AF(C)-1-1 COPY NO. ___ fliGHTMANUAL MODELSU-2C and.U-2F AIRCRA" !llOTICE THISREVISlON,DATED10MAY1967,SUPERSEDES FLIGHT AF (C) - 1- 1DATED15 DECEMBER 1966,CHA."'iGED15FEBRUARY1967. THIS CHANGE,DATED15 OCTOBER1968,AFFECTS INFORMATION IN SECTIONn. DESTROYSUPERSEDED DATA INWITH AFR- 205-1. LATESTCHAHGmPAGESSUPBSEDE THESAMEPAGESOFPHVIOUSOA. TE ...... 0aso....r ... 10MAY1967 Changed15 October1968 AF( C) - 1-1 NOTETk ...,_ ., - llnll .."'" ..,. ... ...... C...S by--nr.l '-ia clllr-" _,._. el rlllr.-.r iliSTOFEFFEGJVEPAGESfJ------------; TOTAlfofUIUlOfPAGISINTMtsJ>UalJCATlONI:S ' o. A OB(Adaed) C(Bhnk) Ithr..:\. v1!-1 1 -2thru1-3 I--i 1-:S 1-oth:u!-7 1-1-9:.h.ru! -10 1 - J OA (Added) I-1 OBBlank) 1 -11 l - 12 !-13 l-H 1-15 -!7 !-.s 1 -2o I- 21lhru1 -22 :hru!-2o !-27 1-28tiu'ul - 29 !-30 !-31th:u1-32 . -33thru:- 3; ;-35 1-Jo J-3&.6..tiJruI-36B (Added) l - l7 1-38thru)-..;9 I -SOBlank) ! - 1 2-2 2-3 2--itbruZ- 5 2-o2 - !0 Z-11 ! - ll UlrUl - !3 !ssce 15 Oct b8 15Oct os !5 Oct o8 Sept 68 Ortg.n.a.l Ortg.aal ISept 68 Or:gtn.al 1Sept 66 0 ' O'Io'o7 Or.gi.nal I::,:::pt68 o . 'o"o7 o'ov67 o. ov 67 o Novo7 Origmal 0t7 On;.nal JSept on OnOP.E.iL-\.OF PH070GRA?H:C .:.U.:: -;: EQUIPME).""'!" . . . . .. . .-:-I (UXDER SEPARA:-.ECOVER) OPERATINGLIM!':'AT!O.o s. . . . . . . . .5 - l FLIGH':'CHA.RAC7ER.;STICS.. .....6-1 SYSTEMSOPERA ':'10..... ..........-; -1 CR.E\VDUTIES oT APPL:CABLE).8 - 1 ALLWEATHER OPERA710..........9-1 PERFOR.M.AYC..::.'JA'!A... . . . .A-1 ALPHABETICAL.... .. . ........ .X-1 v / v ! ' A::(C)-1-1 DESCRIPTION: SECTIONI TABLEOFCo.:-EX7S 'I'liE AlRCRAF 7 . . ..... . ..... .. :2::"\"Gl.."\"EFUEL SYS7E.M...... E- OIL SYSTE.M........ . NOR..'\fALSYSTE.M CO. n.,tGOUS IG.fiTION... . ... . S:"ARTER SYS':'EM. . .. . . . .. BLEED SYS Ts FUE.:.... ELECTR.:CAL SYS:'EM HYDRAULICSYS':"EM. F:_:GH':' THE AIRCRAFT PAGE l-1 1-4 1-4 1-7 1-9 1-9 1- 9 1 - 10 1-10 l-11 1-19 1-24 1-26 TheU -2C andU -ZF are stngleplace jet aircralt designee forhigh altitude.long rangeoperaoon.TheU -ZFis airrefuel-abte.Both models canbeequtppedwith "sli?per" anti dro? tan.&s. 7 hebasteconfiguration is fit:ee forphoto re-coona!ssance.Other equipment can also beaostaHed forspecialpurposes.Referto figures1- 1and1-Z for general configura-tioninformauon. .3A.S:CDD.i.EXS!OXS v.ingArea...... . .. ... V.'tngSpan. . .. ... ....... . .. Aspect Ratio............. ,.,.togAverageTiuckness :..engti:J. 'Se?te.tnbe:- 19o8 600sqft 80ft 10.67

49 ... ft ............ .. .. . RETRAC':"ABLESTALL S7RI?S SPEED BRAKES........ . ... .. 1-A4""1DU'GGEAR. . .. ..... .... STEER:l.G ........ . .. WHEEL BRAKES.......... . DRAG CHU7E. . .......... . ... U sTRUME.. 75.............. . FIREWARl'CNG..... . SPEEDWAR.:W:GSYS':"E.M.. CA.."'lOPY. . ................. AUXILIARYEQUIP t. --:.. ... . APPROXllt.AT GROSS\"EIGH7S PAGE l -l8 l -28 1-29 l-29 1 -30 l -30 1-30 1- 32 1 -45 1--iO 1-47 ConditionGrossWetght U-ZCU-2F Full matn and20.680lblO. CJSOlb empty au.xtanks (1020 gat) Full main andll. 650lbll. 9 50tb fullawetanks (1320 gat Fullmain.aux23. 970lbz.;.z;olb andshp?er tanks (ISZOgal) Full main.ailJC,l3, iiOlbl{, llOlb and dro?tanks (1520 gat) Zero fuelweight13s-o tb14. 110l-1 I SEC7!0Nl .::...:.=(C-1 - l FLAP SCR.E'1JJACK OJUTI: ACCESS0 Oi!.QPT, IV'X n E'"CAPS _J .ua cosmna....-.cT COCl!.!NG A!ll EXRACST COMPAJLTMOC':ACC!::SS.- -.. ACTOP'..L07 5TS"'':W(l llAD!O COMPASS a.I:Cl:!"'l:R KFitADJO .EOCPL'O' !lAY I..O'ii"ER KATOI 1\DT S1!QEM-'"1 ES'A XT!:JU'At. AC A.''D !)CECEPTACL A!ll COl.lPAll"!'"l.l.Oo T I:OVlPl:Dr:" BAT l.!PP.EA HA"!Ci" BAl' PA5St!aE RGU!.A.TO't .PilESSt...a.E SAFETYVALVE TAc:"!C..U.. Ql."lPWOOT ln{F AA.l)JO

VHF l!.A:IlO ECUIPWO:T L AUXll..lARY GI:Ail POGOSJ MA.L'4 C!:.AA Oh.. AlASCOOP ANTtCOL.LJSlC.. :.A....t.:GKT COMPA..Rn.to.""7 ' Figure1-1 1 - 2 AF (C)-1-1 GENERAlCOFIGURATIO -. /\; DJLOP TA!Ot(tOO GA1J Sl..IPPDl TA.."'t (100 GAL A!3. BEATAn XHACS"r SEC7!0N-\OOElU-2f :rt.'S1.AGl: I.:PPE:R IFA:IU:'-"G AilS (A1:A!A1..

A.iUAL GC!!) ..!CHTS 2r.'DZVOL'S SAOO.So. aT-JHF ii.AD!Ort."N11. :aY1G.A riO.SUCHT AOC5St..,_"DJtF ABI.-.c;

ESGI.s Ol.L Fl.l..Lit ACC:E:SS E:QCIPloiC."T 8A YtrPPit HATCH BA'tPit..5s::a.E:a.GULA-:"Oa PaE:SSUR SAFETY VAL.V TOli:!PW.:0.-:" t.'HIFRAD!OA TC TaA....:SPOSD.it VRF aA.D.:OFIT:e:t.. StJWP "tA..'Q!: HFii.AD:O v f"" A.G

STS'::'"e::-ationa!.equipment load assw:ned to beequival ent to

and"T11 with sys-temsl,9,lZ,and13. Z.These weightsare based on aspecific fuelweight of 6. 58lb/ gal. 3.7heU-l.Fairplanei sapproximately 300poundsheavier:.han theU-ZC. 4.These are app::-oxim.a:ewetghtsand shouldnot be used fordetailed nrission plann.tng. ':he aircra!t i spowe::ed byas i ng!e,15-s:age, J""" 5P-13B :ypenona!te::bu=ningengine (!igure1-3,,which employs an a.xia!!:ow, twinspool co:mp::esso::,andasp:it :hree-stage turbine.:'he f::ont compressoris an 8 - stagel ow pressu::ea.:.n.itwhichis con.neaed by ath:oughshaf: :o thesecond and:.!lire s:age turbinewhee"!s.Thenigh comp::-esso:: hassevenstages0: conlpression independent of and followingthelow compressor.andis con.:::tected byahoilow sha.!t:he !i:rst stage o::=bi.newheel.':his arrangezneet pern:rits thelow pressurerotor :o turn at its best speed andal!.owshigher compressorratios. A:owpressureoverboard bleed valveis provtded on each side oftheHigh pressure compressor case.T11eengineisrated at approxu:natety17.000 poundssea level statlcthrust. The:-15 engi nefuelsystem consistsof the followingmajor engine :mountedcomponents, aschema.uc dtagram. of whichisshown in !igurel-4. 1.Two-stage geartypepump. , l-4 2.Hamilton Standard hydroJDech.anical fuel con.tto!. 3.Fuel manifoldpressurizing valve and automatic fuel :manifold drainvalve. 4.Forty eight dual -orifice :!uel nozzles. ENGINE FUEL PUMP Th..eengine-driven fuelpw:nphasalow pressure stage and ahigh pressures:age and suppliespressure for boththe no::m.al and theeJDergency fuelsystems.Du::ing operauon.thelow pressure stage ac:.sas an engine-driven boos: pwnp ant!increases fuelpressure totheinlet ofthehigh pres-surestage.-:'heengine !ue! pum.pwill supply sufficie:1t !uel to maintain !1igh: if theairp!ane no=-ma! andauxil ia...-yboost pwnps !ail.providingtheai=7lanehasbeen at a!titude fo::approxi.Inatelyonehot:=, whichi ss.U::icient timeto becote:!soaked o::I weathered.In theevent of a!ailu:e o!thelow ?ressures2ge.adequate!ue!pressure a: thetnle:tothehigh presscre (maL::!.)stage o! :heengine fuelpun:1pcan bemaintained bytheairplane OOoSt aby-pass valve.l! ue highpressure stage o! !he enginepu:np !ails,!lameou: wit: result and ares:art cannot bemade. .-iAIN FUEL CO_ -:rROL Thefue!.controlregulates speed bymeanso! afly- ball governor forall operating coruhnons,includingstarting, acceleration a!ld deceleration.Du:ing starting and acceleration.thecontrol limitsfuel flowto prevent compressor su.rgeand overtemperatu.re.D-..1.r ingde-celeration.thecontrol sched\lles aDtini -mwn fuel flowtopre\eot !la.meout.':'his mini.J:nwnflowschedule also c:!etennines theidleRPM at altttuee.ln addition,the control incorporatesamaximumpressure lim.iterwhich !imits:.hemaxi -mumoftheengineto asafel everso astoprevent da.magetothecoJ:nbustion chamber case dueto overpressure. Changed1Sep:ember19o8 I 24 23 A.F(C) - 1 - l J75ENGiaE CUTAWAY ICOMP1lSS02 GtnDE:YA."ttS A.."t1loPPRESSC a Pa!.WA..RTFt.'!. F!.O'Ii EJ.I.EitGE.NCYFUEL CO!i'TROLS1r.:'CB SECOX:>AATF'tJL FLOW Pa.LSSUIU: SE:NSE FU:E:LROL !SODY PilESSUR..Ellll:TOllN

FUEL Da.A!N Figu:el - 4 CAL FU2.

AF(C-1-l During climb at afixedsetting,the fuelcontrolin general Wlllreduce engine speed.However,exhaust gastemperature (EG7willincrease d.Jringatucedthrottle chmb.Someengineswillrequirethror'".ling to observe .EGT limttsand fu.:::therthror..Iiog may berequi:::ed at altitudeto observe EPR limltS. E.MERG.E. "CYFUEL 7heemergency fuel system bypassestne compensatingsec:ions ofthemain fuel controlso th:a: fuel flowis manually selected andcontrot!ed.-:'herets altitude compensa-tion toonly30.000 feet;however,it i s necessary :o makeextremely careful throttle movements during emergency operation in ordertoavoidoverspeediog andovertempera-ture. Aiuel sys:em. selector switch isonthelei: side of themst:'W:nencpanel._ msisatwo-position switch a.x:dtsno=-mal!yup for "OR:-!uelsys:e.:n O?eranon.Plactngthe switch down activa:esthe fuet sys- An emergency fuelsys:em hght is on theannunciatorpanel.:'hisis an amber light whichis0:-i when operating onthe emergency !ue1system.:'he light also g l ows du: i ng:.hepordon of anormal engine star: but should beout beforethethrottleis movedfrom:heOFFposition. NOTE :'beemergency fuel lSnot automaticand must be n:t.anually selected when desired. Tri.RO:"TLE Enginepoweris controlled bythethrottle. ':'h:ott!emoven1.ent causesthefuelcontrol tometer fue!totheengmewith automatic !or RP.:! and burner pres-sure.:'he th.rot""..lebasOFF,IDLE.GA':'E. andFG.:.-L InOFF positionno !ue!reachestheburners.Duetopossible ecgtneoverspeed o:- over:eznp.agatet)-pe thro:.t.eSt.o?!.s to!i.mitta.keo!! powe::- to 93:o 95._ RPM.':'opassthis ga:.e,the:h..ro:-..!e.s moved outboard,thea forwa..-d,orthe gatestop can beremoved by movingasmalllever onthe !orward throtde quad::-anttothe:x.BOARDposi :ion Thega:e au:oma:icallyween t!:e th.ro:tteisretarded c.nless:.hegatenas been manuaUy opened. CAUTION Avoidmanually opeOUlgthegatestop if ?Tactical.":'htswill?recludethe stop betng opentnadver:ently.':'he gatestop sbou dbeinposttton during landinggo-arounds or touch and go's. Thrott.e friction.s :-egulated bythesma!l knob onthe..."lhoa:-dsideoftilelowe:- tbrot console.Athrottle vernier wnee!on the same consolei sused !or verysmal!ti:t:ott adjustlnents.Amt.c:ophoneswltch andthe speed brakeswitch a:-eonthethro::le. :'heengineotl systemisa.nomanc and requiresno controls.7hesystemis c om-prised o! apressure oilsystem.scavenge oilsyste.I:l.b::-eatherp::-essuriztngsystem and oe coolingsystem asshown in figure 1-5. Thepressu:-esystemissu?pEed wi:h oH from atank mounted ontooo!theecgtne compressor section.":'h.s::anx.contains 5. Sgallons. Otl from.:het:aM!sfedroan engme cirivenpumpht.chforcestheoil throughdteoil cooling system consi sttng of a14- incb air-oil cooler.a9-inch au--oil cooler,and afuel - oil cool er .From thefuel-oil cooler,theoil i sforced bv theenginedrtven main engtneoilpresso.1re pumpintotheengine components whic!:t require!.ubrtcation.-:"bemaUl engineoil pressu::-epump dischargepressure is regulated by apressurereliefF1veengined::-ivenscavengepu.mpswi :h-draw oil !rom t!:tebea::-tcgcompartt:ten:s an accesso::-iesandrerumi ::o :hesupplytanl< l-7 SEC':"!O. .i AF (C-1-1 ENGINE OIL SYSlEM !-8 3- E:.'iC0!:!. P3SS.Pl..'XP C- !.AS7 CHA.':C 0!:!. SC.:U::J::i =>- SCAEPUl4PS 0!:.. F- 3R4A 7HR P.iU:SSU"a..!Z.L"'GV.U..Vl: DG L.-xi: . pli[Kla;J 't plDili[KI[I[][...:DtJDIAIROIL FVE:l..INFB.OWFtr.:.L BOOST PUWPTO....IIIZZI'*al*GAAv:-:T F'i:':'"!> PJU:'SStm 0!1.. f1111111SCAV!:SGE OIL wMw*BOOS7 PRESSUIU: BR.E:A 7H!:..'ti Figure1-5 s AF(C)-1-1 I Theoil temperatureshould be monitored du...""ingflight.particularly at high power. Thebreather pressuriz.ingsystezn is pro-videdcoU:nproveoil pumpperlon:nance at altttude.Thepressureis automatically controlled by an aneroid operated valve. . oRMAL SYS'r'EM Thenormalignition syste::nisahigh energy capacitor-dischargeZO-joule:ype.consisting o!twoidentical.ind.e?endent exciter uniu; oneforeachof twOigniter plugs.Oneplugis in ccxmbustion cha:Inbernumber4a.cdtheother is in number 5.Thetvroexciter u:Utsa:e powered !roD!electrical circuit breakers sothat !allure oi one will not cause completesystenl failure.Asingle-xcteris for makingan or groundstar:-Ignitioniscontrolled by asingles?ring -loaded switch on :helowerle!: instru.:nen:panel. ':'he ignicon :s wired ctirectlyto:.heZ8 - vo!: DCbus.Ptacingthe:gnition swi:ch in star: posttlon energizestheigniters.regardless of BAT - G.ENsr.a:b position.

Theairplanes a:-eequipped with acontinuous ignirioosysteDlto minimize thepossibility o! fl.a.I::leoutduetotranSient condition.sat high alti.wde. ':'hesystem isenergizedthroc.gbtheBOOST PUMP-CON':':GN- ONswitch.Thecon-tinuoustgnitions y sten1andthefuel boost pUIDpare energizedsin:lultaneously when :heswitch isi.:ltheON position and the AC Generatoris ontheline. Thissystem consistsof aseparate .S..joule exciter and utilues:heignition plug in com-bustion cha..mbe::munber5. Changed o 'ovemoer1967 Operation 1.Bar+..eryswitch- BATlot Z.ACgenerator- ON. 3.Auxiliaryboost pump switch OX. NOTI :n theeventtheAC generator fails. power !orthe continuoustgnition is supplied by:heicver:er.ln order to prevent inverter overload under this co::tdition.the APX 135 beacon. andcontinuousignttton shouldnot be operated st.multaneously.E i:herthe boostpump anc. continuousigni tion or thebeacon shoul.C beturned off as operating co::u!itionsdictate. TheACgenera:orbeon bus ior opera:Ion oftheauxiliary boost pump.However.i! :heACgenerac.or or theauxiliary boos: pump fai!s. :he auxiliary BOOST CON:'switch shouldrem..ounintheONposi-tion asrequi red foropera:ion o! con-tinuousignition. S7AR7.ER SYS':'E.M An air turbinestarter isfor ground starts.An exte:na!airsupply fur-nishesthenecessary power.There are no airplanesforthissystem.I: is tu.rnedon ando!I by tllegrow:dcrew accord ingtos ignals giventothepilot.Airstarts donot require astarter andare made by windlnillingtheengine. 1- 9 1 (C)-1 -1 B!...EED SYS7EMBLEEDVALVEOPE_ T.LIGHT Du:ingreducedpower and.1dledescent con-dl:ionstheP - 133 en.ginerequiresintercom-pressor bleed since engine operation under :hese conditionsis :1ear COin?ressorstall. Onelowpressure overboard bleecvalveis provided on eachside o!tilehighpressure compressorcase.":'beseautomaticor manuallyactuatedva:vesservetocompressorsu.rgeat high a ltitude by ducting low pressure compressorair overboard duringlowO?e;a:ion.High pressure compressor airis used :.oactuate:he bleed valvesmbo:h tile Ope:l anc c!oseC direction.s. Acam Of)eratedswitc.D mounteconthe :hro:tle linkageac::uatesti:te valve which controlsthehighpressure air.In auaTn:;r.. rooeratio-c.thebleedvalveswill open or close be-:ween84 and RPM. '::hevalvesoperate as afunctiono:throt-.le posi:ton and ill actuate at ah igherRPM a: alnn:de whenidleRP. tShigher cueto !uel !low li::n!tations. .BLF.EDVALVE CO_ -:RO:. TheBi.EED\rA:L Y:Scontrol switchis located ontherigh: side ofthelowerinstru-ment panel (see cockpit arrangement illustra-tions,tiussect1on) .:: is a3-posu:ion lever !ock switch.In the up or OPENposition :he b!eec valvesare open,inthecenteror C:..OSEpost:1on :he bleed valves are closed and in theC.ownor AU70 posi:ionthevalves will operate automatically as afunctionof thro:'tleposition..DC 'tXnrerisrequired w au:o1r.aticallvo=oo.....theoleed valves.LOssol DCpowerwill Closethe o.eed valvesii they a=e open.or keepthe b!.eedvalvesclosed if they are closed. 1-10 Two cunber bleed valveopen lights.B T'SED AIR LEF':" and 3L.EED Al.RRIGH':'.are locatedintheannunciatorpanel (see cock-pi:. arrange.xnentillustrations,thissection). 7hese light.sareactuatedbyswi:.ches mountedonthe bleed valveactuatingsha!ts andilluminate whenthevalves are open. ENGIHE:NSTRU.ME. -:-s ':'hebasicengine!nstru.ments areshown on figure1 -6. OtL TEMPERATURE 7netemperature o! theoil ent.erutgthe engineis monitored in :he aOCpoweredgage. ENGINEPRESSURERA.TIO (EPR) SYS":'EM :'bepressu=era::!oglVeSthept!ot an indtcauoc.oi :hn!st forall throttleset -ungs.":'het:ransnli:.t.ersenses engineinlet andexhaust pressures.andelect:="ically transxnitstheratio o! thesepressu=esto theindicatoron'theins trw:nent paneL Power fortheoperation oi thissystemis su?plied b)eithertheour:lberoneor nUinber I twoinverter. Changed 6November1967 0!1. INDlCATOil Changed6. ovemoer1967 FU 0"'-.LPlU:SSUR.:: :xDlCA70R A.F(C-l-1 PiU:SSORRATIO U"D!CA !'OR Figure1-6 SEC-:':ON! E:XHACST GAS

D-'D!CATOit 1-lOA/1-lOS AF {C)-1-1 SE:C':'IOX 7ACHOYE7ER ':'hetachoxneterindicat-espe:cent ofrated high press\ll"erotorspeed. engine speedts ncnnina.lly 8730RPM.However. theJ - 75 engine is thrust rated,and "Military" t.b:us: is usually obtained at d.if!erentRPM forcii.Heren=e:1gines. TheRP.Mshould normally beused asa secondaryo! enguu:: It also sco...u1oe :r:noruoorect 1or overspeeding 1{103. 0, marmu:m allowable)and !or starting. ':'he:achom.eteri sasel!- gene:atinginsttu-Inent havingi:s own engine -driven genera-tor. EXHAUST GASTEMPERATURE '!'hisindicatestheturbine dis-chargeteroperam.rein deg::-eescentigrade. Temperature imllcationis?resented on a digital counte rforofhigh accuracy, whileaneedlepointerindicatesthetem-perattll"eonthe dial !or aquick or coarse readicg.Graduations on r1:edial arein incrementsof 50C overa::an.geof 1000C. An integral ::-ed warningight on thedial glowswhen theexhaust gasten1pe:-a.ture l exceeds671 C .Ared OFF flagshows whenevertneinverter powerisofi or fails. E ither cormat or eJDergeru:y inverter power will operate :heEG'!'tndica:i:lgsyste:rn.....o wannup tim.eisreiU.ired.Although the instrument is capable of followingteJDpera-ture changes o!150 Cper second,theindi-cation wi!l be because oi thetime required fortheprobesin theengineturbine section tosecsetb.etemperature cl:.a.nges. Changedo -ove:nber19o7 PRESSURE ':'hisinsttument snowsdlefuelpressure thelow pressure engi::tefue: pum? andprovides an indication o!theout?ut fromthe aL.-planeboost pump. Thepressurewtl!varyfrom14toZS;>si. At full :hrot+-leta..keoffpower,pressure InaJ drop toz.ero.Thissys:emisremote indicating andispowered byeitherthe number oneor numbertwoinverte:-OiL PRESSU:t.E Thisinstnunent indicatestheengine oil pump dischargep:essure.':'henormal rangeis 40to55psL:'hissystem is re.z:noteindicatingispowered by eithe: thenumber oneor numbertwoinverter. A!RPL'\.N:EFUELTheair?lane!ue: systemisverysimple andrequi reslittle Iro.mpilo: otherthan monitonng of :he boost pw:np !uel pressure.thefue!quanntytndica:or. andthe uelwarutngligh:s. FUEL SEQU::."C:NGSYS:"E M TheaL-p lanehasfourinteg :av.-ing!:a.nks, a!use!agesumptank andprovis!ous !or slipper anddrop::ac_1u.:an..tU!eec in:othefuselagesw:nptank as shown :.::: figure1 - -.':"he!uel !:om t.hesump::ank feedstheengineasshown 1n figure-9. 1-1! SEC7IO. 1 AF {C) - l - 1 FUELSYSTEI,'.'ODELU- 2C 1- 12 :"RANSFER A.1:D !>C- !P SYSTEMS crc:a C3ICICIC CIO'+'"::a. rr &JPPE& YA!.TI: Mi:S'T-

nz:_----nz:_ ::lmi&P Figure !-7 AF(C)-1-lSEC":IO. -r: F Ul:..L Qu... TAB.:Z (A.PPROX) ":'anksPoundsGallons Sa..anp6Z595 Main6,08692.5 Auxiliary1,974300 Full :Internal8,685J, 3ZO Slippers1,316zoo DropTanks1, 316zoo F ull with Slippers10, 00 Ll, 5ZO Or Dro? Tanks NOTE Each airc:raft is individually placarded in the cockpit-Fue!. from alltanks!lowsintothe sumo !an.k ov and/or pre::.sure !eed.E.nginc: compre::.sor bleen .sL.....r egulated :o 2.psi to pressurizethetna.in:awd!ia::-y.ana. sUu:>ertar-.ks,and ::oI-;a tne a..roptanKS.:"hes -;aukisnotores-su-ri ze.d.":'h.emain wmgt.a.IL'c::.:.eeame right -hand side of d:teswnp.andtheauxi-liary!a.nks!eeC.intotiLe!.e!: - hand side oi :.he sump tank.:"he !ue! levelin theleft and right sidesisequalized by alarge cross-over il.ne. J -:'wosetso!loa::vahesconc-oltrans-fersequence and propersump tank iuellevel.These dua: f!oat valvesp r event blockmgof fue: ilow dueto asinglestuck va:ve. Theuppersec o! !loa.t valvescoor:rolsdte fuel !low !rom the d r op ta.n..luor slipper taaks,andauxiliary:anks, insequence, so asto maintain :.hesw:nptank fuelat the float valve level until tanksare empty. Whentheaboveta.nksare empty.thesu.m.p :ank fuel :evel dropstothelowerset of !loat valves.These lowerfloat valvesthen control fuelflow from the :maintanksto maintain :his fuet :e..-e!in theStlJ:!lptank until the main tanksare empty. Changed6Novem.be.r1967 Aset::ondaryfloat\-a:veisprovided for par.J- SPL of 'l:ernal wtngtanksattheas aoacKu?in casep:n-xna::-v V?lvesshoulabeand to ensure e:avitv :::eecitng. NOTE Drop andslippertan.ksshould not becarr1edat :hesa.xnetime. FUEL SEQGENC:XG Thefueltransfe=sys:em ontheU- ZFisthe same as ontheU-ZC exceptthe dro; tan.k fue 1 feedsintothemain tank !eed lines which arephu:nbedmtotheleft - hands ide of thesump tank.The fuelusagesequencei s as fol!ows :-.n.aintanks.shoue:-ranks_.sum!)":'he a=optanks,andmamtatiKS Hrst becausetneDla.lll:anks a:-e::heonly ones which can bereiue!edin !l.ghc.:'hemain tank f!oa:7ab>esin :hesu.mpthe:-efore, are higherthantheauxil iary !loa: valves. See !igu.re1 -8. TA1iK sw::-cH P=essu-:-iza:ion a.r tothe a\!.Xiliary !uel tankscan oeu.:-nPa on o:- ou byatift loc k sw!tch on r ight-r..andcock:nt(Oppernght-haacinsrU.Inentpanel U- ZF.)Beforetax.eoif. :heAt:X :'AliKshould beOFFi! lheauxiliarytanks are empty and0.,.ti :.heycontainfut: 1. .MAIN PRESSuR:ZAT:ON SW:::'CH Aguardedswi:chu!enti.fied "':'A_.;K PRESS.usedto over::-tdethemam tank a i r shuwfi float swatch andprO'-rtdematntank pressurtzaaon._is one:uc:c::... '-'Oso.e !orwa=d o! thelateraliue1t.rans!erswitches. ':"heswi:ch has a (gua:ci down)posi -tion.and aREPRESSpostoon.::"hisSWl.:ch must be rnovedfromtheNORI ...... o:o theREPRESS posu:son azt.:rco allowthe !ue. :hesu.mptank torise above thefloat.valve andno:=ma!a.irn=es-su.riz.anon.:"'neSW!tc.b..s ::em=nedto:he beforethemain tanksare agai neznpttedtoensures lippertank pres -sc.rization and comple:efuelrraosfe=. 1-!3 SEC':'ION1 AF (C) - 1- 1 1 - 14 TR...a\.NSFERA..."'ID FUELSYSID I r-.,.QA6 SC::ilC--

lOll &. WOOII':'C> .t.::n:s c:rca c:;;a.ooc

&rT S""..=PP1:oo.sx :s 110:" c:m.ca ..:::57 u;PRESSURlZA7!0X VEX':".......I.1"1:0.. T.,_ NISS 11!nc:. IJ/0 YDIT ----F1:%:.t. !li:XP U- 2F Figure 1 - 8 YA!-YD a-c.t..t.a s=. ..,. ...rn:::. T'.A&'t S'WI%'CII (Sa G.UI ... AF(C) - 1-lS.EC:-!0. 1 This airplanebas!or slip;er tanks.'::'besetanksare ext..rnalpodsthat sl.? on ove:- the!eadingedgeo! tilewing app:-oxunate.yten feetfromthefcselage. !rom theslippertanksis forcedbyatr pressure intothe a.tXiliarywingtanks . From be:rei: feedsinto:hesum?tank through tnenormal awci!:aryt:a.nk:ransfersystem. Asmall electricpumpisinstalledmeach slippertanktoensure completeutilization of avatlable fuel.Thepumps arepowered bytheAC generator. NOTE Fuel !rom :hes!ipper::anksv.ill not g:::-avityat:d!or p::-essu:efeeduntil empty.!t :s posstbletila: 20to.;o gal.oas wHlret:natneach tank. u.o-less:he:an.t stripperp..:.:.:nps are used. Refer :o 'liT. Syste:ns Ope:::-a:ioas, !or s!!ppertank operation. CROSS7RA1"SF.ER in order ::oprov1deameans of correcting wingheav .ness duetouneven {\lel feeding. asmall 5 - gallon- per - mUlute electrtc fuel pumptsinstalled.Therever siblepump is controt!ed by athree-position S""--itcbon !heerlei:tns::rumea::sub?ctnel .It transfers fuelfromctthe rmatnV."lngtank totheother.Pl.:shin;; swttch tolheleft transfersfuelintolhc maintank.and vtceversa.An ann mciatorpanel lightwill be onwhenthetran:..Icrpwnp is o;erating. Ceangeci:September1968 CROSS TRA. SFE:::t?GYP Thesystem is ide!Uical totheu - ZCexce?t that ontileU- ZF.:wo fuel cross L-ans{ersystems.Oaeis betweenthe:wo maintanksandtheothe:- is betweenthetwo auxiliarytanks.:."hea"..lXt!2ryt:aru0 I StS ... lot!3 AF (C)-1 - 1 ANUNICATORPANEl F igurel - IZ T hisr ed war ntngltght.in :he annunciator g!owswheneverthegeneratorisi n -operative acdtheDCbusisenergized.The b a r..e:-yswitch mas tbem theBATE MERG o: 3A-: &GEX position.o=:.heexter nal powe:- must be coru:ecteci. BA77ERY: >ISCHA.RGEWA.R:..'UXGLIGHT T'ne::.-ec 'W'a..-ci.nglight will H!c::oi.natewhen batter yhasbeen d i schar ginga: arate of SaUlper e sor mo::.- econo..nuously forat leastlSThelightindicatesthat the geuera.to::.- casinsufficient output o ris .switched of&'::he!.me.: : isthereforepossible !or theba tter yc!.schar ge warning! igh:to glow and:hegeneratoroc.twarninglightnot to glow.Wi:lt thiscoociti on.:he action to betakenis:.hescu:neas:ha: !ora!:>Cgenera-:orfailc.=e . NOTE .:Uun:unation of the bat terydischarge light may occu: c!u:!.nglow engine RPM opera:i on.!! t.h:soccurs. groc.nd per sonnelshould ber equested to check theDC vo:tageregula!Oradjust -z:neat. AC ELEC ':'RlCALPOW .::. RSY S':' E M ACe!ec:rica:power !or certain electronic intelligencesys : ems.:he auxiEa:y boos: ?c::tnp.andnormal powerfor connnuous ignition. provtded by::heengine-dr:ven AC-he genera!O=.srated at 10KYA.Z08/lZOV.3Z0- .:50C)cleAC. Avoltageregulator anc!supe:-viso:-ypanel a :-ernountectn tilewheel welLFeeder !aalt cu:r ent trans!orme:-s a:e mounted a: the AC bu.sanc!asan :.nteg:-a: part o!titeAC generato:- .':'hesuper v!sorypanel pro-ricesprotec::i on agau::.s:o v ervol ta.ge.unc!er-vol:age.anc ieece:- !at:lt. ":he ACgenera!Or provi des a source oi Z8 - vol :!>C?OWe rw::uchtst:sec! in :he sys:em control circuhs andthe::.-e!o'!'e c!oescot requiresht psZS - VDC!or nor-mal operation.However.shipsZS - VDC.s also supphed:h.rough a5 - ampere breaker in theeqtLpment bay as backup in caseof failu=eof :he:>cpov.-e::- geaera: ingcircui ts in :he A Cgenerator systen1.Athree-pos ition{AC:'OR.OF F RESE':'.EX':' tson:heloer !e!t side oi thei nstrc..ment pane: .AnAC GE. ou-:light(::-ed}is o ntheannt.nci atorpanel. ':' helight wi.Hcome 011v.heneverthegenera-t o :::ist=ippedoff thel i ne.':'heHgh':wi!. go ou:whenever:heswi:ch isp !aced in ' be OF?/RESE7 posi non . 1 -Z3 ! AF (C)-1-1 The ACwillt:>i?o!f whenever it. is below 320CPS (approltl.mately 80engineRPM)and auto::n.a!ical!y wheneverthefrequencyis ahove320CPS. A :rip duetoundervo! tage,over-vo:tage.or feeder !ault requiresthatthe AC generatorswi :cbbeplacedin OFF RESE":' post uon at:dchenreturnedto AC GEXERA:'OR posi ti oni norder toreset tile genera NOTE In order toprevent re?eared momen-tary feedi nginto afaultedsystem, only cmereset o!. ACgeneratorsys-tem be at:eJD?teC.. Th"VER :'ER ':'he ACi::.verter?Ower contto!l ed bya fou.r-posi:Jon,(OFF,1,2,i nver -terse:ectorswitcho nUlel ower lef:inst:ru-n:ent scbpanel bel ow :he bar.RAU:..:C':'h_ehyerau!icsystemassho'WUin figure 1-13 ope:-atesthelanCing gear,speed brakes.wing ::la?s.fue: ooos::pw::npc!rive mo-:or.and ontheModelU - ZF.thelatch and.receptac!.eInecha.nts-mo!theARS. ":'herelSahydraulicositetilepointer. Thisprovides an accurate me:hod of moni-tering le!t or right-wheel disp!a.ce.ment which may occur as aresul: of uneven .fuel ieedtng. AF (C)-1 - 1SEC".:":OX-Theai!eronsare controlled through :::-otation of thewheel.Su=facetta,-elis16 degrees up and 14 cieg:::-eesdown.Wit!:lactuation. o! thegust contro!..::hese:rave:s a:::-ereduced tO0-1/2 degreeS C? and5ceg:::-eeSdO'Wil from:heshifted &euttalposition.An a.:nber light illuminates whentheailer ons have shl!tec :Dthegus: position.and aHgh: !Uurnjn;a:eswhen :hey arein the !aireci posi-tion.:'he e:ect:ical:y actuatedtrimtabis ontheleft aileron.Tb.ettim. tabswitch is ootheleit conso.e.Ag r ound adjustable bene tab:.stnstalled on ther ight ailer on. ELEVA:'OR CO TROL SYS7 E.M 7'aee!eva:or syste:m is conventionalwi:h col\!n:l'lcoc:ro!.Suracettavelis30 degrees up anc Z.Odegrees down.The e:ect=ica ty ac:ua:edpi:ch ttil::ltabsare at theinboard endo! each elevator. Two con::rolswi:ches are on thewheel.':he le!t- hazdswitch controlspowe:::- tothe .l:lanual l and a u:o.ma:icelevator::ri.::ls y s :en:t.7 he rigbt- hacdswi:ch pos i:ions:hetab.In add:tiontoelectrictrun thetabs have anaunaticservo opera tion:oreduce longia1dinalconttoforces . ELEVA7 0R 7 R.nd':'A.BP OS:7 :0N DID!CATOR Aposi: ionindicator belowthe gear handle gtves:hepilot avisua.lreferenceforttiln tabse:'d.ng.Theindicatorispowe:::-edby 28V:X: andthec ircuit is controlledthrough theelevatort:rimtabpowerswitch onthe !eft- handgrip o! thecoouol wheel. E1evaoort:runcabpostti.onisindicatedeven though:hettun ?OWerswitch is o!f. RUDDER C0 7RO!..':'her uddercontrolsys:emis with pedal controls.&:::-!acet---avelis30 degrees!eit andd.gh:..Agroucd ad;us: -ahle bendta.!>isinstalled ontilerc.dder. Therudder pedals maybe adjusted fore anda!t to accomoda:e dille :-eatleglengths 7'ne adjusc:nent !ock ontheoutboard sic!eof each pedal can bereleased byou:-boardtoep : essure.7he:-eisno:-udder deviceinthtssys::em. COLLAPS!BL.ERUDDE RPEDALS C ollapsible:udde:- ?edalsa:-eins:alled :o ::-educe ?ilot fa:iguebype:-mit:icg ! r ee extension o! :hep:lot' slegs.In thecollap-sedposition the upperportion of each pedat tsrota:edto ahorizon:a!?OSition, ?e:-:ninicg:hepilo: toandstretch hislegs. O?eratioo: 1.:'o co!lapserudderpeda_s.pash rud-derpedalpusher forwardwith toeand stea.Cy O?posite:-ucderpedal at the sa.me:ii:newith oppostte !oot.Repea: on oppositestde. 2 .To:::-eru:::-orudderpedalstono:-tnal posinon.lift collapsedrudderpedal with toeor swabs:ick whileoppositepeda!v.-i:ho:herfoo._. l - 21 i (CJ -1-! W:O'lG ':'bew.ng !laps a:-eactuated byhyci:-au.lic motors wruchareby aflex-iblesha.!:.II onemotorshould !ail.:he other :no:o:- w:t! bo:ll i!aps.but a: a speec!. Aseconefunctionof inte:connec:ing sh.a!:!Sto rna.in:a:nsynch:oc:z.a:ion of left. ane!!ap posi-:..ons.li theleft and:-igh-:. !laps becomeunsrnc:-honized fo:- anyreason. asymme-try:sto amaxi.mwn o!5 cegrees by anS'-'-itch device. ':'his sa!ety !eam:-e precludesthepossibility o! la.:-gec:.!.ferences:!lap position dueto ma.!u.nc:.onor fa!!u:e..A!:e:- e cu:.out SW\tcbhasbeen act!latec.i :isno !onger possib!eto move:he flapsuc.:i!:-ese: on :.he

:"he:-e!Sr.oeme:-ge::cy rnethoe o! operating :hew:ngi:aps.However.flapsmay be lowe:-ed with nor-ma!enginewmdzni!hngin :heevec: of anengine !a1lure. An so!enoidveisused:o con-:ro. tilec1:-ec:ion o! !low o! bydrauhc !!uic to :hereve:sib!ehyd:-aulicd:-ivemoto:s. :'hisiscontro!led by the r.a?switch onthe! eft console outboard ofthethrottle. :'beswitchhasthreepost:!ons:OFF.UP. am! JnICA TOR :'he wingflap positionindica:.o: onthe left lowerios1:::-:.unentsubpanel.lt has a range !ro:n minus4deg:eesto plus35 deg:ees.which comcides withthemaxi -mum flap travel.Thisis an elect.:-icinstru-ment operating from DCpo"'e:. !anually ope:-atedretractablestall strips are installed ontheleading edges o.fthe Wlngabout midway betwee::r.thewingroot andtheWlngtip.':'"ney?:-ovtde bener stall cha:-acteristics whenextendeda:low a!titude. 7!:tes:allprot:-udeapproL..Ina:ely one - half inch whenextended andare flush with thewing leadingedgewhenretracted. :"hey are exrendedbypu!:ingthev.::ite S:'A.Ll.. S7RI? 7-banc:!!eontheou:ooard sadeo! the:- ight- hand andmoving outboardmto adeten:.7he} are :-eo:racted by :r.lllingthe':"- handleou: of the detent andallowmg :he handletoreturns!ow!.)- by resisting thespnng:etu:-n !orce o! :he system. RE7RAC:'ABLE S':'ALL STRIP POS:::o. ::ND:CA:'ORUGH:'S There aretwoamberlights (left and ::: ight stall st:r ip)onthe:- tgbt-hand:ostrunlent pa;:telwhich illw:ninate wheneverthes:all st=ips areretracted and:helanding gear is down andlocked.Thelights go out when thestalls:.rips are extendec!.When the l.acding gearis not down a:u! :ocked,the lightswill not i!lcmina:eregard.essoi the position ofthestall strips. .AF(C)-1-1! SPEED BRAKES ':'hespeed brakes a:e ad:ag device used to decreasespeed.::'hespeed brakesextendto amaximum o! 50degrees.Thedirection of c::avet may bereversed a.t anytime. SPEED BRAKECO:XTROL Thespeed brake controlis athree?OSition center-o!.f slideswitch on thetop of the th=onleleve:-.7he hydraulic fluidflowto tileac:uariogcylindersi sso:enoid valvecon-trol:ed.':o OPEX thespeed brakes.the switch 1spul!ed back;to CLOSE.theswi:ch is pushed {o:wa:rc!.Thespeed brakesmay bestoppedman) post:.ion on eitherthe or ret:rac!ion cycle by rew.rning :heswitch :o its OFF position_.However. ai=loadsmayslowly ctosethespeed brakes f:ozn anypartially open position if theswitch isposi1::.onedOFF."':hlsvnl!no: occur with theswltch in theposition.1ntheevent o!enginea..ilure.norm.a.lenginev.-mdxnilling w!ll developsu!ficient hydraulicpressure to actuatethespeed brakes. '!he airplane1seCicipped wiu ahydra.ulica.Uy acru.atedbicyclelandmggear whichis con-tro!led by alever on theleft !or-wardside paneLBo:.h maUl gear andtai! gea..rhave C:u.a.lwheelsandretract forward.Lateral balance1Sby!eft a.nd:::-ightdrop-pablegea:::- (pogos)located out -3oa.=donthe An electrically operated !:tdicator and wa-.""ningsystexnisp:ovided !or tilemain and:ai: gear only.Aoezner-gency dropsyst.enlisprovidedtoextendthe :r.ain andtail gear in case of failureoi the norma!. EMERGEXCY EX':'E. s:o. TThisisaf=ee!aUsystem.Both t.."'te-ain andtail gea: are mechanically released by acablesystem.winch is connectedtothe emergency gearrelease handleonthelower center subpanel.Gravtq andslipst.rea..xn forcethe gea:rtothe down:.he gearis mechanicatly lockedin place by a sp:ing - loadec!downlock mechanism. The landinggearis controlled by aleve:r on theleft forwardsidepane!.'":!uslever actuatesswitchestha: ope:atean elect=ic solenoid va!vewhich directstilehydraulic fluidtothelandinggear cylinders.The levertsheld down by asolenotd lock coo-trolled by asc:.ssorsswitch onthemain landinggea:.The :s a .... :oma:1ca!ly released fori"'l.'ltgbt::-e::::-ac :.on.Fo::- eiDer -gency gear:etrac:.on w1ththeweight on :he gear orin case of solenoid lock malfunctionin flight.thelock can be manuallyre:eased byp:ressingtilered buttoninuneears!o:- each gea:- ::hat isU? anC.:ocked.7.!thegea:- is at anyinter-mediate ?OSitlon.cEagonalst:i?es appea:-. POGOS ?ogos are :ns:al1ec abouthal!-wayout on eacn ..r.ng and can swive.3o0degrees.':'he ?Qgos?:-ov:de !a:e:-a:suppon C.!.!ringg :-ound handh.ngand!! :nepogosare not ext::actec?=:orto:a..iteofftheyshouldfall oc: o!the.:- socke:s as:hewingsbeg:nto :t:: .?ogos can be:-e:ai ned !o:- !hgh: by safe:ypms!nsta:leci. o cockpi::tndicationisp:-oviced. 7he a i =p!.ane:ss:ee:-able bymeans of :he ta:!w!:ee!wh!chhas an:-angeo! 6 ceg:-eeseachsideo! cen:er.':'he?ilo:con--::=o!st:tes:t:e=rc; :n=ough the:udde:- pedals wnch a:-ec:rect.yconnec:.ed thetail gear by =neacso! acao.eWaenthe2-il gea:- .s :-e::-actee.:.n:ssys:em !Sinactive. l-30 WHEEL BRAKES Apair of spot and discbrakes are installed on each main wheel.':he o:ake systemisan inde?endent ::nanually ope:-ated hydraulicsyst:e:masshown on figure1-14. Asmallreservoirjust forwardo!thecock-pit feedsasingle conventional master cylinder.':"hebrakesare operated by con-ventionaltoepedals.Since:here isno dille:-ential h:-aking.ei:.hero:- bo:h pedals will operatethesingle maste:- cylinder. Thepressure:-omthe master cylinderis carried to all b:-akesby :neanso! a?res-su:e manifold.Apressure relief valve limitsthemaximumb:-a.kepressure. CHUTE A!6 -!oot drag cha:.e may beinstalled!n :he comparttnent JUSt abovethetatlpipenozzle. ofthereleasem.echan.sm:s mar!l.:.aHycon:::roBedbyacablefr01nthe cocjcpi:.Thechuteis:.Cs-:.a:led!ntheco:n- v.i:.h:he a:ta.ch.icghooiCunlocked. Thisallowsthe chute toleavetheairplane in case oiaccidentalopeningo!thedoo:s duringtakeo!f or :ltgh:..::'hechu:e!s ope:ated byateehai:cleon thestde oftheconsole belowtil.eth=ome.':'he:.eeh.acd!.eis ?ulled, rotated90 clockwise,and ?laced on the "step" 1norderto deploythechu:e.7he handleisau:oz:J.a:!ca!ly!ockec on thes:ep :.opreventit !:-on1snapping back into place andreleasingthechute.Aleve:- adj acent toI thehandleis operatedtoreleasethehandle !o:- returntothe stowed?OSi:ion.Rotating thehandleanother 90 clockwise anrlpulling::. outunlatchesthehook a.cdallowsthe tojenison. ChangecSep:embe:::- ! 968 .?B.:SSUiU::t AF (C) - 1- 1 : BRAKE0 IAGRAM \FILU::R/ -----J LJ '-------- BRAKE ASSZMBLY --------J Figu.:e1-14, 1-31 SECTIO.'IAF (C) - 1 - 1 li the crag dmteisin normal flight,itwill notSta)intact but wit:soon dtsin:egrate due:oengineje: st.rea.meffects. O:ltakeof! or go-around:heshould be jer-..tsonedsmce i: may cot always gra:eilr.mediately. NOTE Adragis ::to::installedi! defen-siveS)Stenl.Sare tc.stallecmthe drag cc'l!teco:nparonent. ":hose1ns:ruments which are not properly apa;-: oi aCOJD?!etesys:em are covered be!ow.(See::.ga.res1-15.! - loand1-li for?2-De:a:rac.gemen: .. AI...ttSP..::.ED!XD!CA70R Acon"ectiona: .;G-to400-.cno: airspeedind:-cator on theupper :e:t side o! thems:::-u-lnent pane:.':'opoin:erssi::nu!taneously indica::eactual airspeed andmaximum aU.ow-able ai:speed.':'beouter dialis graduated in 5-Ja:o::ccre.men:s.A:-otatingdrum.. visible:.hrough a"---imiowin thedial,is graduated ircu:n 0to100in .l-kno::increiDents !or :::ore accurateindkat:on. Tbe max1mum a : :-speec!potn:er showsmaximumst-"""Ucm:-alspeed forthe atrspeed co:-respondmgto the!U:nit nuzn:,er,whicheverts'!ess.Below about a 40, OOo-footattitude,thepom:er willindi-cate :he !unit indicated al!speed o{Z40knots. .Abo"e40, 000fee;thepointer wi:lmdicate lowe:- ai:-speedscor:-esponciingtolrmi: Mach nu.mhero! 0. 80.An airspeed co:--recti.on card isf>OS!ed:.0thecockpit. 1- 32 ALTIMETERS Twoaltimeters a;-einsta!.ledin :he cockpit. Theai:-planealtitcdeisshown bythe a!ti -meter on thele!t sideofthe1nsttuxnent panel.:: is aconventionalsensith,.etype with a:-ange fromzero !o 80, 000 feet. The 10, 000 footpointer has aspecia!notched cisc and apointerexteQSlOn for better readability.Astripedsection warning indlca:or appearsthrough rllenotched disc a::altitudes !elow 16. 000fee::.An altil:neter correctioc. card isposted in the cockp.t. -he secoud altimeteris on thelower right instrument subpanel.By :neans o! amanual selector above:herightside console, ::hetns:rw:nent wi:!readeither cabic alti -tudeo:- ec:_utplXlentbay a!tiwde. YER':'!CAL SPEE..:> IXDICA:'OR ':'hever:ica:speedindica::.oris con\en-tionalandthera:e at which !he air-ptaneis clu:nbhg or descending.based on therate of cha::tgeo! atxnosphericpressure. Thedialis g:-aduated !roD: zero to6000 i"eetper .minuteon :wo adjoiru.ngscales. Pl707 S':'A TIC SYSTEM ":'wose?3=atepicotstaticsystems are ins:allec.Each system contains onepi:o: tubeandtwostatic ports.:'he pitot rubes are located on the bottom fuselagejus: a!t oi thenose.':'hesta::1cports are !lush with thesk1n,each system oneon each side oi the fuselage.!orward o{the Onesys:en:11susedonly bvthe actopi:ot Mach senso::;ttle otner provtdes ap1tot soarceforaltizneter,alr-speed acd verucal speed inciica: ors. AF(C) - ! - ! SEC:'IO: COCKPITARRA,GEME.t\IT J l1 C-F .gu:e1- 15(Sbett 1) ! - 33 s.::;c-:Io. ::: :C=..!..D.:lotPiU>H: I?O:CA70R STA!.!..A10 WAR..-.:!.7S AF(C)-1 - ! DrwlA wo:l!:!.. U - ZC omnB Fgure.l - 15(SneetZ) l - 3.; ..---- ).!."-5 :.. ?CAu;:-zos !..!Cih-:" - Atnc "'ZA.."ilt A:R PRESS. l.:XB--'t ..s-: L"lV'-:RC:tOP TA.,"K,SYS7EJ.fJ. A:XD,9z_A.'\."0 S!..IP?!:.a ?t."YP cas-:-ao:.. PAX::!..S Cba:cgec:!.Sep::ember1968 AE''C}-1 - 1 COCKPITARRA, GEA\ENT DfWlJ Figu.re!- J 5Sbee:5 ! - 36A SEC::-!0 .IAF'(C) - 1 - l OOCKPITARRAGEMNT onAnL onlllK .I.A.S'f..U.. Y ECHE:CX PANE!. WODLl.t11.F C->3 Figure1- 15Sheet 6) :l - 36B ChangedlSep:eznbe=- ! 968 onAilM A C'X!!.!AR TFttE.:.. SWT:'CH-DOAJ1p COW.W Sl:U:C'!Oll WOD!:L U-ZF Changed1September1068 AF (C) - 1-1 oma.P COWloo&SE: LC70il PA->a:L- WODI:!..U-l.C F igure1 - 15 7) SEC -::0..i ----_. 0 --..,-_ onmQ IUG14 SID SWITCH PAM! c-: l-37 SEC-:-:Io.IAF (C) - 1 --TYPICALCOCKPIT- ,10DELU-2C LEFT SIDE Ftgure1 - 16(Sheet !) 1-38 AF (C) - 1-!SECT!OX! TYPICALCOCKPIT- MODELU-2C F igure1 - 16(SheetZ) 1- 39 ~ E C T I O .l.AF(C)-l- 1 TYPICAlCOCKPIT- MODElU-2C RIGHT s::::>E Figuze1-16(Sheet3) ! - 40 AF (C) - 1 - 1SECTIONI TYPICALCOCKPIT - MODElU- 2F F tgure1-17(Sheetl) 1 - 41 ;ECTlo.I AF(C) - 1- 1 TYPICAlCOCKP.IT- MODElU- 2F F igu=e1- 17(SheetZ) 1-42 AF (C) - 1- 1 TYPICALCOCKPIT - NODELU- 2F RIGE:' SI:>E: F igur e1- 17( S h e e ~3) AF(C)-1-1SECTIOXI Beadinginformation issupplied:otherota-tingface of th.einscrmneru: bythe actrude heading ::-eieren.cesysten1(AHRS).An mdex at 01etopoL:hesno""s mag-neticheadingas theca..=dr otates.A!!ux. valve in thewing:ip !u--nishes :magnetic headinginfonnation. the AHRS a:mplifier and gyro plat:fo:rm which in tu:D.feedsthe ln!oriDatiou to the faceof theindicator.In caseoi amalfunction of thethe gyr ocan b ebypassed by se.ecting COMP ou themodeselector;the !lux valveheading in:fon:nation is :hen CU:::?!.ifieconly(!lOt: by me AERS and ied to t.heca..-d on theindicator.(':'he gyr o:may also be used a sa''free gyr o11 for in high latitudes.) '!'heAERS con:=olsare onther igb:c-hand console.ACO:Dlpete expla.nanon oi :ne A-'13.5will be !ou:n.C.bSection IVA . Thereis a;>rese:ect h.earling!ea!n.::'ein the indicato:=wluch worksin conjunc tio::.with :he A''bug" controllec! by aknob in :helo-wer r ig!lt- b.ac.dcornero! thein.st=u-:m.ent. :.heprese.ected !:leadb:g. ':'heautopilot will m...-n::heairc:-ai: to:.he preselected headi:lgwheneverthe liDG :::node (on theautopilot con:=ol panel)isselected. :"he "bug" can be used as an adjus2ble lubbe:=lke wh.en not inFOGmode. Thein.strw:nen: hasC'WOpointerslabeled! andZ.Thepoi:ltersca::t d!s?Laye ither =adio D.avigatio::1systezn information (ADF/ vo.a.)0:" dead reckoningnaviga!ionsteering ioiorm.a.tion (AS.X- 66)cepen.ding uponthe position of !he A.DF/ VOR-AS. - 66 pointer t:ra.n.sfers witch: !.n:he ADF/ VORposition.the o. 1poin1er displaysADF in!orJ:Dation andtheNO.Z poi.n:e:- displaysVORi:l!orma:i on.When thea irplanei sheadingdirectly towardthe s tation.theneedleswUl?Oint totheindex marka ctheto? o! thein.a t:l"lDneut.The a ctual lD.aguet'icbea:-in,gof any s::ation m.ay be read a.stheneedlepointon the rotating c.a,_""1i. In :he ASN-66position.theN0.1 and NO.2. point.e:s display deadreckoningnavigation s tee1::ingin!o!"'Dl.ation asdescribed in Section IV. Theins t:ruJ:nen.thas ared OFF !lag which appears wbeneve.rtheheadiaginformation isdoubtful or incorreet due:o the gyro platform not being errected proper ly.or dueto aloss of powe::- tothe flag .I! head-ingi:Uormation isquestionedseleet COMP modeon compass control panel. Thein.sttuznea.t a lso hasnautical m.i:es distance- to-go cou.nte:-swhich unction when thenavigations yst.eJDi sO?e::-ating. ':'hes:a.::.dbyis onthele!t s ill. :.'hisisasra ... da-d compa ss for cb.ecking :he AHRS and !o:- emergency heading :eie.rence. C!..OCKS Aneight day clockonthecenrer::::::..eo: Ab=acket is a lso provided .for am.as t.e = watc !1.. FIRE SYS-:'EM Adua!warui.aglight above:hein.s::rument pane: anddght of :he d r iitsigh: will U::dl -ca: eaii:-eo rover hea: conrl.ition.E ither conditionisindica ted by asteady light. "!'hen:noswitches!n the forwarde:tgit:e COJD part::nent provide firewa--ningand switches in th.ea!: fuselagesection provide overhea: warning.Tht- a:e no:inter-connected.Thethennoswitcnes1nooth cucutt:Sa.:eto closea::.n.esa..J:Det.ent-pe:ratu.re.The:-e!or e.e!:tter-..o>WQ be au.ecied by either !ue or A c i rcuit t es: swi:ch ou thelowe=l efts-witch panel test:s:.heci..rcuitsup to bu: not in-cludingthethe::m.oswhches.7 heswitch. is m.ovedup !0 :he F::.RETES:.'position and downtothe()IEE.A T":ES:' position. SEC:':OX! AF(C)-1-1 ':""nespeedwarn:ng srs=.emv:arnsthepi!ot oi excesstvespeeds ior agnen gust con-trol con.ftgu:ation by activatingthegear wa:-nin.gsyste.m.!: wasnecessttated by the:-a:>idacce:erat:it:gcharac-:eristicso! the ai;crait andthese:!ousst:rccru:al con-sequenceo! excesstvespeed.:'heincEca:ed ai:s:>eedismonitored by asensiuve pres -su:e. swi:.ch in the nosesection.!! the .s !lying -cn:hthegust !aired. thewartung occu:s a: 2201:. JOk!lo:s.:! the ai.rc:-a!tisfiyingwt:h thegust concol in gust.:hewarningoccu:sa:ZSO( IO)krots. CA."\OPY ':"heatr:>!anehas ao:::te-piece._:e:::isona.b!e canopyhlngeC.one left-hand stde.:'he ccmopy:sraiseI.E An emergency ca.ngpyjetuson handle. yellow.is locatedonthelef: SLde o!thecockpit ueartheforwa:dedgeo! the canopy.It is protec:ed !romrelease byacover whileonthe grcnnd. ':'ojettison t:!lecanopyOXLY.depressthe handlere!easeandpullthehandle ait.This fuesthetorquerod th.rus:ers andreleasesthecanopy mechanically on both sides.Theaft portion of the canopy risesa.Ddissuubbed by acatch ?late a: thetop aft ce:lterto providepitch and late:-al cont:rol of thecanopy.The forwa....-d thrusters !ire androtatethe !or-ward por-uon of the canopycp and aft aroundthe ca:cb :.oc!ea: thecockpit.Thee:::tti:e. sequencetakesapp:-oximatebrPRESSURE SEAL Atubularrubberseal ispro\-tdedtoseal :.hegap betw'een :he canopy frame andthe cockpi: siU a:::tdwmdshle!c.Engine coln-pressor b!eee ai=.suitablyregu!a:ed.is normally csed totheseaLIt is conuo!led by atnanual valve onthele!t side console. Anitrogen gassupply isto auto-matically increase canopy seal pressure u.aderconditions wheretheengineccnn-p:resso:rbleed sou:-ceisnot at ab.igh enough pressure toseal p::-oper!y.Refer :o Section:Vfordescription and opera-tion. A:F(C) - 1 - ! ! EJEC::'!ON SEAT :'heejection seat is oi si..cnpleligh:weigh: eesign usinga"low- g" catapultto min.imize thepossiliillty oi ejection injury.Theseat hasno adjusone!lt provisions.Pilo:: posi-!.n:heseatadjus:ed by u_seof wood '!>locks.Ashoulde:lock- and- release _everis on theleft- handside.':'heejection seat i sequippedwith an au:omaticrelease seat be:::.There are no a--::nres:.sonthe seat cu::.dejectionsequenceis started by pul:ingup on aD - ringloca!:eda:thefront oi !heseat between:.hepilot'slegs.See !!gu:e1- 18. PullingtheD - ring actuatesan M3 iaiti.ator whichsta=:.sthejettison/ ejection cycle.The iirs: initiator provides gaspressureto start thecano?Y sequenceandtodisconnect theelevato: coottol and stowwheelfor -wardto clear thepllot's kneesa:td !eet.lt also actua:es a:.' - 34 lnitiator.The7-34 ini:iatorhas aone-second del ay be.fore simultaneously lockingtheshoulderharness. acruating:he ca:apul: and another":" - 34 ini:iator also with a1-secondtimeC.elayto :el easetheseat 'belt.':'hecatapul tunpa:::s amaximum of l.>g accele:ationtoa350 ;ou.ndseat- man.:'hisissufficient to clear thevertical !:n by7feet a: Z60 1cno:s.7he additional one-second. dela;- in theseat belt re easesystem allowsthe seatto bewell clear of :he a i !7la.:leprio:rto opening o! the belt. Onepin isprovidedin theM3initia:o:r onthe:right- handsirleof :hesea: pan.This znast be:ren:1oved !or theseat to!ire. Referto Sections4Aand4Bfor descrip-tio:t and O?eratioc of :he followingauxiliary equipzDe !l::: Air Cocc:.nooicg a::tdP:ressurization System. Changed 6 ove=nhe:r!967 andCa.copy:>eirostiog Sys:.en Oxygen5;-s!e.m Co:n:nunica:ionsand Associa:ed E !ect:rot Equi?me:1t LightingEquipment D:iftsight System Sextant S)Stent Ha:cbWindowHeate:Photog:aphicE lec:.:oc!cI.n!e!l.ge:tceSystems F-ZFo1l System P - 3Pla-::fo::-=n Sys:ec B400Ra:eRa:eMe:er Observer Weather Su_.-veyEqui p:nent Dest:uctor CompassSysten1 Autopilo: S y stem

Ae:iatRe!uehng (ARS) DeadReckoc.ing- a"igaooa Syst:em 1-47 1- 48 AF(C) - 1-l SEC':': ONI CAOPY Jffii SOANDSEAT EJECTIOSYSTEM(SHEET1) 1J.! 11( XJ.l U) CA.'"'?Y ':'Hllt:S"!"ll lC.U."'PT R..!..AS :.A ':"oa::5 ,3 Pl..ACS1 1ZS (n6) 4C.U\OPYL.A. TCH :>aN RO!>ASS:.:.31. Y BTV::: f:'D.l.S ! ) s 0 10 .l 5CA.'"'PYUPl.JFTDl) c.!.IllXl.Ul - CA.'"'?YLATCHR.!:!..E.A.S':"'RQU!:':"1!3!: oCH!:C!t VALVANC>24'9-4J 10CA.'"'?Y JU:LLt.S!: HOOKS( lPl..ACS1 11( 72.5) INJ'I'!An>RAC7UA TD BY !7.o.l 7) tluz- ':"l.5) INrr!ATOaACTUA!':> BY 17U 15) 13CA.">PY PULL HA..'OL CAB!..!: 14CA.'"'PY HOOK RO:> ASS:::..W.S:. Y , BL-.r":".:::WS1i C lSCA..._OPY!.:.!PULL F..A!i:>!.E Fig.u-e1-18(Shee:I) AF {C) - 1 - 1SECTIONI CANOPY JffiiSON AND SEAT EJECTIOSYSTEM(SHEET 2) c:=:t a::!:) n:'S!:.'IG - ROSE (&J3li.EJQ - IJ05X (Mr:A.U

fWT:1I ocr.:Ea. aoon w.urtL\.Ll..TEJ"EC!:C.A. 'C>.u; . .. :sc:c STS:"'::WS.w.um.u.1.TPe': ::s;; CA:JIOPT PC't.!.. &.UC:U. OIC.T CA-'roPT .1E':"':"!SCKwu ( TbI OO"nATO& s:t:A-:- Sl.:P : CICin ( Qln. Q;Hj NO"!"E I -

8001; Dll.-rl: llOO A.SSE:W!I!..T ( L.EFT s:!JEI tt'EJo,CSSHI)'WN "Wr.'1l AJtL o r-:-ta:5A":" .."lX1:JDDC STSTD&.. OF '7X!: CA.'l?Y J :.::specialP:-t-se:as brieiec o::- as !:.-o:n app::-op=-iateeC!u1pment Prc:-ss-to-:est :!ghtsoi appUcab:e spc:-c:a! .... 1p:nen:. Oxyge:: quick c.sconnec:- C.:--:ECKE.::>. o6. co::nec:!ons- Cr::.EC.K=:D. o9.:....O'Aalti:u.deescape l.anya.:-d-CK::C.K=:D. 70.?-! :-e:ease- CHECKE..:>. -1.?acepiece :.a:ch- Cl-ZCKE..:>. 72.E::me:-ge.c.cy!ace hea:. core-7neassis:ant shOt.:..lc.nsu::-ehot.h c:scon.nectsa::-ep::-ope::-r)CO:l. -:r:ec:ec. 7 3.app:e- CHECKED. f o :- evidenceoi hav!c.gbeen inaC.ve.:-:.en:lypu:!ed. -=-Ex:e::-na:::-ea::- vtew mi::-.:-o::- - Cr::EC.KED. 7 5. A.JF 21:dVOR- C!iSC.iG:D. Check at! :funcuo::tso! ADF and\"OR. o .Canopy ba.od:e- DOW.'. 11.Canopy- C.:.05E:D LOCKED. 78.Canopy aandleco..er - 0\'"E.:>. 7he S:.a:::-:E ngmc:and Afte::- S.ar: checklists w:ll be pe::-fo:-mf"cbythepilot the L!Seo! an assi s-::a..nc.':he canopyv.i.ll be dosed anci ?::-ior :oenginesta::--.:. 2-6 becauseoi thepossibility o! enginedam.age if looseitemsshouldbec!::-a-wnintotheair in:.a.ke. I. B:-akes- HO.:...D. Eold bra.ltesu:1ti.!readyto:a.x.i.. 2.S:.a-::--ti.cgunit. - S7.AR T. GiveW:ndup(ci:-cularrno:ion o!: index fi.t:gertos:a::-: al!Xilia.rys:a-::-ricg unit.) 3.Sta::-ting air- OX. .i!Ut.ersta:-ti.n.gurut ::-ea.ch.esIu!J.. :-ai se handwiththwnb U?tosignal crew chie.f tha-.:.youa.:-e::-eac.y!or sta:ting ai=. NOTE :>-.u-ingsta=t. obse::-veemergency !ue! sys:.em !.tg.i:tt..:...igh.tshouldgo out between 3toJOe:!RPY...:! .ight isno: out by101R?_..{.discontinuesta::-:. and grounC. checKsystem. 4.J:gn:tion Switch- 5-:"A.R:- A."'DHO.L!l {at .."":lof12e-ll RP. !) 5.:'h.ro='o.le- ::>:.E. Place :h=ot::.;.e!ntdlew'henengineRPM reaches18;"..':'he .EG::'ind.ica:Jonwill beverys !o'O\ . CAUTION Although:be desi::-eds:.a:tRP. tis18c:-: pneumaticstarter.imn.ations mu..s: be observed.-he th.:-on emay be mo,red :o idleat aminimu::n of R?:Y..if necessary. : nonnai start is notindicateuby a .:-isein EG7 and/or oil?::-essu.::ev.-ith-in 30seconds a!:e::- thethrottleis placedinidle,release1gnitioo switch. :-em.rnth::-ott!eto OFF.andsignal s::a.rting air OFF.Allow excess fue"i. to drain !::-omenginepriorto ingnext stan. !f EG7 exceeds400 Cduringstart releaseigrutions-witch.throttleOFF. and allow air sou.::-ceto :-orateengine !or 30seconds. Changedl !968 A.F(C)-1-1SEC-:":OX!.! o.A?U andstarter air- SlG. PL_ COXXEC:'. A: RPM.re:easeigm:!on sw-itch. Signa! t.hum'b out to discon..nect A?U andSta.r"terair. 7.Genera:or- Banery Swit:ch- BA 7& GEX. P!ace:n 3A':' &GEX posttton ai:er auxiliary eleci.-ical poweris dis -connected. A.FTERS:'ART 1.:d!eRPY- CHECKED. !c!ebe approxi.ma:tely .:s-r.. Z.Engi=tein.st--u:nents- CHECKED. Check :.ha: a!!ecg!neinstruments and hydra.U:.tcp r essure gageindicatenthin norma: opera:ingrange. 3.Caco?Y andequi:m:ent 'baysea! valves--ox. 4 .?ressur!za:.ion- CHECKED. Check !or decreasetn cab.ne. Recheck a!l enginecu:_d!light instru-ments fo:- properindications. 7 AKEOFF .=.ines;:,eedai:.d:-e!usa!speed computation and u:i.'izatlona:e not nnrmal!y feasiblewuh :hisaircra!t deeto :he rapid acce!era:ion. extteme!y short takeou::u.nand tion of :hep1.ot W!:.h direcuona! control. However,thetacncal situation mtght require :he useoi takeoff Ca.taforve:-ysho:-t:-un-ways. Ad-.-ancethecl:t:-ot*..!e-:o80 Release ...... :l:tebrakes . CAUTION ::'hebrakes nu:.st not beu.sedtohold morethan socr.RPM or landinggea:-failu:e mayresu!t.EngineRP).f inc:-ease may !ag bebicdth=o!'t!e advance::nen: due:ostow eng:.::eaccele-:-aiion.Ca:-emustusedto avoid overshooting desi:-ed Changed o Xove=nbe:- 19&7 Con.:lnuethrottle advaccetothegate.:.'hts will gLveapproximatelyRP).!. :?he:.hror-Jegate stop is iulportant because the autcunattcsensing deviceshave been reznoveci !rom :he fl:el contro! andtl:estop protects against overs?eeding andover-teznpingtheec.g ine. Whenusing:he gatestop,:tis notneces -sary toclosely monitor engineRPM arui EG": du:!.ng:akeoff. Full throttletakeoff should be avoidedsince theengineis fee! !lowtinuted at sealevel .-hen operating at maximumpower.The th=ottle will haveto beretarded to control theEGTto 630 Candor thec:o100... at about :.h.eti.Ine-=hea i=-pLanebecomes air -borne.F ull must bepaid :o the control oftheaircraft Hold ronc-o!. co!unm ceu=al duringinitial ::a._"arpo.seshocld develop on ::a.. At ?ilot sd:sc:-etion.engage autopilot . Check au:.opi.ottrim and flightopera-t.on du..ringdunb between 40. 000 and 45,000 fee::. WARNING ?::-:o::- toengagingtheauto?ilot,the at::-p!a.nesnould be:lea: b.ac.dsofi.Do notengageautopilot if :::m mdex shows fu:l cieflec-:ion. Prior :o engagingor disengagingau.to-p!lo;:he t::-imiru:exesshould beobse::-ved !or near ceot:al position. ).E:J.orosci!lat:oas may be present but sCoc.:d?::-ese::t!:::_oprob:em.:!t=iln icdexes a:e no:nea::- neu::ral,t=an.-sien:ssho:.:!d:,e antici?a:ed. WARNING Subcomponent failurescan occu::-:he au:o?ilotsyste:n which can render any oneaxis or all:h:ee axes:n.ope:-auve wit.o.ou:bene!i: of the CAUTION 1xght.the AUTOPIL07 :>lSCO..wa=n.tngt.gh:.or thedua.audiotonelntheheacset.Do'lOt:-ely exclus .. vely onthesereciicationsto that theauto?ilOt:isengaged and connolhngprope::-ly. 55, 000 - FOOT CHECK l. Gt:s:control- F.:::mina! cl.zr.u"'as maceaGGS7. 2 .NA. VLght sv.ttch- OFF 3.Bleed\a!ves- WHENBLEED VA.:..VELiGHTS ::..Li;. ill'A 7E.(For ma.xunumrange:-ec:i..tced?Owe:- opera-tion)observe mini.mu.-nEPR h.rn.ts!o:- c;osec:i. 5.Y.achHo.d- ON (a: cO. 000feet). o. mocese.ec:o::- -(If appLcaole. ) 7.Spec1a!equioment- 0. ASBRI.EFED. 3.P:-esst:nzauon- CF..ECKED. 9.Slippe :- pump sNi:ch- 0. asreqcired. WARNING Donotsh?perpu.:npuntil !uel load.s below 800 ga.lon::.:'1U-!C or 300 gallonsanU -2.F. CRUISECLI!-.U3 ":hecruise c lur.b'-tills:.a:-:a::an a:n n:deoi o 7. 000:o o9. 000fee:exceo: lorthemaxi -r::u:znrangemiss:onluch s::ar:s a:57.000 to59. 000:feet.':"hecru:se c!unb comprises Utez::1ajorportiono!thetotalflight:ime amiis flownmama!:Ule rto obtain rr.axL"Dw:n pe rionnanc e. )---. :> (C- 1 - l thewnh mach hold!s usedto controltheax.:-c :ra!taboveoO, 000 U:-:.::bule>:ltcomhaons a:-eenco...tnte:-ed o!theholdIT'.aybe":"i::.eCeSt!'eCC:'"L-1Sec!unb a:.::-speerlschecule i s:10t acor.:s:ant Maca nl.!.l'nber;:.he:-e -io:-e,:.:Je .!denser.:so:- w:l!not coot=o!:he exac:.y. WARNING gbtinsu-umen:s, u-imindicator, and ::-iminc:cessnould be i :-e -c;uent!ysca:'lneCtoir.:su:-ethat :.he ce-s!rec ::. ght a:=!tucieandalrspeedis be!nt; l;se:!le !ac!::=::..--:::whee!asnecessa:-yto :na. n:atntile? :-cpe:- :n.ti:ca:ec a.:-s?eec. I:1S''eryunpo:-:a.n::o fly:..:tereco!T'.I:Oencerl S?eecscneet.le.At aln::cudes wi:e n: na ?Owerc:-u. se c l u:nbtl1e at:-c :-a:: must be!:ov.-:t between very t:a:-:-ow s?eedlL--::::tsjest un.ce:- :he.lac!: !)u!ie:!.unit. See::gu:-es o-Z.o-3,a:lCo-4.A:S?eeCS !:o3JC":Ots!as:e:- :.na:1:hes:anc.a:-ci speedscheccle,:yp:ca! tach e!!ec:s of Mach or nosen:.ck!osmaybe eocoun-:e:-ed.if anyo!theseS')"lllptomsa :-eencoun-tered.andii the :AS is a: o::- abovethest:and-a:-Cspeedscherlt.:e,red'l.lcespeed no mo:-e :.ban2.kno:sbelow c!unb speedschec!c.!e anCSta!lbu!!e: orsta!.l b.!encountered a: speeds5to 8knots s!o'"e:- :nar.:thes:anda:-d c.;.mbspeed sched-\!le\l."aer.!!y:r.g:a a::nax..mc.mpower.maxi-c :-..:.1se!.! bc!.fe:ingis eococ:t:e:-edand.:A.Sis oelowthestandar d c!hnb speecsd:edu.e,incr easethespeed :o c:::nbspeedschedu.e. WARNING Duri.."1gmaxi.mUJnpower c r uise clU:nb, n:tsdanger ousto aowthea: r c :-ait toap1>r oach speeds o! 5:itnotsor more below :hestanda:-d c!unbspeedsched-ule,because asta !canReco-ve:-}'f r om.as:a!! a:mavbe ext:re::1e:y dif!1cc.!t duetolack o! a1ler on res?onse when :he w1ngiss:a.Hed. Highspeed Mach bcl!et and :ow speed stall bu!fe: feelsimila:- .AHe:-onr esponse.s goodtnbu!iet andve:-)poor:n :he low speed s:all :-he at:-speeciruhca-to::- :n.:st be:-elied on auitn dete:-.:.nicu:g whether ts d..:etohtgh or !ow speec. li the:-eisany qc.es:ion:-ega:-c:ngtl1eaccu-:-acyo!the ai r speed !nc:cato:-,o:- the abi!i:yto C.isce:-cwhethe:- bt!ffe: :s o :-s:a!l bu!!e: .a lways:est byl!lcr e a s!nga i :- -speed.Xeve::- tes: byr educ .nga nd :- tsk stal!tng.-:'heai:-c r ait can he !:own sa!e!yinto buffe:4knots(assho""-non !igu:-eo - 3)mo :-de::- to estabHsn pos::.u.\e!y bc!!e: ishighspeed ! a ch bclie: ace ob:am aone a.:- speed Tnese\e:-::y o! bc.!!e:mayincr easeto :node:-a:e o:- beavybcl!e:11 when thischeck.A lso,a:ucAingor ?itchdov..-n tendency may develop,requtnng aback stick for ce of 10wlOpot.ndstop:evenl thespeed ! :-om bualdmgup. !.ncreastngthespeed mo:-ethan .;knots tntothe!-. !acb bulie::-esion v.-i!.U::c:-ease thesttcit !o:-ces, tuck,and may :-esult in wingro!lo!!.Do::lOtpenet:-a:etheMach b.:.!.fe tmo!'ethanthearnoun:sta:eC.as seve :-ettye!Iec:.sv.-i'!.lbe encoullte:-ed. (C)-1-lll WARNING Hon actopilot when making :he above checks.bac.dsshould be on :he. wneel :.n:.heof possible clutch slip-page.:! :.heacto?ito-::isdisconnected, stick forces must be :maintainedto avoid:-api.C.?ia:hdown. !I thecannot be !.own""'ithou: bci.fe;reducing po\vers:igntlywill provide ::-e:ie!.':'he aircrait vr..Udescendseveral hundred fee: wh:enpovoerisreduced.Power shoC.:d bereswred assoon astheairct"a!: ca.:1be{.;ownwtthout bui!et::0obtain maxi -m.t!IDal:itude.I! :.ile aircraf: cannot be flownlknotsbelo""s::a.ruiard. s?eed schedu:e wit.hout highspeed buffet.:.heai:s?eed/alti-metersystemsshould bet:ho:-oughly checked a!:er the lligh:. NOTE !.!inor rando.mbuffetdistu:bances due lOeitherauto?.!ot operation of the sensor or c.ea: a.r ru.rbu-!enceshowdcot be acause for.reduc-U::.gZkno::sbelow schedu:e ai:-speed. Anigh a:titwie:he "g" capa:!::nbtyis limited because aircra!: is O?e:-ating at high 8: coeffic.ents.Codersome cocdittons hu!:fe: -...;;::beencountered a..:!. .:g.ln a :u...-na:a.ng!.esin excess o! :bestanda:-d 1Z0 roug"m:-nit isimportant tomaintain ai:-speec3andto.erate buffet to avoid Wheea: maxtmum a:!owab!e ecgine ?O-we=.the a t rplane .f!iesat aco:n-bica:ion of altitudeand wing:ift. coe:icien! :ha: aifec:sthe!lyingcharac-:.e::-istics.It can be flown n:anua!!y,but no:!orpe::-:oeso! rimesincei: ::-equiresthepilot's .fcl! a::":en:ioc.The::-efo:-e.a?rope:ly !1.:nc ::ioningautopilo::is necessary!0 sans -iactori!y acco:mp!ish :he mission. F uele:reexac: informa:io::. Changed 6. ovember19o'"" I AF(C)-1-1I! d-escent :ust be:ov.speed ior start o! bu!fet.":'n.s:s approxunate!y10to15 knots belowthe warn1ngneedle,varyingwtth weigh: ancaltitude.WhenZOOknotslASis reached,contnue ciescentat thisspeed un:essru::-bulencetspresent. In :o obtainrna.xirnumrange.remain a: c::-utsea:ti:udeunt..lapproximately75 nau::cat mles fromthelancingbase.Then s::ar: a for ast:aight-Ul approach. :'hiswilloringyoupattern altitudeat the !ie!c.:athisproceUo:e,only asmall inc:-easemrange:srealized;however,pre-rnzn:.:::-ecescent maycause alosstn range dt=.e10c:ncountermgheadwinds. FAS":' Re!er:o Sec:Jon :r: !orontni s ScD.Jec: . CO!\":' RO:..LABIU 7Y Du..::.ngcescent.i! thespeedis a llowedto get above:he warnic.g::teeele.bu.Uet--g ana:.t;;ckwiU :,eno:ec a.ru!ca.:1becor-:-ec:ec !o::::bysloeo"WC.:!. in aturo a: :.he::.me.decrease a.:1gleo! barut.See Sec:!ooV! for comp!e:eon !!igh: c!:a:acter!St.cs. CAUTION extecctilewtng !!aps above 000 !ee: s.cce dangerousp1:chlng ef!ec ::sare Cc.a::geC.1September19o8 .::>ESCE:-t7CHECK Accomphsh descent 10 accordance ..ith :he foUov.ingprocedures:o eosc.r-esa!e ar-c:afta.nctopreclude damage:o equ.psnent: l. Q,qgen- PRESS- 70- :'ES:'. Check oxygen andpress..:resuit by use of PRESS-70-TES":'beforere"carding throttle!or descent. Z.Bleed ""alves-Bleedvalve - 0:-\. 3 .Defroster- 0:-\. ""'Heater-b!ower cefroste::::- OX. o.Sh?per pu.mps,., .tch- 0. !or- 5 :n.nutesti necessa:--.tos:rt? tanks com;>ie:e!y).ACgene:atorpowe:-15rec;ut:ed. 7.Lanci nggear- EX-:"E. 'DED. 8.Speed braJtes- EX7.EXDED. 9 .AUXAlRS"'- i :Ch- PRESS OFF. NOTE For U-ZFthe AUX7ANK AIR swt:ch mus:remam i nthePRESS 0. j)C)Stt.on!or descent if auxili arytanks conta.ned faeat ::a..c.eorr. l-Z3 I A:F(C-1-1 10.Thro: ::e- Reta :-c.EPR. WARNING tAro:tleat o:- nea:- cab1n mays.O'olo:- .se :.oa.mbtent E ,.;amp.e: bolchnga!20. ooc 1 LA.rspeec - app:-op:-iateschedule !o:- thetypeof descent oemgmade. !2.E qci?;:::tent:nodeselector- OFF. ! 3.Spec :.a:equ.p::nen:- 5 7 Set as b =!efec o:- as.ncaca:ec by specJ.al NAV ::gn:OX(a: 55,DOO! ee:). 15.AC ge:::e:-a:o:- - OFF3.5::::7he:l !.g!:l.: co:':'leso-:o:- :::o:.:::eecec). !o.G - s: cor.::-ol- GGS:- A-:- .;5,000 .EE7. (:! :::o:C:ot:ep :- .o:- j! :i .S:a:!s:: ips--!..&Ra.I:'lbe:- !::nts ("lrit:tta_-c:.cg gea:- CO"i!.'l:lanc !ockt:C.. CAUTION :i i:.asoeec:::::tea"rno:sn.:-e, cemay !:a\ie:o:-mec:n:..-:1estast:-1p v.e:ls.:i th!sOCC'u:-s,::.may oeneces-sa:y;o cela}cxtcnSlOC of tneStall ....t:::!!:.he..below thei : eez.!::gleveL!! !Ce.ss ... co:::o:exe:-: ab:::o!"':':'la!pt:l: !o:-ceo::tile sta1.s::-:pT- han. As speec:s cceck :ne :.rim b}not:.cg:.!leco:l:::o!w.i::ee.posi -tion..Shoulc be:hesame a s!Cwason :.hea!:e:- t:a.ke oil t :-i.. -::cceck. )Co ::::-ec: !o:=any wingbeavmess b):ra c.s! e r:-icg :ue! !:-0:::1:he neavy.og be!o:-e:anding. Re::::tovestov. bag belov.caoao a!:::udeo!10, 000!ee:. 2Z.A 7C- CHECK:>. Z3.Altuneter- R.ES 770 S:'ATJO_ A.!...:::.M.E:'ERS.E7TI1"GA 718,000 Z-L.:....0-..a!: ituceesca?f:ia.nya:-d-HKED Z5.Slip?f: rpump sv.i:ch- OFF.(.:i appltcaole. ) AF(C-l-1SEC7IO.'G 5, 000-FOO-:' CliSCKDSCE);DL.G) 1.F uecoun:e-:- - CHECKED.SPF..E"D

ChecktheIue!:-err.ainicg and cete:-rni:le tne:n.:-esholcspeee for!acdicg app:-oach. 7hecor:-ec:: thresholdspeed c an be oo!a.ned f:-o::::1Par:: 8of :heAppendix as ao! !cet :-e.::nain..ng. CAUTION .n:e:Jgcs::')r.nc conditions add one ha.! o!thewutd gust !ac:or W!threpo:-ted gus:s:c.excessoi !tve lu:ots.7he co:-:-ec:-on !ac:or .s app:icab!eo::tly:othe !:.na. app:oach ai:-speed. ITh:onle gate- c.:..OSED. A!:!:ough:ite airp:aneisdd!tc\tl: :o lacd,!: doesba\.--ecertaic cha:-ac:e:!stics :.ha: d..!!er !:-on:.o:.ner ;e: at:-c:-a!t.:t is esse:1tia:::ha: ti::tept!o:ha.reatho:-OI.!gh k::ow!ecgeof :.hesecna:-ac:er.sticsill.o:-de:-:o beabletoacco:np!:shlancicgswith a n!gn degreeo! prec.ston a.nCsa.!e:yunder a!!!"t!!lwa)wea:bercor:C:oo::tS. Whh wi.!lg!1aps up.the:oral dragisso low :ba: :he ai:-pla.neill :::la!ntain level !!igh: a: ?4!tte:o a!:.n..:dewi:h enginespeed on!)a!ewpercent aooveidle.=: ... e!l'\11.-ith gear and pa:-nal wingextended, tileglice-a.ngleissh.a!tow.necessitatinga flat approach.?..owever.wttn fullflapsa powe:- approach can bemadewith as m.ucb as SSI:':eeg.ne Uponreducingpower :oid!e.touchdownwt!l occur with am.int-mt:.In !!oa:when usingteep:-oper :.hresholc speed. NOTE -:'here!s 1:'.0loss ofraccer o:- a:teron e!iecc..vez:esscit:etoustngfut:flaps. Ho,ever,:.here:isshgh:!y more bui!e-:.ngat ..:mt-sandshgh: direction-athuntinginrougn air.1'b.tsts not constdered obJeCttonable. A:ypica! land:n;pat:.ern,us.ngme3&0 overhead approach.:s s:town:n i .gurel-Z. Fla? posttioa forla.nf!ingmay be ct-ter-mmec bythep.lot w::.::regard:c- Cl:-Uton UsEngiuH!laps wiU:-esu:: Laam.o:-eco::t'loentlon.alapproaC'h..'With shor:er:!oa: Ols::anceand as!lor:er ground ro!L WARNING l>ocot exceed30 o: bank curi:1g any pa:-:o!tne:=a!!ic;>a::e:-:!d..:etothe decreasecsta.l ma:-g.n as bank : s ..ncreased.Atrc:a.:: cont:-o:.s a:so ciiificul: uncer condinon:iof moderate IX::-:_-\..:.A..??.ROACH Makeint:.a!approach su.!.iiciea:engi:le tonu.nta.ini.h: :-akesearlier and ha.:-derti:a.:1 no :-mal. 5.Shut o" engmeasea.:lyas possible. :'his witt oo:-m.a:'!.y :c::.eanu:ru:nedl.atety ai:er:oucbdowo.,however.:he ellgin.e may beshu: downa: :.he:hreseotd i! lack o! ava!.lablerunwayshould cii.c:a..te thisprocedure.Eagmetdlethrust is aia:gefactorinlecg:hoifloatdis -ta:lce and groundroll. CAUTION :I ue deciston is .madetoshu't down theengu....e.: tn.:'esaotd,ex.ce.me c ........:rc.q.Ured cu.:mg::h.etoucb-dvwn _ ...,ine powerisnot ava1.Lt.h:e!or go-arou.od,ana.Ute drag '-.ca.temay c.o: come out o!the if deployed withengine shut orr. Z-31 AF (C)-1 - 1 GO- AROUND ::>-..:.e:o cite:a:-gean::.ounto! excesstll:!:'usr.. cautionbeexercised :.omain-ta::l conttol o! :he a.L7lane.":"".o.e powe:- shou.lcbe aededs!ow!y anc only as m.uch powerasis:-equi rcd.':be 93CO':t:.o slopshould beobserved except Ulcase o! d i :::enecess ::y.':'heappticauon of power causes a:x:noc.e:-ateaose'-P::-u:n change. ':'rus:nus: be for by ap-p!.cationof nose COw:l:r:..m.a.ncirnoee:-at.e coc:ro: push !o:-ces.1:.isnot oecessa:y :.ore::ac:. :hew:cg !lapsto ::ecccedrag.:m::.hey a:-e re:ractedin o:-C.er:o eLm:oa:el-eneed:.oobserveue :'.ap p:aca:cspeed.Re:.rac::o:: o! ::!lew'...ttg flapsa:So ca..;.sesanose up:rim change.: :!.sno: necessary 4.0:::c:r::-ac:the gear or speed brakes. Be!oreTouchdown '!.!:oeceC:sionismade:.ogo arou.'lCwh.!e s:i!!i:: !Ugh:.:.he!ol.ow.r::g? :-ocedu:-es a::e usee: Applypoweras rapidly as dest red. Resis: :.he::ru= change. l .W'i:1gflaps.maybe :-e::ractedunmedi-ately.sUlce:.hea i rplane will be accel-eranng acd altin:cielossdue:o !lap r e:rac:ioc will be A!ter 7ouchdown !! tiletouchda;:-nhasbeen !':"..ace.t:se:.ne !ollowu:gp::-oceca::es: ! .!! : U:neper:nits.sta:-t wing flapsup. l. S:ar: application of nose coWl:trim. 3.Ad...-a.ncepowerrapiclyto RPM.. l-3Z 4.Asaircra.!:speed inc r eases andeleva-to:=becomes effective.inc::-ease?OWer as desi::-ec. 5.Do no: allow:.henosetor tse abruptly upon b::-ealongg ::-oand. CAUTION :X,not exceed:hewtng ilap placa..-d speed with !laps eJCT.endec. ':'ouch- a.:ld - go :aneings wi:.h !uel loads o! 400ga!lonso ::less a ::- ea:uo::!zedm aircrait and can berout:inel)- accomp!tshed without d ; ft}cu!ty.accel era:ion 1s ::-apirl at:e!.n:nway !ength :..Snot acritica l fac:o::ci:.:ricg:.occh- and- go operations. A!ter::o:::maltoUchdown.the aucra!t should be allowedt.odecelerate to50kno:s.a: whicn tix:ne:be !"..apsshoc.ldberetracted ane:JJee!e'I.'"2.:.0r:riJ:nrese: :o=a.::-dthe ne:u:.:::alD-..1etothe:-ate o! c!lan.ge in position o!:.hee!e'l.'"2.to::- :r-inl:.ab. app::-oxi -ma:e:y 8to13 seconds will berequiredobtain neutral :rim position.liscallyitlS sl.!!!icieotto apply :wse downtrim d:urmg theti.:ne::-eql!ir ed !or the to 'When tiletakeoi! !smitiated.engtnepower should be advancedto at least ss,;RPM and:.hecontrol colt:mn placed forwa_-d of :henec:t:::a!position to:-aisethetail ap?roxi -m a tely1foot abovetheru:nway.As:akeoff speedtsreached.back- p r essureshould be applied gentlyto:he control co wnn :.0ay the atrcra!t!romt.herunway.Until ex?erience is gainedin the a ucra!t.con-siderable a : tentionis:o prevent excessspeed.7her eis acommon :endency to gain excess altitudein theclosedtraffic pat!ern.When zna.kingaclosed pattern. use:he .Before !..a.ndingcheck a!te::- n:rn!ng downwind . A:(C)-1-! SEC':'IOX!I CAUTION Ao! excessive powe: app:.icatioo and ase o! !ull iorwa=d cocr:o: colc:mn z:novemeo-::will: e-sclt in the ai:c:ai-:: beco:mingair-borne and!'!yingback ontothe way be:!o:estt5ciea:: elevator ba.ck-pressu:e can beobtained 10keep tileai:-c:a!t: a:.rborne. -:'AXI:XGW:':'HOUT POGOSA.F-:'ER Theairc:-a!t can beeasilytaxied W:.thout ?Qgos!ns::a.:led.even with acrosswing com-pooent of ZOkcots.::is possible 10tu.rn theatrcraf:: anC.co:meto ast:op downwtmi l.tcde r:h.eseconditions. is cesired to ::a..x:.the at:-pla:leo!:!t!leactive:-u.n:way l.andicg.:1:!e!o lowingprocedUie can be 1.S!.ow ai:c:a!t :o 30to402 ..7'ettisond:-agchu:e. 3.Adc!sl!gn: a.m.oun:: of powerto maintain speed. ':'oa idin:u.rning90 degreeswith mini::nttr.1 radius.hold:Aewioglow onthes!c!eo!the C.esi ree !Urn for at :ease 1000 .feetprior to tc.rning.':'hiskeepsthedesired wingtipoo :he grou.od dUiia.g:he tu.rnsincetlt.e!uel wi.1 i:averuntothe :ow wm.g.:! thisis not done. forcein theturn wi.U:hrow ate oa::s::cewi:g covo-nandincreasethem=n radius.:'he m i ni:num:r.rningradiusis approxi::nately150 !ee:. :'ake !'u.l: advantageof inte:sectio::1sby get-':U:gtooppositeedgesa.nd cutticginside corner of i::cersection.".:'akecar enot to h!: runway an.d::axilights with tilev.-ing. -:'hischeckl:st shoult!be completed assoon aspossible airerthe!amhng!s comp!.e:ed and:he a:::=-c::ai: brought toastop: 1 .E jection seat i n i tiatorsaie:y pin- :-A:-:_c:n. Z.Sealva:ves- OFF. 3.A'.:C- OFF. HF:rac!i o- OFF. 5..:.anding- OFF. 6 .P i tothea:er- OFF {i! apphcable) . 7 .A.uci!.iaq :Soos: ' Conti nuousignition-OFF. 8.Ha:ch hea:ers- OFF. 9 .3leed va!.'"es- CLOSE. 10.StaLst=: ps- RE:7RAC7. .:.LHea:e-:--blov.-ercefroste: sv.;.tch- OFF. IZ.Equipment master s"" itcb- OFF. :! it is desired totaxithealrcraft v.-ith ?ogoslancing.!oUow tilesamep:-o-cedu:es as outlin edon page2 - 10. CAUTION. Donot ta.xtwi::hcanO?Y open. l - 33 SEC'::O.IT A:(C-- - ! 7h!s chec:ts::o ... :c oeco=np:etecassoon as ?OSSl::>!eai:er a.:-c:-a.!:ts.,arK.ed: 3.!.nve:-e::- - OFF. ;. AV:.gnts- OFF. :..X...riga:.ioneqc!p.ment- OFF. o.Car:opy ceiros:e:- OFF. i.:'h:-o:::e- OFF. :I .:.:s: p::-!ortoshe: cown::heenginehas been ope::-a:ecfo: mo:-e!hanZ minutes a: t.h.a.:lRP.!.ope::-a:ea: !o: at !eas: 30secones.Snt:: down:he e"lg.necpooo:s:gr..a!f:-0:::1c:-ew ch!ef o r wnencesi:ed b)' 8.Co:nma.nd:-adios- OFF. 9.3a::e::-y- Ge"le:-a;o:- - O?F. iO.Canopy ,:e::.sonco,.e :- -:);S! 1.Ca::o?Y- u,;:..ocKS:> A..'C) OPEN. ! l. ?e:-sor:a!eq!p:nen:.- UXHOOKE:>. :ns.Jre:1-.a.:.a!!,e:-so:12.lec;t:ip:ner::!s =coo:ted pr1o:- toa::en::p:i::.g:.oge: ou: o! tilecockp.:. l3. -a!- W:-:te.:pal: c.sc:epaocies.n ce:ai!. l-3-i FUE!. DU.MPDlG !! it is c.ecessarytodu:np !.:el prior :o landing.accomplish thep:-ocedu:e: 1.!ligh:.15.0:o180 knots.flaps !aired. ote wheelpos:uon. Z.AOX'i'AF"'LU ... .L AUX O?BNandRAUX lightsshould iilw:ni.n.a:e..Make..-isual check. CAUTION !! ti:ewheel positio::l moves apprecl-ably whiledw:nping.:.b.evalvein the light wingshould beclosed.Check !orf::-o=nheavywing by wheel ren::aing !.0:.heor:g.n.alposi-non.:! wheel remainsmd.sp'!.aced position.du.m:pingsbo.:.d be dis-con:.Jru.J.ecar.d ba'lancedwitn :h.e :.ransie:switch. . ....''hc:n:...CO-!.?RCO.!Pco.:neon. c!ose:-especttve dump "-a!ve. :..AUXTAXK AlR swnch - PRESS OFF. b.?osttion bo:h:.. andRma!ntank dump switches :o DUMP,:..MAINOPE.. andR-!A:N OPEX lightsshocldH'!.c-reinate. visualcheck. CAUTION :f :he wheelposition IDoves appreci -abl? dt!D'lping.t.hevalveinthe l:go.t wi:1gshocld be closed.Check iord.I!D!p:ng!rom heavvwingby wh.eelre::u:aingtotheo:-tgina!?OSi-.:Jwhee!.re.ma.LOst.ndisplaced posi!ion.dw:npi.cgshould be dis-coati.c.uedacd fue! balancedW::hthe t.rans!e:- swi:.ch. Cr.anged o. o..-embe:- l9o7 AF (C)-1-1 7 .v-cen :..COM? anda.COM?lig!:::scome on.c!osedum_pvalve. 8.Upon com.ple":iono! 5na1:a.n.k,.pcl! !uel quantity circuit breaker.se: cou:nter to300 andreset circui: breaker. !! rni.ai.Jnumdumpn.meis essen:ia!.all dUJDpswitches m.a.ybeopenedsimultaneously but w!:tentheEghtsi:lurnina:e.:hey must be closed select"!ve!yto ensurethat both main andamcilia-y ta..nksare completed. CAUTION !! dumpi:lgis accomplished in o:!::.e::: than level !Hgh: at:imde.or if the vahesare !e!t open a!te-:- :he col:l -p!e:ion Egh:siCcr:tnate.i: is ?OS-stble :o dUJ:I:? 3e:owe !30 gallon !eve: :he ::nai::. :a::ks ( .:);GPROCE:>t:RE.... . ............ F EX7E:-.-r>E::>?A77ER.....;..... ... . ................ :R.E:"RAC7E:> PA 7':"Eit:."......... .. .. . ............ .. !....!L"\"D:. "GRGE:\"C::ES. . .. ... .. ........ . .. .... . ........ !..A;'I.l>C"GW:7H"A,..._ "GFLAPS OF:ZSSTH-o\S!5...... .. .. LA3DL'\;GO:SUXPREPA:U:D SURFACE.. ..... . .. .. ..... . .... m.-cHUGPROCEDt;R.ES E).iERGEXCYDESCEX7.. .. .. .. ...... ... ...... ... 3-3 3-3 3-4 3-4 3 - ..u\ 3

3-7 3--3-8 3 - 8 3-!.0 3 - 10 3-10 3- . o 3-l!

3-13 3-15 3-. -3' - -. 1 3-lll 3 - l.J 3-lO i-t:G!iMACHRECOVERY. .. . ........ ......... . .......3-.!l FlR.E... . .... ....... . .. . . . .. .. ....................... . .3-.ll F!RE..... . ... . .. . . ........... . ................. 3-Z! FIREOR 0\'ElU-::EX::...:GH': :>UR.I:\v-:A.KEOFFROL- . .3 - Zl A.!RSOR.."\'1::.... . . . . . .. . .................. .3 - Zl COCKP!7 .FCX::OR S 10KEE L:.).!!:XA7!0. .. ... . .. ....... .. .3-ll COCKP!:'................... .. . . . ..... . .3 -ll EMERGEXCYCASOPY ....... ... . . .... . .. . ....3-.ll E:EC:"lOX ........... .... ..... ........ .. ... .....3 -.! 3 PRIOR :'0 E.;Ec:-:ox............ . ...... .. ... . ... . .. . .3-24 E:EC7:0X ?ROCE:lURES. Seat)...................3-l' AF7ER E.;EC7:0......3A!!...OU7PROCEDURESE;ec::o::tSea: .Fat\:-:-e). ... . . .. .. ...OXYGEX SYS7E. f.UR!.."'I;G .... ... .. . :>ROP:'AXK SYS:-E.! c-:-:ox. . ..... .. . .... .. .. ....... . :>R.OP7A...XK Fu"E:.DOES "0:' .FEED ............ :>RO? TA. "Kf S XO-:'RELE:."'-SE . . . ..... ;::!..EC7RICA.:..SYS7EM !\!ALFG::'I!C7:0X. . ............... . . .. . .H:GH A!'.!!'.!E'::'C::RDC-:'ORC OY..?:..E :-:EE!... C :' R!CALFA:.:.t; R::: . . . . XO. lOR XO. 2:.'\"YE:t:LR FA:LGRE(!\!am . . ... . . NO.! "0. ZAX:> EMERGEXCY ::.XVERTER.FA!:..URE... . .. 0:::.!'.L+\.:...?CXC :-:ox..... . ................ . ... . . . :'R:...\!:'ABR::NA WAY7R:}.i ONF!..:.GE7 . . . ..... R"-i:'\AWAY:'R!.M OX AC:'OP:!...07 . . . . . . . .. Gi1S7 CO. ":'RO:. . . .. ...... . . . . . Wl_'OGF:..FUXC :'!OX. . . .. .. . . ..... RE7.RAC:-AB:_;: S-:'A:..!. S:'Rl? ... . . . ... FUE.:....... . . . .. .. . ...... .;:R CO.:\'D:':"10X!XG. .. .... . ...... .. CAB:. COO.:.ERFA:.:...;JRE COOL;:R VA:..\'EFA.:!..':JRE.. . ..... .. .. ?RESSUR:ZA:-:0 SYS':"E ! O?ER.-\.:-:OX . ?OGO .R.E.....EASEFAlLUa.c::.......... .. . ..... . ..... ..... EPR SYS7EM "C ':'lOX....... . . ....... . . . . . .... CHECK.L:S':" lsscedte CI 3-3b 3 - 3 .. I 3-r 3-37 3-r 3 -38 3-38 3-38 3-3Q 3 -39 3-39 3-.W 3- ZCilaogec1Se?tember 19o6 EEEE AF(C)-!-1SEC 710-.ill itODUC :'inssecrion proceeures:o:>e follo":ec:o cor:-ect anen:e:-gency conC.iuon. -:l:eprocedures,.! !o:.owed,voiUensu::-e safety o!toep1lo: and a:r?la:::euon!asa!e lancim.g:s :nadeor other a?p:-op=2:eac:to:l saccor:":p::shec.emergencies, adverseweath.e:,and oth.e=?eCuliarcon.c! -:tonsmayrequ1re:nochfica!:onso!these ?l"OCe!e:o consu.: acheck!istbefore aner.:l?ti:tg:.o a:leviate an e.rne::-ger..cycondf:-:ioo. -:o assist the?::otwne:lau emergency occ.::-s.bas:.c::-.L:esa::-ees::a.b!:sb.ecwhicn a??:r :o most er::e:ge::ciesocc\!.!"i:::ga ! rbo::--ne.7hey shoulc be;,y the?t.o':.7he::---.:!. Sfollow: 1.a1=c:-ai:3. ?roper ac:ioo. :'ce majority o! eag. 'lerr.a:iOJ:tcnons!n :h!s airplane are !lameo..ts a: alttru.ceso: a??rox!.ma:e.yiO, 000tobO. 000:ee:.7es-:s show :.ha:- c!im:,inga:-eC.':.lCedpower w.:.l prevent i:1tn:sa ! : imde:egion O:he::-an:byengtnecom-pressor sta!..andar--eecac.seci by :hro::!e rna12.ge..."T:e"lt.. ::..ltea:rspeed dro? ':.Oo!ow!ai ... =e:o obse=ve E?R !:.a::.:saru! c au.ses.!! !la."'tleo...t:s due: o:he above cond:-:.onsa:-esta=: cac usu.a:!y be aCCO:::l?:isned.!! a!"..a.r:1eou1is cac.sed oy c:ecnanzcal o= fai:urewi:hin :he engtne.a:-es:an may:>e?Ossible.de?-en.d-t:tgon tnesenol!Sntss of the !a.:.. re.and fl..gb:contu::.J.edat.ov.erpuwe:- sen.ngs and a.:!t..des. Va.:-}:r.gceg:-ees o: lov. insta ormay occu.: at en.g1ne p:-esst..:eoe!ow:.neE?R versusa lnwciescheau.eforbleec1.alves c!osecsnov.n on!igu:e5-..I! theo:eed ... :gntsfa .. :ot!h.;.n-a.natewne'"lti:te m.nrm..un EPR foro:eeci..-alvesc!osec .sreacnc=c...-ahesoe rnanuall)- opened:oper:rn::-eeact:on io:- ciescen-:anaa"ctcina..neouc. CAUTION F lame ou'=as a.resu:t o!low com-pressorstalltsWt!hoc: a:-1d :oosurldentoavotdedoy cc.::-0\\"X. (I! -::izneand conditions3.s:::a:.:strips- .:r.end . 4. b=alescent. WARNING aia.sc descent.ca:e mu_st be exe:cised :.hat:.:teat::-speec !in:tta:::.ous a:e notexceeoed o: s::-uc :1.!-.-a!. !'a.i!'-1:- er:::ayre s .J.:.:'he gl.!St :::1us: oeac:ua:ed GCS-:' at 4.5.000!ee! o:- thespeed wa::-n:.cgsys:ezn...!tnsta:led,wi!l sounde ho:-a as :aespeed bai!ds upl.OZZOkno:.s:AS. Thespeed wa--nicgS)"S!.e.mw-Lllbe ..nope:-ativeu:ege:::tera:o:-swuch isCano?ylwir..dsluelrlfogand.:cing willoccl.!::-in descent and may becmne qui:eseve:-e cn.Ce=co::d!::.onso! cotd arui hlgn .aam.id!:y.7!leblowc:- should. be ope:-atec aslongastJte DCgene:-a:o=stayson.:he! t ee.When:.he DCgenerato: CO?Soi! :he line.only :.!:.e blowe::po:-:!onWtl!ope:-ateace hasa5-cu:n.pe::ecu:rent d..-aw. 3-5 AF(C) - l - 1 1: an u:nme6.a-:e!.andinghas:o :,e made,the canO?}- should be Jer-soned as al as: ::: eso:-"t when:hereisno fo-:-wa:dvisiliiaty.E xtend-:ngthe:une i.etheai:- by u.s ing!15 Kfo-:-max1mu:mg!1de o! course give mo:-etimeforlhe windsiueldto clear. "'i:'bebar...eryis a35-aJnpere- hourbacery butlast an est::Jnated20to30c:iependn1gon:he t:eD'lsbet:lg operatec.such as: a .trr-::!"racioO::l- i 5. 0b.UHFradio- 20.0 a::npe:-es. c.Windshlelcblowe:- - 5. 0ampe:-es. l.Ar:imdetndica tor. 3.ADFVOR neecle. e.?ito:. beat - 13.0 res. :Uterp.boee(requir ed ior :-acio)-l. 0ampe:::e. g.Face heat- 1. 0a.rnpere. h.1.A:nncollision7. 0amperes. Z.18.0 o:taM:e.: hefol!owtngp:ocedu::::eshould used.: SE!.-ECTSYS':'EM. Z. - If; :o 1/3 OPE 3 .- S:'AR':"HOLD. FUE:.. SYS7EM MALFUNC-:'!01\"'S 7M most se:-ious:ype o! malfunctionm:he !uel control 1src:nawayengice ove:rspeedlng. Co::-rec:.ve actio::: mast beta1teu qcic..clyo:-comple:efaH-=e.nresu!t..Complete:.he fol.ow-.::gproced ... re: 1.T:iROT:'.U:- OFF. Shut eng.ceoE i:mmedia:e!yto p:-e'l.'"e!lt ove:speedillg-3-10 3.PRESS- :'0- TES':' REGULA-:"OR- tf scit doesco::tnfl.atea: 4Z. 000 feet cabin. 4.Head!or nea:est sc.!.tab!elandtDg field. 5.:::o=-m.ala i :-start. o .:: o'erspeed condi:io:1-sw.ttb to!uelsystem. wi:h th:-o:+.lein idle. 7.I! o ... coruhtions::i!lpersisu-throttleo!i.and attempt a trsta::-:ou ezne:-geccy fue!systell"!. 8.li overspeed still- atten::p:: !t.:e! conco: regclatio:1 with betwee:: idle andoff. 9.I! overspeed cannot he con::":"o!.:ed-o.hro:-tleoff and:or fia.I::tecn:.: lanc:kng.G!.idemay beextended O)' starring a.nCS:.0P?t:.6engtne as necessa....-y. JO.D-.:mpfuel asnecessary be!ore landing. E ... "G::X:: ATLOWAL'!"''::"UDE If thereis tnscl!icieot a.l:::.tudetoshutthe e::gineoi! anda:tempt arestar:.:.ne !o!...oW""..ngprocedureshould !:>eused: !..RE:'ARDTHROT:'LE. Z.SE!....EC7 SYS-:'EM. 3.:"HRO::':":...EOFF IF 0\""ERSPE.E:> PERSIS':"S. EEEE . AFfC) - 1-!SEC -::oxI!! F U.E:. :'ne !l.!el:.asbee:: useo up-z. 000feet.AH!:hro:-..lemove--en:s must bemadeslow.y anc ca:=e!cl!y when operanng on thissys:en::.?Cl!"ticu!ady at high a!tin:de. D:..1nngclimb.the c:ust be g:adi.l.&Uy r-etardec aboveoO.OOOfee: :o keep:he EG:' and EPR within lirni:s.

descent.the!.!lrOt+..!emay be to gtve :hesa.r!:leas on :he sys:e=. :'he m!ni.mUDl EPR Vbe :'he chaogeove::- !:-om nor=.a!tosystems iseast.yzr.acie.:'he pos:-tiooag1veoRP:!\!1scot :hesa..... eo c:he emergencysys:em as on :ne system. :'he:-efo:-e.theR.P!.!'"!:l v.:he:1t..:le ,s n"'.ace.Cp:o ao a!:.:..!ceof -o:;000 :hecha... oeove:=o e:"""!:;a G:ice d:s:a:1ces.n !.gu.:-e3 -Z are cec:-eased....:orag areusee.Red..!ce:he g!uied tsta:::.c:es.,y :he!ol!owir.gper-cer.::ageso:ne :- :ilan c!ean Gear cown-SpeeC. orakes o..:t- 3911': .... .. Gcs: ?OStt:on St:ppe:- tacks-Dragitet:lSshou!cico: be usee tu:::! :::ecessa::-yif max.n:.u:n g::ce.s impo:-ta.J:t. 3-!J -'fEE' E ."E E E ;... ...

0 -0 oO ..:. -.....50 . ... o-< ...... :::: < 30 ...... z < !0 =-u: !0 s . .:.. 0 3-lZ lAF (C-1-! DEADE.\GrE GLIDED ISTACE 50:oo 50zoo XAU:'ICA!. .M!:...=:S(. o \\Th'"D) NOTE ! .'.."'!:-H:..ESS:":.-:._; GA.:..:.0:-\5S7AXDAR:> SPEE!l SC:iEOC.:.ZL:\ 7:!.. :15 1e o:-s DESC.E.'\7A 7!15 Z.\.'::-H7:;;-...:oOOGA.L.:.0:-\5 S?EE:>.... . -:-:.:...130ICo:-s,7:-IE.-CO);:-:x-vE:>ESCE. '":- A 7! 30K"O:"S. 250 EEEE AF (C) - 1 - 1 SE C:':ONill Fla.meou: :andingsshott!c be ...-:.ade:la?s extended.! ...a.cdi:tgs-.rith :la?sre::-acted wtl!beavo:ded i! possib!e. AlteraP.a.::neout no: associated wtth electric o rhydraulicfailureor eogtne :he eog:ce-d::-tvenhyci:aa:tcp=:npW'll!su.fiideat hyt!::-ao.1!.c? r essure:o actt:.atew!ngHaps.A: e-tgbesoef'csas to.a. as7 ...RPtanuwt:n an !AS ofllUmots. theflapscan bel ov;e:-ed:o l5 cieJtreesin approxt.mate!y30seconcs.A:ntgner a ! r -speedsnot acco:cpantea byu:creasedwinc -m:Hingthe!laps maylower at a s lowerrateduet oincreasec a i rloads. Mo re:ha:: Z5degreesof n ap can oe ob:ai::eti bu::::e=-a:eo! ex:ertstoo wil! be sowr r.F mayoere:::ractedasreq:: t red to extendd:.eg u de.Ho.,.,-eve r .care mas: oe exercssed:o avo.c. ove:- shootiag:nerunway. i! 6 Hdecii s:acce.s cot a.!ac:o:-,:.he coa!:g1:raUonsncn:coees:ab!:sneda: ac a!:;tudeaoo,e:.-:elugh :keypotct.con-ditionsper:n.t,:his a!ntudeshould behigh eno1:gbto makeaseriesof onen:at!onru:ns :o eotertngt.:le.:ughkeypoint as ce::.ned l!l !:gures 3 - 3and3-4.E aco descendicg3o0 :--.srnshould beflown:o lose ac.tcc rement of :o tilea :ti:wieof thehtgh keypo:nt fo rthe.nvolved and to ente:- thehigh Iitevpomt: at :he pos:t:on. W'"ne'"\t?a: keypoUlt or a..:lOVe. : s!eas:bte:o ente:-:nena::ern a: one of :he !ower !iteypoin:s. -he reco1n:neoded:ral!icfo::- a flameout :he360a5 Shown fig1.:::-es3 - 3ace ':'hepoint ove:- :.hetouch.c!owneo.dofue ruowayts defioed as t:hehigh if.ey?Otnt.:'he down-wind,ointthee:ldo! therunway i sthelow pomt and teebaseisthe 270point. P!an :oa: :J:ehigh?O:c: with :.helanding gea: ex-cenried.s?eed ::ues ::-e:rac:ed,s:::- .psexte::ded.a.ndZ5 !:ap ex:enstonifa:e ava:!a:!e._::s ..mpo::-:anttoestabhsh thehighandlow Iiteypo.ntsasbelow so :h.a:prope::-thresholdspeed and a.ttt'.u!e.s :-eached. F.:.APS E X:-E:\"DED(See::gc::-e3-3. ffiGHKEYPQI1 7: !.Altitude- 3000.fee: aoovetilete r::-asn . 2.A:rs?eed- 100.c::ots.AddZ100 ga.lons. 3.!..a:::Cinggea::- - extenciec.. o.Cock.pi: c anopysea..ralve- OFF. Stal!s:rtps- ex.e:u:iec. LOWKEYPOIXT: 1.A!:itt:cie- 1500feet abovethe:e::-::-ai:1. Z.Ai::-s?eeci- !00 :k.ao::s.AdciZ 100 ga!loos. 3.!...a.aC:iCigear- - exte::.cec. 5.Speed- ret:ac:ec. 6.Stall st=ips- ex:e::aed. 3-13 SEC710SID AFC-1 - 1 r-'\ _J:JIIoKT's.cer-: A.SOV::YJSG F:....APS- zs-SP!:.!:D 8tA.KE.SJU:"'JV.C-::1:!)-%K.-.cr.s- A!)!) z11:'0GA!.. s-..AL!. S":"il!PS 00"7 nNA.!. APPS.OACH \::.)F':' ABOVE: F!.APS !.So SP'I:I:!> 8BAIQ:S lt"P.Z!' :s ASSl:3ED = r.-o-:s- A:>:>:JCr.S.oe CA!. s".c..:. s:A!PS oo.

.0 F"' ASO'L,ee KSo:'S -ADD Z!:.ACH--GA!.. Ovt:Jl 001 CA!. Tl..APS - tWAT !l!: a.E"'&Acr.E::> ASi'OC LOX} STAL.!. S7!UPS 00":" ....AT A -- JC>;O':s T"..JJ'S!S0 IA80"Vl:Z5KS SPE:J:!) s nlt!PS at::"- TMUSHO!.:l 3-to 10 F'T ABOVET.E:1aA.tS SPttJ) STAl.l.. S':'lUPS OCl T AF (C -1-l F igure3 -.Z l'i'\ H:GR Ja:TPO::N"'r \!.1 l r= ASOTl:'t'E.AJlAlN GEAJt- DOWN SPZ:I::) !lli.AKES .C':!lJC>"'!'S.co GA.!. S7AL.:.. STalPS OC7 EEEE AF(C) - 1-ls:c:c:-:o. !..OWKEYPOINT: 1.Altitude- 800to 900fee:abovethe :er=aic. 2.Airspeed- 100xnots.2kno:s/100 gallons. 3.Landinggear- 4.StaHs::-ips- extended. 70 21'0PODiT: 2.AirS-:leed- t.C.=eshoe pl.:s0 I (See!igu:-eAS-2.) 3.l...a.r:tdinggea:- - exte:::ded. ..t.S:al!s:-:l?S- ex:.ecC.ed. F!.XA!... APPRO."'-CH: l. A.::tude- 250fee:a'bove:heterrain. 2.Airspeed- :-ed.:.ce:o :hreshold plus I5mots.(Seei:gure AB-2. ) 3.S:a!!strips- ex:e:::dec. 1.A.!.:speed- speed.(See Ifigure AS- 2.) I z.Drag caute- deployed (i! !UStal:ed). CAUTION Dono: exceed thresho!.dspeeC.as icze:-ofla?sothe:--wise:he d!sta!lCeY.H heexcess:ve. S:.'.f'GLA:'ED R.ETR.AC7ED F 1.Arrive a: high key poi.nc:a: 100;mo;s (acid2knots r100 ga!lons)w;.thl.anrl..cg gear down.speed b:akes ex:e::ded. !5 wmgflap,o7,. eng.ceRPMacci scan sr::ps oct. 2.3et"Ween!ow keyand270 po..n: a1rspeedtot!t:-esho!d?lus10 :icnots, w:.ngfiaps15andWtth 07engine RPM. 3.3etwee::tz - oo penn: a=.c!..ca!app:-oac..'l :-educe:othreshold o!cs5 !c:o:s,?QWe.:a: c,;:;RPM.lS0 f'.aps. -t.On !i::.a! reduce a.:speec :o :.'ftresho:dspeed. 5.:!.!a:u:Lng!:om ?G.:teroreduce :o.d!e.Otr.e=wtse.!:oa: dis-tance.sexaggerated. WARNING .P:-iorto any a.bno ::-D'lal co:rl.gu.=ation or exte:na.l damageto thea t rc :-a!t.s:al!. speed so.ou.lcibe checSINGGEAR. 3. SPEE:> .3R..urt:.ne::ta'!.n !ull pa:-2-cht:Urleplo,.-rnen.: a:. n::a.xi-mumter rain clea:-aru:e- this_s ext:e.me:y impor!ant fo:- low a_::i:ude eJectio::.s.....:theseat 'be1isopened m.anually.the automaticfeature o! theparachuteiseli:minat.ecL:"'.ne:::e-!ore.unde:- thesecircu:Jnstanees. theparachute armingmus:. bepulledif a::.ove14. 000or :.heD-ring must be pu:led if below 14. 000 !eet.. EEEE : . A:F(C)-l - 1SECTIONill z.pul: D-rtl'lgb.:ne-c!La:ety!ol!owingseat. sepa:ratioofo:--aUejection$ 3elow 14.000!ee:.This i.sap:--ecautiona.rymeasure since :he should deploy a w.o-:naticaUy. 3.Facepiece- remove aite: co:-ma.l pa::-achutedeployment at or below 14.000 fee:. 3AILOU7?ROCEDURES (EJec:uon SeatFa:!ure) 1.PULL GREE!Il APPLE. Z. SE..>\. ":'PACK QUICK DISCONXEC7. 3.::E7':':SOX CA-..... O?Y. WARNING 3e prepared !:0:eave-.he:.m.med!ate!y as :becano?Y mays::=-il:":"IOXS, E.;EC7 ..EAS7000 Fl:7 ABOVE ':"HE:"ERR..:.\!N'.\"HE.-:..'/.:..!t.POSS:31...E. E.:EC7:0X SPEED AT 7HE:.OWES':'AlRSPEED!ZOA 7 '"'":J A!-7:-:'UDES. Be1ow1 ZO1CA5,a::-flow !s no:sci!:c:en:to assu:e :-a?:rl?a:acrn:te -:::en:.:-:te:e-fore,!t beco:nesext:eme!yCt::.ng .ow al:i:-.:Ceejec:.onto ob:a!n a: :east !ZO K!AS,.I poss.bie,:o ensc:-eCOD'l? !e:e j)C!!"a-cbt..terle?loy:nen: a: tnete r :-a:n.:>-... :ing a!.:.!.:z::Ce ejec::onobse:-v:ng:h:srn.n_.-n-:....-o (! 20K!AS,beco-mestess1rnpor::ar..:sicce tS r!.Olef.o:- ?ilr3.-

3 -2o Tbe to be a tthelowes:?OSsible;ur-speed downto120 K:AS ?riortoe j ecrion is? r edicated on maD)' f a ctorss uch as a voidingbodilyinJury,precludingpa=a-chuteo :- seat structura liatlc.:-e,acdpro-"idingadec;'!!2tetail clearance.:he a::--c rai: :s con::ro::a.ble,a t rspeedv.l!.be to asnea:120K:AS asp:ac:ica !, whtcb e l im.i..n.a:esh!gb speedp:-ooteJ:Os . IIaircraf:not controUab!e,ejection must :>e a: ,.,.bateve:- speed existss :nceeJeCtion offers the ouly opportu-nity !orsu:vi'--al EXC.ESS!\S OXYGEX A:"Unningd:::edt be rnain:amedof :heoxyge::.p:-essa-re duringa.oy ::ntsstoo abo\elO, 000feet-:.o ::he :>ossthHi:yo!:-unn..ngouto! oxygen above asa.!.ealtitude:! a.ea.k sbou:doccu:.7ne should bechec:t.edat fre -quent a.x:.d?!o:-.edon theoxygen consam?rior.. cha:-t eve:-y30 minc-:.es.Due :o t.necoohngof theoxygensc?p!.y,theoxy-ger..pressure c :-o? willbe !air:y =apidat first.T his: sexplai nedio detail:.nSecnoc !V.Genera!l; in h:-st hourof p::-essu:e wil1d:op about500:o 000psi ar..dshoulc:o !all of! a: areduced :-atea!ter::hls.:! ontheU-2C,:-a.:e o! consum?tion a!ter:wohours o! !'.ignt at a!:ic::.Ceexceedstheva!ues!..Ls:ed. belowpro_: ec:oxygea ?o:sto rl e :e:--mineii :necancmnptetee wuh at ! east 500rem.aLD.mgat desnaat.on. 1!thistsimposstble shal:be discoo-:inu.ed.SincetheU-ZF has a!.a:-ge::-oxygensupply.the ma.ximu.m desi=ed con-sc.:nption :-a.t.esin ?Sihr a=e... 5of U..-0 -ZCr;rer EEEE AF(C)-1-1ill If theoxygentsexcessive:he oxygen ?ressu.rehashelov. minunu.mshown !or the a!:t:ude beingtilept!o: v.-i:: descencso as toma!c!a.ir.:be p:essu:ealutude:atios. iJ - ZCOXYGEX PR.ESSi:RETA3l..E OXY A!-:'!:'U:::>EOXY?RESS. 60M100psi 'b:500?Si 150?SiO.r250 175psi/hr 30- {zoo?S!h: :! tneoxygen?ressarehas:a::ec beiow 250 ?Sithe?i.lo: wi..!!descecdto !0000feet cabm a!titt.de. WARNING Senoi.ls cons.cie:a:1on m\..s: betotne:ype of miss:o::1 be:ng !1own.as v.e.las :he availaoi!!:yof sci:.ahle alte:-::ares.befo::-ecoc:!nuingaJD.ission when oxyger:1consc:r:r.?tiontseven s:.gnt.y ..nexcess of t.oa:.c.esi::-ec.. NOTE !.! at high a l:!n:de wt:h nosiup oxygeity pu!lthegreen a?p-e andm.a.Jtea!ast descen::to a10000 ioot caotn a!t!tude. ano:-ell'lo\efacepiece. WARNING :! tile?t!ot is un.a":>l e:o:-egain anoxy-gen supply.he "Vo-i!l!::.aveto open :lte !acep:.ece1n !Lgh.:.Cse theemergency descent andexercise extreme caut:.ontoavo:d f!a.meou: and. ing!oss o! OXYGE:X DIF.F.:CC!. ":Y :f thepilot SUS?eC:SOX'_ ge::.:o sym?:ornsof bypox!a o:- b\ not'.ng:ne hetmet bladder colla;>stng.hesi:toc:c the!ollowinga c:ion: l.?t::...:..AP?L. l. AC70A:-EPRE:SS- :'0-":ES":. 3.:.."'SPEC:" SU:T7 -F::-:-:..xGS.QU:CK F.ACEP.:.ECE. ..!.d1fitcu!qis cot cor:-ec:ted: -l. (:o cabin a:c:uce o!.0. 000fee: anci remove NOTE :!. a: an.yciur:.cg!:!gh:::-:e?.lot findst:::1.ecessa::-y:o O:ler.:ne !ace- o:r.er !o::- com?:e:eoxy-gena:::m...-r.ca.a:.e w!:: oemace:o an a!::-craf: :trle of .;5. 000.fee:p:!.o:- tOopeningt.?:e faceptece.-:he!ace?i.ece v.'i!! be chec.edforpro?e:- seactng":>y ustng:.nemir:-o:-s.n thea i :-c:-a!: anawil!a:sooes .... o_,o::c:edto Press - to- :"es: ?:-ess .... :-e.If these chec:d.s-appear. 3-ll I E E E -EEEE SEC7:0X!!! A:F(C-. - ! AlRCRAF:'OXYGE:'\!>uF!Ct:l-:'Y . ::thee"en: :he oxygen v.ra:-r::ng?:-i:n.a:-y of!hhtco:neso::.: ! .:':l:-n?=-.=:arj..-aheto :: :o "":a:-rn-=?ancti:.a.v.o ... :. l.:'u:-nca:,:nheat cp as asi?:-ac::cal to a:co:'l3.Descendtoasa.!ealt::uaec:-eq\:!:-emen:spe.:-r.:lt.:i :: . sno:pos -st'b! eto c escend;o asa!e a !:!':'Zde; :e=::-u:-:1va: ..e OX r:'!omen:a:- ..y:.odete:-:n.nev.he:.::e:-tne blockage!'lasw .... en :n.s cneck:-es::::s1r.;hePalM OFFgo:::g o:;t.-:.;:e:3:-::na:-yva.vesho:.:.lco e .e!: 0);. I! whenope:-a-:.::gontheseconca:""."va:ve oo!y.tileoxvgen v.-a=ni:::g:_o PRESS !ig::: co:oesor:: l.hgh:s.Bo:h ligh:.sshould be outif ?=- ..'"!'la:-y"-alvetsclear.!! aot.h h !;h:s:-em.a:non.p:.sUgreen a?pleacci descendtoasafea!tttud.:and:-emo1;e !acep.ece. h'"Y.::>R..U:=-.:cSYS:-EM. EMERGEXCY OPER.-\ :':0 :'heretsnoa.c:lonwh.cb can be:a:...ng!laps cannot bemoved tot.'leGUS:' theplacarci speed !or m-st be o'bse::-ved. 7ne:>oost i!' on.willove:- !o:- the ooost pumptntile event of faHc ::-.: . high al:i:udewi:n thea ux.haryboos: on, ia:-y p:-essc:-e:s abo"e10 psibu: below -:henonna.lfuelpressur e. FaHure ofhyci:-aulicsys: em show zeropressu:-eand acec:-easem !ue!pressu:e.Afa.:ureo! uristype does no::-eqc: :-eacescen:,and:he r.-.aybecom?:e:ec. EEEE AFc -1-!SE:C":'!O!!! HY:>RAU:.:.CPRESSCR.ELOSS Acase of parna! pressureossrnayoedue topt.:..!'n:l trouoleor :o an.:lte:--!la::nthe A.:se::-v.ces operate bu: at:-ecuceciS?eec.:.:the?=es-sure1Stoolow,thel anct::ggear::r..ayno: fu!ly:-etract. :'hee:ne :-geocy!andi:tggea:- ex:ens:o:1sys-tem 1sarnar.ual!ree !a!ls,-s:e:n. ?Owe:- ::o:-?::-esst::-ereq-neeto O?e:-a:e:r.:ssyste=. 1.Gear hacc!e- co::. l. E:ne :-genegearre!ease- 3Gea:- downa::d!oc:ted -cae"CJtea. (!n caseo! ane.ec::-:ca: !a. .Jre,:to 1::c:ca::on.s a,-aHaole . A'ICA :-: o"!'\' c.:_:_'\m !! the: ow l e ..: igh: comes on dur!':lg:be cU'no,nr..us: bea.ssln:leeUle!ue: :s "10':uans!e:-ring!r.totheS!:m?:an""and oat} 50 of !-e. : sa,a t :ab!eto continue !'! igh:.\'.'benti:usoccu:-s,:-ec!uce:-o eve: off anc?!"OCeectO nea:-est sttabl C'..aruLngHeld.V.neoanc . "lg!1elc .sg! id:ngrangec