1000 cmkg Cmkg Basic Empty Weight (Use the data pertaining to your airplane as it is pres- 496.7...

  • Page 78: Loading Graph

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 7-6c NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 LOADING GRAPH Fig. 7c - 4 –Loading graph...

  • Page 79: Center Of Gravity Moment Envelope

    Airplane Flight Manual Cessna F150L Nr. 160 Converted with kit 7-7c NS402S with ROTAX 912 S3 and Page: HOFFMANN HO-V352F/170FQ+10 Revision 1 CENTER OF GRAVITY MOMENT ENVELOPE Fig. 7c - 5 – Center of Gravity Moment envelope...
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F150l series

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