SOP Cessna 150-152

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    SOP C150/C152 - Issue 08 Page 1 - 142

    Standard OperatingProcedures

    (SOP’s)

    Cessna 150

    PH-RUD / PH-NOD / PH-HVP / PH-TGACessna 152

    PH-JVB / PH-CDS / PH-STQ /PH-WEE / PH-SCX / PHSKG 

    Name:

    COPYRIGHT Stella aviation academyNo part of this manual or its extracts may be reproduced in any form, by print, photo print,

    microfilm or any other means, without written permission from Stella aviation academy.

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    ISSUE RECORD

    Issue Number Issue Date

    01 09-12-2005

    02 01-10-2006

    03 01-01-2008

    04 19-10-2011

    05 07-11-2011

    06 01-05-2012

    07 01-10-2012

    08 06-02-2013

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    TABLE OF CONTENTS

    CHAPTER 1 .................................................................................................................................................... 7 

    1.0  INTRODUCTION .......................................................... ................................................................. ..................... 7 

    1.1  SOURCES .............................................................................................................. ........................................... 7 

    1.2  STANDARD OPERATING PROCEDURES .................................................................................. ..................... 7 

    1.3   AIRMANSHIP ............................................................... ................................................................. ..................... 7

    1.4  CHECKLIST ISSUES .............................................................. ................................................................. .......... 7 

    CHAPTER 2 .................................................................................................................................................... 9 

    2.0 

     ABBREVIATIONS USED IN THIS BOOK: ......................................................................................................... 9 

    CHAPTER 3 .................................................................................................................................................. 11 

    3.0  SPEEDS FOR DIFFERENT FLIGHT PHASES ....................................................... ......................................... 11 

    CHAPTER 4 .................................................................................................................................................. 13 

    4.0  DIFFERENCES WITH STANDARD PROCEDURE ................................................ ......................................... 13 

    CHAPTER 5 .................................................................................................................................................. 17 

    5.0  NORMAL CHECKLIST C150/C152 .............................................................. .................................................... 17 

    5.1  CESSNA 150; PH-RUD/NOD/HVP ....................................................................................................... ........... 17 

    5.2 

    EXPANDED NORMAL CHECKLIST C150: PH-RUD/NOD/HVP ....................................... .............................. 23 

    5.3  CESSNA 152: PH-JVB/CDS/STQ/WEE ....................................................... .................................................... 35 

    5.4  EXPANDED NORMAL CHECKLIST C152: PH-JVB/CDS/STQ/WEE .............................................................. 41 

    5.5  CESSNA 150: PH-TGA ........................................................... ................................................................. ........ 53 

    5.6  EXPANDED NORMAL CHECKLIST C150: PH-TGA ......................................................... .............................. 59 

    5.7  CESSNA 150: PH-SCX ........................................................... ................................................................. ........ 69 

    5.8  EXPANDED NORMAL CHECKLIST C150: PH-SCX ......................................................... .............................. 75 

    5.9  CESSNA 152: PH-SKG ........................................................... ................................................................. ........ 87 

    5.10  EXPANDED NORMAL CHECKLIST C150: PH-SKG ......................................................... .............................. 93 

    5.11 

    EMERGENCY CHECKLIST C150 PH-HVP/RUDNOD ...................................................... ............................ 105 

    5.12  EMERGENCY CHECKLIST C150 PH-JVB/CDS/STQ/WEE ......................................................... ................. 118 

    5.13  EMERGENCY CHECKLIST C150 PH-TGA ............................................................ ....................................... 123 

    5.14  EMERGENCY CHECKLIST C150 PH-SCX ............................................................ ....................................... 131 

    5.15  EMERGENCY CHECKLIST C150 PH-SKG ............................................................ ....................................... 137 

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    CHAPTER 1

    1.0 INTRODUCTION

    This book contains the Standard Operating Procedures covering the VFR operation of C150/C152. Thebook is a integral part of the way to handle an aircraft during VFR conditions. It’s not possible to cover alleventualities and there for good airmanship and common sense is expected of the crew. The speeds andprocedures in this part must be preferred above the AOM/POH. No marks are made to indicate changes onthe previous issue due to the amount of changes.

    1.1 SOURCES

    Material used from:

    -  AOM-  POH-  SOPs VFR General

    -  Company Notams

    1.2 STANDARD OPERATING PROCEDURES

    The SOPs  in this chapter have a direct relation to the execution of a safe flight. They shall be knownthoroughly and used throughout the rest of your career as a pilot. Basically these SOPs inform the studentabout the margins within which to operate, and step-by-step how to execute different flight manoeuvres in astandard way.Using SOPs greatly enhances the safety of flight, especially in non-standard circumstances.

    1.3 AIRMANSHIP

    Definition: All facets that allow the pilot to control the airplane at any time during the flight in accordancewith regulations in a safe way, on the ground as well as in the air.

    During the ground school all different facets that compose airmanship will be illustrated. Safety is a veryimportant part in the mind of every conscientious airline pilot. Adherence to rules and regulations is only thefirst part to incorporate "airmanship" into your existence.

    1.4 CECKLIST ISSUES

    Pay attention to the fact that this SOP document might have another issue number than mentioned on thevalid checklists. For the valid checklist issues refer to the document control list of SAA.

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    CHAPTER 2

    2.0 ABBREVIATIONS USED IN THIS BOOK

     AGL Above Ground Level AOM/POH Aircraft Operating Manual/ Pilots Operating Handbook ARO Aerodrome Reporting Office ATC Air Traffic Control ATPL Airline Transport Pilots LicenseCVV Carburettor heatFIR Flight Information RegionICAO International Civil Aviation OrganizationFIO Flight Information OfficeIFR Instrument Flight RulesITM IFR Training ManualME Multi EngineNOTAM Notices to Airman (Part of Aeronautical Information Publication)OM Operating ManualOPS Operations department of Stella aviation academyORP Outside Reference PointPIC Pilot In CommandRT RadiotelephonySE Single EngineSOP Standard Operating ProcedureUTC Universal Time CoordinationVFG VFR-guide (Part of Aeronautical Information Publication in the Netherlands)VFR Visual Flight Rules

    Speeds:

    Vrotate Rotation speedVcclimb Climb speedVcruise Cruise speedVdecsent Descent speedVglide Glide speedVstall Stall speedVs1 Stall speed, clean configurationVs0 Stall speed, landing configurationVslow Slow speedVhigh High speedVx Maximum angle of climbVy Maximum rate of climb

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    CHAPTER 3

    3.0 SPEEDS FOR DIFFERENT FLIGHT PHASES

    For calculation of the speeds from kts. to mph. add the factor 10, for example 80 kts is 90 mph.

      TAKE-OFFVrotate normal take-off 50 kts. Other take offs: see POH.

    Flight Phase Powersetting

    Flaps C150 C152

    normal take-off full throttle flaps up 70 kts. 80 mph. 70 kts.

    obstacle take-off full throttle flaps up 60 kts. 70 mph. 54 kts.

    obstacle take-offPH-TGA

    full throttle flaps up 56 kts.

    short field take-off full throttle flaps 10° 60 kts. 70 mph. 54 kts.

    soft field take-off full throttle flaps 10° 70 kts. 80 mph. 70 kts.

      SPEEDS & POWERSETTINGS

    Flight Phase Power setting C150 C152

    cruise climb full throttle 70 kts. 70 kts.

    best angle of climb full throttle 61 kts. 54 kts.

    best angle of climbPH-TGA

    full throttle 56 kts.

    best rate of climb full throttle 68 kts. 67 kts.

     Airwork 2300 RPM 85 kts. 85 kts.

    cruise flight according POH

    slow flight 1800 RPM 50-70 kts. 50-70 kts.high speed 2400 RPM 100 kts. 100 kts.

    steep turn 2500 RPM 85 kts. 85 kts.

    Descent 1700 RPM 85 kts. 85 kts.

    Glide throttle idle 60 kts. 60 kts.

      SPEED & FLAPSETTING IN CIRCUIT

    Power settings are indications and can be different for each C150/C152! The different in power settingbetween downwind and base leg is approximately about 400 RPM in no wind conditions.

    Flight Phase Power setting Flap setting Speed

    cross wind leg, climb full throttle up 70 kts.

    cross wind leg,circuit altitude

    2100 RPM up 80 kts.

    downwind 2100 RPM up 80 kts.after downwind checks 2100 RPM flaps 10° 75 kts.

    base leg 1700 RPM flaps 20° 70 kts.

    final 1700 RPM flaps full 60 kts.

    strong crosswind landing 1800 RPM flaps 20° 65 kts.

    flapless landing 1600 RPM flaps up 65 kts.

    glide-in landing idle flaps full 60 kts.

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    CHAPTER 4

    4.0 DIFFERENCES WITH STANDARD PROCEDURE

      No trimming

      Vs1 or Vs0 + 10 kts. Keep direction with rudder, aileron neutral

      Approach to stall, landing configuration:

      Short field take-off:

    Short field take-off  

      flaps 10°

      line aircraft up at beginning of runwayand check runway direction

      check heading versus desired runway

      check wind direction, yoke about halftravel into wind

      apply brakes

      smoothly apply full throttle

      check engine instruments

      brakes released

      maintain direction with rudder

      elevator slightly tail low

      after liftoff adjust attitude, accelerate toclimb speed

    Approach to stall, landing configuration: 

      check outside clear, O.R.P.

      reduce throttle to +/- 1900 RPM

      apply back pressure

      ailerons neutral

      white arc, full flaps in steps

      reduce throttle to +/- 1700 RPM

      stall recovery:-  simultaneously full throttle, CVV

    cold-  maintain attitude and heading-  flaps 20°

      passing 60 kts. flaps 10°

      passing 70 kts. flaps up

      with Vclimb, back to altitude

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      Soft field take-off:

    Soft field take-off    flaps 10°

      hold control column aft

      line aircraft up at beginning of runwayand check runway direction

      keep aircraft rolling

      check heading versus desired runway

      check wind direction, yoke about halftravel into wind

      smoothly apply full throttle

      maintain direction with rudder

      keep control column aft and fly theaircraft off the ground

      after liftoff adjust attitude, accelerate tonormal climb speed.

      Crosswind landingWith a crosswind component above 10 kts reduce flaps setting to flaps 20°. The final speed mustbe increased with 5 kts, final speed will be 65 kts.

      Flapless landingWith a flapless landing increase speed at base to 75 kts and increase the final speed to 65 kts.

      Glide-in landing

    The glide-in landing must be made with the best glide-in speed of 60 kts.

      Touch and goNormally during a touch and go, after the touch flaps will be selected up. However, during a softfield touch and go, the flaps can be selected to 10°

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      Go around or wave-off:

    Flight Phase or EventSTUDENT

    Go around Initiating go around  “GO AROUND” 

      select full throttle

      carburettor heat OFF

      maintain direction with rudder

      attitude for climb

      “FLAPS 20°” 

      select flaps 20º if flaps weremore than 20º

      “FLAPS 20° SET” 

    Wave-off Initiating go around  “WAVE OFF” 

      select full throttle

      carburettor heat OFF

      maintain direction with rudder

      maintain attitude to accelerateto climb speed

      “FLAPS 20°” 

      select flaps 20º if flaps weremore than 20º

      “FLAPS 20° SET” 

     After initiating the Go around or Wave-off continue as follows to resume normal climbout:

    Positive airborne,positive rate of climband above 50 ft AGL 

      check brakes

      “BRAKES CHECKED” 

      attitude for climb, increasespeed to 70 kts

      attitude to climb speed

      speed more than 60 kts.

      “FLAPS 10°” 

      select flap 10°

      “FLAPS 10° SET” 

     At 200 ft AGL   after take-off checks

      “FLAPS UP” 

      select flaps up

      “FLAPS ARE UP” 

      “After take-off checklist” 

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    CHAPTER 5

    5.0 NORMAL CHECKLIST C150/C152

    5.1 CESSNA 150 PH-RUD/NOD/HVP

    PREFLIGHT INSPECTION

    Note:Visually check airplane for general condition during walk-around inspection. In cold weather, remove evensmall accumulations of frost, ice or snow from wing, tail and control surfaces.

     Also, make sure that control surfaces contain no internal accumulations of ice or debris. Prior to flight,check that pitot heater (if installed) is warm to touch within 30 seconds with battery and pitot heat switcheson. If a night flight is planned, check operation of all lights, and make sure a flashlight is available.

    CABIN

    Pilot’s Operating Handbook ............. AVAILABLE IN AIRPLANEControl Wheel Lock .................................................... REMOVEIgnition Switch ..................................................................... OFFMaster Switch ..................................................... .................. ON

    WarningWhen turning on the master switch, using an externalpower source, or pulling the propeller through by hand,

    treat the propeller as if the ignition switch were on. Do notstand, nor allow anyone else to stand, within the arc of thepropeller, since a loose or broken wire, or a componentmalfunction, could cause the propeller to rotate.

    Fuel Quantity Indicators.............................. CHECK QUANTITYMaster Switch ..................................................... ................. OFFFuel Shutoff Valve ................................................................ ON

    EMPENNAGE

    Rudder Gust Lock ................................... ................... REMOVETail Tie-Down ..................................................... DISCONNECTControl Surfaces ............................................................ CHECK

    freedom of movement and security 

    RIGHT WING

     Aileron ........................................................ ................... CHECKfreedom of movement and security

    Wing Tie-Down ................................................... DISCONNECTMain Wheel Tire ................................................. ........... CHECK

    for proper inflation

    Fuel Tank Sump Quick Drain Valve ................................ DRAINBefore first flight of the day and after each refuelling, use

    sampler cup and drain small quantity of fuel from fuel tanksump quick-drain valve to check for water, sediment and

    proper fuel grade.

    Fuel Quantity ............................................... CHECK VISUALLYfor desired level

    Fuel Filler Cap .................................................... ......... SECURE

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    NOSE

    Oil Level ........................................................................ CHECKdo not operate with less than four quarts. Fill to six quarts

    for extended flight.

    Strainer drain knob ............................................................ PULLto clear water and sediment.

    Before first flight of the day and after each refuelling, pullout strainer drain knob for about four seconds to clear fuel

    strainer of possible water and sediment. Check strainerdrain closed. If water is observed, the fuel system may

    contain additional water, and further draining of the systemat the strainer, fuel tank sumps, and fuel line drain plug will

    be necessary.

    Propeller and Spinner .................................................... CHECKfor nicks and security

    Carburettor Air Filter ...................................................... CHECKfor restrictions by dust or other foreign matter

    Landing Light ...................................................... ........... CHECK

    for condition and cleanlinessNose Wheel Strut and Tire ............................................ CHECK

    for proper inflationNose Tie-Down ................................................... DISCONNECTStatic Source Opening (left side of fuselage) ................ CHECK

    for stoppage

    LEFT WING

    Main Wheel Tire ................................................. ........... CHECKfor proper inflation

    Fuel tank sump .................................................... DRAINBefore first flight of the day and after each refuelling, use

    sampler cup and drain small quantity of fuel from fuel tanksump quick-drain valve to check for water, sediment and

    proper fuel grade.Fuel Quantity ............................................... CHECK VISUALLY

    for desired level

    Fuel Filler Cap .................................................... ......... SECUREPitot Tube Cover ................................................ ........ REMOVEPitot Tube Opening ................................. ...................... CHECK

    for stoppage

    Stall Warning Opening................................................... CHECKfor stoppage

    To check the system, place a clean handkerchief over thevent opening and apply suction; a sound from the warning

    horn will confirm system operation.

    Fuel Tank Vent Opening..................................... ........... CHECKfor stoppage

    Wing Tie-Down ................................................... DISCONNECT Aileron ........................................................ ................... CHECKfreedom of movement and security 

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    NORMAL CHECKLIST C150 

    BEFORE STARTING ENGINE

    Exterior Preflight ..................................................... COMPLETEPosition.......................................................................... . CLEARPapers ..................................................................... ON BOARDLoose Items ........................................................ ........ STOWEDSeats, Belts, Shoulder Harnesses .............. ADJUST and LOCKFuel Shutoff Valve ................................................................ ONRadios, Electrical Equipment ............................................... OFFBrakes ................................................................ TEST and SETCircuit breakers ....................................... .................. CHECK INStart Up (if applicable) .............................................. RECEIVEDBriefing ................................................................... COMPLETE

    STARTING ENGINE (Temperatures Above Freezing)

    Mixture............................................................................... RICHCarburettor Heat ............................................................ ... COLDMaster Switch ..................................................... .................. ONLights ................................................................................... SET Annunciators ...................................................... ........... CHECKPrime .......................................................... ....... AS REQUIRED

    (Up to 3 strokes)

    Throttle ............................................................. OPEN 1/4 INCHPropeller Area ............................................................... . CLEARIgnition Switch ......................................... ....................... START

    (Release when engine starts)

    Throttle ....................................................... .................. ADJUSTfor 1000 RPM or less

    Oil Pressure ........................................................ ........... CHECKStarter Warning Light (if installed) ...................................... OUT Alternator Output ........................................................... CHECK

    BEFORE TAXI

     Avionics .............................................................. ................. SETFlight Instruments .......................................................... ...... SETFlaps.............................................................................. UP SETTime .............................................................................. NOTED

    TAXI

    Brakes ...................................................................... CHECKEDGyro Instruments and Compass ............................... CHECKED

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    BEFORE TAKEOFF

    Parking Brake ..................................................... ................. SETCabin Doors ................................. ............................. LATCHEDFlight Controls ......................................... FREE and CORRECTFlight Instruments .......................................................... ...... SETElevator Trim ............................................................. TAKEOFFFuel Shutoff Valve ................................................................ ONMixture.................................................. RICH (below 3000 feet)Engine Instruments ....................................................... CHECKBack Area ........................................................... ............ CLEARBrakes ........................................................................... ...... SETThrottle .............................................................. ....... 1700 RPMMagnetos ............................................................ ........... CHECK

    (RPM drop should not exceed 150 RPM on either magnetoor 75 RPM differential between magnetos)

    Carburettor Heat ............................................................ CHECK(for RPM drop)

    Engine Instruments and Ammeter ................................. CHECK

    Suction Gage ...................................................... ........... CHECKThrottle ................................................................. CHECK IDLEThrottle .............................................................. 1000 RPM SETFlight instruments and Radios ............................................. SETFlashing Beacon, Navigation Lights and/or Strobe Lights...........................................................................ON as requiredThrottle Friction Lock .................................................... ADJUST

    Wing Flaps ............................................................................. 0 Brakes ....................................................................... RELEASE

    RUNWAY ITEMS 

    Pitot Heat ............................................................ .................. ONLights ................................................................................... SETCarburettor Heat ............................................................ ...... OFF

    Transponder ....................................................... ...... - - - - SETRunway heading ............................................................ CHECKTime .............................................................................. CHECKTake-Off Clearance(if applicable) ............................. RECEIVED

    TAKEOFF 

    NORMAL TAKE-OFFWing Flaps ..............................................................................0ºCarburettor Heat ............................................................ ... COLDThrottle ................................................................... FULL OPENElevator Control ..................... LIFT NOSE WHEEL (at 55 MPH)Climb Speed ....................................................... .... 70 - 80 MPH

    MAXIMUM PERFORMANCE TAKE-OFF

    Wing Flaps ............................................................................. 0°Carburettor Heat ............................................................ ... COLDBrakes ........................................................................... ... HOLDThrottle ................................................................... FULL OPENBrakes ....................................................................... RELEASEElevator Control ....................................... SLIGHTLY TAIL LOWClimb Speed ....................................................... ........... 70 MPH

    (with obstacles ahead)

    SHORT FIELD TAKE-OFFWing Flaps ........................................................................... 10°Carburettor Heat ............................................................ ... COLDBrakes ........................................................ .................... APPLYThrottle ................................................................... FULL OPENBrakes ....................................................................... RELEASEElevator Control ....................................... SLIGHTLY TAIL LOWClimb Speed ....................................................... ........... 70 MPH

    (Until all obstacles are cleared)

    Wing Flaps ................................................................ RETRACT

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    LANDING

    NORMAL LANDING Airspeed ................................................. 70-80 MPH (flaps UP)Wing Flaps ..... .......................... AS DESIRED (below 100 MPH) Airspeed ...........................................60-70 MPH (flaps DOWN)Touchdown ............................................ MAIN WHEELS FIRSTLanding Roll .......................... LOWER NOSE WHEEL GENTLYBraking ................................................... MINIMUM REQUIRED

    SHORT FIELD LANDING Airspeed .................................................. 70-80 MPH (flaps up)Wing Flaps ........................... .................... 30° (below 100 MPH) Airspeed ..................................................... MAINTAIN 70 MPHPower .............................................. ............................ REDUCE

    to idle as obstacle is cleared

    Touchdown ............................................ MAIN WHEELS FIRSTBrakes ............................................................ APPLY HEAVILYWing Flaps ..... ........................................................... RETRACT

    BALKED LANDINGThrottle .............................................................. .... FULL OPENCarburettor Heat ............................................................ ... COLDWing Flaps ..... ................................................. RETRACT to 20° Airspeed ............................................................. ........... 65 MPHWing Flaps ................................... ................. RETRACT(slowly)

    AFTER LANDING

    Pitot Heat ............................................................ ................. OFFLights ................................................................................... SETWing Flaps ........................... ................................................. UPCarburettor Heat ............................................................ ... COLDTransponder ....................................................... ........ - - - SET

    Time .............................................................................. CHECK

    SECURING AIRCRAFT

    Parking Brake ..................................................... ................. SETRadios, Electrical Equipment ............................................... OFFMixture............................................................... IDLE CUT OFF

    (Pulled full out)

     All Switches ........................................................ ................. OFFIgnition Switch ..................................................................... OFFMaster Switch ..................................................... ................. OFFFuel Shut Off Valve ....................................................... ...... SETControl Lock ................................................................ INSTALLWindows ............................................................. ......... CLOSEDTime .............................................................................. NOTED

    STALL

    Briefing ................................................................... COMPLETESafety Belts ........................................................ ..... FASTENEDLoose Items ........................................................ ........ STOWEDEngine Instruments ....................................................... CHECKCarburettor Heat ............................................................ ....... ONMixture............................................................................... RICH APOS ......................................................... ................... CHECK

    AFTER STALL

    Flaps.............................................................................. UP SETCarburettor Heat ............................................................ ...... OFFThrottle ................................................................ ....... - - - SETMixture........................................................................ - - - SETEngine Instruments ....................................................... CHECKDirectional Gyro ............................................................. CHECKOrientation .......................................................... ........... CHECK

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    5.2 EXPANDED NORMAL CHECKLIST C150: PH-RUD/NOD/HVP

    BEFORE STARTING ENGINE

    (This checklist shall be performed after checking the weather and the crew briefing and before start up.)  

    Exterior Preflight……………….  COMPLETE See AOM/POH supplemented as follows:  When removing control wheel

    lock, check free movement ofcontrols, and full travel of trim tab.

      If draining is applicable, drain firsttanks and then strainer.

      When turning master switch on,check proper working of beaconlight and if mandatory for flightalso landing light. For other lightsthe check at daily inspection issufficient.

    Position ..………………………..  CLEAR Check that the aircraft position is free ofobstacles and is free to taxi out to taxi-way. 

    Papers....................................... ON BOARD Check OM for mandatory papers. 

    Loose items ............................ STOWED No heavy objects shall be left loose to avoidrisk of injuries to the occupants or damageto the aircraft in turbulence or during airexercises.

    Seats, Belts, ShoulderHarnesses.................................. ADJUSTED and LOCK  Adjust  your seat and pedals in the same

    locked position. Check Shoulder Harnessesof all occupants are fastened.Make sure passengers know how to close,adjust and open the shoulder harnesses.

    Fuel Shutoff valve.................... ON

    Radios, Electrical Equipment. OFF

    Brakes……………………………  TEST AND SET

    Circuit breakers...................... CHECK IN Check that circuit breaker are in. Fuses onlyhave to be checked if one of the systems ismal functioning. The C152 and C150F havecircuit breakers only, the C150 has onecircuit breaker and further fuses. Circuitbreakers may not be reset.

    Start up (if applicable) RECEIVED If applicable.

    Briefing................................... COMPLETED

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    STARTING ENGINE (This checklist shall be performed just before engine start.)

    Mixture.................................... RICH

    Carburettor Heat.................... COLD Check carburettor heat is COLD.

    Master Switch………………….  ON

    Lights.......................... SET Set warning light for indicating starting up of

    engine or running engine. Set NAV lightsduring night or visibility less than 5000 m.

    Annunciators................... CHECK Check all annunciators working properly (ifpossible).  The starter warning light can beof the "push to test" type. Push the light on

    the brim, it will then illuminate. Releasingthe light will leave it out.When the starter warning light remains ONafter starting the engine immediately shutdown the engine.

    Prime...................................... AS REQUIRED Before the first flight of the day the first(Up to 3 strokes) stroke may only be half filled.

    Three strokes will be required for the firstflight of the day or if time betweensucceeding flights exceeds 1 hour,otherwise one stroke will be sufficient.Lock primer after priming.

    Throttle.................................... OPEN 1/2 INCH

    Propeller area........................ CLEAR

    Ignition switch………………….  START Turn starter key to "START", release as(Release when engine soon as the engine is picking up.Starts)  Starter engine operation is limited to

    30 seconds ON / 30 seconds OFF30 seconds ON / 30 seconds OFF30 seconds ON / 3 minutes OFF.

    Throttle.................…………...  ADJUSTFor 1000 RPM or less

    Oil pressure............................ CHECK Pressure indication should be rising withwarm temperature within 30 seconds, invery cold weather within 60 seconds.If pressure indication is not showing withinthis time, shut down the engine.

    Starter warning light ............. OUT Check starter warning light is OUT.(If installed) If starter warning light remains illuminated:

    shut down the engine.

    Alternator output................... CHECK Check ammeter shows load. If ammeter isstill indicating a discharge switch master

    switch OFF, both sides, and then ON again.If ammeter is still indicating a dischargeshut down the engine and inform OPS.

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    BEFORE TAXI(This checklist shall be performed after engine start en before taxi.)

    Avionics.................................... SET Avionics panel: Select intercom switch to "phone" if you are using headphones,

    otherwise select intercom switch to "speaker".The switches on the avionics panel have three positions:Speaker-OFF-PhoneSpeaker = UP, OFF = middle, Phone = down.Select mic-selector to COM-1 (there is only one com)Select COM to phoneSelect NAV OFFSelect ADF OFFSelect DME OFFSelect Marker OFF.

     Avionics Master Switch Select ONIf there is no avionics master switch, turn individual avionics ON.

    COM Select required COM station,Test volume with squelch button, adjust volume to desired audio level,Select a suitable stby. Frequency.

    NAV Select a NAV beacon. If you are receiving its signal on the ground:Identify the beacon: set NAV on the avionics panel to phone, checkmorse code, select NAV on avionics panel to OFF.Check current radial, turn course selector 10 degrees to the left andcheck full scale deflection to the left. Turn course selector 90 degreesto the left check TO/FROM change, select course selector 10 degrees

    to the right of centre radial, check still full scale deflection, to the right.Turn on to original radial, check indicated radial centred.If for first part of flight a radial shall be flown, select this radial.Select a suitable beacon as stby.

     ADF Select a NDB.Select ADF on the avionics panel to "phone" and adjust volume todesired audio level. Identify its morse code. Select ADF on avionicspanel OFF.Set ADF in ANT mode, check ADF pointer will go to 90 degreesparked position.Set ADF in ADF mode, check ADF pointer returns to current QDMthrough shortest way.

    Select NDB frequency for departure.

    DME Select a DME frequency.Select DME on avionics panel to "phone" and adjust volume to desiredaudio level. Identify its morse code. (might take some time!) SelectDME on avionics panel to OFF.

    Transponder Set transponder to designated frequency (if no designated frequencyreceived: set to VFR code) and STBY.

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    Flight instruments ................... SET Check OAT in accordance with ATIS.Check Air Speed Indicator indicates zero.Check Attitude indicator shows level flight.

    Check Altitude indicator shown field.elevation, set to QNH.Check Vertical Speed Indicator zero.Check Directional Gyro is aligned withcompass.Check Turn & Bank indicator shows no turn,ball in the middle if aircraft is on levelground.

    Flaps....................................... UP SET Select flaps UP in stages, check if flapposition stops work, or that flap-selectorstop works.

    Time........................................ NOTED This is the Off-blocks time to be noted in theaircraft journal.

    TAXI(This checklist items shall be performed during taxi. The checklist at the holding position beforethe run up.)

    Brakes.................................... CHECKED Check gently the brake pressure on thepedals, but do not stop the aircraft

    Gyro Instruments and Compass... CHECKED Try to make the turns during taxi-route.Check in a left turn the turn and bank

    indicator with needle to the left and ball tothe right. The Directional Indicator shouldbe decreasing and Compass decreasingand the Attitude Indicator should be steady.Visa Versa for the right turn.

    BEFORE TAKE-OFF 

    (This checklist shall be performed at the holding position, preferably into the wind just beforedeparture. If possible leave room for other aircraft to pass.)

    Parking Brake.......................... SET

    Cabin Doors…………………….  LATCHED

    Flight controls......................... FREE AND CORRECT  Yoke fully forward and left. Check leftaileron up and right aileron down.Check elevator down.Yoke fully forward and right. Check rightaileron up and left aileron down. Returnyoke to neutral.Pull yoke fully aft. Check elevator up.Check rudder free moving. Do not give fulldeflection on rudder since that would onlywear out the bungee system.

    Flight instruments ................... SET Perform a check on all flight instruments

    if they are set correct.

    Elevator Trim............................ TAKE-OFF Normal trim position is indicated with a line.In case of a forward centre of gravity trim

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    one stroke nose up, for a aft centre ofgravity trim one stroke nose down.

    Fuel Shutoff Valve………………  ON

    Mixture..................................... RICH (below 3000 feet) In case of high elevation airfield, see AOM/POH.

    Engine Instruments…………….  CHECK Check engine instruments stay in the greenarc.

    Back Area.................................. CLEAR Check that there are no aircraft, glider, orpeople standing on short distance behindyou.

    Brakes........……………………..  SET

    Throttle..................................... 1700 RPM

    Magnetos................................. CHECK (RPM drop should not exceed 150 RPMon either magneto or 75 RPM differentialbetween magnetos)C150 max drop 150 RPM, max diff 75 RPMCheck first right, then left magnetoSelect Magnetos to BOTH after test.

    Carburettor heat....................... CHECK (for RPM drop) Select carburettor heat ON and leave ONfor 20-30 seconds. Note drop in RPM.In case of icing the RPM will increase.

    Leave carb. heat ON until rpm remainsstable

    Engine Instruments and Ammeter CHECK Check engine instruments stay in the green

    arc.Check ammeter is indicating a needle widthabove zero. Battery should normally becharged by now.If in doubt check proper alternator functionby switching ON the landing light for3 to 5 seconds. The ammeter will remain

    within a needle width of its original position.If ammeter is still indicating a marked

    charge, or shows a significant drop whenlanding light is ON either alternator and/orbattery has a malfunction.

    Suction Gage............................ CHECK Suction indication should indicate between4,6 to 5,4 inches of mercury.If indication is below 4,6 expect AI and DGto malfunction.

    Throttle …………………………  CHECK IDLE Check idle RPM between approximately500 and 800 RPM. RPM values above 1000are not to be accepted.

    Throttle…………………………..  1000 RPM SET

    Flight instruments and Radios........SET

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    Flashing Beacon, Navigation

    Lights And/or Strobe Lights..... ON as required Flashing Beacon on, strobe lights on,Navigation lights on when visibility becomesless than 5000 m.

    Throttle friction Lock.............. ADJUST Set friction so that you can easily move thethrottle, but it will not move by itself.

    Wing flaps............................... 0 

    Brakes........……………………..  RELEASE

    RUNWAY ITEMS

    (These checklist items shall be performed by memory. In case of single pilot operation theseitems shall be performed standing still. Line up clearance(if applicable) must be received.)

    Pitot heat................................. ON Pitot heat should be on during flight

    Lights....................................... SET Select taxi light off, landing light ON, strobelights ON

    Carburettor heat..................... OFF

    Transponder ........................... - - - SET Select transponder to ALT, if applicable

    Runway heading..................... CHECK Check compass indicating + published

    runway magnetic track and DG still aligned

    with compass.

    Time......................................... CHECK Start timer .  At this time your flight plan willbe activated the start of the navigation plan.Note time when circumstances permit.

    Take-off clearance.................. RECEIVED If applicable.

    TAKE-OFF

    (This checklist shall be performed by memory during take-off.)

    NORMAL TAKE-OFFWing flaps……………………..  0˚ 

    Carburettor Heat……………..  COLD

    Throttle………………………...  FULL OPEN

    Elevator Control……………...  LIFT NOSE WHEEL at 55 MPH

    Climb speed…………………..  70 – 80 MPH

    MAXIMUM PERFORMANCE TAKE-OFFWing Flaps................................ 0°

    Carburettor Heat..................... COLD

    Brakes....................................... APPLY

    Throttle..................................... FULL OPEN

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    Engine instruments................ CHECK Check oil pressure and oil temperatureindications are within green arc.

    Throttle..................................... FULL OPEN

    Mixture ..................................... RICH Lean according POH.

    Landing light............................ SET Normally off, but Subject CaptainsDiscretion.

    CRUISE(This checklist shall be performed after levelling off for cruise.)

    Engine instruments................ CHECKED Check oil pressure and oil temperatureindications are within green arc.

    Power…………………………….  1900 to 2550 RPM(No more than 75%)

    Elevator Trim…………………….  ADJUST

    Mixture..................................... LEAN For airwork exercise mixture will be rich.

    Otherwise mixture should be leanedaccording AOM/POH.

    Fuel Quantity…………………… CHECK Check remaining fuel with calculated fuel 

    Directional Gyro...................... CHECK Check DG is aligned with compass.

    DESCENT(This checklist shall be performed after starting a descent.) Altimeter................................. SET When descending to an altitude set

    altimeter to local or regional QNH.

    Engine instruments............... CHECKED Check oil pressure and oil temperatureindications are within green arc.

    Mixture.................................... SET When flying with lean mixture enrich mixture

    during descend. Often it will be possible toselect full rich. When starting descent from

    high altitude, selecting full rich mixturemight cause rough running engine.

    Carburettor Heat...................... ON Select carburettor heat ON whenever you

    fly at low RPM settings

    BEFORE LANDING(This checklist shall be performed when cleared to an altitude (if applicable) and inbound for a landing.

    Items may be delayed until on final, but must be completed before reaching 500’ AAL. During circuit training Stella items must be omitted, except for the items “ENGINE INSTRUMENTS”, “BRIEFING” and “FLAPS”.) 

    Altimeter................................. - - - SET Set altimeter to local QNH or to regionalQNH.

    Directional Gyro...................... CHECK Check DG is aligned with compass.

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    Engine instruments.............. CHECK Check oil pressure and oil temperatureindications are within green arc.

    Seats, Belts, Harnesses……...  ADJUST AND LOCK

    Mixture.................................... RICH

    Carburettor heat..................... ON Selecting carburettor heat ON reduces rpm(Apply full heat before with approximately 100 rpm. Reset throttleClosing throttle) to desired rpm.

    Landing light.......................... ON

    Briefing………………………….  COMPLETED

    (The check of the items below shall be completed when established on final)

    Flaps.......................................... - - - SET The check of this item shall be performedwhen established on final

    LANDING(This checklist shall be performed by memory during landing.)

    NORMAL LANDING

    Airspeed ..................................... 70-80 MPH (flaps UP)

    Wing Flaps.................... AS DESIRED (below 100 MPH)

    Airspeed ................................. 60-70 MPH (flaps down)

    Touchdown ................................ MAIN WHEELS FIRST

    Landing Roll .............. LOWER NOSE WHEEL GENTLY

    Braking ........................................ MINIMUM REQUIRED

    SHORT FIELD LANDING

    Airspeed ...................................... 70-80 MPH (flaps up)

    Wing Flaps.................................... 30° (below 100 MPH)

    Airspeed .......................................... MAINTAIN 70 MPH

    Power .............. REDUCE to idle as obstacle is cleared

    Touchdown ................................ MAIN WHEELS FIRST

    Brakes .................................................. APPLY HEAVILY

    Wing Flaps...................................................... RETRACT

    BALKED LANDING

    Throttle ....................................................... FULL OPEN

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    Carburettor Heat ................................................... COLD

    Wing Flaps........................................... RETRACT to 20°

    Airspeed ............................................................. 65 MPH

    Wing Flaps......................................... RETRACT(slowly)

    AFTER LANDING

    (This checklist shall be performed by memory after vacating the runway. The checklist may beperformed rolling during single pilot operations but on straight taxiways only. The checklist shallthen be read when on the parking position.)

    Pitot heat................................ OFF

    Lights...................................... SET Select landing light OFF.Taxi light ON if so required. If no taxi light isavailable, use landing light instead.Navigation lights OFF, during night orvisibility less than 5000m navigation lightsremain ON.Strobe lights OFF

    Wing Flaps............................. UP

    Carburettor heat.................... COLD

    Transponder.......................... SET Normally select transponder to STBY, if

    applicable

    Time......................................... NOTED Note time as end of flight.

    SECURING AIRCRAFTThis checklist shall be performed when on parking position.)

    Parking brake ........................ SET

    Radios, Electrical equipment. OFF

    Mixture................................... IDLE CUT OFF

    (Pull full out)

    All switches........................... OFF Except master switch.

    Ignition Switch…………………  OFF Before switching OFF ignition switch waituntil propeller has stopped and take keyout. 

    Master Switch......................... OFF

    Fuel Shut Off Valve…………….  - - - SET

    Control lock............................ INSTALL Install control lock with red flap before theignition switch.

    Windows................................... CLOSED Windows and doors shall be closed when

    leaving the aircraft

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    Time........................................ NOTED This is your ON BLOCK time and be notedin the aircraft journal.

    PRE STALL(This checklist shall be performed after the stall briefing and just before the (stall) exercise.)

    Briefing.................................. COMPLETE

    Safety belts........................... FASTENED

    Loose items………………….  STOWED

    Engine instruments............. CHECKED Check oil pressure and oil temperatureindications are within green arc.

    Carburettor heat................... ON

    Mixture.................................. RICH

    APOS……..............................  CHECKED

    AFTER STALL(This checklist shall be performed when stabilized on altitude/level after the (stall) exercise.)

    Flaps.................................... UP SET

    Carburettor Heat................. OFF

    Throttle............................... SET Set throttle to cruise rpm.

    Mixture................................ SET

    Engine instruments........... CHECK Check oil pressure and oil temperatureindications are within green arc.

    Directional Gyro................. CHECK Check DG aligned with compass.

    Orientation......................... CHECK Check position and direction.

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    INTENTIONALLY LEFT BLANK

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    5.3 CESSNA 152: PH-JVB/CDS/STQ/WEE

    PREFLIGHT INSPECTION

    Note:

    Visually check airplane for general condition during walk-around inspection. In cold weather, remove evensmall accumulations of frost, ice or snow from wing, tail and control surfaces.

     Also, make sure that control surfaces contain no internal accumulations of ice or debris. Prior to flight,check that pitot heater (if installed) is warm to touch within 30 seconds with battery and pitot heat switcheson.

    If a night flight is planned, check operation of all lights, and make sure a flashlight is available.

    CABIN

    Control Wheel Lock .................................................... REMOVEIgnition Switch ..................................................................... OFFMaster Switch ..................................................... .................. ONFuel Quantity Indicators.............................. CHECK QUANTITYMaster Switch ..................................................... ................. OFFFuel Shutoff Valve ................................................................ ON

    EMPENNAGE

    Rudder Gust Lock ................................... ................... REMOVETail Tie-Down ..................................................... DISCONNECTControl Surfaces ............................................................ CHECK

    freedom of movement and security 

    RIGHT WING

     Aileron ........................................................ ................... CHECKfreedom of movement and security

    Wing Tie-Down ................................................... DISCONNECTMain Wheel Tire ................................................. ........... CHECK

    for proper inflation

    Fuel Tank Sump Quick Drain Valve ................................ DRAINBefore first flight of the day and after each refuelling, use

    sampler cup and drain small quantity of fuel from fuel tanksump quick-drain valve to check for water, sediment and

    proper fuel grade.

    Fuel Quantity .............................................. CHECK VISUALLYfor desired level

    Fuel Filler Cap .................................................... ......... SECURE

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    NOSE

    Engine Oil Level ................................................. ........... CHECKdo not operate with less than four quarts. Fill to six quarts

    for extended flight.Strainer Drain Knob ....................................................... .... PULL

    to clear water and sedimentBefore first flight of the day and after each refuelling, pull

    out strainer drain knob for about four seconds to clear fuelstrainer of possible water and sediment. Check strainerdrain closed. If water is observed, the fuel system may

    contain additional water, and further draining of the systemat the strainer, fuel tank sumps, and fuel line drain plug will

    be necessary.

    Propeller and Spinner .................................................... CHECKfor nicks and security

    Carburettor Air Filter ...................................................... CHECKfor restrictions by dust or other foreign matter

    Landing Light(s) ............................................................. CHECK

    for condition and cleanlinessNose Wheel Strut and Tire ............................................ CHECK

    for proper inflationNose Tie-Down ................................................... DISCONNECTStatic Source Opening (left side of fuselage) ................ CHECK

    for stoppage 

    LEFT WING

    Main Wheel Tire ................................................. ........... CHECKfor proper inflation

    Fuel Tank Sump ................................................. ............. DRAINBefore first flight of the day and after each refuelling, use

    sampler cup and drain small quantity of fuel from fuel tanksump quick-drain valve to check for water, sediment and

    proper fuel grade.Fuel Quantity ............................................... CHECK VISUALLY

    for desired level

    Fuel Filler Cap .................................................... ......... SECUREPitot Tube Cover ................................................ ........ REMOVEPitot Tube Opening ................................. ...................... CHECK

    for stoppage

    Stall Warning Opening................................................... CHECKfor stoppage

    To check the system, place a clean handkerchief over thevent opening and apply suction; a sound from the warning

    horn will confirm system operation.

    Fuel Tank Vent Opening..................................... ........... CHECKfor stoppage

    Wing Tie-Down ................................................... DISCONNECT Aileron ........................................................ ................... CHECKfreedom of movement and security 

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    NORMAL CHECKLIST 

    BEFORE STARTING ENGINE

    Preflight Inspection ................................................. COMPLETEPosition.......................................................................... . CLEARPapers ..................................................................... ON BOARDLoose Items ........................................................ ........ STOWEDSeats, Belts, Shoulder Harnesses .............. ADJUST and LOCKFuel Shutoff Valve ................................................................ ONRadios, Electrical Equipment ............................................... OFFBrakes ................................................................ TEST and SETCircuit Breakers ......................................................... CHECK INStart Up (if applicable) .............................................. RECEIVEDBriefing ................................................................... COMPLETE

    STARTING ENGINE (Temperatures Above Freezing)

    Mixture............................................................................... RICHCarburettor Heat ............................................................ ... COLDPrime .......................................................... ....... AS REQUIRED

    (Up to 3 strokes)

    Throttle ............................................................. OPEN 1/2 INCHPropeller Area ............................................................... . CLEARMaster Switch ..................................................... .................. ONLights ................................................................................... SET Annunciators ...................................................... ........... CHECKIgnition Switch ......................................... ....................... START

    (Release when engine starts)

    Throttle ....................................................... .................. ADJUSTfor 1000 RPM or less

    Oil Pressure ........................................................ ........... CHECKStarter Warning Light (if installed) ...................................... OUT Alternator Output ........................................................... CHECK

    BEFORE TAXI

     Avionics .............................................................. .................. ONFlight Instruments .......................................................... ...... SETFlaps.............................................................................. UP SETTime .............................................................................. NOTED

    TAXI

    Brakes ...................................................................... CHECKEDGyro Instruments and Compass ............................... CHECKED

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    BEFORE TAKEOFF

    Parking Brake ..................................................... ................. SETCabin Doors ........................................CLOSED and LATCHEDFlight Controls ......................................... FREE and CORRECTFlight Instruments .......................................................... ...... SETFuel Shutoff Valve ................................................................ ONMixture.................................................. RICH (below 3000 feet)Elevator Trim ............................................................. TAKEOFFEngine Instruments ....................................................... CHECKBack Area ........................................................... ............ CLEARThrottle .............................................................. ....... 1700 RPMMagnetos ............................................................ ........... CHECK

    (RPM drop should not exceed 125 RPM on either magnetoor 50 RPM differential between magnetos)

    Carburettor Heat ............................................................ CHECK(for RPM drop)

    Engine Instruments and Ammeter ................................. CHECKSuction Gage ...................................................... ........... CHECK

    Throttle ................................................................ ............... IDLEThrottle .............................................................. 1000 RPM SETRadios ........................................................................... ...... SETFlashing Beacon, Navigation Lights and/or Strobe Lights...........................................................................ON as requiredThrottle Friction Lock .................................................... ADJUSTFlaps........................................................................... - - - SETBrakes ....................................................................... RELEASE

    RUNWAY ITEMS

    Pitot Heat ............................................................ .................. ONLights ................................................................................... SETCarburettor Heat ............................................................ ...... OFFTransponder ....................................................... ........ - - - SET

    Runway Heading ........................................................... CHECKTime .............................................................................. CHECKTake-Off Clearance (if applicable) ............................ RECEIVED

    TAKEOFF 

    NORMAL TAKE-OFFWing Flaps .................................................................... . 0º - 10ºCarburettor Heat ............................................................ ... COLDThrottle ................................................................... FULL OPENElevator Control ........................ LIFT NOSE WHEEL at 50 KIASClimb Speed ........................................................... 65 - 75 KIAS

    SHORT FIELD TAKE-OFF

    Wing Flaps ........................................................................... 10°Carburettor Heat ............................................................ ... COLDBrakes ........................................................ .................... APPLYThrottle ................................................................... FULL OPENMixture............................................................................... RICH

    (Above 3000’, LEAN to obtain maximum RPM) Brakes ....................................................................... RELEASEElevator Control ....................................... SLIGHTLY TAIL LOWClimb Speed ....................................................... ........... 54 KIAS

    (Until all obstacles are cleared)

    Wing Flaps ..... ........................................................... RETRACTslowly after reaching 60 KIAS

    AFTER TAKEOFF

    Engine Instruments ....................................................... CHECKCarburettor Heat ............................................................ ...... OFFThrottle .............................................................................. FULLFlaps.............................................................................. UP SET

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    ENROUTE CLIMB

     Altimeter ............................................................. ......... - - - SET Airspeed ............................................................. .... 70 - 80 KIAS

    NOTE:If a maximum performance climb is necessary, use speedsshown in the Rate of Climb chart in POH section 5

    Engine Instruments ....................................................... CHECKThrottle ................................................................... FULL OPENMixture..................................................... RICH below 3000 feet

    LEAN for maximum RPM above 3000 feet

    Landing Light ...................................................... ......... - - - SET 

    CRUISE

    Engine Instruments ....................................................... CHECKPower ............................................................ 1900 – 2550 RPM

    (No more than 75%)

    Elevator Trim ................................................................ ADJUSTMixture.............................................................................. LEANFuel Quantity ................................................................. CHECKDirectional Gyro ............................................................. CHECK

    DESCENT

     Altimeter ............................................................. ........ - - - SETEngine Instruments ....................................................... CHECKMixture ................................. ............................................... SETCarburettor Heat ............................................................ ....... ON

    BEFORE LANDING 

     Altimeter ............................................................. ........ - - - SET

    Directional Gyro ............................................................. CHECKEngine Instruments........................................................ CHECKSeats, Belts, Harnesses ............................ ADJUST AND LOCKMixture........................................................ ....................... RICHCarburettor Heat ............................................................ ....... ON

    (Apply full heat before closing throttle)

    Landing light ......................................................................... ONBriefing ................................................................ .COMPLETEDFlaps ........................................................... ................. - - - SET

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    5.4 EXPANDED NORMAL CHECKLIST C152: PH-JVB/CDS/STQ/WEE

    BEFORE STARTING ENGINE

    (This checklist shall be performed after checking the weather and the crew briefing and before start up.)

    Preflight Inspection...………….  COMPLETE See AOM/POH supplemented as follows:  When removing control wheel

    lock, check free movement ofcontrols, and full travel of trim tab.

      If draining is applicable, drain firsttanks and then strainer.

      When turning Master Switch on,check proper working of beaconlight and if mandatory for flightalso landing light. For other lightsthe check at daily inspection issufficient.

    Position ..………………………..  CLEAR Check that the aircraft position is free ofobstacles and is free to taxi out to taxi-way. 

    Papers....................................... ON BOARD See OM for mandatory papers on board.

    Loose items ............................ STOWED No heavy objects shall be left loose to avoidrisk of injuries to the occupants or damageto the aircraft in turbulence or during airexercises.

    Seats, Belts, Shoulder Harnesses ADJUSTED and LOCK  Adjust  your seat and pedals in the samelocked position. Check Shoulder Harnessesof all occupants are fastened.Make sure passengers know how to close,adjust and open the shoulder harnesses.

    Fuel Shutoff Valve...................... ON

    Radios, Electrical Equipment... OFF

    Brakes……………………………  TEST AND SET

    Circuit Breakers.......................... CHECK IN Check that circuit breaker are in. Fuses onlyhave to be checked if one of the systems ismal functioning. The C152 and C150F havecircuit breakers only, the C150 has onecircuit breaker and further fuses. Circuitbreakers may not be reset.

    Start up (if applicable).………  RECEIVED If applicable

    Briefing................................... COMPLETED

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    STARTING ENGINE (This checklist shall be performed just before engine start.)

    Mixture.................................... RICH

    Carburettor Heat..................... COLD Check carburettor heat is COLD.

    Prime...................................... AS REQUIRED Before the first flight of the day the firststroke may only be half filled.Three strokes will be required for the firstflight of the day or if time betweensucceeding flights exceeds one hour,otherwise one stroke will be sufficientLock primer after priming.

    Throttle.................................... OPEN 1/2 INCH

    Propeller Area......................... CLEAR

    Master switch……………………  ON

    Lights.......................... SET Set warning light for indicating starting up ofengines or running engines. Set NAV lightsduring night or visibility less than 5000 m.

    Annunciators CHECK Check all annunciators working properly (if

    possible). The starter warning light is of the"push to  test" type. Push the light on thebrim, it will then illuminate. Releasing the

    light will leave it out.When the starter warning light remains ONafter starting the engine immediately shutdown the engine.

    Ignition switch………………….  START Turn starter key to "START", release assoon as the engine is picking up.Starter engine operation is limited to30 seconds ON / 30 seconds OFF30 seconds ON / 30 seconds OFF30 seconds ON / 3 minutes OFF.

    Throttle.................…………...  ADJUST 1000 RPM or less.

    Oil pressure............................ CHECK Pressure indication should be rising withwarm temperature within 30 seconds, invery cold weather within 60 seconds.If pressure indication is not showing withinthis time, shut down the engine.

    Starter warning light ............. OUT Check starter warning light is OUT.(if installed) If starter warning light remains illuminated:

    shut down the engine.

    Alternator Output................... CHECK Check ammeter shows load. If ammeter isstill indicating a discharge switch master

    switch OFF, both sides, and than ON again.If ammeter is still indicating a dischargeshut down the engine and inform OPS.

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    BEFORE TAXI(This checklist shall be performed after engine start en before taxi.)

    Avionics.................................... ON Avionics panel: Select intercom switch to "phone" if you are using headphones,

    otherwise select intercom switch to "speaker".The switches on the avionics panel have three positions:Speaker-OFF-PhoneSpeaker = UP, OFF=middle, Phone = down.Select mic-selector to COM-1 (there is only one com)Select COM to phoneSelect NAV OFFSelect ADF OFFSelect DME OFFSelect Marker OFF.

     Avionics Master Switch Select ONIf there is no Avionics Master switch, turn individual avionics ON.

    COM Select required COM stationTest volume with squelch button, adjust volume to desired audio level.Select a suitable stby. frequency

    NAV Select a NAV beacon. If you are receiving its signal on the ground:Identify the beacon: set NAV on the avionics panel to phone, checkmorse code, select NAV on avionics panel to OFF.Check current radial, turn course selector 10 degrees to the left andcheck full scale deflection to the left. Turn course selector 90 degreesto the left check TO/FROM change, select course selector 10 degrees

    to the right of centre radial, check still full scale deflection, to the right.Turn on to original radial, check indicated radial centred.If for first part of flight a radial shall be flown, select this radial.Select a suitable beacon as stby.

     ADF Select a NDB.Select ADF on the avionics panel to "phone" and adjust volume todesired audio level. Identify its morse code. Select ADF on avionicspanel OFF.Set ADF in ANT mode, check ADF pointer will go to 90 degreesparked position.Set ADF in ADF mode, check ADF pointer returns to current QDMthrough shortest way.

    Select NDB frequency for departure.

    DME Select a DME frequency.Select DME on avionics panel to "phone" and adjust volume to desiredaudio level. Identify its morse code. (might take some time!) SelectDME on avionics panel to OFF.

    Transponder Set transponder to designated frequency (if no designated frequencyreceived: set to VFR code) STBY.

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    Flight instruments ................... SET Check OAT in accordance with ATIS.Check Air Speed Indicator indicates zero.Check Attitude indicator shows level flight.

    Check Altitude indicator shown field.elevation, set to QNH.Check Vertical Speed Indicator zero.Check Directional Gyro is aligned withcompass.Check Turn & Bank indicator shows no turn,ball in the middle if aircraft is on levelground.

    Flaps....................................... UP SET Select flaps UP in stages, check if flapposition stops work, or that flap-selectorstop works.

    Time........................................ NOTED This is the Off-blocks time to be noted in theaircraft journal.

    TAXI(This checklist items shall be performed during taxi. The checklist at the holding position beforethe run up.)

    Brakes.................................... CHECKED Check gently the brake pressure on thepedals, but do not stop the aircraft

    Gyro instruments and Compass CHECKED Try to make the turns during taxi-route.Check in a left turn the turn and bankindicator with needle to the left and ball to

    the right. The Directional Indicator shouldbe decreasing and Compass decreasingand the Attitude Indicator should be steady.Visa Versa for the right turn.

    BEFORE TAKE-OFF (This checklist shall be performed at the holding position, preferably into the wind just beforedeparture. If possible leave room for other aircraft to pass.)

    Parking Brake.......................... SET

    Cabin Doors…………………….  CLOSED and LATCHED

    Flight Controls......................... FREE AND CORRECT  Yoke fully forward and left. Check leftaileron up and right aileron down.Check elevator down.Yoke fully forward and right. Check rightaileron up and left aileron down. Returnyoke to neutral.Pull yoke fully aft. Check elevator up.Check rudder free moving. Do not give fulldeflection on rudder since that would onlywear out the bungee system.

    Flight Instruments……………...  SET

    Fuel Shutoff Valve………………  ON

    Mixture..................................... RICH (below 3000 ft) In case of high elevation airfield, see AOM/POH.

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    Elevator Trim............................ TAKE-OFF Normal trim position is indicated with a line.In case of a forward centre of gravity trimone stroke nose up, for a aft centre of

    gravity trim one stroke nose down.Engine Instruments…………….  CHECK Check engine instruments stay in the greenarc.

    Back area.................................. CLEAR Check that there are no aircraft, glider, orpeople standing on short distance behindyou.

    Throttle 1700 RPM

    Magnetos................................. CHECK C152 max drop 125 rpm, max diff 50 RPMCheck first right, then left magnetoSelect Magnetos to BOTH after test.

    Carburettor heat....................... CHECK Select carburettor heat ON and leave ONfor 20-30 seconds. Note drop in RPM.In case of icing the RPM will increase.Leave carburettor heat ON until RPMremains stable.

    Engine Instruments andAmmeter.................................... CHECK Check engine instruments stay in the green

    arc.

    Suction Gage............................ CHECK Suction indication should indicate between4,6 to 5,4 inches of mercury.

    If indication is below 4,6 expect AI and DGto malfunction. Malfunction of gyro suctionshall be reported to operations.

    Throttle …………………………  IDLE Check idle rpm between approximately500 and 800 RPM.RPM values above 1000 are not to beaccepted. Return to home base. Informoperations.

    Throttle…………………………..  1000 RPM SET

    Radios SET

    Flashing Beacon, NavigationLights and/or Strobe Lights.... ON as required

    Throttle friction lock............... ADJUST Set friction so that you can easily move thethrottle, but it will not move by itself.

    Flaps………..............................  - - - SET 

    Safety belts………………………  FASTENED

    Briefing...................................... COMPLETED Brief amendments by ATC.

    Brakes……………………………..  RELEASE

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    RUNWAY ITEMS(These checklist items shall be performed by memory. In case of single pilot operation theseitems shall be performed standing still. Line up clearance(if applicable) must be received.)

    Pitot heat................................. ON Pitot heat should be on during flight

    Lights....................................... SET Select taxi light off, landing light ON, strobelights ON

    Carburettor heat...................... OFF

    Transponder ........................... - - - SET Select transponder to ALT, if applicable(= mode A + C).

    Runway Heading..................... CHECK Check compass indicating + publishedrunway magnetic track and DG still aligned

    with compass.

    Time......................................... CHECK Start timer . At this time your flight plan willbe activated the start of the navigation plan.Note time when circumstances permit.

    Take-off clearance.................. RECEIVED(If applicable)

    TAKE-OFF(This checklist shall be performed by memory during take-off.)

    NORMAL TAKE-OFF

    Wing flaps……………………..  0˚-10˚ 

    Carburettor Heat……………..  COLD

    Throttle………………………...  FULL OPEN

    Elevator Control……………...  LIFT NOSE WHEEL (at 50 KIAS)

    Climb speed…………………..  65-75 KIAS

    SHORT FIELD TAKE-OFF

    Wing flaps……………………..  10˚ 

    Carburettor Heat……………..  COLD

    Brakes …………………………  APPLY

    Throttle…………………………  FULL OPEN

    Elevator Control……………...  SLIGHTLY TAIL LOW

    Climb speed…………………..  54 KIAS

    Wing Flaps…………………….  RETRACT Slowly after reaching 60 KIAS 

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    DESCENT(This checklist shall be performed after starting a descent.) Altimeter................................. SET When descending to an altitude set

    altimeter to local or regional QNH.

    Engine instruments............... CHECKED Check oil pressure and oil temperatureindications are within green arc.

    Mixture.................................... SET When flying with lean mixture enrich mixtureduring descend. Often it will be possible toselect full rich. When starting descent fromhigh altitude, selecting full rich mixturemight cause rough running engine.

    Carburettor heat...................... ON Select carburettor heat ON whenever youfly at low RPM settings .

    BEFORE LANDING(This checklist shall be performed when cleared to an altitude (if applicable) and inbound for a landing.Items may be delayed until on final, but must be completed before reaching 500’ AAL. During circuit training Stella items must be omitted, except for the items “ENGINE INSTRUMENTS”, “BRIEFING” and  “FLAPS”.) 

    ATIS......................................... RECEIVED Make sure the complete ATIS is receivedbefore entering the CTR or at least 5minutes before starting the approach.

    Altimeter................................. - - - SET Set altimeter to local QNH or to regionalQNH.

    Directional gyro..................... CHECK DG is aligned with compass.

    Engine instruments.............. CHECK Check oil pressure and oil temperature

    indications are within green arc.

    Seats, Belts, Harnesses……...  ADJUST AND LOCK

    Mixture.................................... RICH

    Carburettor heat.................... ON Selecting carburettor heat ON reduces rpm(Apply full heat with approximately 100 rpm. Reset throttleBefore closing throttle) to desired rpm.

    Landing light.......................... ON

    Briefing………………………….  COMPLETED

    (The check of the items below shall be completed when established on final)

    Flaps.......................................... - - - SET The check of this item shall be performed

    when established on final

    LANDING(This checklist shall be performed by memory during landing.)

    NORMAL LANDING 

    Airspeed……………………….  60-70 KIAS (flaps up)

    Wing Flaps....…………………  AS DESIRED (below 85 KIAS)

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    Airspeed……………………….  55-65 KIAS (flaps up)

    Touchdown……………………  MAIN WHEEL FIRST

    Landing Roll………………….  LOWER NOSE WHEEL GENTLY

    Braking………………………...  MINIMUM REQUIRED

    SHORT FIELD LANDING 

    Airspeed……………………….  60-70 KIAS (flaps up)

    Wing Flaps....…………………  30˚ 

    Airspeed……………………….  MAINTAIN 54 KIAS (flaps up)

    Power…………………………..  REDUCE

    Touchdown……………………  MAIN WHEEL FIRST

    Braking………………………...  APPLY HEAVILY

    Wing Flaps…………………….  RETRACT

    BALKED LANDING 

    Throttle…………………………  Full open

    Carburettor Heat........………..  COLD

    Wing Flaps…………………….  RETRACT TO 20˚ 

    Airspeed……………………….  65 MPH

    Wing Flaps…………………….  RETRACT (slowly)

    AFTER LANDING(This checklist shall be performed by memory after vacating the runway. The checklist may beperformed rolling during single pilot operations but on straight taxiways only. The checklist shallthen be read when on the parking position.)

    Pitot heat................................ OFF

    Lights...................................... SET Select landi