SEE RP RP eS Ss ww = ZS-KVW C172 Pilot’s Operating Handbookee we ee es ® civieaviarion ‘AUTHORITY ’ Pat te 300 want os . Ne Sinisa fae a oe i ‘APPROVED FLIGHT MANUAL Registration Mark: Zr — KV OU? Manuiscturor Crscay Mikecary Co. Designarino Area: #7 &P Dsvcra Siatnembor: 192 14774 Aieworhiness Catagory, “ Swen ORD Manual Part humber: D112 b= [BPH Voce Dato ottamat 1 ee. p53 “Te appleableoperaing itasons inthis manual have been approved ‘bythe SOUTH AFRICAN Civ AVIATION AUTHORITY 1 ‘NOTE: The onus rests withthe owner or operator of tis alert to ensure {thatthe revision status ofthis manuel s kept current at al tes. LBA BoOe AVIATION Dale (/ THIS MANUAL SHOULO RETURN IT TO 7AE ‘SOUTH AFRICAN CIVIL AVIATION AUTHORITY.RE Re ew SE wee Se = SS a a a ae a a 7 cessna, ‘cononaTULATIC Sobe: ivaP ee CONGRATULATIONS .... red Gareyouiterst npelomanes ecosomy sndcaon, rsa donee seg ig Lestat hetaee pas spend pital ple andy rl par apne ones clean at ate Ces Srelwe ghee by tite eens am Bing gz ha not ad a yout ur» ei ‘Wot de fe Cine Gite Grin bcs by te Ces tome eet pre te ose yee ltonng serie aeedby mn cans * ere el ee eee mee ete el ry ant Ennis aren FACTORY RAMED PERSONAL provide ou wth cores eget vc. FACTORY APRROVO SERVCE LQUIMIN to pronde you licen and seca Some STOCK OF GENUINE ESA SURVICE PARTS on and when You ned hem, + must sumonarnenfonnation fom seeicne cee 8 ‘vt Oy Sees tensa ce News Lene, babe by tens Nera We pel Cena omnes we he Cena Orgaintn fthe e Ase ma aie Seco acpi tense the ic ‘ieee roe coy ie suns “Seam melons to 7oe as = aa SS \OB/REVISTONS/ ‘SBSENA covena: 2 > Ss a ee ee oe ee ee SHEERS woes [| A aaa pe PERFORMANCE - SPECIFICATIONS soon om - ICATIO! ncn ee as a it gt “a stg, serenore | Sieelagiemcomihtenseiea onto 12 KNOTS. REVISIONS: "Eiiee won tte Sc get ten pay ea | Sp ee "ten dnatenmnd anaes naneahen | = oe yo) son | kate am SASS AS mai thant conent | a oe reeeeceiaeeen ne ee | yer Be ccna re ee te me ton renee | BE ewe wr, | Martin tnmmummmnrenenn, adastttats Odo cece ur emer reanminbenniatabeetetes ARERR sig ncn i | saGBBBisTr oe oo: SrA scien ) EHR: icra agra eis Desh 180 /os- arate | a oxy 1080‘2S Seas ‘TABUR OF CONTENTS cossna TABLE OF CONTENTS ' SECTION | ) GENERAL... LIMITATIONS. . : EMERGENCY PROCEDURES. mers roy NORMAL PROCEDURES. PERFORMANCE. WEIGHT & BALANCE/ EQUIPMENT LIST ... AIRPLANE & SYSTEMS jr) DESCRIPTIONS «2... eeceseseeee AIRPLANE HANDLING, "SERVICE & MAINTENANCE . SUPPLEMENTS ) ) (Optional Systems Description & Operating Procedures) . o 0 may 1680,eSB SESS SSS = ke es eee ee gESSNA section » MODEL rap LIMITATIONS INTRODUCTION ean nce oe an npamen mares en spoSeentte eto ups ere i oh ava suc tetren,n mteoge nce a ipsa Guerin Sarat mete Acre seks ae! Nor, [Refer to Section 9 of his Plot's Operating Handbook for smpended operating lmsations, broly ‘Mlormation ows Cosen is crtfieated under FAA Type Catifoate No. 3A12 48 (Cesana Mouet No, 7a 0 May 1980 2oa Se ale hh eo Ce ce cassia seerioN 1 Moat ine CoMERAL, SECTION 1 . GENERAL TABLE OF CONTENTS igh Penning etic Wott And Balance Terminology ne ‘0a 1500, 4Cs ee ee ee essa seorioN 1 MODEL ive ‘GENERAL. INTRODUCTION nitions ore ferminology commoniy used DESCRIPTIVE DATA ENGINE Namrata oma Engine Nodal Muster Oca bae ‘ngine Type, Normally aspirated, direct drive, air-cooled, horizontally. shpond,arurtoreguppes four ylinge gine wih Sibi Horsepower ating and agine Spe: 100 rated BHP at 2700 RPM PROPELLER : Propeller Manututarer: MeCauley Acoestory Division Propeller Moe! Namen 00) DTM umber of Binds © Propeller Damolor, Maximum: 7 inches "002 Grade Aviation Fuel (Green, Nove ‘oprony alee! or etylene giyeal monomath ether no ened eon nechan a ay et ca ‘monomeitiv! ether. Refer to Section 8 for ‘0 Mey 1080 1Ce Ms Rm Cm Ce em ce ce ce ee ce ee a a a a een a ee a ‘section: ‘crsena ‘GENGRAL Mosier Pos) Capacite Eee open ee Ort as am ne viene SEA ee any ERA wate Foal Gakte So tne | wae | SEES sone | Nore | ‘To ervure maximum fust eepacity when refveling end Inari one foding when Paskodone sloping suage, sector valve in either LEP or GH ' on 01 Grade spaitenton: OS Se tonne Steg Mineral Oi Ue orepeish i ‘pple during tire hour td att fim bento Seen ‘ontioe to usa unt ota of S0 hours has accumulate oF a Sonsumption has masa ‘Mil-r2361 Ashiens Diapereant Ol: Tsoltmuatbevanditeriret 60 ‘hoereor off omaumptoe has taboo Recommendet Viscosity for Termpertare Range: Tino Aviation Grae Srsgh Mier Oi: ‘Anove 16°C (6° wee GAB 5, 1 (0°P) to °C GO") use SAE 40 i 0c aie (To, wes SAE #0 oF SAB 20 Below ie-0 (0 oe BAR ID ‘ a 20 May 1960 ceSSNA, seorion ope ier GENERAL MAXIMUM CERTIFICATED WEIGHTS. amp. Moral Catagory: 807 ts Uy Category eter om ‘Takeott, Normal Category 240 ow. Ui Category 2100 tne ‘Normat Category: hil en) Station £2 to 08: 20 108 to 4°50 ne. Se note blow. Nore ‘The maipem combined weight capacity for bagsage ) “*tamae tmparnon sa soa ea abe ecg eo STANDARD AIRPLANE WEIGHTS. ) Standard Empty Weight. Skyhawk: 1414 bs ‘Skyhawk 40 toe mesa Maximum Use Lod oy suo se Signe Sine CABIN AND ENTRY DIMENSIONS ried im Seaton y BAGGAGE SPACE AND ENTRY DIMENSIONS rot and bagsngs door opening, 0 | SPECIFIC LoADINGS ng Henn: 19g ‘nate 1980 6De Ce Cle CRD COED Cee CD Ce Cee Ce CD SYMBOLS, ABBREVIATIONS AND TERMINOLOGY GENERAL AIRSPEED TERMINOLOGY AND SYMBOLS. act cle speed sequal tw RYAS a asad IAS Kote tndleated Atrpood is the speed shown on the ‘speed inalotor ard expreseud okt, TAS Kote True Airspeed ia the airspeed expressed in knots Felave fo undistaraed alt wih i OAS carrot for Manuevering Speed i ha maximum speed at which you Ye Maximum Flap, Extended Spada thighs: speed y, Maximum Struiural Grlaing Speed isthe sped tht odastvecrweelncepisencot atten oy wit over Bxoeed Speed Inthe spied limit hat may not be og Spe anu windy gm peed st vu Saimptents te itoee uaa rt aoheS eS ‘Rest Ane at lin pea ie he speed which rman METEOROLOGICAL TERMINOLOGY a Ce Ca Oe Co coe cane ciais| ease, ‘seorion 1 DEL rae GENERAL Standard Standard Temperature is 15° at ges tovel preaure alte ompere- tude and derounes by 2 for edd 1000 feet of ate aches of mercury (Oidmy). nt nee= set O2888 ENGINE POWER TERMINOLOGY BHP. ‘Beake Horsepower i he power developed by the engine ie rnp whe aplane tn‘ te gn ood AIRPLANE PERFORMANCE AND FLIGHT PLANN ‘fenMiNoLogY GHT PLANNING Denontzid Crommind Valo ote waoay of te plane during takeof and landing ws sotvally demon Vaooiy” Rrkieg uring criti ote the salve sha ot ‘Usable Fuel Usable Pulls the fuel arallable for light planning. \Unusable _Unusable Pua the quantify ofl that cannot be safely Pet ‘ered in fight w opr Gallons Fer Hour is the amount of fuel (in gallons) swra . {fs acceleration du to gravity,Pe a ee ea Cee SC Ce Ce a Co Coy Ce Ca mo SBSM ‘cesana serio 1 Spe ap SinERAL WEIGHT AND BALANCE TERMINOLOGY Maximum xin Landing Weight is the maximum weight ap $xfernce__Relrece Datu i an imagiony srt ase fom Gerding” pevatiorite lating aco, Bice SSS onal Ananadieecn age tom wean purposes Tare Tarajethe weight chocks, bloccs, stands et, used whe Seen jane os he ror ata = gate ddd the Sete roading coche sal ey rps eg am ora itncromiherfrmovtumto thecentorat gravity Nouns Moma site pilaf bewietotuntencutigies | Sema amt eipelearmrel Metin ong tals coeaioes gee erate orgy Genre! camer of Gravity ise pint at wien an wiiane or) |) Gravity’ Silpinen would vaiane'f snpendes ss uibcae es | Ej" Reitene ata sins ty ving tela eae Bye taal wie of tesla 6. {enter of Gray Arm ethene sinned by sting the ) Sem Stn teen on Sd ing ee oy ‘hetutl welgt £2. enter Gravity Limi ar tet cetert grvity sinita fea in nen te imiasemus bopantac en weigh ) Standard Standard Bapty Weight i he weight of standard Son ne. inclang Unosaie fe, opeeating hae | Basle Empey Basic Empty Weight oe standarsempty weighip the Weight" Selgnt or opsond equipment yoy Veelsl Woot adi tne stterence etwoon mp weigh andthe one beste empty wets Weishe ete elantotaacs es imum “ 0 My 1880ee ee Re ae Cee Cee le Ce es ee Ce Cee ee ee Ce Cle Oo Cy ea, gzomons | SEE NS | SECTION 2 | LIMITATIONS ) TABLE oF CONTENTS 20 may 1089 24/22 bien2 CRO CR CRD CRD Cee Ce Co Ce Ce Ce Coed cee Ce Ce ce Ce seonon moses AIRSPEED LIMITATIONS. Airy linitains a ei operations sgicnce ae sows ‘gute Magouverine spsedn shot soply Sr {SSha The iy catagory maneuvering spied ie 2iiAS aiSiOOpoande Va | oe | Oona acnseuamae Cesena section 2 MODEL iver unniTAnIONS == =e | eroeeate Sees, aon ne 9-1 | Spel aig ema ee Fa tae | 10 | oo see aed io 1S rage | "8 | | tts Se Bape wesw Om |e | | Opens igure 24, Airspeed Liitatons AIRSPEED INDICATOR MARKING: POWER PLANT LIMITATIONS Eps toate ase "tan Continscus Operations: eens — ia eeeeerms Se orsqnmescnennent eeePOWER PLANT INSTRUMENT MARKINGS sco REE enue mastngs ad tir calor code seiiane | one Pa | ieoee cons Swat | Cegeinm |) mare | ccf | " caters Pigure23, PowerPlant Insrament Markings WEIGHT LIMITS Mastmam Ramp Weight: 407 om Mdimuee Tact Welghe 200s Nasi Easing Ween oe eagagn Aves or pectoge on le see» Station 620 18 120 Bagge Ares 2 Sabon 8 to 14:6 Ib, Se following note ‘CESSNA Secrion 2 uniiry category Maximum Ramp oleh 107 ch ein Baggage Csrprtment ote wily category CENTER OF GRAVITY LIMITS NORMAL CATEGORY Conte of Gravity Range: ‘atc 473 inches afl of eatum sl weight. Reteence Datum Lower porn seffon face of rel vumuy caTeGoRY enema 30 a ot cen wfign ine “Gis tnchor aft of aan aa weighs MANEUVER LIMITS NORMAL CATEGORY ‘This airplane se caritcated in both the normal and wit estogory ‘tye normal lategory ie appleabe fo sicra toned Tor now aorebetke persion, These itelade any manewvoreincventn to norma yin snp whip al ny rh connie, naar bh ne umiuny category rious onifeaten such ne cormeretal pilot and fight.a eee eS ee Enea non Mosat iat never areapproved expt ose etd [RECOMMENDED ENTRY SPEEDY cn ‘gece ge Stalls xcpe Wisp Sain “Abrupt us othe controls prohibited above 89 kts spt at oy poe hi nda bold notte FLIGHT LOAD FACTOR LIMITS NORMAL CATEGORY ‘igh Lond Pactor (Maximem Taeot Weight - 2400 Ib): rispe Up 3, -152¢ ‘Flips Dows : 4 “Peet yi sre a ecteattemrnam te uy exrecony sion eon et et te tie tennant te os so may 190 sen ee se cpesva. secrion 2 ‘ae ndrTATIONS KINDS OF OPERATION LIMITS 1 yprTMegtpane te equipped for day VFR and may beequipped for night gited instrumentation and equipment for theses Bee sie. pe f fight pean on th operating limitations place ) PE Into known fing conditions is prohibit FUEL LIMITATIONS , scary ate Se A wy ous. cane “oll Pas: o4 US. gallons SaRE Re GE ns ge See a cane ) a ee ati ate SERVE eam v2 ee ‘Takeoff and and with the fuel elector valve handotn be BOTH poston. Maxis sip oF sk dation with one tank dry: 30 stoonds Win 5/4 sank oF 18s, prolonged uncoordinated light isprohbited when ‘operang om ltr ie or ght tas eval igh 3 india eenaot be ately uoed ia fghe. NM tnlemeor reads empty ‘Approvd Punt Grades (and Colors): "ott, Graae Rvintice Ret (Sloe {00 formar 10/35) Grade Aaton Fuel (Gree: == eeoponsa. seoTioNa opeL OTHER LIMITATIONS FLAP LIMITATIONS, ‘Approved Takeott Range: 0° to 1 ‘Approved Landing ange: 0° to 0% PLACARDS “Tn following information must bedisplayed in theformofcomposite 228 ee se es ‘ESSA MODEL rap SECTION UNIFATIONS 2 On heel a valve (ean anny > BOTH J0GAL ALL PLIGHT ATTITUDES, ‘TAREOR LANDING - RBERSz0 Sats EeVEL ruice ony Blo}tT “29 GAL. LEVEL FLIGHT ONLY or (nthe fe! selector valve (long range tanks or india putas 1. tn tlt iow of tho plot: (The “OAY-ATGHT-VERCIER™ entry ‘Shown on the example below, wll vary se the itplane 1 Satippet BOTH 60 GAL ALL PLIONT ATTITUDES, Eopren Oat CEE muscire omy ovr aegery ir in tbe Uuliy Category ae Canaiend in oe Pla Opersiog oak and FAR Approved Alrplan Fight Hata Normal Category Noacrabatie mansvers.ncting spins spproved No aerobatic maneuvers spproved, SREY Bose ined ne the ‘uiity Category compartmentandsea ata ‘Rud wot be 2epted, Opposite rudle-orwardelevator- ‘tuialze cents in Recovery Fight into known icing conditions probit. “Thsnleplan scored for he following Might operations asofdate Morigul atrwortinese series DaY_NigHT—ven—tPR 240 sa aty 1980 (nthe fel saacor valve (integral tanks: BOTH GGA. Ara, FLIGHT ATTITUDES, ‘TAKEOFF, LANDING. Lepr 3 GAL, LEVEL PLIGHT ONLY ‘lone kt Levin igi os 3. Near fuel tank tier cup (etandard ane FUE JonLt/ 100m, ORADE AVIATION GASOLINE Near fuel tank filer cep (ong range tanks) "WoL 100 MIN, ORABE AVIATION GASOLINECoe Cm coe CO CO CO Cee CP ce coe ee ree ree rep rem ces ree cep cen Cl seovion 2 cxsewa cassia sponion a Eharanions Monet ie MoDEL rar LnMiTATIONS ‘Near fuel ankle op tage tanks: 8. On control lok FoR, i ‘CONTROL LOCK. REMOVE BEFORE STARTING ENGINE 10011.) 190 MIN. ORADE AVIATION GASOLINE ([[ conrion ce “nenove nerons START ENGINE] NGAP 94 US, Gate CCAP. 240 US. Gals 10 BOTTOM OF FILLER COLLAR, 10, Nonrairsped indicator: ; | MANBUVER SPEED - 00 KIAS "AVOID SLIPS WITH FLAPS EXTENDED y , {On fap conto inaiator . oom arial fla cange with ve color “Seana ff ee oct ana i ‘Bechanieal ten at 10) yoy | | sewer -feamaumreececam Serene areata 6 Inbaggage compartment: 1 POUNDS maxis BAGGAGE AND/OR AUXILIARY PASSENGER. i FORWARD OF BAGOAGE DOOR LATCH ’ so PouNDs waaneund BAQOAGE APT OF BAGGAGE DOOR LATCH [MAXIMUM 19 POUNDS COMBINED. on ADDITONAL LOADING INSTRUCTIONS ily SEB WIGHT AND BALANCE Dat 1. 2 cllratoa eas provided o nite the sceacy of he ‘agnatis compass in" inoremente 4 onaits an 0 May 1090 ‘90 May 1980 2ray(eta bak)Cm Ca CD CD CO CRD CO OR CS Ce ee ee ee ec cessnn, SECTION Move rap EMBROENCY PROCEDURES SECTION 3 ), | EMERGENCY PROCEDURES TABLE OF CONTENTS é CD] 1 sateatstion OPERATIONAL CHECKLISTS f 2S eee eeeeegeesey: AMPLIFIED PROCEDURES2 CRS COD CORD CORD COR CR CORN CRD CRS Ce CD CD Cee Ce Ce ce co Ce es “| seeniows woth seotiine seenonvcy SEER TABLE OF CONTENTS (Continued) rea INTRODUCTION gn feuds (Vacuum Sysem False) $12) omamntes a yet Se for coping with a Spiral Di Me dnadverient Pigs eng Conan ut Rough nine Operation Gr Last Ot Power se) Spare rg Fouling te | | RoR abs ae peas Era tae .)) Sa cms OPERATIONAL CHECKLISTS : ENGINE FAILURES ENGINE FAILURE DURING TAKEOFF RUN 2 Brakes” APPL, ‘ store ioie cur.ore.sections cessua SMEHOENCY PROCEDURES MODEL te [ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF [ENGINE FAILURE DURING FLIGHT ‘lcepeed 65 KAS. (Gxtbortor Het “OW, fet Slecior Valve BOTH, \iteh=- 80TH (or START if propeller is stopped). Th end LDCKED. FORCED LANDINGS [EMERGENCY LANDING WITHOUT ENGINE POWER ‘Aespeed~ 45 IAS (flaps UP), ‘0 KIAS (ape DOWN. Mixture ~ DLE CUP-OFF, Hel Eaotor Vales OFF. ‘Sein eespeser rain angcaratos en Fettuot lap upon ouing wanfe atte a ale [Rules Powar Sten and letra Switches ‘ne Piao or a porns. Rater Swit GFF. Store -- UNUATCH PRIOR TO TOUCHDOWN. ee per ae ‘9 May 1980 3B COO CO COD CRD COO COD COD COD COD Ce CORD Cee oe cee cee ee cee com oe ool Slope ap EMERORNCY PROGEDURES 8, ‘Tovehdown - SLIGHTLY TAIL LOW, lon Switch “OFF BBtakor== APPLY HEAVILY. orrcHiNG 4. Radio TRANSMIT MAYDAY on $01 5M gi Intentions ana SQUAWK 7700 ra ‘ns a ne powers avalabe, approach at KIAS with apsup or nbn RIAS win Io cpa ‘fouehdown"- LBVal ATTITUDE AT ESTABLISHED RATEOP Face. CUSHION at ouchdown with 40 cou, ‘Airplane -= EVACUATE trough ean Sore I necessary. open ‘tindow aad foog cabin to eelize pressure t0 doors can 10, Un Vests and Raft INFLATE. FIRES DURING START ON GROUND INUE. to getastatwhich would suck teflemes fuel trou the carburetor and int the engine 2, Power 1709 REM fr a fow minuter, ‘SHUTDOWN and iarpect for camage 5. Miu" IDLE CUT-OFFgucrion 3 cesswa EMERGENCY PRocEpURES Mops i ® CONTINUE, leniton Swe OF il Sean Vsives "Orr. a. Be EXTINGUISH ig ti atingiser moo basket ordi. 18 Fie bkmuge = IMBPECE. repr dene or tplnce Saad components or wining biti cst nthe Rg ENGINE FIRE IN FLIGHT vane penance, SE on ompt meen et aera rem: reed anding Without gine ELECTRICAL FIRE IN FLIGHT 1 Mastor Switch OFF. FR Or orn ‘© Vonta/Gavin aiertast--CueEED, STACTIVATE (i seuabe, Alle discharging an extinguisher with ‘eniate the She Wire appenrs ut und electrical power escesary for continuance fight 2 Gite Bremere S SHECK tor tuty cre donot ek © Radio Swittes'- OFF 18, Ragiofstecrien!Swition ON one o tne, wit day ater ‘ich shor sirout a tocaon, 7 EXECUTE (as doserbd in Bnergeney Landing Power loon cabin, ae . 30 May 1980 CRS CD COD CD CRD CD Ce CD CO ee ce ee ee a Ca a ae cESeNA section 3 MODEL ap -BMGEROBNCY PROGEDORES M1, Venta/Cabin Airiteat ~ OPEN when it is ascertained tha fees completely entoguiched, CABIN FIRE 1 Master Switeh OFF. 2 Vents/Cabin Aries. CLOSED (to avoid drat, 3. Firefixinguisner = ACTIVATE Gi svallaste ‘ent he capes neater 4. Land the aeptene ) WING FIRE IcING | INADVERTENT ICING ENCOUNTER so may 1989 a7oEssNa EMERGENCY ProceDuRES MopEL Tae ‘nat ag rquiged. An enexpitined lost in engine wpead cout! to Tatake fier en Lota the ixtare a 12 Perform n landing i eve atte , STATIC SOURCE BLOCKAGE (Erroneous Instrument Reading Suspected) 1 Allrnat Satie Cures Valve PULL ON. 2 Arspred-= Consult appropriate ealloration ables in Section 8) LANDING WITH A FLAT MAIN TIRE fl 1 Approsch ~ NORMAL, 2 Gzendown:-GOODTIREFIRST noldsirplaecft atte aon ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS AMMETER SHOWS EXCESSIVE RATE OF CHARGE | (Pul'Scnle Detection! ‘itenator Gireut Bresker- PULL ) ‘Noseszontia aciial Suipment-~ OFF. Fight TERMINATE ne foee se racial a8 20 May 1080 SE SB 2 2 @ 2.2 2 Ss 2 2S eS Sw opssxa SECTION 3 Slope imap BMEROENCY PROGHOUNES LOW-VOLTAGE LIGHT LLUMINATES DURING FLIGHT (Ammeter Indicates Discharge) ore tation of lomealings Neh ay esa daiog re ‘HED condition with an eesra! fond ce ine speve ring alow RPM tax Undorthese conditions tre wor i owoltnge Light = CHECK OFF, ‘Avionioe Power Swit = ON, ow voltage light aminaiae & Reseacontiai Ratio and Bletrcat Bquipment OFF. 8 Phght®= TERMINATE as soon au practon so May 1380 2.97010 bunkDC CS CD RE CD OS a eS ce ee ee SS a ee ee om a ae | the theehiet ifthe engine examot bo Fear Cessna SECTION 9 Movet i EMBSGENCY PROGEDURES AMPLIFIED PROCEDURES ENGINE FAILURE. peedandenabisha glide nto exeeute 180" piding tora necessary to rturn 0th “th chocilot procedures neue thas adequate tins existe 0 tn fool ane gutionsysteme prior 9 chown ‘Alte an engine flur in gh hebest gis epted ss shown ntigure 2: ahoatd be enabled uae faire time permite power most be comp 20 & a0 I 2 wa SZ é > § rid 2 x0 Sceroretce winomuune feriavsu'szen0 WIND sb2 ree re ee ce cee SECTION 3 FORCED LANDINGS mmingnt elect suitable field and prepare for the landing se discussed Under the frnergeney Landing Without Engine Power chest Before stomping an ot airport landing with engine power nea: vn ESBS for ching by string or etsoning hey objets oeted Ieeton sad intone and sque Sra a asepeteer ‘Avoids landing flare becmeo dita judging neigh over wor LANDING WITHOUT ELEVATOR CONTROL. oor rn rea Shir es cee adjusting power exclusivaly. ” ‘oat potion un the power aajurted soa the isan rare thehonZotal aituae for oschaawn. Clos ths tate a touchdown FIRES ough engine fue xray an Ethos of te oe 0 my 1880 cP a ee ee ee ee ee ee ee ee ee seorion 2 EMERGENCY OPERATION IN CLOUDS (Vacuum System Failure) 1 he event of «vacuum systom ulure during gh, th drotional {naicator and attr dotnientr wil tw dlscbod a he pit el ees aon ie enone Uae ia EXECUTING A 180° TURN IN CLOUDS ‘Seoep ocond hand on te lon "symbolic sirplan wing op cond Toon rll bck 1 ave light ty ovsing the inioee irpiane, 4 Ceo tocurny of the turn by observing the compass hending ‘on shoul be te secprocal of he orion! headlong 5 Tnecomoesy. adjust besding pre ‘uther tha folling motions fo thatthe compa Sorc 6. Maintain sittade and ieee ppliotion of feat Aveldowercenrainghy Kapital spe conch EMERGENCY DESCENT THROUGH CLOUDS erent through & Slows deck fo VFR condition may be dopropete it Seat te rant, GreteSERCENCY PROCEDURES Moon ae ‘Apply ul oh nator. ggnaaeoee Eee Es www mp nner 2s Grae came tara a i EN Pee ae mcmmneaaate, Screeions with rerio so the Te 1 Uponreaking out of clos: Feuine Roem erusing Nght RECOVERY FROM A SPIRAL DIVE ES gles a nt Sep acig at eae ore a BRERA hc mist uoy mae ¢ BS rine mutans ater, * Eeees Scar os an genase Upon tren ou of souds, resume norma erulsing igh INADVERTENT FLIGHT INTO ICING CONDITIONS Fight so in omton rtd An invert comune STATIC SOURCE BLOCKED 1s ofthe latic source inatraments(arypen, ede suspected, the sienat sae ata “erat sppiying ats peoesreto he cassia secrion 2 MODEL trap EMERGENCY PROCEDURES Nore 4p so smerency on sleplanes not equipped wit on ennai i sopcas toh Rock tere ener eee ap never ib natal opring ng th i SPINS ‘Ton oF Rotarion 4. JUST APTER Tas RUDDER REACHES THE STOP. MOVE THE GoNTROL WHEsL BRIOKLY FORWARD FAR ENCUOH TO SREAI ith STALL. Pulldown eavatoe may be required tt alt 5. Hou mfsse CONTROL INburS UNH ROTATION STOPS. 6. AB RotaTION stoPs. NEUTRALIZE RUDDER. ANDMAKE A SMOOTa RECOVERY FROM THE RESULTING DIVEROUGH ENGINE OPERATION OR Loss OF POWER CARBURETOR ICING A eradutlossof Pa andeveatual engine roughness may resultfrom | ‘ontinued ue ofearburetor heat teraiae ight une the minha SPARK PLUG FOULING 2 slight engine rouphness inflight may be caend hy one or more spark plogs becoming foued vy eatbon oat Gepost Tis tay Oe ‘ented by turning theigniionswitch momentarily fom BOTH elder runs of spark plog or abeale esas Amteangtapckpiagoet {homore kal ees tnnemisture tothe lst en she poem ao nt cee up vera mie Gt pried toe enon pr fo opal nage BOT oan a ‘enitlon pono MAGNETO MALFUNCTION nagneto price Swtening tems HUTH setae Lor gaion seo iy Semi etic ct Eptsabatmete up rat ett deters Low Olt PRESSURE {oa ln of ot prea aecompania hy ane nol empert 3 Cm Ce cee ee ee eC Oe ce eS ee a Oe a a a a EMERGENCY PROGHOUNES ‘gngine power immettatly and select a suitable forced landing ld. Use ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS penitent sere! power uly ese canbe detects Ss mea ies ae rete eerie citer numa wi cipae eatin oma foe ae EXCESSIVE RATE OF CHARGE (ch i extend tain) tne btery someiion il be iow emcug to attected ‘by higher than ‘ormal veltage. Tne saat seat eit an charge shown on the ammeter tke alleraator should INSUFFICIENT RATE OF CHARGE Mjumiation ofthe low-voltage ant and ammeter dix:Se ae ee ee ee ee ce ee cee EMERGENCY PROCEDUTES ose in ne tcl. egw gat Sewers eS ) 30 May 180See ee ee | SECTION 4 ' NORMAL PROCEDURES ) TABLE OF CONTENTS ) Page Introduction 4 Speods Far Nonna Operation 8 CcheckList pRocEDURES | (Prag tspecin ‘ane icin sre: SSSSeSSTes aes eEaaeeE Ba: yo4 aurctieo enocxpunes saree aa oot 0 a |= os = szcrion cesava cesona suction « NORMAL PRoceDURs Mostar Nope ie NORMAL PROCEDURES me Oe ee ce Ce TABLE OF CONTENTS (Continued) INTRODUCTION ovides checklist nd amplified proceduces forthe conduct el Ta nate Seed rau nena paar Sms ieee oa | Taheccht | Sore | SPEEDS FOR NORMAL OPERATION pean efolowing pnts rstanedonsmanimar sat sng With A Cosens Beonamy Mixture Indicator (a7, 7 | ‘distance, the ah : Fa ‘Normal Landing’ ae . a 70-80 KIAS, 1 ‘Short Field Landing +20 ) ) short Field Takeoff, Flaps i0°, Speed at 60 Feet . (Crosswind Landing +20 ‘Enroute Climb, Flaps Up: a marie & a cali # mh eae i Seri Pe a. cca | three S|) BRE eee vn era, fa a Maer a, ‘Noise Characteristics ts | ‘Best Angle of Climb, 10000 Peet . ve | omm .Ce Ce CR Ce ee es oe ce ce ce co NORMAL Procenunes cessna mont i SS a a i a ee NORMAL PROGEDURSS CHECKLIST PROCEDURES PREFLIGHT INSPECTION Deasin 5. Pilot's Operating Handbook - AVAILABLE IN THE AIRPLANE, Iaition Swick = OFF, uel Quantity Indiewtors. CHECK QUANTITY. ‘Avionics Costing fan = CHEEK AUDIBLY FOR OPERATION. ‘inte Pressure Alleraete Source Value ata Demrennace Gino Suraces "CHECK retdom of movement nd sour | @aiokr wine | @ ricer wine FF Sep and Santi euamtig's tn Seen ocean une eee hia wena in sgnipeh wit een Kal Zan ck densi cesena NORMAL PROCEDURES Monel FP Arun valued oh for wales sediment. and proper un gras 4. Relcuenty © CHeCK VISUALLY for arsed oral 3. Pit Fl Cap "SECURE: HEC, donot pea ithe un tive ‘quarts Pl fo coven quar for exondea ight ret ht of fe a, a ater ech rf. ot ‘omble mater and andiment Che sins drain closet. raat pap eee Overs wine 1 Main Wiel Tie - CHECK fo propor inflation, 2 Bete in LEFT wine tating Edge 8 CHECK for fesdom of movernent and secur. a seeiees Te von n BERS: CRUISE | E Bester nes aan | Eee aiternsnmag ace escent 1 # RRSSRER ean mites 2 ERE Pi wear no noaomen to roa ‘hrburetrscig) BEFORE LANDING F CURE. 4 Guburir Heat 8 Cappy het before reducing power, & AlsCondioner if inaeg)- OFF, LANDING ) NORMAL LANDING 1 Airspeed 6-78 KIAS (nape UP), Mag Fane AB DBSINED 10" below 10KTAS, 10-30 blow 3. Rirspeed 0070 248 (aape DOWN), 4 Ranharwas" ain Waa i » Bttking-— MIvMOM REQUIRED. ‘SHORT FIELD LANDING aeeeaen Wing Pape etHACT 20 May 1080 ovf NORMAL PRocDunt BALKED LANDING a cow. SECURING AIRPLANE sone Parking Brake ~ SET ‘Retonea Pow etal) = OFF, Mixture ~ DUB CUT-OFF (pulled fl ov. Ignition Sutton OF, ater Seiten OFF (Contra Lace INSTALL. ‘opsswa Sich, Electrical Bquipment, Autopilot ( mo May 1800 co ro co ee ee ee ee oe 2 a a a cassa secriON + MODEL trap NORMAL PROCEDURES AMPLIFIED PROCEDURES STARTING ENGINE During engine starting open th tote approximately 1/8 inch. In NEE emberatres, ne oF wo strotenot te place snouts eee {n'cola weather up to six stokes ofthe primer may oe sreneee ve engine ) tones Ing Nore ‘Aitional eats concorning cold weather starting and {Speration my be found under COLD WEATHER OPERS ‘THON peragraphe in ia section, TAXING When taxing ie smportant that speed and un ‘minimum ad tnt al contol be wie (ose a ) Bhomainsin directional sontrot endian Diagram: figure’ nob should be pushed in during wt ‘sbaoitely echoes: When ie knoe ntoring the engin i notsscriow crssnn ean seoTION « ‘NoRNaL- PROCEDURES MODEL I So0et iran NORMAL PROCEDURES sect nt atiage ote propaiee spe BEFORE TAKEOFF WARM-UP. ipann era for wot | 1 magneto cHeck . . me! ) aT magneto check should be made at 1700 RPM as follows, Move Gin iar theater total pags en ove seca eee ce ‘ole RPM and etre seh tothe BOTH position, AEM drop seceook Sere Ato {xcend 129 RPM on liner magnet or show greser ian S0REMltfores, +) Hi "Stteen magneto i there te x doubt concern ) igual cine bane ‘An sbeance of RPM drop may be an indication of ely grounding of ‘one ud of the ignition sytem or abouts be ene for susan tat tne ),ignoto ming etn ndvence ae sing spate ALTERNATOR CHECK Prior to Might wh sont ni pain rintrument Tights) ¢ ) omentaris (9 to § seconds with the landing light ot by spersin he ingle ding te epgne neo 7OORFAIS The ammeter wi rem ) TAKEOFF POWER CHECK ‘important to check ful-hrotte engine eperaion easly in the Phyto 12, Testing Diagram eae) so May 199 aessa Stell en, ny i fou egg opr or Husieh engine teieott ‘gatempte gins should a mole ur appro {Emportantthe the trot be adranced slowly. Thisaliows he siplane Sh ofthe propeller Staertan pute nt Whee anovoaste soe ts desorbed is Section 8 under Propeller Care prevent the trolue fact cesping tack from a marmom power postion Simiaeeeton lok jusiment sould be mace neegulred ‘ther Might conditions wo ainsi aT WING FLaP serrines ‘learance epeed of 85 KIAS should bene. See eet a es NORMAL PROCEDURES cROSSWIND TAKEOFF ‘ipimum lp stg anaanay for the eld eng, Omimimiae tant Dorma then plied off absupay fo peevont so RENEE IM ding ton hearer ENROUTE CLIMB Normal ac et 2D Map up and ul thot anda CRUISE [REM and corresponding fuel consumption for vaio ‘determined asing Sour Corane Power Compateron NoreTees SS ee ey ey seoTioN 4 ss ‘stills winga lot intormation to determine nesnostfavrabiaslt vce fry toensichen the mixture sighiy t obtain envoth operation Should tbe neossnty terse at higher than 75 power theme rigina! REM etn eta) wete minimum amount of het yal and ‘rr to prevent ice rom forming. Since the hen tir cause richer ‘rvtave, oud th ature sting when caturavor heat ‘Shnuinucury tm oraon gmt | Stooteat operation Power changes shoul be sade callous) oltowed ‘y'promptaejutment of the miata for smoother operation NORMAL PROCEDURES LEANING Wirt Ni MY MIXTURE INDICATOR ea A CESSNA ECONOMY MIXTURE INDI inisnandbook secompanied by approximately «not dovease un pc STALLS SPINS Intentions pin are approved inthis aizplane within certain estied ondings. Spine with baggegs loadings or ooupied rearsens) are not comes mtn it ee tee aie sires meeritnete st eerante {round level Atleast {000 fo of alitute loss show te alowed for 1 [tt spin and recovery. while a tum spin and tewovery may Togs Entry allude for 64am pln ould bo 600 fet tose seouae level ‘bbve the mintman logo fect sbov ground foe! regteed oy PAR acta ao or ei hgh sce or pacing pei tha 8 powers he etry will aneure more sonsstnt an eee tothe acura bot sever ang user conte snout el el isa ned shout nd TUptsziira.thenpin wi progressio Sontrols will produce prompt secavertes thin 1/4 arn) During sx Rea BE TS Se eS SS Se eS Se MODE ep SECTION « NORMAL PROCEDURES sender stesgot tm many tune he pin igheldrow tiated he * SEAS ae ie steer ove stewie SEGRE roe caren asain ors Nore {Yaratons in base alzplane rigging or n weight and batance due to sonal slpmen n ren enya war ren tendencies for spins of more than urea However.therecovery okeles ended are prohibited, sinoe the high sens winch ma occur during recovery are potently damaging toe LanvinG NORMAL LANDING2 es ee ee ce ce co Stepan sow b avid wi lp ntingy greta 3 du ot the Sepecalytmportane in tou ‘SHORT FIELD LANDING Snditona)Aitralleppronch cotacon are cierauprogrseivaly race ‘without alding tht tes ‘CROSSWIND LANDING ading in x sg ssw: oe he minima ap eating ‘ientipa with fll radar detection, ovataroteillation may bee Se ted ite wien mahod vesleuen snttns Secrisonaes ad Stunt couse with Ue streie ase shee and oossvona racing ‘Te maximum allowable ctosawind velocity dependent upon pilot gna aaieahimtions Operation ac BALKED LANDING aed Iago rand lin ee he a ning 3 400 oat 1980 SESENA gecmion + Sout rae NORMAL PROCEDURES She go-round lim reduc ‘ "clearing any obstacles theflape ay 6 plane ssesvrsies tothe ermal lape-up canes COLD WEATHER OPERATION STARTING ine Tetiuoe Sa Rinne beam ae rot a 1. gation switch OFF enatroti closed, prime the gino four {oh stokes a the propellar i Sing ted sues Wy eae {poked postion foavold posabiliy ot engine ruming fetcme OP CO ee ce ee ee ee ee ee ee Pe a seormn 4 ‘cesswa NORMAL PRocEDURES Momieime SESSA SECTION « MODEL ir NORMAL PROGEDURES Mixture ~ FULL RICH, “Throe OPBW Ve INCH. FLIGHT OPERATIONS Ignition Switch START. Fleas ignition swith to BOTH when engine start Oil Pressure CHC. i col, ain wnperwers blow evo wing para ras, where lng is ensienl under seria weneophnls 4 Pump thre rapa to fll open twice, Retara to 1/8noh pan ) en ronewat ate o the Seo ‘Seplanenolse onthe pobli the ngine docs net start dur i{ copne lining misses in steast, {hespare plage hove oon tried over. Prebont must be ied fotos atser sas is aemptod oTON epg tesa amt crm cevincmieameacces =) er aceeaeece IES eb Sree ee ceercteamoricmrammanerests | ce agreeeaine eae. | SasSc ae cae cae ee ee oe ee om ea SECTION « cpssya | NORMAL PRoceDuREs ope ta ‘fas than 2000 fet i neeasary for him to adequately ‘heraas hie duty to awe una sold other scoat, Th cerieaed nolae level for the Model 172° at 2400 pounda maxi.) |) ‘pum woight ina aB(ay No secrmisation babnon matey tne Pedeca ‘vition Admiaitation iat thonoieelevelnofthsirplans ever ahoata ie sccepable cr nacoepialeforoperation mina. oroutol ay srpare om so ay 190Nope PoRPORMARCE SECTION 5 PERFORMANCE TABLE OF CONTENTS aazee 7 2288.SC oe ee ce oe cc eee = eS a ee ESSA secni0n s MODEL 17 PERFORMARGE INTRODUCTION shih the irptan a Tohniques 1 should e ded int the performance information presented in the sppegandentntes se tn ows mint enna ‘ommended on ‘nba Some indeterminate variables sc Bropelior condition, and air ius ay 20 et Sr more in range and thuranenTherelavy i ie imporant oeelee Svailble information to etimaie the fant required forthe particusy ‘ent USE OF PERFORMANCE CHARTS nde prtculr portormance igure with reasonable searacy SAMPLE PROBLEMSECTION 5 PERFORMANCE See “Toa detnce $20 Nauice nes ‘Bxpucet wind onsoute {0 Knot Hendin ‘ltd presere aie 200 Poot Bartel 500 Powe TAKEOFF smusP itil tance cas gure, hou be vole xepig in int bai de town afe aoe on the abort fed ta 43°C ous be uaed andres inthe lowings ne meer sm ttitettchare "Tee cormtion fort #2 knot bead i ‘This routs inthe fotowing dstano4s, cores for wind ontttaiande con ee et 1) me ate Cm CS CCC ce ee ee oe ee a | cruise ‘plas winds alt antesteiane'yperormance.Aigpial creep broben, However: te power sang selection forervite must bose prot chart Consierabe ds eavinge an longer range result when ‘Deer owas gears For tesa rviem nrc power o ‘hing oped chowen is 2500 RPM. which exties the following ‘Feu rape i ‘ton mere scouately aug the Tight manne ‘FUEL REQUIRED Tipare® hows meta lin fom bo e100 ot oguires 16 galls {or moat hight panning parpones However urker corrosion TortSECTIONS, esa BERPORWANCE MOSEL FP With this tat nolued, the fue artinata would be cloulteds follows ust elim, standaed eperatare 8 ‘See eons pate cores tim Bomone ing simi procure forthe tne limb resin 2 ute! £8 wan nen be ground speed for eruiee te “Therefore the ime required forth orise portion of the xp $04 Nautica Mies 39 Hours kaos es “The uel rauind for eras A galone/hous = 222 Gallone {A minute reserve roquires: Bor patone/nour= 86 Gallons “Te oa eatin fel sogured i follows: teenie ea EST acne ‘Once the igh is underway rou scouts beter animating the i Essa sEcrion Mopen vp PERFORMANCE ‘required to complete the rip with ample reserve Lawoine ‘A procadure simiar to takeott should be ured for estimating the landing Sstanes te eesnntion tpt Figure 16 presents lasting distant iformator free sigue, The Gmetoes cones, A corretion for ne eect of wind may be made based ao Note ® of the ‘ading chart ustrg the seme procedure as outlined for tks. DEMONSTRATED OPERATING TEMPERATURE Stlistacory engine cooling nas ben demonstrated fr this sieplane swith an ounce airtemperaiufe 9° above stander This wot be 1 ‘Sentderet "as an operating limitation: Retcrense shoud be made € Setion # for engine operating limitationsSe Ce ome cm coe ee ce ee ee ee op a a a , cssana snonioy s Pie eSB Ete con SDE IRSPEED CALIBRATI AIRSPEED CALIBRATION SUC AERATION NORMAL staTic soURCE EATER/VENTS AND wNoOWS cLoseo ‘Ser oe gt itd A sereiiteas| SS AS SW NY Be ye | Fone? ws | gaze Rrematenas| 8 RAY BS occ RS | BSR 8s suceer rears rommunns | @ 2 mm a s2ene Atrimoiehas |S SB BS z a fos | S28 one oO HEATER /VENTS OPEN AND WINDOWS CLOSED FarsaP | vara )) Prtaesior Figure 6-1. Alrepee Cali yomminas | 2 @ @ w — w wo ne ms itreiaiens| $3 8 3 8 8S We og ) 1 | romuasns, | 10 50 © 70 ) see BS Senins| 8 SS SSS 7 re [soratiitins| SSR SRE Figure, Aeeped Caran (Show 0 3s 30 Say 1080 may 1080 *Senronance, Mopper Mobe rar TERPORMANCE TEMPERATURE CONVERSION CHART STALL SPEEDS MOST REARWARD CENTER OF GRAVITY | | i w l«lalo|ala ao oo i w | w fslalalelelela|o e - a} |] wo] » a MOST FORWARD CENTER OF GRAVITY ee ee ts a [= or ® B40 so may 1080 m0 May 1989 « suSBE BeBPrur es Bs SF ee ee 2 Ss = SS cesswa srcrion MODEL rar PERFORMANCE casswa (ives) sooner noores, 3.814 2 eEEgEE: 2 20x] so awl ms a ae 2a ry cats 1uOHS ‘S81 0002 aNY Se o0zz SONVASIG 440aNWL ‘0 ny 1680 2a 2a Bae Bet seotiows jaraia ivORS| 81 0082 LHOIEM WAWIXYW SONVISIG 44O3NVL[SPE eS Se eS SF G22 2 SS SS SSS SD SeerIONs gesena | BOSE ner PERFORMANCE, MAXIMUM RATE OF CLIMB. TIME, FUEL, AND DISTANCE TO CLIMB MAXIMUM RATE OF CLIMB coro cours Fen Cody yong, 1" 1 ta ond i sl get soe Ecstacy tm 1st tne tmp ) [ews |omesse [seu Jame rrowsentevee tus [ALTITUDE | TE free “Tae [os use Porrance] | OW | BS Gee pepe] oo of eff yep e fe &|:lelelele mefotafee {sf ] Se): )}E)2/8/8] 5) Siitfetsy els aS | 4 | @ | : wofstnlo fel a | ow P68, Mes ao in mfofalatafa fo. y , 8000 2 )om fw an 2 | oo fatal fal a fw i wm || fae fala | om[Pa a SP eS SPS Pes ses es eS ee ee egg ZS RANGE PROFILE 45 MINUTES RESERVE a0.GALLONS USABLE FUEL, CRUISE PERFORMANCE Fressne|p,] aS an | STR | cE Score cgee oom eye Te [A] cow | ate [eras] me] ty ocas ore] =) |) mn om Ia 5 z too wo | : : ) so wo |e 2 : | > i ie = g & Bom HRS 250 a & 5 eras ash ae =| BW) E) ee yt) no BPS) R/H/ BRIE) 2) , a Pigure 8, Range Prtile (Sheet 13)a wl RANGE PROFILE retail AOE =a cess secre SOR ven RIES RANGE PROFILE sSmnres nesenve o2/GALLONS USABLE Poet SE so nue toe = ‘ev lw fo ef eigen nd mee igure 65, Range Profile (Sheet 9 of 3) 20 May 1890 .Se Se SO SOS SBF SF FFT 89 S282 Ss = 2 = Fe mo SEEN SEB nn ew ERE ENDURANCE PROFILE g 28 oA MITES Me. Fg iBBE CONDATIONS. | u FEES nme owe | ae Sicmemttmwemenswanunene | fp iRfe on day | . i i ai t | HE joe age | Bf] obs Ls j alt i 258 | ei 4 il : ft foo z d 1 u : : al jes hoa uit - y oRE [Be Lie Hee ig diet [Bad |=, ee 1 bay Hus [p HEE LE Figure 8. Endurance Profile (het 303) see so my 1090 0 May 1580 S124 blame)PO ees ar asrrcT a= cpsswa SECTION 6 MODEL 2p argu & Batic MONT List | | SECTION 6 | “WEIGHT & BALANCE/ | EQUIPMENT LIST | | , ‘TABLE OF CONTENTS 20 Mas 1000TSS SPS SEI STF SF SF SF BSF Iae es 22 2 Ss a pana, section 6 Sopnt ine waraut a BALANCE! j aumaNiNGes INTRODUCTION | eid zttion decries the procedure or entablishing the basi ems i ‘Meigh ‘and moment of the sltpane. Sample forms See pranised Fst vst pct ermaton oar weight a, 1s th esponsibility ofthe pilot to ensure that te airplane loaded ropes ae AIRPLANE WEIGHING PROCEDURES nate iret rsmende operating pressures ; rae Oya anon a Ne ane ) ‘move oll sung siin blog din so Nerang ete ab a a ag, Eom itt ay lc a 2 bevel ay) nc fer exch wheel (minimum seale eapacity, 500 ees ons psn cya © ey Sr be bien ene oe waeeCe weighing, Spe Snir Tina) hat ane gma tally long he fae eer {Using weighs trom lem 3 and meneuremente frm item 4 the 4. BabieEpty Welght ny be dotrmined Oy sompleting figure 6,Dee VE/IT aS TGe. .FSe0Eer — T SEecI0N 6 ‘cesswa gEsaNa secrion @ Serorre pavanon opal 5 5 MODEL rae wears BACANCE, BavPMeNT Lior i BQUIPNENT Let {oe aon ny SAMPLE WEIGHT AND BALANCE RECORD ES eerie ; to i i i i Sate te te i . ene = ie = ib cH fanaa | i 9 May 1980 6oe Re ee eC ee | SECTION ‘cEssna EQUIPMENT Liot mops WEIGHT AND BALANCE ‘rn following iformation wil enable you to operate your Cees witha te prescribed weigh an ontarof gravity aatione To igre ‘Tmgsiandbeiace uve Semple Probiom, Loading Oph na Ceior, “Take te tasicempty weightancinoment trom woightand ‘puanee tcp carried i yeur silane snd ener hs ihe Sores {hed YOUR AIRPLANE on the Gunple Loading Proters Problem 7 {obdenditiavalgewsedaa\temoren/ 000 one onding ew tae Loading Gimp to cerning the, momen 10 for et ‘Ballona ee ob otic then it these on te fonaingprolom pet prs sea ea tara Soon cineca fears eitaeea ene iisierneaete aie ake ‘caine ce te str ios meueaenceteceeome ie rea eee Seas eae eae Riese Exes Tol the weights and momen/1000 and plot there values on the elope a dtermine wheter the poets oudingt acnpatle; oa 0 stay 1000, ccesana Devine geovions mo woroutr « BALANCE! BQvIPRENY List LOADING ARRANGEMENTS: 0 May 1980, Figur 63, Losding Arrangementsee eee eee eee ee eee oe seorions cosexa Witont « xcancer MODEL IP crsswA cwcnow 6 BaUIeMENT UST Moet imap WeioHT « BALANCE, CARIN. HEIGHT MEASUEEMENTS | ‘SAMPLE AIRPLANE | YOUR NRPLANE é ae eee Ee] i fee | 3 i ~ i 42 i] TL. ze J 1 Oo az | & g | ° g on ‘wana 1900 so nen5 oe oe ee ee ee ee ee | section essa cpsswa wecrion @ Beloit ¢ natancsy MODEL rat Moet irap wei a SALANGE RE BES 2 se ‘prot anon aerauiy exavon & f gf 8 8 § € g B ti ail iP gif F § 8 ei > ' ei zs ; z su § : ti Bg : ae }O : fe i s § 5g = ’ ES e 7 . | eee SH Ree F FR Y : eer PER PEE EE 0 aay 0 Bo nay wapeee cA rR ec ee | Seorion asswa Wetoter& eatancey mona ee gasana secrion & ise ‘ar \Wergur & BALANGE Faience EQUIPMENT LIST t : ' etocaesperlee nae Jee : a i z, fe sche iae tear ei re a= Ee ta F fe Rie | c k 5 r . “°° eum ST end me" 0 att iL gs tome eaianmesesyes 3 gi Toru orsspute FAs poe nee Bs a il | SemateronaGerettamfattes nite sy ie roca is : a PEttitried fetianee enc ‘onno HIM awe a3a¥0 Hy "anathema compan dowshot ees elss i Fae | wwsew wan sg biry qx ase mmred, a | eh TREE i eae ‘UBER ah iat f ponnieou BEER Be ie Ss SENDA i th & Nowsteas3a Ish Wiawaimos [evar] 2 = ees # Tz ‘ i i sro cs Lee MATE | ovance z g See 8 wariduty Tefaly erie nore Be ish Piteceoard Ht aber ele rue \s SPUN ate Bavirsee ioe Te NolLdhH9S30 1S7INaWAINOS SECTION @ Rw ee ee éBe Ce a ee ee ee ee a a cesswa sEcrion? | Mooet-vap AIRPLANE & SYSTEMS DESCRIPTIONS SECTION 7 AIRPLANE & SYSTEMS DESCRIPTIONS TABLE OF CONTENTS ‘Compartment . : rit Sei at crn © He Shoulder Haroasues 2 72 isereee OD mi nonin nos D |) ytd SE ei Ht Exes ge Ao Ca Ste ~Se Ce Oe CA CE a aD COND NS ca eB SECTION? cpssna AIRPLANE & SYSTEMS DesonIPrioNS MoBEL fa ‘TABLE OF CONTENTS (Continued) » 299 Allerator Control Unit And Low-Voltage Warning Light °° 7a Seta oer ten g Lighting Systems 738 eT: g is eee a Adin nis cs fecbasttatahehine nes 00S Vertical Speed Indicator ret 74 ‘Vacuum System And Instrimer & : eT naan is i :# Siete Ee some su i Sn RTE Ele nn 8 uae s 8 vs 0 amy 1800 Seba ap AIRPLANE & SYSTEMS DESCHIPTIONS, INTRODUCTION operation ofthe airplane and its is optional and'tany not be ‘Supplements for des of Moe. high- wing. sngte-engine ‘at and erage Ter gene 8 fuselage Is conventional! formed sheet meta! inger.and skin desigh retereu tone commonocanee Mea tring sro “oot pore nnd ene on tat gs ans ot "ttingers The enlty structure fn covered with aluminum sn in ieee inves oe tikmccaeanearineee era the Ristptrarcptnaebatenee sags, ara cigeirties elaine it at vGpcatcaaneinti me one ec penetrance Se ee ie! inpanel whieh tip, a rou ‘Aefuntabte ri ab te bce of tho ttalng eae Fhe Sp ateoe ee Incorporates Yeading egeexiension which cosine e Sean weaCn a Ce Oe ee co co co ce coe ce LS ees ‘seor10N7 cHssNA ‘gessna secri0n 7 AIRPLANE & sYerEMS DESCRIPTIONS Moni iat ops rer AIRPLANE & SYSTENS DESCRIPTIONS gern : SUBVATOR CONTROL SYSTEM, we > bd Figure 7-1. Plight Contra and Trim Systeme (Sheet of) Figure, Flight Control and Trim Systems (Sheet 2 of 2) 0 may 190 ome 1609AIRPLANE & SYSTEMS DESCRIPTIONS ‘crENA, NopeL ner (wor ensign sr, “nue ernst ‘igure 72. tnetrumant Pane (Sheet 2 of 2) 0 May tan‘The horizontal stabilize Is construtadof forward and aftspar, sibs and {Sim tab ctor Construction ofthe elevator gonsits of formed nding bike icv im ah cotsee st apar ne cease {nSorporais extension which nia tatance weights FLIGHT CONTROLS. miurenecu gue bs teria et Seles abo for tharuddor/ brake pata They consistots TRIM system yal be, Insaled (ob igle 7-). Elevator trimming ie tong the ne ws uy ine a owe-dowrnconerseyaltrotation wi tm noe-ap Rado imine Ena’ trim lover mounted on th ool pedestal, Rudder timing fe ‘Stomplised by iftng the rig ever up te clan ‘the tori tothe desired rm ponton. Moving Tih hte plane nome ig conerely mom INSTRUMENT PANEL ‘Tne instrument panel (6s tgute 7-2) 6 designed around te bate“ Ewe eee ee ee ee en ee ae AIRPLANE & SYSTEMS DESCRIPTIONS GROUND CONTROL ‘ght redder ela to stn sleet asa unamattanateretasegsTRB SE TR ST STS ES Ss a SS ‘cEssNn MODEL Fa WING FLAP SYSTEM. ‘Tae Hesloslot type wing Nap (en gure 79) ar extndad ot ssitiday potion swing pesca eer ona anise p el {Bie eave ap election pain Tue stn ore sonted oy ot aes lap revel i ogres. Fe wing em ict protected ty a 0 ampere ciel breaiar abled EAE, Shite eta of a swe aha coal pel LANDING GEAR SYSTEM Peletingarsicieceye nin steaming no bitarut ttm easter SELAL Bae else ey ‘erode firing over tack brake nae sn may 19 ceeeaet section AIRPLANE & SYSTEMS DESCRIPTIONS, BAGGAGE COMPARTMENT | BRUINS Aeod ates ae ie si a SEUSS a iy ree i SEES Mati mente tetern oaetn i caesar angemietconsst of wo inavduaiy adjustable four i plotand on soa aasenger ena (Te four-way seats may be moved forward or aft and the ang of the ) seat occ i itinitely adjustable. To postion te soak Ut tee aoe Sate ‘ew the soto af the eer ire aye ena la fxedone ec et otiom with ‘ever ioaiedtsiow ine comerSECTION? psa AIRPLANE & SveTEMS DEsentPTiONs oseL in {ie ea eae. Two pec seatback ae jsyos ‘buttons recessed into ski rt pari ‘mounted onthe icorboara Wea not cebupic. tad peinty eaerece ‘otating th wat bttem up and stant tcontaca the afesun baron neat aaa er an ot me cntgarinexcet ne shut nat Tondjnt th heuares apply onoughpreeure oho lower tothe nr love The heat maybe Fomove aug ae ising unt Saengagen toms be yo fh sat be SEAT BELTS AND SHOULDER HARNESSES at bls ae altuaed to tings on the Nooboard The inboard ofeach seat anathelinrhaltinoutnnrdtenchsent, Tranmere ett sarees 2S ae Se aera si earth eta toate teen a ‘SHOULDER HARNESSES "eh opt seat shoulder harness (ne igre 7-4) tached tm 08 te 0 may 1090 PPS | FS Essa secrion 7 MODEL rap AIRPLANE & SYSTEMS DESGHIETIONS, (uorsstarsnowny Plgvre 74. Seat Bolt and Shoulder HarnessesSECTION 7 organ stove he window tne Sarnes of te rear window Each rer geal barnes i sowed boning ‘To us a tron or rar sot shoulder harness fasten and ee Sennectng ink firmly nto the retsning stud onthe seat at int hae ‘Then adjust to longth A propery adjesed eneos wit rete ‘ecupant to lean forward enough to at complealy eevee ote ScSieraton” Ais the pit wil atthe eet cee oan ‘Removing the souldorarneae x accomplished pulling upwerdon peter inept tari eesti en ‘Mushed oie ni nus seu ee ope ea ee eat INTEGRATED SEAT BELT/SHOULOER HARNESSES WITH INERTIA REELS board of the two feat seu A septs ceat fat” Toeate othonsd ofthe seas inertia els iio complete resto oy lik onthe tagntes oat low sullce et pl neh to Sart ‘waware and insert te in ina neta belt bec Adjust bok roneton Cee Se eS Te Se SS SS a AIRPLANE & SYSTEMS DESCRIPTIONS scrote the ap by pulling upward onthe shoulder harness, Removal ix scropolicned by felensing toe seat Sok Bock which Wit etoee ae ENTRANCL DOORS AND CABIN WINDOWS Entry to an! ei from tho airplane in acompliched trove ler ot [TESA doors, one on each ude te ein athe ons Soul postons (Weer to" Seto 8 for cnbia and eatin door aieeestens) Thee Mosrporate «reoceed exterior dor taadle x converting aioe geet sedis openbic window ine uianor Races area ance paling oon. “Toston os ‘he doors from ie te ‘otaing the door andi forward tothe LOCK position (ash with the any Sige wil nota {ora and should not tly shove the doce outward aighly, and force close ‘equipped with » spring-loaded retaining atm which will help rose theSECTION? cesswa see re nar facet Gutiertanareeqecntagean aici ‘CONTROL Locks -surites to prevent damage to then aystsns by wind btteuog ee ‘tepane paso. Th loss const of shupedstn red wun geooraee ite stacked to tue athe sivas in'n sigh Wallng" ce dent ek ee ENGINE ‘The altplace fo powered by a horisontally oppose, four ) [ls an bo expected wer th | st TT - . = so Figure?.8. Fuel System (Standaed and Long Range) 00 at 1980 0 May 1090 oeBem eet es ws ws eee 2 2 2] Ss Ss SSS SECTION? casa AIRPLANE 4 SYSTEMS DuecRIPTIONS mos tat ousahn seomon (ODEL rap AIRPLANE & SvSTENS DESCRIPTIONS Het copiot') eto ue pets which are intoroonncl ‘Spin epake foth mala vie rate aye sty sos taimam brake kept bake pete properly mann eee eitactemcrarcatears cee eee thes ang ah ene se Spe Gatatemgone Paria aioe aa leant gayene™ wi wine monte maser ss ELECTRICAL SYSTEM te ars a eaenteele mae aero eee Heaney eure ar) et Se Seen cee ear omens ore erat ‘Hons ris netic oatremte TTT ‘tne rapping nant pow vores. naviones shmaging te avionics Suigmeat em PONE om masten switcH \woN'in the up potion sada sine ate postion te ane sansthe Figure 77. Blessos! EystomNinPeaNe DESCRIPTIONS mooie at pute Ibelag BAT conto al lsricel power tothe irae. The et AVIONICS POWER SwIToH Interrpid aa thei wil imately move ec off psiton. stra peng he ech ‘tones power smi sbosldbeplsced sn AMMETER ARJERNATOR CONTROL UNIT AND LOW-VOLTAGE WARNING ‘Sa enaeeewewee S S e e S ee SECTION? AIRPLANE & SYSTEMS DESCHIPHIONS SST ae marae tteare Sischarge rate on the ammeter'Under ieee sondiians preci oe eset by turning the master wrth of and beck am seein He ee ’ ‘hargeinclotons may coca Sere low ene higher RPM: “Themarier itch rod okey tince the alternator system, ns MORENO Oackiwaie Tv wenn ight may bo tated by Hang on te landing Hehe ane mena arog i he AL ponon of tre maces Swiss ee AERO HHH vic 8 CIRCUIT BREAKERS AND FUSES eset" iypecireult breakers mounted onthe felt rae of toe alice ate ‘evs which arnt protecting by eirouie beakers are {he brary contactor closing (estraal pow) ciruin clock creat at figathour reoorderciseule Tum ciouie eve poteccel Sy ees point Aafscon tote Satbe ees fF fF Pe fs sess SS SSS :oTON > crsawa AIRPLANE & SYSTEMS DESCRIPTIONS Monti rae GROUND SERVICE PLUG RECEPTACLE A ground service plug rceptace may bento permit haus of imainonance work onthe etcial tne serene eae a LIGHTING SYSTEMS ‘Convention navigation lite are losatad onthe wingtips and tp of| tue Fula. singe luning Kent i ose tte Cowl es oe Be odo he re raat ston nce mc in door, Deis he stots igh apatom ne prensied in Secon 3 Sopot, tm eure ei ac operate Wy BONE LOTS tes nein n teeta conte pan pees Weroeohes ‘The ftashing beacon shou ot be used when Biying through clouds or overcast the using phir romuntr dria patie tine “Soupere: patel ainigtean proaure verona apse INTERIOR LIGHTING ‘ocelot ote, Asie steht taag)on heoverkand asrumen: pane andawitcand contro pane loodighting conic {ie foe lighting mote hes rhc suns overncee eee ees cBsewA SECTION 7 HODEL rep AIRPLANE & SYSTEMS DESCLIFTONS. ight dosing aos. Post ligt itistli) RADIO Ut kn fullcouniercloorisa Check Sarteeioes eee 1gfeiaieta i cpitosnasetnracbateestes ‘A cabin de ght, in heat part tne overhen ‘A contol whee! map lights available andi mounted onthe ottom ot sng pes coal wh, Fe igh imines ne owe prt ee Riggins dig lee perationn, soporte tw igh rat non the ‘ype ebcomtat control located st the bltom ofthe contsl eiea ‘oth red and ‘white bubs and may be positioncd to ihereoae soe Sear cei The igh ented ya eh below sit Postion will provide a red light tn the bottom position, standard way The most probable cause of 9 light failure to « burned ot but tommy erent nye ihltgproma tani Wine ‘opened (white button popped oul) and there is no Obvious Indientens ofaCABIN HEATING, VENTILATING AND DEFROSTING SYSTEM pe tton ofS pskopt Gas hi and UA ik aed temperature, pall the CABIN HT knob oot approximately 1/4to tack Fon eabin heat and ventilating ire supplied by outlet nles paced sero cata mania just forma af tbe ptr aa comity feet Rent Separate adjustable ventilators supply additonal ale one near ech oventatorsa aor lt ad land PITOT-STATIC SYSTEM AND INSTRUMENTS. Ssootcet ses es SEMA section 7 AIRPLANE & SYSTEMS DESCRIPTIONS S sl ¢ ‘auras atte fF oY aoe Tee a a mas am eto Figure78. Cabin Heating, Ventilating, and Deosting SystemCee ee ee ee ee oe oe osena section AIRSUANE & sysrEMs DescHIPTIONS Monte Se moore ABTLANS 4 EYGYOALa UIEURIPTONE if) cons of hening element in ovensoano iting Th sth andere brniar ne loon on he — JZ 1 1ronous instant resaings are eprint lo wae Fen ti acum RELIEF vac seni ste sores valve shoud be pala wee ™weuresowee te AIRSPEED INDICATOR ‘The sitspeed indicator fe calibrated in knots and miles per hour, ) Limitation ane range masking in IAS) inluue the whe ae OO len arto 7 kns), yellow are (2 f a8 ena) a TS mera 3 vecsection» essa VERTICAL SPEED INDI: ALTIMETER Alrplane studs depeted by «barometric type altimeter. A eno set the tower let porn af abe iaticuor pre sajineeaa of Ie TOR VACUUM SYSTEM AND INSTRUMENTS ‘apne roe acum stem ne gre) prod ation inerrant pat end nsramensineasings secon fag) ee ATTITUDE INDICATOR cu tenner pet etn gh te ane DIRECTIONAL INDICATOR, ony sree ee teers ne Sih “feed ‘To jut the somce card to corso tr v8 Do ntay 1680 SRF eK Ss Ss TM PZ Pe Pee Nopat ine AIRPLANE & SYSTEMS DESGHPTIONG SUCTION GAGE carat rene sete 00 ‘The sill warning system should Ye checked during th preflight a lan Neherciat over tn vot openg St AVIONICS COOLING FAN lone cooling fan system te provided whenever a factory se RS Go ini sent ee hese limite ne posi of melaturo containaon gs Power to ae electric an ie supplied directly trom xpul-ol ypeAIRPLANE a svsTEMs DESoRIPrIONS pled te the fan antine temaste ISON. This arangomeat proves tif ciouluaon through te ‘adion o remove sponsible Nut tour condition twfore toe vad tnt {ured on At engive sar iio recommenced thas he crit beer te 1e1C ON zoo ding periods of Teaghy muitonane wih oe mosat MICROPHONE-HEADSET INSTALLATIONS ‘juste for volume level by weng tho lected fcever volume control, Nore ‘men tranansting, withthe bandneld microphone, the Pilot sulky to meroptone pace tue morpho at lo a pote wo he ips und open recy tt STATIC DISCHARGERS trea rane, elon of ck pe tai Aisehargre te eecom tio aa Iie rough deat or various fort of prsoiaton (en snow ‘nsalaion of state lschargers reduces interference rom precipi roe oaay 190 SS See oe os BSENA Most imp SoTION 7 in, stale but A is peabe to encounter savers preci unaitions whic might caume th iogs of radi gale sdlschargers installed Whenever possiba. vend eke ‘lo rue to prevent oso phen sith atte awotoance te porary tose of radia 9 hay sen aa SECTION Tahaan AIRPLANE HANDLING, SERVICE & MAINTENANCE TABLE OF CONTENTS: 90 May 1100-Ssere oS ESSN seorion a MOTEL rae HANDLING BERN SPRINTS ANSE INTRODUCTION hie section contain factory sesommended prosedures tor proper ‘ntcling Aad routine ere and survicing sour Ge if your alrlase i= to ain that new plane pevforetsoy ee ependabiity ‘it ie wit to ollow a planned eehesuie onto oe Brmutnve maintenance tasedon cunationnd iyingconstns ween ‘Bred your tou oe stare wrakenstearpae io he eepane, The code may be acd in sonhoneticg ‘with an applicable Parte Catalog if tnieh andtrim information i needed, OWNER FOLLOW-UP SYSTEM es nou ap yam may strane Sa gion yaeetenttaaiaee nme Eilon diet aceeattecann tare ‘Sta tara er Sereeniercpte ata ercaerga anne wblestons and Might operation side are urnabed ia eosection 8 cossua S Pilgrs creerisns P EGNER Sohne The following ational publications. lis many other suppiestbat + INFORMATION MANUAL (Contains Pilots Operting Handbook + SERCH tauats AND Pants CATALOGS Fon YOUR: Your Cosa Dealer has & Customer Care Supplies Catalog covering epee hy contacting your eae Came Services para Comnt inining the owners name, airplane serial number nnd ‘etuets snc the lots Operase Handoos nd PO Reprod Alpliemigsthansaiskeatodorspecic : AIRPLANE FILE tousdas information and censen hat ace part) ‘tw spline ie Ts following ia choc fo aa fe aed cESSNA anpuang SERVICE ‘A, Toe displayed i the airplane at al times: 2 Aira Reghaston Cathe eee 8 oom S08. 8 Aieratt Rodio Station License. iffranemiter neaied (PCC Form ting Handbook and FAA Approved Airplane Flight ‘ad Balance, and associated papers (atest ony of the it Aitortisn Paras Pa Posse oof aohcaeey 2. Engine Log Bowe beeatried inthe plane at ll ines me AIRPLANE INSPECTION PERIODS FAR REQUIRED INSPECTIONS ‘Asrequired ty Federal Aviation Ragustion, al eit lrrattof US. aSmonthe In adaltion et @ ANNUAL tncpoction cecrat ‘petaied sommoreatiy Yor hire) mus have x complete ospetion es ents lt io therasponaity athe ounarlopeeccoo pat seenel ees Sita aoa lewonieredactvused- whan enopeconn are SASS Sansone aaocnterpcaoHANDLING. service open ime UMAINTENANGS: name ‘npn motern progressive iepcion soeaia he ont ‘appueable to Cea ttplanen Te program ponsbliy tcomply wit all a iepeeaon rene a factory cso pasar a es Paan CESSNA PROGRESSIVE CARE Soe ceo ccheemen gtr tans ot apectin within ihe lra'é monihsot awserthpstne cuergetayoe iplano atthe factory, plonso tale it to your Dior reasonably ata des soero so c YoU take delivery, so the aii! inspection may be performed lowing te Beateeto tke say minor adjussnente wich my be necossasy ‘Shom you purchased the rp PILOT CONDUCTED PREVENTIVE MAINTENANCE eats ite hereon is eu of eee ‘be performed by piles, ce to snare that proper ‘procedures se foliowed. Your ALTERATIONS OR REPAIRS GROUND HANDLING Towina son TRS Mpa Is most ually and ally maneave ‘eee! thenowe gene turning a ‘eee wi out tteSECTION 6 cescna LE NAINTENIANGE ‘esulting conic with low hangar doors or structure. Ast pose tire or ‘ened svat wil ln crease at beige PARKING ag tet pet ee ring lath oh er Ihgn wind conditions. te the aleplane down ae ouilined inthe flloong TIE.DOWN, tue pad atatane By guy o tng wines to eda heneans 2 Installs surluce contra lock overt in tnd onsen 3 The euiciealy strong sopon or chins (pounds tensile ttengt) to he wing land nove ie dome tees aes Sees Seen ap tea JACKING Whe a requirement xii to jacethe lire airplane ofthe ground. or IECL.Tn et poate ae wed he Jung Sperone oe Incr mn nt myo ache ang tk ad we snl eric ps sy te rc wl _ ‘ust then be loveredfors second jacksngoperdion Doser Teer teresa, ‘Shoes shutlanesuaty using te inalieel eae weer at ‘te sround by pressing down of a tlcene buinhens Jou ences horlsonal stbiierandallowing asta o ean thotal ic downsine Note ‘oral in aising and blaing the nose wheel ofthe ground we ee ed gpsswa HANDLING, SERVICING, Sorat ally placing snd bags or suahe weights on ach ie ofthe ‘ea sould be securely ted down, ™UnA ANOS aTeaattabie, ondlio. by meane of uae signe of coppet det ‘weights ‘pporingtbulkhe LeveuNe intieleval ervrponing ptstcon ttn pper ator ins stats ’ Fuvaste sToRaGe ) 7 WARNING. OFF thetic ielaend,omigtare cept et ‘Biotin carla snr foe {After 30 days. he airplane should blown for 90 minu:es os geound ‘unup should te made jst long enough to produce ea el tompeeiens thin the lower green aze rage: Exeessive ground row eae fe uuerln hit dom andamer sc apaeseintncengine heerseoTions cesana Ee MAINTENANGE MOpek wer SERVICING Conihiets servicing. nopecton tater roqusencnts oryoarstans ata pion thon aa wick soe tsting wt Special interval, ‘egute soci, tapection, ‘Since Casena Daler conduct sit 300 contact your Coo Dealer oonceraing those roqdemente set ‘begin seedling your alsplanefor service st ne resomncsiea oes, ‘epocton a provoualy covered these rgatstonyeguiretone thou check with ocala ‘tiie where the airplane is being operate _ or quick and ready seference,quanttae, material, and specifica: ‘ons for iequenty ened serie ese re oo ftows ENGINE Ot, GRADE AND VISCOSIFY FOR TEMPERATURE RANGE ‘hs plane ea dere from he tory th ition grade ‘toperation, andthe following oil used as specified forthe evorage ‘Siaon ir imparsture ins operating MiL-L#082 Aviation Grade Straight Minera OM: Uo replenish Supply during the fret 29 Rout aid at ibe frat 25s a faeos, ene uns tl ot50 hours hax tocando Si = an et aaa 350 208) to 920 (00°, urn SAB 40 30°C (°F) te BG (70°) ues SAB 49 oF BAB 90 Betow "12°C UOry, ase GAS 90 ‘argon or anata a Rin icici Secon e tats on.axo ot nize cine Peer antes ninngn on ump etree {ier Renae cenanear aaron ets seeslitacin i ctemecianttin farses Sterna maencemimrmnteay as leer vagaaiirccmae astra ‘oni et fe tein nears by Jonged operation tn Gaty nfoas, cold climaten, or when short GIgNe SHiguhemosatn naar anohe Nore Drone fa gt eg ae Strid cstewsatyeatraaies sic ieceuice eeue once ‘Shot eeamanr es eweie ibe coe ta er dence of lsalmge, and security of attachment. Engine Seca ane ana ee Sere ae eee ‘burning. defective insulation, Iooae or broken termi nile 90 May 180SETIONG cassna eMamnrenanes moves ea FUEL APPROVED FUBL GRADES (AND COLORS) - ots Gensa Aviation Fue (hos) {00 (Forman on 130) rade Nove mn Fuel (Green. i (CAPACITY EACH STANDARD TANK ~ 24. Gallons. CAPACITY EACH LONG ANGE TANI 2 Gallons CAPACITY BACH INTEGRAL TAN 94 Guns, Nove care mas fe apa, who ruling ad Pace the fool selector vave'in either LEP of RIGHT position , ) Service te tat eystm alter each fight nd keep ae ‘ful to minimize copdenastion im aks yo) ‘ne exception to this can bo encountered when operating une he combined effec of (2) use of ert fute, wah) Men hum ay Sten nde rn oly gh atgh acest ESSA Mooet imap tiple yest mone supp The Introduction of let or EGME compound int thee lwo ditinet tees itabnoros ted 2Shd @) loabol has teste ten Aleohol fused, eto be bland with he iy volume, Concentra ‘The manner In which the alcol is aed tothe fut ie significant Seca alotel iment effentive when tinovmpletalyaicealeoe ns ‘el Te ensure proper mixing. th ‘enpnscoel sowage wi some ue in ene sete jroximately 23 guion capacity) and teen isenaterrng ths mature to thetan porto tne el oparation SY high quahiy isopropy? aleoto! may be used, such as Ant-tcine Fu tise) or nopropy!Alaakol (eteral Spavieaton ‘HSn). Pigure 81 provi alcatel mieing Pets lesan "thylene glycol monomethy! ether (SOME) compound. compliance SiS Eye Pl Pek SD, fond ma we Crealy Figure 61 provides EGHE-ful mixing sate inforowtions aro {mportantbecause aconotatration inexesst ofthat recom ‘Mendes (15 by volume maninun) wll route ‘mental flect he fa i lending equip {rer to obit proper proporteningSECTIONS cnasna MAINTENANGE Pte g2 Lai eE me PAE Figure 1. Additive Mixing Ratio Tarn Prolonged slorageof he aepia wil elt ina water bale in ine ‘cola eke ou hed Annee furan LANDING GEAR NOSE WetteL rine PRESSURE ~ 94 PSI o0 5005, Pty Rate Tie MAIN Witte. Tine PaESSUNE ~ 26 PSI on 8008 Ply Rad Hes [NOsh ORAR SHOCK STRUT = Pincare nowt so foad on tae ota aes ar ae POL eat ‘MoDEtraP MANDLINO, SERVIOING CLEANING AND CARE WINDSHIELO-WINDOWS ‘The panic windshield andwindows should beclesned with an srerft ‘indie cleaner. Apply the canner springy wits ext ante asso sow coe motnened wie Star sane edamame enna th ‘Novos e gasoline, bepsin, alcoho, xeon ire extn- {shor or enti Bald. laoqueritinaer or plas lease {Sean he plate Those maerai wll sash the ess 4390. A tia, even coe! of was. palished ou by hand with clean soft faa ‘hia, wil it in minor eratshew ac bp proven furter ecratcaigy ‘lean ost aes teoarng period wl aye bon umpletes peor {story othe trplna, nthe avon tt paliening or bai tore ‘within tn curag pertod ita reommesied thatthe worh'oe done Toons Sreeenen in handing wneuna ain, Any Conn Dea a py ere cme hy om seis cp. trey ec {St Sraihes should never bee, move saabor cand grease witha Semel eS ‘Waring inunneceasaryokep the palttadaurfacee bright However. .Sting ot wax as tout vot tthe ograed ell tadon neeang ‘nose cup and propeller spinner will help reduce te abrasion encountered When theairplaneis parked oats inealdelimates adie aceaeery se samans eee igh cre show aan ret to ed White wpplying tedeiolng solution kaypitamey from tnewindahtels and cabin windows ios ibe tenho mil atc te asic and ney cee PROPELLER CARE ENGINE CARE ‘The engine may be sloened with Stoddard solvent, or equivalent, then TaTON eraoula care soul to lacrcn equipment ‘Stunt ng y INTERIOR CARE ‘lot up any opted guid promptly with cleansing mus or rage. > Cesena, section & secede. Continue Botting unl no more liquid Is taken up, Serape off stctymaterias wih dul ale then spose the es sng Beto uni a reat simetructionaCutae Sontaane? bri ita voata olen hay Snnage vw peading end cng ‘eting the fabric, keop th foam as dry as possible and remove it witha, Sie cee aheoeeeesuatenaas Rea ‘ontybaeipadotfuithn dary cloth: Dilan grensesm tecontot clan ‘Sincehietd must never be sed ines they soem sad Srase the plastic + 20 May 1860 171/618 bianke)