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