Cessna 150 Aerobat 1975 Owner'S Manual Download | Manualshive

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Summary of Contents for 150 Aerobat 1975

Page 1: ...SHIELD Cessna 0 Nj MORE PEOPLE BUY AND FLY CESSNA AIRPLANES THAN ANY OTHER MAKE MODEI 1975 A AUSTRALIANJETCHARTER MsmSSF Mms BATCHNUMBER AJC AJR12 CESSNA AIRCRAFT COMPANY WICHITA KANSAS WORLD S LARGES...

Page 2: ...either for b sinesTor plells ure auplLeasaLnti aon Sr experience O SMa mal tos b enJprepared as a euidetohelPyoueetthe most pleasure Md utm fromyourl5 AMObat Itcontainsinformationab i yourC essmT e t...

Page 3: ...obeuB Msare mstaued 3 PRINCIPAL DIMENSIONS 8 6 MAX SECTION I SECTION II SECTION III TABLE OF CONTENTS Page OPERATING CHECKLIST 1 1 DESCRIPTION AND OPERATING DETAILS ___ _ 2 1 AEROBATIC MANEUVERS 3 1 S...

Page 4: ...flieht7A mo c onven plaLst e s d cu il stowed themapcompartmen checkingthat all important procedures have been sm cevlgilancefor other traffic is so important mcrowde7twmil nall air asl u is imPortant...

Page 5: ...main wheel tirefor proper inflation Beforlnrstflight ofdayand aftereach refueling use up anddrain sma11 qumtity offueifrom fuel tMk sump quTck drram alve to_check for water sediment dprope7fu l4g Visu...

Page 6: ...CHECK for RPMdrop 7 8 9 a on either magneto or 75 RFM different b Carburetor Heat CHECK for c Engine Instruments and Ammeter d Suction Gage CHECK Flight Instruments and Radios SET Throttle Friction L...

Page 7: ...5 MPH Wing Flaps RETRACT slowly NORMAL LANDING w Touchdown MAIN WHEELS FIRST landing Roll LOWER NOSE WHEEL GENTLY Braking MINIMUM REQUIRED u AFTER LANDING 1 Wing Flaps UP 2 Carburetor Heat COLD SECURI...

Page 8: ...trol Knob T hrotlle withFri tiBnLock 26 Microphone Opt 27 Elevator Trim ControI Wheel 3 carburetorJHeatControl Knot Electrical Switches 30 Fuses 31 Radio Dial Light Rheostat 32 Panel Lights Rheostai 3...

Page 9: ...URETOR TO ENGINE CYLINDERS MIXTURE CONTROL KNOB Figure 2 2 2 2 FUEL QUANTITY DATA U S GALLONS TANKS TWO STANDARD WING 13 GAL EACH TWO LONG RANGE WING 19 GAL EACH USABLE FUEL ALL FLIGHT CONDITIONS 22 5...

Page 10: ...N LIGHTS AND OPTIONAL CONTROL WHEEL MAP IIGHT TO TRANSMITTE8 RELAY NAV DOME STARTEB CONTACTOB BATTCRY CONTACTOR A R f BATTERY GROUND 5EBVICE PLUG BECEPTACLE OPT IGNITION SWITCH TO WING FLAP FUSE G i k...

Page 11: ...I K ttTSL f wm de u altel ese_li ti ert Soff th nL thesmtches for replace the NAV JD6MET atrerSd it tLi te ci per mit its us e omtSntoo etn lt hltran mltter rela7M untilthema n c tio7haTbeuernnc onrS...

Page 12: ...cip ul theJrnobI70r nd as ga thrs ksYsh esc ed Th c atto eup h tpo Uona L Tf inoendthpTon turnihe back of the The back ofthe s7ats wil l Ifoo n b ottomedge ofthe back aiTto sTowinro S Tc SHOULDER HARN...

Page 13: ...USE UP AILERON ON LH WING AND NEUTRAL ELEVATOR USE UP AILERON ON RH WING AND NEUTRAL ELEVATOR USE DOWN AILERON ON LH WING AND DOWN ELEVATOR USE DOWN AILERON ON RH WING AND DOWN ELEVATOR CODE WIND Dff...

Page 14: ...ernat dc TAKE OFF POWER CHECKS i3 s xu e a s tte oica fo di s K sl shM Ma el r lustifiedinmaking th gh f3hI tttiTe 2L uthls occurs youar e to r s T to r 2 12 ESSt t b c b blownback oTth p7opeUelrTa Mt...

Page 15: ...ds alcft informatTon determine the most favorable altitude and power settingYor agiven trip To achive the lean mixture fuel consumption figures shown in Section VII the mixture should be leaned as fol...

Page 16: ...40 flaps u su Vn l eg Tato er alra csStly r le r m iw MPQ e The srro fEers fcirr tt I h d shfouid be made with wwer offan m1heumcalun e F kt n Immld a tely aitSLtouchdown lower the nos7whe era ndlppl...

Page 17: ...iZspSi to Lmlmtes at 100 0 RPM a y a erat scX heuS sptoesh rrSne RP theairplaneis readyf rutaTe offpressure remalns normal and steady conditions 1UB ls crnlcal under certainatniospheri c Refer toSecti...

Page 18: ...N S st w s minutes that thepiToT cMobeuc r l te dtoa maximum of 30 to 45 niihTa tud thna leot TcayoTmhL LOOSE EQUIPMENT AND BAGGAGE SIS te anF o I X pm l l CM seat belt and shoulder h a eTs s 10 aerob...

Page 19: ...s EgElzrdelseg er dce w h_the a7rPTaneu dTteTaS UVh h LlLt areasshould be ina cco rd cieul ovpTJls l eclw nla cases afTer ns nguS S0 CABIN DOOR JETTISON SYSTEM ffw m s s daath tion dthe7h c eL sulTsc...

Page 20: ...sition NOTE K a spin is entered inadvertently from an aerobatic maneuver it is important to close the throttle promptly The use of enginepower in the spinwill tend to flatten the spinningattitude and...

Page 21: ...MPH BARREL ROLL AILERON ROLL accompanied by higher roll rates cuver ana is MPHTheT eanntehuJe r e nterie fromn strMght winSSlevel Uveat130 S i SE rc tSi s Figure 3 3 BARREl ROLL SllS i iBS 3 6 ft0 ss...

Page 22: ...ightly etoedca alhealf HALF ROLL FROM INVERTED SNAP ROLL CONSTANT 3 5 TO 4 1 PULLUP fullrTu d srnaHP S i an alceleratedstaumaneuver inwhichyawfrom i c Sn produces r axrhi l nTl i w MPHTheAte Ll Tpir o...

Page 23: ...dTn te udi andl ecr0 in the OPP te direc timT On recu s dt re estabush a ste ptm n unl a banked tarnkwi thlno dnisrt rbrrye akthen S shOTlllsmoo uy mMe ver may b pYrfoIrmuedu r m etomng motion vertica...

Page 24: ...50 MPH This condition should be avoided as much as practicable FLAP EXTENSION The use of flaps in the executionof approved aerobaticmaneuvers is Sectivii If EMERGENCY PROCEDURES i c s byaircraftor eng...

Page 25: ...rs UNLATCH PRIOR TO TOUCHDOWN Touchdown SLIGHTLY TAIL LOW Brakes APPLY HEAVILY7 5 6 7 8 9 Master Switch OFF orL UNLATCH PRIOR T0 TOUCHDOWN Touchdown SLIGHTLY TAIL LOW 1 Switch OFF Brakes APPLY HEAVILY...

Page 26: ...mo_MPH Hfire textingui d increase S SuSeed to fmd an airspeed whieh wiu Provrde an inc mbu sotrble Execute a forced landingas outlined inprecedingparagraphs ELECTRICAL FIRE IN FLIGHT T he lnitial mdic...

Page 27: ...su fnlSakingoutof clouds PPly alcruisingpo erand FLIGHT IN ICING CONDITIONS c S f r S c Pr M i u S h at switchoN ifinstalled t2 K d e I sKe r t l y m and airflow u 1 u nl r01 to Set maximum defroster...

Page 28: ...g leslthantTneedle widths f char gmgcurrent If the gi r e ere var m Lt S l Jft o e rate the eleetrolyteatm excessive rate Electronic components fn elect cal system could be adversely affected by highe...

Page 29: ...5g or more over a short time period I2LEoLrTJaAsIS Jf g lsw h uatlTO q st oned following eS S b S8 to the ELT wd ELT CONTROL PANEL TO TRANSMIT AUTO OPERATION SET SWJTCH TO ARM ft E MOT E OPERATFON7 3...

Page 30: ...i11 be hai py to assist uin Sn st S a Lml be operatedm accordance withallFAA approved nlarklngs and placards ln theaircraft Ifthere isany informahoT uth s sst adicts the rAA ro s s smi i MANEUVERS ACR...

Page 31: ...7FTapsExteI uepd cu uo o Maneuvering Speed 118 MPH 5 2 The maximum speed atwhichyou may use abrupt control travel AIRSPEED INDICATOR MARKINGS ingsTchlsTfloomt eg S fthecertificatedcalibrated Peedmark...

Page 32: ...mtfu selagJ Le Z UuoS t ithl em b emgk aded must be made ifThe po siUoanuof the load is different from that shown on the Lo cUng Gralph CentJrotofl l g s nd oments loooand Plot these values on the s s...

Page 33: ...9 0 1 4 0 13 3 1 7 55 8 Weight Ibs Moment Ib ins 1000 11 0 1 issx ss ss ss Baggageand orpassengersonchild sseatnotauthorizedduringaerobaticmaneuvers U1 3 SAMPLE LOADING PROBLEM WITHOUT PARACHUTES L uc...

Page 34: ...0 2H m M i i I s 9 0 D VI l t c 1 3 s i TO n Iill l t ll i 11 till CT Q I i TO S iltl Ijp I s i 1 t 3 2J 1 ra LOAD WEIGHT POUNDS 0 0 0 0 I M TT H_t 4 T4 LTT g g S3 1JI I Pl 0 1 m If I s I I 8 I M JII...

Page 35: ...I CARE OF THE AIRPLANE GROUND HANDLING MOORING YOUR AIRPLANE SaF s t set parking brake and insta11 control wheel lock 2 3 S S ce cln lio l be eene r and flap sufficiently strong ropes or chains OO pom...

Page 36: ...heengine noT ap d7roTelTeMTogn pgrel i ewlnisMdt encountered ui the euai easupcuer splnner wil1 helP reduce the abrasion te r s M tt a c s o 1 C eT ae lrd incg De we St lo d be tok nto P te athet cpSn...

Page 37: ...ombmation of the a i cra 6 elc S5 ls i ES This plate is located adjacent to the MAA plate AIRCRAFT FILE tT5et m sc e ne sdata mformation dlicenses that are a tt ItheS u Thefollwine ls a chec addition...

Page 38: ...redANNUAL inspection aircraft operated commercially for hire must have a complete inspection every 100 hours of operation Jnueu of the above requirements an aircraft may be inspected in accordance wit...

Page 39: ...v7 hT g requirements70 wners aviation officialswhere the aircraft is beYng operated OWNER FOLLOW UP SYSTEM nYO ULCe s T DJaleLhas nowner Fo ow Up System tonotify uenw sehrZiTavirf t app Iol3o nu if vT...

Page 40: ...rformMC7tofa T cEThSi ahefiiroldm reserve headwtods take off aiiTcSl e Tmgt AllowaDces fol _f el i sSSSSSS I 10 m orTmlumSS aSee atmosphere may account for vaTiaU onus1 ondsm h pS S e d I ot MCd 8ta...

Page 41: ...sd h pa r t totalto cf ar 50ft o b5t acTe fi 1 ll reaseaista s b th P oundrun ud totu toFcTaa r 5 0 It Secle by7 o the MAXIMUM RATE OF CLIMB DATA TOTAL TO CLEAR 50 FT OBS 2440 1875 1375 GROSS WEIGHT...

Page 42: ...94 113 110 104 98 90 6 6 6 1 5 4 4 8 4 3 3 8 3 4 3 1 6 0 5 6 5 0 4 5 4 0 3 6 3 2 5 5 5 2 4 7 4 2 3 8 3 4 3 1 4 8 4 3 3 9 3 5 3 2 4 3 4 1 3 7 3 4 3 1 ENDR HOURS 3 4 3 7 4 2 4 7 5 2 5 9 6 5 7 3 3 8 4 0...

Page 43: ...Section fill OPTIONAL SYSTEMS COLD WEATHER EQUIPMENT WINTERIZATION KIT GROUND SERVICE PLUG RECEPTACLE K 8 1...

Page 44: ...sure altltudeTTet baro e iT a pafSme r 29 92 _an d e Proe s eu dce Sa ti e0 n BeKswlto retonaltimeter bar T rb oabltSnreTetric7etting a 8 2 RADIO TRANSMITTER SELECTOR SWITCH tiv o atl o Lof ther a dio...

Page 45: ...mmeter 2 5 Approved Maneuvers 3 2 aileron roll 3 7 barrel roll 3 6 Cuban eight 3 9 Immelmann 3 10 loop 3 5 snap roll 3 8 spin 3 3 vertical reversement 3 11 Authorized Operations 5 1 B Bail Out 4 9 Bal...

Page 46: ...in flight 4 4 engine fire during start on ground 4 3 engine fire in flight 4 4 Flight in IcingConditions 4 6 Flyable Storage 6 5 Forced Landings 4 2 ditching 4 3 emergency landing without engine power...

Page 47: ...Operation Or Loss of Power 4 7 carburetor icing 4 7 low oil pressure 4 8 magneto malfunction 4 8 spark plug fouling 4 7 Sample Loading Problem 5 6 Seats 2 8 Securing Aircraft 1 6 Servicing Requirement...

Page 48: ...fro h haa SI g a s eq ppe w anoptlomloilm S d e nu he ou pressure screen each 50 hour theTeafterx On ISdwehdiS e n LOTlfflt e l c n n Sae dnSd o oo hour nt e s _ ovidi S e d atJO hour intervals change...

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