Aircraft CESSNA F152 Flight Manual Download

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Summary of Contents for CESSNA F152

Page 1: ...RIMS CEDEX French Type Certificate No 38 Serial Number Regisation Number at Cs Sections 2 3 5 Pages 2 1 a 2 7 t45fr o3 06 fl j This is the exact ixanslation of the F 152 French Flight ManuiI approved...

Page 2: ...1 C 11 U U C El U...

Page 3: ...NANGF SHESTS ND iJPPLE ENTS C R NtSQDiMT U flS NfAiUM OtCANDTflE Y tt C4 q 7fz oywr I itS c rn A Thflo fl rn c C49 4 cio as 7 49 4 e 1729 t A Steov 5 c 4e s 7 8 rec sr IC I 15 CA C iGi C SI ggT kO js...

Page 4: ...I U A...

Page 5: ...9 Model beginning 5Izc 1 6 thru j_g with Serial Number 1 10 1 l2thni N F 13201529 1 16 2 2 thru 2 7 fr 3 1 thus 3 8 te 4 7 thm 4 28 r 5 3 jl 6 1 6 2 1 and I 6 2 2 6 6 1 asic 6 7 1 2 0 3 0 4 1980 Model...

Page 6: ...LI U El El El El El El U U U U I...

Page 7: ...ation in the Flight Manual LThITATICNS 1 Thic type of aeroplane is eligible for certifi cation mt the Transport Category Passenger However this particular aeroplane may be restricted to another Catego...

Page 8: ...NY A s i 14...

Page 9: ...ete Electrical Failure This failure causes the loss of all radio the turn coordinator or turn and bank indicator the fuel quantity indicators and the wing flaps Turn the master switch to Ofl and land...

Page 10: ...t...

Page 11: ...nd the starter motor will continue to rotate until its electrical supply is terminated in which case twitch off internal and external electrical power complete the engine shut down drills aM investiga...

Page 12: ...c V C 4...

Page 13: ...2 LIMITATIONS Certification Basis 2 1 Indicated Airspeed Limitations 2 1 Approved Maneuvers 2 2 and 2 3 Engine Operation Limitations and Instrument Markings 2 3 and 2 4 Placards 2 5 thru 2 7 SECTION 3...

Page 14: ...Stall Indicated Airspeed 5 3 Performance Specifications 5 4 and 5 S Take Off Distance 5 6 Rate of Climb 5 7 Time Fuel and Distance to Climb 5 8 Cmise Performance 5 10 and 5 11 Range Profile and Endura...

Page 15: ...data of the Model F152 Standard Ecole and Liaison Li DOCUMENTS AVAILABLE The following is a check list of the data information and licenses that are part of the aircraft file and required by Regulatio...

Page 16: ...g tpan is 9 95 555 Max must be iglit shown ss in nC gear depressed all tires and sine steal properly inflated and flashing beacon iantal ed I Wheel base length it 1 47 in 4 Propeller groun dclrarnnce...

Page 17: ...Airfoil Type NACA2412 Wing Area 14 8 m2 Dihedral Angle 1 at 25 chord Angle of Incidence Wing Root 1 Wing Tip 0 AILERONS Area 1 7 m2 Control Travel Up 200 t 10 Down 1S 1 Droop 1 1 2 WING FLAPS Method o...

Page 18: ...bsorber Nose Gear Air Oil Main Gear Tubular Spring Tread 2 31m Nose Wheel Tire and Pressure 5 00 x 5 2 10 bar 30 psi Main Wheel Tire and Pressure 6 00 x 6 1 45 bar 21 psi Nose Gear Shock Strut Pressur...

Page 19: ...SAL 20 below _12cC MIL L 228S1 Ashless Dispersant Oil SAE 40 or SAE 50 above 16 C SAE 40 between 1 C and 32 C SAL 30 or SAL 40 between 18 C and 21 C SAE 30 below 12 C Propeller Diameter Maximum 1 75...

Page 20: ...4 X 07 7 Flight Manual REIMS CESSNA F152 tUILLULI Revision 2 May 19 I A I Si 4 4 1 0 c J I I 0 Vc0 c a a V 1 1 0 i Fimlre 1 2 ThSTN MEt4T PANfI...

Page 21: ...19 ADF Bearing indicator 20 Additional Instrument Space 21 Low Volta ge Warning Light 22 Ammeter 23 Map Compartmen t 24 Cabin Heat Control 25 Cabin Air Control 26 Circuit Breakers 27 Wing Flap Switch...

Page 22: ...RAIN J bRAIN VALVE VALVE FUEL SHUTOFF VALVE 01w I ocron erd nq I eIseI ank he IsIss should hr sr 001 sI slIer rach IrlurLiol 10 j 155111 050 II mum sasacs Iv FUEL LINE DRA PLU FUEL STRAINER C o FUEL S...

Page 23: ...9 1 13 US Gal each 24 S US Gal 1 5 US Gal 26 0 Us Gal TWO LONG RANGE WING 1 42 1 6 1 147 1 each 37 S US Gal 1 5 US Gal 39 US Gal FUEL QUANTITY DATA H U H 1 I I x FUEL TANK SWAP QUICK DRAIN VALVES Each...

Page 24: ...LTAGR wAlillIrlO LIGIIT OIL FPETS flL I _eJe_1_TC3IUTNLIMESTRACIO CUjSS LONIACTUR LTN ETa OIL TEMPERATURE GAGE FLIGHT H OUR TO TURN COOTIGINAIOR IILCUROLS OR TURN ANG PANEl NOICATON n TO AUDIO MUTING...

Page 25: ...led ALT controisthealternator 3 Normally both sidcs of the master switch should be used simultaneously however the BAT side of the switch could he turned ON separately to check equipment while on the...

Page 26: ...ng the master switch off and back on again If the warning light does not illuminate normal alternator charging has resumed however if the 3 light does illuminate again a malfunction has occured and th...

Page 27: ...power circuit clock circuit and flight hour recorder circuit These circuits are pro tected by fuses mounted adjacent to the battery lIGHTING SYSTEMS EXTERIOR LIGHTING Conventional navigation lights ar...

Page 28: ...in the BOTH po sition The engine instnjment cluster if lighting is installed radio equip ment and magnetic compass have integral lighting and operate jude pendently of post or fLood lighting Light in...

Page 29: ...the instrument panel that provides mechanical stops at the J 10 and 200 positions FCr flap settings greater than 10 naove the switch lever to the right to clear the stop and position it as desired A...

Page 30: ...sure to the pedals and the reiease the parking brake knob To release the parking brake apply and release toe pressure on the pedals while checking to see that the parking brake knob is full in STALL W...

Page 31: ...ever Exceed Speed 276 149 171 Maximum Structural E 0CruisingSpeed 206 111 128 VA Maneuvering Speed 193 104 120 V Maximum Speed FE Flaps Extended 158 85 98 INDICATED AIRSPEED INDICATOR MARKINGS Red Lin...

Page 32: ...Occupied Optional Child s Seat Aoproved if Fitted With a Safety Belt NIGHT VFR AND IFR APPROVAL c4 i 1 For night VFR and IFR approval the aiicraft must carry the additional equipment specified by cur...

Page 33: ...gine stoppage Intentional spins with flaps extended are not approved Inverted flight maneuvers are not recommended The important thing to bear in mind in flight maneuvers is that the airplane is clean...

Page 34: ...25 PSI Normal Operating green arc 4 14 6 21 bar 60 90 PSI Maximum red line 7 93 bar 1 ISPSI FUEL QUANTITY INDICATORS Red Line Indicating Unusable Fuel TACHOMETER Normal Operating Range green arc 1900...

Page 35: ...ghts 175 km h 95 kts 109 MPH U Steep Turns 175 km h 95 14s 109 MPH Spins Slow Deceleration J Stalls except Whip Stalls Slow Deceleration Intentional spins prohibited with flaps extended Flight into kn...

Page 36: ...erated in compliance with the operating limitations as stated in the form of placards markings and manuals No AEROBATIC MANEUVERS APPROVED EXCEPT THOSE LISTED EELOW U Maneuver Recm Entry Indicated Spe...

Page 37: ...GRADE AVIATION GASOLINE CAP 13 us Gal 49 1 Long range tanks FUEL bOLL lao MIN GRADE AVIATION GASOLINE CAP 19 5 US Gal 741 CAP 13 0 US Gal 491 TO BOTTOM OF FILLER COLLAR 5 On the instrument panel near...

Page 38: ...a a a U F U U U U a a a U ci U...

Page 39: ...king 4 Mixture IDLE CUT OFF pulled full out 5 Ignition and Master Switches OFF AFTER TAKE OFF 1 Glide Speed 111 km h 60 kts 69MPH lAS 2 Mixture IDLE CUT OFF 3 Fuel Shutoff Valve OFF 4 Ignition Switch...

Page 40: ...l through the carburetor and into the engine El If the start is successful 2 Run the engine at 1700 RPM for a few minutes 3 Engine SHUT DOWN and inspect the fire damage If engine sta t is unsuccessful...

Page 41: ...cornbustihk mixture 6 Forced Landing EXECUTE as described in Emergency Landing fl Without Engine Power CABIN FIRE 1 Master Switch OFF 2 Vents Cabin Air Heat CLOSED to avoid drafts 3 Fire Extinguisher...

Page 42: ...with delay after each until short circuit is ocaBzed 8 Vents Cabin Air Heat OPEN when it is ascertained that fire is completely extinguished flECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS AM1vTFW SHOWS E...

Page 43: ...required An unexplained loss in engine speed could he caused by carburetor ice or air intake filter ice Lean the mixture for maximum RPM if carburetor heat is used continuously U 6 Plan a landing at...

Page 44: ...NG 1 LANDING WITH ONE FLAT TIRE 1 Expect the airplane to ing off on the flat tire side U 2 Lower the flaps normally and land the airplane with nose up and wing banked to hold the flat tire off the gro...

Page 45: ...for the next landing approach Then retract flaps ujn reaching a safe altitude and airspeed 2 Radio Electrical Switches OFF 3 Wing Flaps 30 4 Airspeed 102 km h 55 kts 63 MPH 5 Master Switch 6 Doors UNL...

Page 46: ...oach with flaps 3Q0 and sufficient power for a 300 ft mAn U rate of descent at 102 km h 55 kts 3 Unlatch the cabin doors 4 Maintain a continuous descent until touchdown in level attitude B Avoid a lan...

Page 47: ...Flight Manual Edition 1 May 1977 REIMS CESSNA F1SZ SECTION 4 NORMAL PROCEDURES 4 i...

Page 48: ...l 93 1 Maxi CC STA 42 0 1 07 Long Range Tanks 37 5 US Gal i42 1 Maxi 67 72 C G STA 39 5 1 00 in Pilot and Passenger station 0 89 to 141 in 154 145 Baggage Area I Or passenge on child s seat Station 1...

Page 49: ...AREA MAX MU N AlLOW sIlLS LOADS AREA 0 54 KG AREA s ItKG AREAS D G3o S4XG NFl AlT sOld POINTS cAcargo tie dc wt set in n evided to sconce Isagsage it the bnggrge area il e net attaches foti as tie do...

Page 50: ...ld s Seat S4 kg MAX Area I Baggage Aft of Child s Scat Area 2 m3 b H f 4tH 4 4 9r LI II V 4 4 4 J zz Dat PC 4JF _i E Ei 4 1 1T11 El it 20 40 60 so iOo 120 140 160 LOAD MOMENT CM KG H 0 Pa 0 r rrr CODE...

Page 51: ...fi i ffflw fl E i fl i j nsswi i ifl IIIINIThI IG4 4I t14 49 b mi 4i4W R 4 iflW P4 I 1 Ls i jI 12 fx ii rtn h J i ftjj_r ti j 4i III I i iLVNEb i tHtfl iHE llLiESE n 7 J j 0 tO S S N 0 Li 3 0 0 a 0 C...

Page 52: ...S CESSNA fl52 C G LIMITS AIRCRAFT C C ARM M Figure 4 6 B F mn im S F EE EEEEE P iull1 ci H IIIIIi A ttt 750 700 650 550 5cxJ I El B Dr Di El El B B flInt 111111 LI z II1I1 Iiiiit r 1J I_I S S Ia4_ L_...

Page 53: ...ound inspection tn cold weather remove even small accumulations of frost ice or snow from wing tail and control surfaces Also make sure that control surfaces TJ contain no internal accumulations of ic...

Page 54: ...ld cause the propeller to rotate 9 d Turn on master switch and check fuel quantity indicators then turn master switch OFF e Check fuel shutoff valve handle ON fl a Remove rudder gust lock if installed...

Page 55: ...at the strainer fuel tanic sumps and fuel line U drain plug will be necessary c Check propeller and spinner for nicks and security d Check carburetor air filter for restrictions by dust or other Li fo...

Page 56: ...s Above Freezing IA NOTE For Cold Weather Starting Procedures refer to p 4 22 3 1 Mixture RICH 2 Carburetor Heat COLD 3 Prime AS REQUIRED up to 3 strokes none if engine is warm 4 Throttle OPEN about 1...

Page 57: ...ORMAL TAKEOFF 1 Wing Flaps 0 10 refer to p 4 18 Flap Settings S 2 Carburetor Heat COLD 3 Throttle FULL OPEN 4 Elevator Control LIFT NOSE WHEEL at 93 km h 50 kts S 58 MPH lAS 5 Climb Speed 120 to 139 k...

Page 58: ...Elevator Trim ADJUST fl 3 Mixture LEAN NOTE B If a loss of RPM is noted use the carburetor heater refer to CARBURETOR ICING on page 4 24 13 DES CENT 1 Mixture ADJUST for smooth operation full rich for...

Page 59: ...0 km h 60 to 70 kts 69 to U 81 MPH flaps UP 2 Wing Flaps 30 below 158 km h 85 kts 98 MPH lAS 3 Indicated Airspeed MAINTAIN 100 km h 54 kts 62 MPH 9 4 Power REDUCE to idle as obstacle is cleared 5 Touc...

Page 60: ...77 RUMS CESSNA F 152 Revision 1 August 1978 SECURING AIRPLANE 1 Parking Brake SET 2 Radios Electrical Equipment OFF 3 Mixture IDLE CUT OFF pull full out 4 Ignition Switch OFF 5 Master Switch OFF 6 Con...

Page 61: ...ed from the combustion chambers by the following procedure Set mixture control in the idle cut off position throttle full open and crank EJ the engine through several revolutions with the starter Repe...

Page 62: ...AiLERON ON Lii WING AND ON RH WING AND DOWN ELEVATOR DOWN ELEVATOR 4 16 Strong quartering tail winds require caution Avoid auddcn bursts of the throttle and sharp braking when the airplane is in this...

Page 63: ...of the warm vp will have been conducted during taxi and additionn1 warm up before take off should be restricted to the checks outlined in tins Section Since the engine is closely cowled for efficient...

Page 64: ...are justified in making a thorough full throttle static runup before another 1 take off is attempted The engine should run smoothly and turn approxi mately 2280 to 2380 RPM with carburetor heat off an...

Page 65: ...ailerons partially deflec ted into the wind the airolane is accelerated to a speed slightly big ter than normal and then pulled off abruptly to prevent possible set tling back to the runway while drif...

Page 66: ...4 POWER 65 94 POW ER 55 95 POWER DISTANCE I DISTANCE DISTANCE TRUE TRUE TRUE ALTITUDE per US Gall per US Cal per US Gal AIRSPEED AIRSPEED AIRSPEED 3 81 3 81 3 81 SEA 185 km h 30 km 174 km h 33 km 161...

Page 67: ...ction 5 shows the stall indicated speeds with respect to I the flaps position and angle of bank of the aircraft for maximum gross weight El With aircraft weights lower than the full gross weight stall...

Page 68: ...setting U required for the field length Use a wing low crab or a combination method of drift correction and land in a nearly level attitude 9 BALKED LANDING In a balked landing go around climb the win...

Page 69: ...reheat is the same as with preheat except the engine should he primed an additional two strokes while pulling the propeller through by hand Carburetor beat should be applied after the engine starts Le...

Page 70: ...zld pull the carburetor heat knob full out until the engine runs smoothly then remove carburetor beat and readjust the throttle If conditions require the continued use of carburetor heat in cruise fl...

Page 71: ...d to the nearest airport for repairs lOW OIL PRESSURE O If low oil pressure is accompanied by normal oil temperature there is a possibility the oil pressure gage or relief valve is malfunctioning A le...

Page 72: ...vide pro per restraint during all anticipated flight conditions However care should be taken to ensure that the pilot can easily reach the flight controls and produce maximum control travels It is rec...

Page 73: ...AI I A PPLY LII RLODEII DELI ECTION IN IIE IlIED DII FCTION AND I EVIL AFT EL LVATO4S CONTISOL POWER OFF AILEHONS NEUTRAL o o 1 0 1 I oIIINITF ISIDDLII SUPIICATION FOLLOWED _ IV FOIDIAIS 0 EL EV ATOR...

Page 74: ...RECOVERIES 5 AS ROTATION STOPS NEUTRALIZE RUDDER AND MAKE A SMOOTH RECOVERY FROM TEE RESULTING DIVE NOTE If disorientation precludes a visual determination of the di 1 rection of rotation the symboli...

Page 75: ...he data given does not take into account the effects of wind navigational errors pilot technique nm up climb etc All these factors should he considered when estimating the reserve required by regulati...

Page 76: ...nsjcessi a Nludel Fl 52 at 753 k certificated maximum weight is 70 1 d 13 A Tic noise level determined according to the above shown regulation at maximum contlimous power is 65 0 d B A The type certif...

Page 77: ...FUght Manual Edition 1 May 1977 iIMS cLssNA F152 Revision 2 May 1979 0 U Page inteotionally left biank tO fl 1 5 lB...

Page 78: ...88 97 107 117 127 136 lAS MPH 46 58 69 81 92 104 115 127 135 150 161 CAS MPH 33 61 69 79 90 101 112 123 135 146 157 FLAPS 10 LAS km h 74 93 111 130 148 158 CAS km h 82 96 113 130 148 156 lAS kts 40 50...

Page 79: ...h 89 km li 106 kin h 00 40 kts 43 kts 48 kts 57 kts 46 MPH 49 MPH 55 MPH 66 MPH I 74 km h 80 km h 89 km h 106 km h 100 40 kts 43 kts 48 kts 57 kts 46 MPH 49 MPH 55 MPH 66 MPH 65 km h 70 km h 78 km h 9...

Page 80: ...s in reserve 75 power at 8000 feet and 93 1 24 5 US Gai usua b le fuel Range 593 km 320 NM Time 3 Ihr s a ii 75 power at 8000 feet and 142 1 37 5 US Gal usuabl e fuel Range 1039 km 543 NM Time 5 2hrs...

Page 81: ...n to any other adjustment of perforiiiunce specified in the Pilots Operating Handbook Flight Manual APPLICABILITY This Change Sheet is applicable to the following Pilots operating I laudhooks Flight M...

Page 82: ......

Page 83: ...and ard Tanks 490 kg With Long Range Tanlcs 492 kg in BAGGAGE 54 kg WtNGLCAD L G 51 Okg rn2 POWER LOADING 9 24 kg kW c i TOTAL FUEL CAPACITY Standa rd Tanks Total 26 US Gal 98 litres Long Range Tanks...

Page 84: ...282 527 305 570 329 616 355 666 kts kts 4000 1219 287 541 311 555 335 634 363 686 392 744 5000 1524 317 600 343 652 370 707 401 770 433 838 58 62 6006 1829 349 571 379 730 410 796 443 870 479 952 MPH...

Page 85: ...l i ft inn m s fr ni n in Is frI mu in s ft no n s 758 SEALE VEL 124 67 77 835 424 765 3 88 700 3 55 630 3 20 c 2000 610 122 66 76 735 3 73 670 3 40 600 3 04 535 2 71 4000 1219 120 65 75 635 3 22 570...

Page 86: ...14 9 120 65 590 2 99 5 0 7 2 6 5 9 4000 1219 7 120 65 550 2 79 6 0 9 3 4 7 13 sc JO 1524 5 119 64 505 2 56 8 1 2 4 5 9 17 60 1829 3 117 63 465 2 36 10 1 4 5 3 12 22 7000 2134 1 117 63 425 2 15 13 1 7...

Page 87: ...Fli t Manual EcIiti 1 May 1977 REIMS CESSNA F152 9 intentionally left bla ID 5 9 1L1...

Page 88: ...0 2400 23 30 2200 21 2000 C 09 iii C 5 3 1 U 5 75 387 101 116 6 1 23 0 70 187 101 116 5 7 23 6 73 180 97 112 5 7 21 6 66 178 96 110 5 4 20 4 63 176 95 109 5 1 19 3 62 170 92 106 5 1 19 3 59 169 91 05...

Page 89: ...59 54 49 45 I 95 I 85 I 76 365 I 56 146 I 9 93 I 83 I 74 65 54 191 I 82 372 63 52 I 85 80 I 70 161 I50 305 00 95 69 84 79 07 I 04 99 94 89 83 103 98 93 S 82 100 97 92 87 SI 121 ItS 109 102 97 91 123...

Page 90: ...9 EPKTAsKTAsKTAs KTAS_L_ p i_ __ ___tO tO itO N i E1OQ 94 87 m KTAs1 KTAs KrAsKTAs 300 350 400 450 500 556 648 741 833 926 RANGE NM km U NOTES I This chait allows for the fuel used fur engine stast ta...

Page 91: ...USABLE FUEL CONDITIONS 758 kg Recommended Lean Mixture for Cruise tandard Temperature Zero Wind El 10000 3048 2438 C 6000 1829 LI 4000 1219 2000 610 S L 2 3 4 6 ENDURANCE HOURS NOTE This chart allows...

Page 92: ...during climb as shown in fl ure 5 6 2 Performance is shown for an airplane equipped with speed fairitigs which increase the cruise speeds by approximately 3 5km h Zkts 2 5MPH RANGE PROFILE 45 MINUTES...

Page 93: ...ROFILE 45 MINUTES RESERVE 37 5 US Gal 142 1 USABLE FUEL Standard Temperature Zero wind El S El U 12000 3658 10000 3048 8000 2438 6000 1829 4000 1219 2000 610 S S L 5 6 7 8 9 ENDURANCE HOURS NOTE J his...

Page 94: ...ft ROll Roil sOh ROll ntbs Roll clear RoE 1670 758 100 1 ni Is 54 kt 62 MPH Sea Level 305 1000 610 2000 1 37 450 142 465 148 485 500 354 1160 361 1185 170 1215 378 240 142 465 148 485 152 500 158 520...

Page 95: ...ps in 11 VS a U 1219 4000 1524 5000 1829 6000 2134 7000 2436 8000 158 320 165 540 171 560 1 78 565 134 605 338 275 398 1 305 408 1340 419 1375 430 1410 165 540 171 560 177 530 184 605 192 630 171 55 1...

Page 96: ...fl En a En ft 0 0...

Page 97: ...which require servicing inspect ion and or testing at speci r srvals Since Dealers cc s ut all service inspection and test procedures in accordance wit as icable Service Manuals it is recommended that...

Page 98: ...8 C and 21 C below 12 C CAPACITY OF ENCINE SUMP 6 Quatts 5 7 1 Do not operatc on les than 4 quarts 3 8 1 To i through breathcr fill to 5 quart 4 8 1 level for L than 3 hours I or extended flight fill...

Page 99: ...very 6 months even though less than the recommended hours have accumulated Reduce intervals for prolonged operation in dusty areas cold climates or when short flights and long idle periods result in s...

Page 100: ...OSE Wl Ji LL i RE PR SURE 2 tO bar 30 psi on 5 5 4 ply r IctI tirc MAIN WHEEL TIRE PR SSURE 1 45 bar 21 psi on 6 6 4 ply rated tires NOSE GEAR SHOCK S RUT Keep filled with MIL EI 5606 hydraulic fluid...

Page 101: ...trong ropes or chains 320 kg tensile strength to wing and tail tie down fittings and secure each rope to ramp tie down 4 Install a surface control lock over the fin and rudder 5 Install a pitot tube c...

Page 102: ...id flying through ra4n hail or sleet tiuring this period Once the finish has cured completel wax or polish may be used par ticularly on the leading edges engine nose cap and propeller spinner to reduc...

Page 103: ...ease ci the control wheel and control knol s can be ti jnoved with a cloth moistened with kerosene Volatile scilvents sucl as mentioned in paragtaphs on care of the windshield must ne er be used since...

Page 104: ...n 11 I a 11 U U Li U a U U Ii...

Page 105: ...AL Whit aiion kit 6 1 1 and 6 1 2 Cr rI Service Plug Receptacle 6 2 1 and 6 2 2 Radio transmitter Sclecto Switch 6 3 1 D Boom Microphone 6 3 1 U True Airpecd Indicator 6 4 1 K7R44sp BADIN CROUZET GlOB...

Page 106: ...11 1 II p B 11 n II B U U U 0...

Page 107: ...Flight Manual RUMS CESSNA F1Sz Edition 1 May 1977 Rvision 2 May 1979 D G A C Approved OPTIONAL EQUIPMENT LIST iiD 6 1 0 2 2...

Page 108: ...0 n I 1 II a a...

Page 109: ...of LI Two shieii5 to paitially cover the cowl nose cap openings An insulation for the engine crankcase breati er line 1 NOTE Cice installed the crankcase breather insulation is U arproved for permane...

Page 110: ...cabin W1NTERIZATION KIT MUST BE REMOVED I WI TEN OUTSIDE AIR TEMpERATURE IS ABOVE 70 C Refer to Section 2 of the airplane flight manual for the other limitations 11 There is no change to Sections 3 t...

Page 111: ...ipment SECTION 2 LIMITATIONS The following inferu ation must be presented in the form of a placard located on the insid of the ground service plug access door CArrION 24 VOLTS D C This aircmft is equi...

Page 112: ...which otherwise might dai ge the transistors in the electronic equipment 2 The battery and external power circuits havc been designed to completely eliminate the need to jumper cross the battery cont...

Page 113: ...l pressure altitude is aligned wil I c side air temperature in degrees Fahrenheit 2 Read tme ai 1 eed on rotatable ring opposite airspeed needle NOTE Pressnu iritude should not be confused with indica...

Page 114: ...n a Ii U LI 1 El LI U U U U...

Page 115: ...ON 4 NORMAL PROCEDURES 1 Slip a hose over the end of the valve 2 Route the hose to a suitable container 3 Push upward on the end of the valve until it snaps into the open position Spring clips will ho...

Page 116: ...a a U Ii tM 1 U II U LI 0 ii I U U Ii...

Page 117: ...through the roll control system The major conIJm its are as follows A flight contrni A roll yaw semi An air distribiif Two aileron cr 1 air driven actuators A vacuum source Mechanical p B Directional...

Page 118: ...AL PROCEDURES I BEFORE TAKE OFF 1 Set ThRN and TRIM knobs to neutral U 2 STAB l WG selector switches STAB 3 Autopilot ON OFF switch OFF 4 VIDE P A A P VACUUM valve OUVERT N 5 Suction gage Check 4 6 to...

Page 119: ...esired heading on the directional gyro compass card ali ied with rnagi etic compass heading 2 Sd IIDG VOR selector switch to HDG 3 Sd F STAB HOG selector switch to HOG The aircraft turns to the select...

Page 120: ...aft is subjected to strong crosswind conditions it is recommended to allow for a certain amount of J drift upon heading selection on the directional gyro compass card not altering the course selected...

Page 121: ...upply source separate from tH of the artificial horizon S One Gyroscopic l iiectional Indicator 0 One Gyroscopic Instrument Power Monitoring System 0 One Rate of CI bindicator One Flashing 13c ccn 0 P...

Page 122: ...U U U a U U U U...

Page 123: ...urijive and Adjustable Altimeter 0 One Pitot Tube 0 One Alternate Static Ptessure Source 0 One Rate of Cflmb Indicator S One Outside Air Temperature Gage 0 One Electric Clock with Second Hand 0 One Fl...

Page 124: ...11 Ii U U U U U U U...

Page 125: ...is essentially constant and this provides a useful lear nd SECTION 4 NORMAL PROCEDURES Operating uctions are as follows Exhaust ga uperature ECT may be used as an aid for mixture leaning in cn ing fJi...

Page 126: ...or throttle peition vifl require a recheck of EGT indicati MD TURE DCIi T GAS DESCRIPTION TEN ATURE n RECOMMENDED LEAN Flight Manual and 25 F 14 C zof Peak ECT C onaputer Performance Li BESTECONOMY P...

Page 127: ...U Flight Manual Edition 1 May 1 REIMS CESSNA F152 U El LI El U Li GAA APPENDIX U...

Page 128: ...El S S El a S S U U U U U U...

Page 129: ...hich cooling is certified is 37 8 C hot day No minimum air temp ste has been established NIGHT VFR AND l FF t ROVAL Refer to pages 2 2 6 i I and 6 7 1 of this manual To be deleted NOISE LEVEL Refer to...

Page 130: ...9 El El El 11 U U S El U...

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