Cessna TURBO CENTURION T210M 1978 Pilot Operating Handbook Download

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PILOT'S OPERATING

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Cessna.

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TURBO CENTURION

1978 MODEL T210M

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Registration No

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THIS HANDBOOK INCLUDES.THE MATERIAL REQUIRED

TO BE FURNISHED TO THE PILOT BY CAR PART 3

CESSNA AIRCRAFT COMPANY

WICHITA, KANSAS, USA

Summary of Contents for TURBO CENTURION T210M 1978

Page 1: ...TURION 1978 MODEL T210M Serial No l Registration No I 11t_ THIS HANDBOOK INCLUDES THE MATERIAL REQUIRED TO BE FURNISHED TO THE PILOT BY CAR PART 3 COPYRIGHT 1977 CESSNA AIRCRAFT COMPANY WICHITA KANSAS...

Page 2: ...illustration affected by the revision is indicated by a vertical line in the outer margin of the page Dates of issue for original and revised pages are Original 0 15 August 1977 THE TOTAL NUMBER OF PA...

Page 3: ...essna Dealers worldwide Specific benefits and provisions of warranty plus other important benefits for you are contained in your Customer Care Program book supplied with your airplane Warranty service...

Page 4: ...Ft Obstacle STALL SPEED CAS Flaps Up Power Off Flaps Down Power Off MAXIMUM WEIGHT Ramp Takeoff and Landing STANDARD EMPTY WEIGHT Turbo Centurion Turbo Centurion II MAXIMUM USEFUL LOAD Turbo Centurio...

Page 5: ...GENERAL 1 LIMITATIONS 2 EMERGENCY PROCEDURES 3 NORMAL PROCEDURES 4 PERFORMANCE 5 WEIGHT BALANCE EQUIPMENT LIST 6 AIRPLANE SYSTEMS DESCRIPTIONS 7 AIRPLANE HANDLING SERVICE MAINTENANCE 8 SUPPLEMENTS Op...

Page 6: ......

Page 7: ...d Entry Dimensions Baggage Space And Entry Dimensions Specific Loadings Symbols Abbreviations And Terminology General Airspeed Terminology And Symbols Meteorological Terminology Engine Power Terminolo...

Page 8: ...with nose gear depressed all tire5 and nose strut properly in flated and flashing beacon installed 2 Wheel base length is 72 3 Propeller ground clearance is 10 7 8 4 Wing area is 175 square feet 5 Min...

Page 9: ...opposed fuel injected six cylinder engine with 520 cu in displace ment Horsepower Rating and Engine Speed Maximum Power 5 minutes takeoff 310 rated BHP at 36 5 inches Hg and 2700 RPM Maximum Continuo...

Page 10: ...rs or oil consumption has stabilized Recommended Viscosity for Temperature Range SAE 50 above 4 C 40 F SAE 10W30 or SAE 30 below 4 C 40 F NOTE Multi viscosity oil with a range of SAE 10W30 is recom me...

Page 11: ...ressed in knots Knots calibrated airspeed is equal to KTAS in standard atmosphere at sea level Knots Indicated Airspeed is the speed shown on the airspeed indicator and expressed in knots Knots True A...

Page 12: ...the greatest gain in altitude in a given time METEOROLOGICAL TERMINOLOGY OAT Standard Tempera ture Pressure Altitude Outside Air Temperature is the free air static temperature It is expressed in eith...

Page 13: ...sumed at a specific engine power setting and or flight configura tion g is acceleration due to gravity WEIGHT AND BALANCE TERMINOLOGY Reference Datum Station Arm Moment Center of Gravity C G Reference...

Page 14: ...ll operating fluids and full engine oil Basic Empty Weight is the standard empty weight plus the weight of optional equipment Useful Load is the difference between ramp weight and the basic empty weig...

Page 15: ...ed Indicator Markings Power Plant Limitations Power Plant Instrument Markings Weight Limits Center Of Gravity Limits Maneuver Limits Flight Load Factor Limits Kinds Of Operation Limits Fuel Limitation...

Page 16: ......

Page 17: ...ted with optional systems or equip ment are included in Section 9 NOTE The airspeeds listed in the Airspeed Limitations chart figure 2 1 and the Airspeed Indicator Markings chart figure 2 2 are based...

Page 18: ...0 Pounds 109 110 control movements above 2600 Pounds 97 98 this speed VFE Maximum Flap Extended Speed To 10 Flaps 149 150 Do not exceed these speeds 10 30 Flaps 114 115 with the given flap settings VL...

Page 19: ...rations Figure 2 2 Airspeed Indicator Markings POWER PLANT LIMITATIONS Engine Manufacturer Teledyne Continental Engine Model Number TSIO 520 R Engine Operating Limits for Takeoff and Continuous Operat...

Page 20: ...UMENT MARKINGS Power plant instrument markings and their color code significance are shown in figure 2 3 RED LINE GREEN ARC YELLOW ARC WHITE ARC RED LINE INSTRUMENT MINIMUM NORMAL CAUTION NORMAL MAXIM...

Page 21: ...UVER LIMITS This airplane is certificated in the normal category The normal category is applicable to aircraft intended for non aerobatic operations These include any maneuvers incidental to normal fl...

Page 22: ...onditions is prohibited FUEL LIMITATIONS 2 S tan d Tanks 45 U S gallons each Total Ftiel 00 U S _ gallons __ _ _ ____ Usable Fuel all flight conditions 89 U S gallons Unusable Fuel 1 U S gallon NOTE T...

Page 23: ...ards markings and manuals MAXIMUMS MANEUVERING SPEED IAS GROSS WEIGHT FLIGHT LOAD FACTOR Flaps Up Flaps Down 119 knots 3800 lbs 3 8 1 52 2 0 No acrobatic maneuvers including spins approved Altitude lo...

Page 24: ...0 MIN AVIATION GRADE GASOLINE TOTAL CAPACITY 45 0 GAL 6 Forward of fuel tank cap FOR 32 GAL FUEL LOAD FILL TO BOTTOM OF FILLER NECK EXTENSION 7 On baggage compartment door MAXIMUM BAGGAGE 120 LBS REFE...

Page 25: ...L FLOW LBS HR 35 34 32 30 28 26 24 22 162 156 144 132 120 108 102 96 AVOID CONTINUOUS OPERATION BETWEEN 1850 AND 2150 RPM ABOVE 24 IN M P 10 On lower surface of right hand wing just outboard of fusela...

Page 26: ...LT210M 2 12 12 On inside nose wheel doors strut doors and main wheel doors WARNING BEFORE WORKING IN WHEEL WELL AREA PULL HYDRAULIC PUMP CIRCUIT BREAKER OFF 13 Near landing gear lever MAX SPEED IAS GE...

Page 27: ...ound Engine Fire In Flight Electrical Fire In Flight Cabin Fire Wing Fire Icing Inadvertent Icing Encounter Static Source Blockage Erroneous Instrument Reading Suspected Landing Gear Malfunction Proce...

Page 28: ...16 3 16 3 17 3 17 3 18 3 18 3 18 3 18 3 19 3 19 3 20 3 20 3 20 3 21 3 21 3 21 Emergency Descent Through Clouds Recovery From A Spiral Dive Flight In Icing Conditions Static Source Blocked Spins Rough...

Page 29: ...ould be considered and applied as necessary to correct the problem Emergency procedures associated with ELT and other optional systems can be found in Section 9 AIRSPEEDS FOR EMERGENCY OPERATION Engin...

Page 30: ...ottle ADVANCE slowly FORCED LANDINGS EMERGENCY LANDING WITHOUT ENGINE POWER 1 Airspeed 90 KIAS flaps UP 80 KIAS flaps DOWN 2 Mixture IDLE CUT OFF 3 Fuel Selector Valve OFF 4 Ignition Switch OFF 5 Land...

Page 31: ...NT AT 75 KIAS 6 Approach High Winds Heavy Seas INTO THE WIND Light Winds Heavy Swells PARALLEL TO SWELLS NOTE If no power is available approach at85 KIAS with flaps up or at 80 KIAS with 10 flaps 7 Ca...

Page 32: ...of the horizontal tail 9 Fire Damage INSPECT repair damage or replace damaged components or wiring before conducting another flight ENGINE FIRE IN FLIGHT 1 Mixture IDLE CUT OFF 2 Fuel Selector Valve O...

Page 33: ...bin Air Heat OPEN when it is ascertained that fire is completely extinguished CABIN FIRE 1 Master Switch OFF 2 Vents Cabin Air Heat CLOSED to avoid drafts 3 Fire Extinguisher ACTIVATE if available I W...

Page 34: ...nches of full throttle manifold pressure will be experienced 6 If icing conditions are unavoidable plan a landing at the nearest airport With an extremely rapid ice build up select a suitable off airp...

Page 35: ...h 7 knots faster than normal or consult appropriate table in Section 5 3 Altitude Cruise 150 feet higher and approach 70 feet higher than normal LANDING GEAR MALFUNCTION PROCEDURES LANDING GEAR FAILS...

Page 36: ...DOWN 7 Avionics Power and Master Switches OFF when landing is assured 8 Touchdown SLIGHTLY TAIL LOW 9 Mixture IDLE CUT OFF 10 Ignition Switch OFF 11 Fuel Selector Valve OFF 12 Airplane EVACUATE LANDIN...

Page 37: ...full flap 2 Touchdown GOOD TIRE FIRST hold airplane off flat tire as long as possible with aileron control 3 Directional Control MAINTAIN using brake on good wheel as required ELECTRICAL POWER SUPPLY...

Page 38: ...J _...

Page 39: ...nway The checklist procedures assume that adequate time exists to secure the fuel and ignition systems prior to touchdown After an engine failure in flight the best glide speed as shown in figure 3 1...

Page 40: ...R CONTROL Trim for horizontal flight with an airspeed of approximately 80 KIAS and flaps set to 20 by using throttle and trim tab controls Then do not change the trim tab setting and control the glide...

Page 41: ...proficient in instrument flying EXECUTING A 180 TURN IN CLOUDS Upon inadvertently entering the clouds an immediate plan should be made to turn back as follows 1 Note the compass heading 2 Note the ti...

Page 42: ...nbalanced rudder force 8 Check trend of compass card movement and make cautious corrections with rudder to stop turn 9 Upon breaking out of clouds resume normal cruising flight RECOVERY FROM A SPIRAL...

Page 43: ...t at maximum cruise reads high During approach typical variations are 4 knots and 40 feet reads high With the alternate static source on fly the airplane at airspeeds and altitudes which compensate fo...

Page 44: ...H position of the ignition switch unless extreme roughness dictates the use of a single ignition position MAGNETO MALFUNCTION A sudden engine roughness or misfiring is usually evidence of magneto prob...

Page 45: ...ESSURE If low oil pressure is accompanied by normal oil temperature there is a possibility the oil pressure gage or relief valve is malfunctioning A leak in the line to the gage is not necessarily cau...

Page 46: ...gear extension time is approximately 11 seconds If the landing gear will not extend normally perform the general checks of circuit breakers and master switch and repeat the normal extension procedures...

Page 47: ...Electronic components in the electrical system could be adversely affected by higher than normal voltage if a faulty voltage regulator is causing the overcharging To preclude these possibilities an ov...

Page 48: ......

Page 49: ...Wing Leading Edge Left Wing Trailing Edge Before Starting Engine Starting Engine Before Takeoff Takeoff Normal Takeoff Short Field Takeoff Enroute Climb Normal Climb Maximum Performance Climb Cruise...

Page 50: ...Crosswind Takeoff Landing Gear Retraction Enroute Climb Cruise CESSNA MODELT210M Page Leaning With A Cessna Economy Mixture Indicator EGT 4 13 4 15 4 15 4 15 4 15 4 16 4 16 4 16 4 16 4 17 4 17 4 17 4...

Page 51: ...rformance the speed appropriate to the particular weight must oe used Takeoff Normal Climb Out Short Field Takeoff Flaps 10 Speed at 50 Feet Enroute Climb Flaps and Gear Up Normal Best Rate of Climb S...

Page 52: ...or snow from wing tail and control surfaces Also make sure that control surfaces contain no internal accumulations of ice or debris Prior to flight check that pitot heater if installed is warm to tou...

Page 53: ...degrees nose up normal nose strut on a level surface NOTE The airplane turn and bank instrument may be used to check lateral leveling 2 Visually inspect each fuel tank for fuel level with the upper w...

Page 54: ...Tire CHECK for proper inflation 2 efore first flight of the day and after each refueling use sampler cup and drain small quantity of fuel from fuel tank sump quick drain valve to check for water sedim...

Page 55: ...ck REMOVE 2 Tail Tie Down DISCONNECT 3 Control Surfaces CHECK freedom of movement and security RIGHT WING Trailing Edge 1 Aileron CHECK for freedom of movement and security 2 Fuel Tank Vent at Wing Ti...

Page 56: ......

Page 57: ...l Pump Switch OFF 7 Propeller Area CLEAR 8 Ignition Switch START 9 Throttle ADVANCE slowly 10 Ignition Switch RELEASE when engine starts NOTE The engine should start in two or three revolutions If it...

Page 58: ...t if installed OFF 13 Flashing Beacon Navigation Lights and or Strobe Lights ON as r _ required 14 Throttle Friction Lock ADJUST 15 Parking Brake RELEASE TAKEOFF NORMAL TAKEOFF 1 Wing Flaps 0 10 10 pr...

Page 59: ...nd 2500 RPM 3 Mixture LEAN to 120 lbs hr NOTE On hot days it may be necessary to utilize the auxiliary fuel pump to maintain 120 lbs hr fuel flow 4 Cowl Flaps OPEN as required NOTE On hot days turn on...

Page 60: ...NOTE In hot weather at high altitudes be alert for fuel vapor indications If fuel flow fluctuations are observed place the auxiliary fuel pump switch in the ON position and reset mixture control as de...

Page 61: ...referred 3 Airspeed 70 80 KIAS flaps DOWN 4 Elevator Trim ADJUST 5 Touchdown MAIN WHEELS FIRST 6 Landing Roll LOWER NOSE WHEEL GENTLY 7 Braking MINIMUM REQUIRED SHORT FIELD LANDING 1 Wing Flaps FULL D...

Page 62: ...0M 2 Cowl Flaps OPEN 3 Radar if installed OFF SECURING AIRPLANE 1 Parking Brake SET 2 Avionics Power Switch Electrical Equipment OFF 3 Mixture IDLE CUT OFF pulled full out 4 Ignition Switch OFF 5 Mast...

Page 63: ...le to the desired idle speed When the engine is hot or outside air temperatures are high the engine may die after running several seconds because the mixture became either too lean due to fuel vapor o...

Page 64: ...L TORI l fii 1 I l air CODE NOTE WIND DIRECTION Strong quartering tail winds require caution Avoid sudden bursts of the throttle and sharp braking when the airplane is in this attitude Use the steerab...

Page 65: ...r shut off the engine and investigate Lack of oil pressure can cause serious engine damage TAXIING Taxiing over loose gravel or cinders should be done at low engine speed to avoid abrasion and stone d...

Page 66: ...r loose gravel are especially harmful to propeller tips When takeoffs must be made over a gravel surface it is very important that the throttle be advanced slowly This allows the airplane to start rol...

Page 67: ...Section 5 is based on this speed and configuration Minimum ground run takeoffs are accomplished using 20 flaps by lifting the nose wheel off the ground as soon as practical and leaving the ground in...

Page 68: ...re 2500 RPM 120 lbs hr fuel flow and 100 to 120 KIAS is normally recommended to provide an optimum combination of performance visibility ahead engine cooling economy and passenger comfort due to lower...

Page 69: ...on at a given altitude can be observed This table should be used as a guide along with the available winds aloft information to determine the most favorable altitude and power setting for a given trip...

Page 70: ...y increased throttle setting or higher RPM as necessary to maintain the desired power Maximum continuous mani fold pressure 35 in Hg is available up to 14 000 feet under hot day conditions using the a...

Page 71: ...that the auxiliary fuel pump has been turned off Descent should be at approximately 500 FPM for passenger comfort using enough power to keep the engine warm The optimum engine RPM in a descent is usu...

Page 72: ...nding roll The nose wheel is lowered to the runway after the speed has diminished to avoid unnecessary nose gear load This procedure is especially important in rough or soft field landings SHORT FIELD...

Page 73: ...details For quick smooth engine starts in very cold temperature use six strokes of the manual primer if installed before cranking with an additional one or two st rokes as the engine starts In very co...

Page 74: ...hereby tend to build public support for aviation 1 Pilots operating aircraft under VFR over outdoor assemblies of persons recreational and park areas and other noise sensitive areas should make every...

Page 75: ...ximum Rate Of Climb Time Fuel And Distance To Climb Normal Climb Figure 5 7 Cruise Performance 2000 Feet Cruise Performance 4000 Feet Cruise Performance 6000 Feet Cruise Performance 8000 Feet Cruise P...

Page 76: ......

Page 77: ...peller condition and air turbulence may account for variations of 10 or more in range and endurance Therefore it is important to utilize all available information to estimate the fuel required for the...

Page 78: ...tance information presented for a weight of 3800 pounds pressure altitude of 4000 feet and a temperature of 30 C should be used and results in the following Ground roll Total distance to clear a 50 fo...

Page 79: ...t shows a corresponding 5 hours Using this information the estimated distance can be determined for the expected 10 knot headwind at 11 500 feet as follows Range zero wind Decrease in range due to win...

Page 80: ...climb In this case assuming a temperature 16 C above standard the correction would be 16 C soc x 10 20 Increase With this factor included the fuel estimate would be calculated as follows Fuel to clim...

Page 81: ...he flight is underway ground speed checks will provide a more accurate basis for estimating the time enroute and the corresponding fuel required to complete the trip with ample reserve LANDING A proce...

Page 82: ...AS 50 KCAS 56 AIRSPEED CALIBRATION NORMAL STATIC SOURCE 80 100 120 140 160 80 99 119 139 160 70 80 90 100 120 71 81 90 100 119 70 80 90 100 110 73 82 92 101 110 60 70 80 90 100 65 75 l4 93 102 CESSNA...

Page 83: ...UP NORMAL KIAS 60 80 100 120 140 160 ALTERNATE KIAS 58 78 101 123 144 165 FLAPS 10 NORMAL KIAS 60 70 80 90 100 120 ALTERNATE KIAS 59 69 80 91 101 123 FLAPS 30 NORMAL KIAS 50 60 70 80 90 100 ALTERNATE...

Page 84: ...CHART 100 t 1 t tt 1 t tt ttt t ttt 1 t tt 1 ttt ttt t tt tt tttm 80 60 t w I z LU a I I 40 u f w LU a w 0 20 O tj t ttt 1 t tt t tt 1 t ttt 1 t tt 1 t tt t t tt 1 t tt 1 t tt 1 t tt 40 40 20 0 20 40...

Page 85: ...T FLAP oo 30 45 60 LBS DEFLECTION KIAS KCAS KIAS KCAS KIAS KCAS KIAS KCAS UP 64 65 69 70 76 77 91 92 oo 62 64 67 69 74 76 88 91 3800 20 56 59 60 63 67 70 79 83 30 50 56 54 60 59 67 79 79 MOST FORWARD...

Page 86: ...TOTAL TOTAL TOTAL TOTAL TOTAL LIFT AT FT GRND TO CLEAR GRND TO CLEAR GRND TO CLEAR GRND TO CLEAR GRND TO CLEAR OFF 50FT ROLL 50 FT OBS ROLL 50 FT OBS ROLL 50 FT OBS ROLL 50 FT OBS ROLL 50 FT OBS 3800...

Page 87: ...1330 2125 1450 2330 1585 2565 7000 1300 2060 1420 2260 1550 2480 1695 2735 8000 1390 2190 1515 2405 1660 2645 1815 2915 S L 680 1125 740 1220 805 1325 875 1445 1000 720 1185 785 1290 855 1405 930 153...

Page 88: ...o 17 000 35 162 18 000 34 156 20 000 32 144 22 000 30 132 24 000 28 120 CLIMB RATE OF CLIMB FPM SPEED KIAS 20 C o0 c 20 c 4o0 c 97 1280 1135 995 850 97 1185 1040 895 750 97 1090 945 800 655 97 980 840...

Page 89: ...zero wind PRESS CLIMB RATE OF FROM SEA LEVEL WEIGHT LBS ALT SPEED CLIMB TIME FUEL USED DISTANCE FT KIAS FPM MIN POUNDS NM 3800 S L 97 1030 0 0 0 4000 97 990 4 11 7 8000 97 950 8 22 14 12 000 97 900 1...

Page 90: ...mperature 3 Distances shown are based on zero wind PRESS RATE OF FROM SEA LEVEL WEIGHT LBS ALT CLIMB TIME FUEL USED DISTANCE FT FPM MIN POUNDS NM 3800 S L 690 0 0 0 4000 655 6 12 11 8000 615 12 25 23...

Page 91: ...NOTE For best fuel economy at 70 power or less op erate at 6 PPH leaner than shown in this chart or at peak EGT if an EGT indicator is installed STANDARD 20 c ABOVE TEMPERATURE STANDARD TEMP 11 c 31...

Page 92: ...NOTE For best fuel economy at 70 power or less op erate at 6 PPH leaner than shown in this chart or at peak EGT if an EGT indicator is installed STANDARD 20 c ABOVE TEMPERATURE STANDARD TEMP 1 c 21 c...

Page 93: ...NOTE For best fuel economy at 70 power or less op erate at 6 PPH leaner than shown in this chart or at peak EGT if an EGT indicator is installed STANDARD 20 c ABOVE TEMPERATURE STANDARD TEMP 3 c 23 c...

Page 94: ...NOTE For best fuel economy at 70 power or less op erate at 6 PPH leaner than shown in this chart or at peak EGT if an EGT indicator is installed STANDARD 20 c ABOVE TEMPERATURE STANDARD TEMP 1 C 19 c...

Page 95: ...NOTE For best fuel economy at 70 power or less op erate at 6 PPH leaner than shown in this chart or at peak EGT if an EGT indicator is installed STANDARD 20 C ABOVE TEMPERATURE STANDARD TEMP 5 C 15 c...

Page 96: ...OTE For best fuel economy at 70 power or less op erate at 6 PPH leaner than shown in this chart or at peak EGT if an EGT indicator is installed 20 CABOVE STANDARD TEMPERATURE STANDARD TEMP _9oc 110c K...

Page 97: ...NOTE For best fuel economy at 70 power or less op erate at 6 PPH leaner than shown in this chart or at peak EGT if an EGT indicator is installed STANDARD 20 c ABOVE TEMPERATURE STANDARD TEMP 13 C 1 c...

Page 98: ...NOTE For best fuel economy at 70 power or less op erate at 6 PPH leaner than shown in this chart or at peak EGT if an EGT indicator is installed STANDARD 20 c ABOVE TEMPERATURE STANDARD TEMP 17 C 3 c...

Page 99: ...6 66 NOTE For best fuel economy at 70 power or less op erate at 6 PPH leaner than shown in this chart or at peak EGT if an EGT indicator is installed STANDARD 20 CABOVE TEMPERATURE STANDARD TEMP 21 c...

Page 100: ...49 149 67 NOTE For best fuel economy at 70 power or less op erate at 6 PPH leaner than shown in this chart or at peak EGT if an EGT indicator is installed STANDARD 20 C ABOVE TEMPERATURE STANDARD TEM...

Page 101: ...0 50 151 67 NOTE For best fuel economy at 70 power or less op erate at 6 PPH leaner than shown in this chart or at peak EGT if an EGT indicator is installed STANDARD 20 c ABOVE TEMPERATURE STANDARD TE...

Page 102: ...22 56 165 74 20 50 154 68 NOTE For best fuel economy at 70 power or less op erate at 6 PPH leaner than shown in this chart or at peak EGT if an EGT indicator is installed STANDARD 20 c ABOVE TEMPERATU...

Page 103: ...limb up to 20 000 feet and maximum rate of climb above 20 000 feet 2 Reserve fuel is based on 45 minutes at 45 BHP and is 46 lbs 24 000 192 KTAS I I I I 155d 176 KTAS KTAS 202 KTAS 1 20 000 I j I I I...

Page 104: ...start taxi takeoff and climb and the time during climb as shown in Figure 5 6 for a normal climb up to 20 000 feet and maximum rate of climb above 20 000 feet 2 Reserve fuel is based on 45 minutes at...

Page 105: ...T GRND TO CLEAR GRN D TO CLEAR GRND TO CLEAR GRND TO CLEAR GRND TO CLEAR ROLL 50 FT OBS ROLL 50 FT OBS ROLL 50 FT OBS ROLL 50 FT OBS ROLL 50 FT OBS 3800 71 S L 725 1440 750 1480 780 1520 805 1560 830...

Page 106: ......

Page 107: ...97 792 New Total 2400 Serial No 21062625 Arm Moments Inches Inch Pounds 7 4 6001 4 64 4 51326 8 64 4 51004 8 40 138 96330 20 2400 Pounds 40 138 Inches 96330 20 Inch Pounds This new weight and balance...

Page 108: ...7 6 A P 3421289 Date 12 11 2020...

Page 109: ...6 WEIGHT BA LANCE EQUIPMENT LIST SECTION 6 WEIGHT BALANCE EQUIPMENT LIST TABLE OF CONTENTS Introduction Airplane Weighing Procedures Weight And Balance Baggage Tie Down Equipment List Page 6 3 6 3 6...

Page 110: ......

Page 111: ...ove sliding seats to the most forward position e Raise flaps to the fully retracted position f Place all control surfaces in neutral position 2 Leveling a Place scales under each wheel minimum scale c...

Page 112: ...ighed X ARM A N x B X w Tare Item Weight Lbs Airplane Weight From Item 5 Page 6 3 Add Oil 11 Ots at 7 5 Lbs Gal 21 Add Unusable Fuel 1 Gal at 6 Lbs Gal 6 Equipment Changes Airplane Basic Empty Weight...

Page 113: ...ER I PAGE NUMBER WEIGHT CHANGE ITEM NO RUNNING BASIC ADDED REMOVED H EMPTY WEIGHT DATE DESCRIPTION OF ARTICLE OR MODIFICATION Wt Arm Moment Wt Arm Moment Wt Moment In Out lb In 1000 lb In 1000 Ob 1000...

Page 114: ...be carried then list these on the loading problem NOTE Loading Graph information for the pilot passengers and baggage is based on seats positioned for average occu pants and baggage loaded in the cent...

Page 115: ...ded forward to create more baggage area If this area is used all six tie down straps must be used Tie the front straps of the net to the front legs of the fifth and sixth seats and the remaining four...

Page 116: ...an be used as a convenient interior refer ence point for determining the location of baggage area fuse lage station C G I C G ARM ARM 37 34 46 71 Cl n 71 Cl n 61 77 I 61 77 r AFT PAss 1 r BAGGAGE 1 10...

Page 117: ...7 L__ 46 J 41 27 6 5 59 FIREWALL DOOR CABIN DOOR BAGGAGE DOOR 65 4 OPENING DIMENSIONS WIDTH WIDTH IHEIGHT IHEIGHT TOP BOTTOM FRONT REAR 31 36 I 40 I 38 19 28 8 14 CABIN WIDTH MEASUREMENTS REAR DOORPOS...

Page 118: ...9 7 8 RAMP WEIGHT AND MOMENT 3816 196 8 9 Fuel allowance for engine start taxi and runup 16 7 10 TAKEOFF WEIGHT AND MOMENT Subtract step 9 from step 8 3800 196 1 11 Locate this point 3800 at 196 1 on...

Page 119: ...51 4 s o i ss o I 1 0 l 30 113 6 ol 175 a 0 I 150 g I I 125 0 100 c3 I 75 20 of 75 7 f f i j f 1 1 oS I ll Gf l1 J O of 1 1 II j l 1 50 25 5 10 15 20 25 30 35 40 0 LOAD MOMENT 1000 POUND INCHES NOTES...

Page 120: ...2000 2100 2200 2300 2400 90 100 110 120 130 Loadings within clear area are satisfactory for takeoff and landing In shaded area takeoff is approved but computation of loading after estimated fuel burn...

Page 121: ...IPMENT LIST MILLIMETERS A FT OF DATUM STA 0 0 11 25 1150 11 75 1200 1225 1250 1275 1300 1325 1350 1750 1700 1650 1600 1550 1500 vi 1450 g 1400 g I 1350 i w z 1300 j 1250 il 0 1200 g 1150 1100 1050 100...

Page 122: ......

Page 123: ...n S standard equipment items 0 optional equipment items replacing required or standard items A optional equipment items which are in addition to required or standard items A reference drawing column p...

Page 124: ...UUM PU IP AV OF 4 TYPES RELIEF V 1LVE MISC HOSES CLAMPS ETC PRIMING SYSTEM MANIFOLD 2 POINT B LA lDING GEAR ACCESSORIES W1 E El BR AKE TIRE AS S Y wf EEL ASSY CLEVELAND BRAKE ASSY CLEVFLAND BR AKE A S...

Page 125: ...L IGl T INSTALLATION OMNIFLASH dEACON BEACON LIGl T IN FIN TIP FLASHR POWER SUPPLY IN FIN TIP LIGf T INSTL WING T P STROBE FLASHING POWEi SLPPLV STROBF LIGHTS IN WING T P SET CF 21 l IGHTS COWL MOUNTE...

Page 126: ...ADING INDICATOR ATTITUDE INDICATO GYPO INS TALLATION FO NCI SLAVED HSI ATTITUCE INDI CATOR M SC ITEMS HOSES GYRO JNSTL CES5NA 300A NAV 0 MATIC ATTITUDE INDICATOR t EACINC INDIC ATOR IDGl ARC GYRO INST...

Page 127: ...OT INFl ATE VERTICAL ADJUSTING SEAT PILOT ARTICULATING VERTICAL ADJUST WITH LUMBAR SUPPORT SEAT CO PILOT FIXED HEIGHT ARTICULATING SEAT CO PIUJT FIXE D HEIGHT ARTICULATit G CLSHION LUl Bl R SUPPCf l S...

Page 128: ...CTABLE CC PIL OT 1 EAOREST FRON1 ROI EAC H 1 EADREST 2ND RO J EAr H 1 EACF EST 3R O FOw EACH 1I RRO R REAR IE APPROACH PLATE HOLDER BAGGAGE TIE DOhN NE1 STPET I FR INSTL CLSTCM AIR tBCXE O USE ACTUAL...

Page 129: ...HANDLE STOWED ARM SHOWN PAINT OVERALL EXTERIOR MODIFIED POLY URETHANE OVERALL BASE WHITE COLORED STRIPE CONTROL CABLES CORROSION RESISTANT INET CHANGE FIRE EXTINGUISHER HAND TYPE PEDAL EXTENSIONS RUD...

Page 130: ...10 0 1 2 8 50 0 SENSE AN TENNAS 21 3960 1 15 0 6 1 31 8 SWITCH I NSTALLATIO N 2 ND AOF 39701 29 l 0 l 17 5 HO l A 4 DUAL CESSN A 4C C AOF 3 9101 60 14 16 l 2 5 7 R 44 t A REC EIVERS 2 1 4 30 90 1128...

Page 131: ...M0LNT t F ANTENNA INSTL WIR 11 i G CABL E A SSE MR LIE S Hl3 A I CESSNA 40C MARKER BEACON REMOTE RECEIVER R 4C2A ANTENN A INSTALLAHCN FLLSH TD I N TAIL Hl5 WE tilt ER RACAR INSTALLATION lf ENDIX RD 1...

Page 132: ...ATOR RECEIVER TRANSCE I VER RT 485A VOP LJC INDIC TOR IN 4 8 5AC H37 A AN1ENNA COLPLE R KIT 1 lOLNT WIR I NG t I SC HARDlo A RE H28 A l EM REENCY LOCATOR Tl ANSMI 1TER TRANS 1ITTER D E M Dl E L T 6 I...

Page 133: ...D Atl A VACULM SYSTEM CESSNA 4008 NAV 0 MATIC SLAVED HEADING INC ICA TOR AILERON ROLL ACTLATOR PA495 ll ELEVATOR PITCH ACTLATOR PA495 2 CONTROLLEP COMPGTER AMPLIFIER ALT IT UDE SEN SOR PI TCl i TR I A...

Page 134: ...LERT OPT CN CONTROLLER 41090 1128 1 3 lt 5 MOCE SELECTOR 42 710 0000 2 6 l3 o PI TCb AC TUA TOR 45850 3012 4 2 154 7 ALT ITUDE SEN SOR 44400 0000 2 3 100 0 COMPUTER 42680 0 00 7 5 8 100 o P IffH TR IM...

Page 135: ...ENNA COLPLER 3960111 1 0 2 5 0 Vf F COM ANTENNA SP I KE CN LH WING 3960113 2 0 5 50 7 Vf f COM AN TENNA CABLE 3950129 0 6 43 3 H44 A REVERSE SENSING SI I T H INSH 0 2 16 0 H46 A AOF ANTI PREC IP ANTEN...

Page 136: ...183 1 2 8 A 1 E l T INSTALLATICN 0470419 1 l A 1 20CA NAV 0 MATIC AUTC PILOT 3910162 16 J04 A I NAV PAC RAOlO OPTION A iAILABU ON TURRC CENTURION ll SERIES Cf LV 1 25 A l RT 385A 2ND LNI T h 300 I ND...

Page 137: ...ntry Step Baggage Compartment Seats Seat Belts And Shoulder Harnesses Seat Belts Shoulder Harnesses Integrated Seat Belt Shoulder Harnesses With Inertia Reels Entrance Doors And Cabin Windows Control...

Page 138: ...System Oxygen System Pitot Static System And Instruments Airspeed Indicator Rate Of Climb Indicator Altimeter Vacuum System And Instruments Attitude Indicator Directional Indicator Suction Gage Stall...

Page 139: ...ribs and an aft fuel tank spar forward of the main spar The Frise type ailerons and single slot type flaps are of conventional formed sheet metal ribs and smooth aluminum skin construction The aileron...

Page 140: ...SECTION 7 AIRPLANE SYSTEMS DESCRIPTIONS AILERON CONTROL SYSTEM RUDDER AND RUDDER TRIM CONTROL SYSTEMS CESSNA MODELT210M Figure 7 1 Flight Control and Trim Systems Sheet 1 of 2 7 4...

Page 141: ...c _ CESSNA MODELT210M SECTION 7 AIRPLANE SYSTEMS DESCRIPTIONS ELEVATOR CONTROL SYSTEM ELEVATOR TRIM CONTROL SYSTEM Figure 7 1 Flight Control and Trim Systems Sheet 2 of 2 7 5...

Page 142: ...SECTION 7 AIRPLANE SYSTEMS DESCRIPTIONS CESSNA MODELT210M N N N co N 7 6 co N Figure 7 2 Instrument Panel Sheet 1 of 2...

Page 143: ...Selector Valve Handle and 1 l i 13 DME Fuel Quantity Indicators I El 14 IFCS Mode Selector 42 Fuel Selector Light CD 15 Rear View Mirror 43 Primer a t 16 Marker Beacon Indicator Lights and 44 Elevato...

Page 144: ...elevator trim is provided see figure 7 1 Rudder trimming is accomplished through a bungee connected to the rudder control system and a trim control wheel mounted on the control pedestal Rudder trimmi...

Page 145: ...ately forward of the handle A parking brake handle is mounted under the switch and control panel in front ofthe pilot All circuit breakers for general electrical equipment and avionics are mounted in...

Page 146: ...ops at the 10 and 20 positions For flap settings greater than 10 move the switch lever to the right to clear the stop and position it as desired A scale and pointer on the left side of the switch leve...

Page 147: ...up labeled GEAR UP and down labeled GEAR DOWN which give a mechanical indication of the gear position selected From either position the lever must be pulled out to clear a detent before it can be repo...

Page 148: ...tch is open A landing gear safety squat switch actuated by the nose gear strut electrically prevents inadvertent retraction by the electrically driven hydraulic power pack whenever the nose gear strut...

Page 149: ...r before placing the landing gear lever in the GEAR DOWN position After practice manual extension is completed push the circuit breaker in to restore normal gear operation LANDING GEAR WARNING SYSTEM...

Page 150: ...re in the airplane For baggage area and door dimensions refer to Section 6 SEATS The seating arrangement consists of four separate adjustable seats and a one piece fixed seat The pilot s seat is a six...

Page 151: ...t apply enough pressure to it to raise or lower it to the desired level The headrest may be removed at any time by raising it until it disengages from the top of the seat back SEAT BELTS AND SHOULDER...

Page 152: ...to retaining stud on seat belt link to attach harness FREE END OF SEAT BELT Pull to tighten SEAT BELT SHOULDER HARNESS ADJUSTABLE LINK Position link just below shoulder level pull link and harness dow...

Page 153: ...is accomplished by pulling upward on the narrow release strap and removing the harness connecting link from the stud on the seat belt link In an emergency the shoulder harness may be removed by relea...

Page 154: ...When the handle is rotated to the LOCK position an over center action will hold it in that position Both cabin doors should be locked prior to flight and should not be opened intentionally during fli...

Page 155: ...5 inches of manifold pressure for five minutes and at 285 horsepower at 2600 RPM and 35 inches of manifold pressure continuous Major accessories include a propeller governor on the front of the engine...

Page 156: ...al resistance type temperature sensor which receives power from the airplane electrical system Oil temperature limitations are the normal operating range green arc which is 38 C 100 F to 116 C 240 F a...

Page 157: ...in at the factory and is ready for the full range of use It is however suggested that cruising be accomplished at 70 to 80 power until a total of 50 hours has accumulated or oil consumption has stabil...

Page 158: ...wise OFF R L BOTH and START The engine should be operated on both magnetos BOTH position except for magneto checks The R and L positions are for checking purposes and emergency use only When the switc...

Page 159: ...ntake manifold tubes and metered fuel is delivered to a fuel manifold The fuel manifold through spring tension on a diaphragm and valve evenly distributes the fuel to an air bleed type injector nozzle...

Page 160: ...ollow the induction air as it enters and passes through the engine until it is expelled as exhaust gases 1 Engine induction air is taken in through an opening in the nose cap ducted through a filter a...

Page 161: ...flow through the turbine When the waste gate is fully closed any change in turbocharger speed will mean a change in engine operation Thus any increase or decrease in turbine speed will cause an increa...

Page 162: ...ions in airspeed This is because the compressor side of the turbo charger operates at pressure ratios of up to 3 to 1 and any change in pressure at the compressor inlet is magnified at the compressor...

Page 163: ...s A slight overboost of 2 to 3 inches of manifold pre ssure is not considered detrimental to the engine as long as it is momentary No corrective action is required when momentary overboost corrects it...

Page 164: ...low RPM When oil pressure to the piston in the propeller hub is relieved centrifugal force assisted by an internal spring twists the blades toward low pitch high RPM A control knob on the lower cente...

Page 165: ...r to an engine driven fuel pump The engiae driven fuel pump delivers the fuel to the fuel air control unit where it is metered and directed to a manifold which distributes it to each cylinder NOTE Fue...

Page 166: ...FUEL PUMP SWITCH ENGINE FUEL PUMP FUEL FLOW 2 INDICATOR _ Right Half of Dual Instrument CESSNA MODELT210M CHECK VALVE FUE L RETURN CODE THROTTLE MIXTURE CONTROL b eic Jj FUEL SUPPLY IIIIIIIIIIIIIID E...

Page 167: ...or vapor purging and continued engine operation in the event of an engine driven fuel pump failure With the right half of the switch in the ON position the pump operates at one of two flow rates that...

Page 168: ...in fuel flow indication To ensure a prompt engine restart in flight after running a fuel tank dry immediately switch to the tank containingfuel at the first indication of fuel pressure fluctuation and...

Page 169: ...the gear up or gear down position When the gear has fully extended or retracted and locked a series of electrical switches will illuminate one of two indicator lights on the instrument panel to show...

Page 170: ...AT APPROX 1500 PSI PRESS TO T EST TYPE INDICATOR L GHT LANDING GEAR AND UP DOWN LOCK ACTUATOR SYSTEM i J LANDING GEAR DOOR ACTUATOR SYSTEM MECHANI CAL CONNECTION ELECT RICA L WI RI NG EMERGENCY HANO P...

Page 171: ...ical energy see figure 7 9 is supplied by a 28 volt direct current system powered by an engine driven 60 amp 95 amp if installed alternator A 24 volt 14 amp hour battery or 17 amp hour battery if inst...

Page 172: ...TO COMPASS LIGHT TO POST LIGHTING TO OXYG EN UGHTS TO NAVIGATION LIGHTS CONTROL WHEEl MAP LIGHT ELECTROLUMINESCENT LIGHTING TO FLASHI NG BEACON TO STROBE LIGHTS TO TAXI LIGHT TO CIGAR LIGHTER WITH FU...

Page 173: ...ical malfunction should occur and cause the circuit breaker to open electrical power to the avionics equipment will be interrupted and the switch will automatically move to the OFF position If this oc...

Page 174: ...anel protect the landing gear system hydraulic pump motor wing de ice system electric elevator trim system and the autopilot pitch and roll actuators All of the avionics circuits are protected by circ...

Page 175: ...se cap Additional lighting is available and includes a strobe light on each wing tip a flashing beacon on top of the vertical stabilizer and two courtesy lights one under each wing just outboard of th...

Page 176: ...e instrument cluster radio equipment and magnetic com pass have integral lighting and operate independently of post or flood lighting The light intensity of instrument cluster magnetic compass and rad...

Page 177: ...aggage compartment light above the baggage area The lights are operated by a slide type switch adjacent to the dome light The most probable cause of a light failure is a burned out bulb however in the...

Page 178: ...HEAD VENTILATORS TYPICAL ADJUSTABLE AFT OVERHEAD VENTILATORS TYPICAL HEATER VALVE FRONT CABIN AIR OUTLET TYPICAL AUXILIARY VENTILATING AIR DOOR AUX CABIN AIR CONTROL CABIN AIR CONTROL LL__ _ CABIN HEA...

Page 179: ...e airplane is equipped with a complete oxygen system refer to Section 9 Supplements for complete details and operating instructions PITOT STATIC SYSTEM AND INSTRUMENTS The pitot static system supplies...

Page 180: ...be confused with indicated altitude To obtain pressure altitude momentarily set the barometric scale on the altimeter to 29 92 and read pressure altitude on the altimeter Be sure to return the altime...

Page 181: ...M OVERBOARD VENT LINE VACUUM RELIEF VALVE DIRECTIONAL INDICATOR SECTION 7 AIRPLANE SYSTEMS DESCRIPTIONS VACUUM PUMP CODE c J INLET AIR 3 VACUUM DISCHARGE AIR t VACUUM SYSTEM AIR FILTER Figure 7 11 Vac...

Page 182: ...ne image and index The directional indicator will precess slightly over a period of time Therefore the compass card should be set in accordance with the magnetic compass just prior to takeoff and occa...

Page 183: ...following paragraphs TRANSMITTER SELECTOR SWITCH A rotary type transmitter selector switch labeled XMTR SEL is provided to connect the microphone to the transmitter the pilot desires to use To select...

Page 184: ...SELECTION SPEAKER 1 2 3 NAV COM ADF AUTO 1 2 3 1 2 0 0 Q 00FF XMTR TRANSMITTER SEL _ PHONE SELECTOR SWITCH AUTOMATIC AUDIO SELECTOR SWITCH AUDIO SELECTOR SWITCH TYPICAL As illustrated the number 1 tr...

Page 185: ...R SWITCHES The audio selector switches labeled NAV COM 1 2 and 3 and ADF 1 and 2 allow the pilot to initially pre tune all NAV COM and ADF receivers and then individually select and listen to any rece...

Page 186: ...frequent FR flights are planned installation of wick type static dischargers is recommended to improve radio communications during flight through dust or various forms of precipitation rain snow or i...

Page 187: ...Care Cessna Customer Care Program Pilot Conducted Preventive Maintenance Alterations Or Repairs Ground Handling Towing Parking Tie Down Jacking Leveling Flyable Storage Servicing Engine Oil Fuel Landi...

Page 188: ......

Page 189: ...r PC and Type Certificate Number TC can be found on the Identification Plate located on the lower part of the left forward doorpost Located adjacent to the Identification Plate is a Finish and Trim Pl...

Page 190: ...Catalog covering all available items many of which he keeps on hand He will be happy to place an order for any item which is not in stock _ _ AIRPLANE FILE There are miscellaneous data information and...

Page 191: ...inspection every 100 hours of operation The FAA may require other inspections by the issuance of airworthi ness directives applicable to the airplane engine propeller and compo nents It is the respon...

Page 192: ...nel accomplish all required FAA inspections and most of the manufacturer recommended inspections CESSNA CUSTOMER CARE PROGRAM Specific benefits and provisions of the CESSNA WARRANTY plus other importa...

Page 193: ...opriately licensed personnel ALTERATIONS OR REPAIRS It is essential that the FAA be contacted prior to any alterations on the airplane to ensure that airworthiness of the airplane is not violated Alte...

Page 194: ...ck points are used in the jacking operation refer to the Service Manual for specific procedures and equipment required Individual main gear may be jacked by using the jack pad whichis incorporated in...

Page 195: ...se periods the propeller should be rotated by hand through five revolutions This action limbers the oil and prevents any accumulation of corrosion on engine cylinder walls I WARNING For maximum safety...

Page 196: ...ions ortests For these regulatory requirements owners should check with local aviation officials where the airplane is being operated For quick and ready reference quantities materials and specifica t...

Page 197: ...on Fuel Blue 100 Formerly 100 130 Grade Aviation Fuel Green CAPACITY EACH TANK 45 Gallons REDUCED CAPA CITY EACH TANK WHEN FILLED TO BOTTOM OF FUEL FILLER NECK 32 5 Gallons LANDING GEAR NOSE WHEEL TIR...

Page 198: ...d since the cover may scratch the plastic surface PAINTED SURFA CES The painted exterior surfaces of your new Cessna have a durable long lasting finish and under normal conditions require no polishing...

Page 199: ...s Never use an alkaline cleaner on the blades remove grease and dirt with carbon tetrachloride or Stoddard solvent LANDING GEAR CARE Cessna Dealer s mechanics have been trained in the proper adjustmen...

Page 200: ...upholstery and carpet ay be cleaned with foam type deter gent used according to the manufacturer s instructions To minimize wetting the fabric keep the foam as dry as possible and remove it with a va...

Page 201: ...a 400 Area Navigation Type RN 478A Cessna 400 ADF Type R 446A Cessna 400 DME Type R 476A Cessna 400 Marker Beacon Type R 402A Cessna 400 Transponder Type RT 459A And Optional 4 pages 2 pages 6 pages 4...

Page 202: ...SECTION 9 SUPPLEMENTS TABLE OF CONTENTS Continued 9 2 Cessna 400B Integrated Flight Control System Type IF 550A Weather Radar Type RDR 160 AM FM Stereo CESSNA MODELT210M 1 pages 10 pages 8 pages...

Page 203: ...ch may be installed in the airplane Each supplement contains a brief description and when applicable operating limitations emergency and normal procedures and performance Other routinely installed ite...

Page 204: ......

Page 205: ...ing the ELT will provide line of sight transmission up to 100 miles at 10 000 feet The ELT supplied in domestic aircraft transmits on both distress frequen cies simultaneously at 75 mw rated power out...

Page 206: ...OVER Removable for access to battery pack 3 ANTENNA RECEPTACLE Connects to antenna mounted on top of tailcone Figure 1 ELT Control Panel SECTION 3 EMERGENCY PROCEDURES Immediately after a forced landi...

Page 207: ...ECTION 4 NORMAL PROCEDURES As long as the function selector switch remains in the AUTO position the ELT automatically activates following an impact of 5g or more over a short period of time Following...

Page 208: ......

Page 209: ...s to the center off position and elevator trim tab motion stops The disengage switch labeled ELEC TRIM DISENGAGE disables the system when placed in the DISENGAGE position The elevator trim circuit bre...

Page 210: ...IRED SECTION 4 NORMAL PROCEDURES To operate the electric elevator trim system proceed as follows 1 Master Switch ON 2 Elevator Trim Disengage Switch ON 3 Trim Switch ACTUATE as desired 4 Elevator Trim...

Page 211: ...e consoles near the aft passenger seats One permanent microphone equipped mask is provided for the pilot and five disposable type masks are provided for the passengers All masks are the partial rebrea...

Page 212: ...the system is completely automatic and requires no manual regulation for change of altitude The oxygen cylinders when fully charged contain a total of approxi mately 74 cubic feet of aviator s breathi...

Page 213: ...a pilot with a red color coded oxygen line foting and passengers with orange color coded line fittings Figure 2 Oxygen Duration Chart 9 For FAA requirements concerning supplemental oxygen refer to FA...

Page 214: ...1400 PSI of pressure will safely sustain the pilot only for 6 hours and 20 minutes The same pressure will sustain the pilot and three passengers for approxi mately 2 hours and 10 minutes NOTE The Oxyg...

Page 215: ...ECT Adjust mask to face and adjust metallic nose strap for snug mask fit 2 Delivery Hose PLUG INTO OUTLET nearest to the seat you are occupying NOTE When the oxygen system is turned on oxygen will flo...

Page 216: ......

Page 217: ...initiated and remain on for two to three seconds if the system is operating properly De icing boots have a special electrically conductive coating to bleed off static electricity which causes radio i...

Page 218: ...lation with one or two cycles of operation Do not repeat de icing procedure until ice has again accumu lated Cycling the de icing boots produces no adverse aerodynamic effects in any attitude within t...

Page 219: ...light into known or forecast icing conditions is prohibited If unex pected icing conditions are encountered the following procedure is recom mended 1 Ice Build Up MONITOR until approximately 1 2 inch...

Page 220: ......

Page 221: ...ents in the anti icing boots located on the propeller blades Operation of the anti ice system can be checked by monitoring a propeller anti ice ammeter near the upper left corner of the instrument pan...

Page 222: ...ntary change NOTE While using the anti ice system monitor the airplane ammeter to ensure that the electrical system does not become overloaded If the total electrical load is high resulting in a disch...

Page 223: ...be stowed in the seat pocket on the aft side of the pilot s or co pilot s seat back Windshield anti icing is controlled by a rocker type switch labeled W S A ICE on the left switch and control panel T...

Page 224: ...ration of the heated anti icing panel without the engine running may cause damage to the panel and crazing of the windshield Flight into known or forecast icing conditions is prohibited If unex pected...

Page 225: ...receiver transmitter or a glide slope receiver or both may be interconnected with the Nav Com set for automatic selection of the associated DME or glide slope frequency When a VOR frequency is selecte...

Page 226: ...s Com frequency readout to display and Com Fractional MHz Selector to select frequency in 05 MHz steps between 025 and 975 MHz In O position enables COM frequency readout to display and Com Fractional...

Page 227: ...ses squelch action counterclockwise rotation decreases background noise COMMUNICATION RECEIVER TRANSMITTER MEGAHERTZ SELECTOR Selects COM frequency in 1 MHz steps between 118 and 135 MHz COM OFF VOL C...

Page 228: ...course card to center course deviation pointer with a TO flag then returns to conventional OBS selection Pulled to outer detent continuously drives OBS course card to indicate bearing from VOR statio...

Page 229: ...ENCY PROCEDURES There is no change to the airplane emergency procedures when this avionic equipment is installed However if the frequency readouts fail the radio will remain operational on the last fr...

Page 230: ...UST to desired audio level ID VOX T Switch a To Identify Station SET to ID to hear navigation station identifier signal b To Filter Out Station Identifier Signal SET to VOX to include filter in audio...

Page 231: ...OM ID VOX T Switch PRESS to T and HOLD at T course deviation pointer centers and NAV TO FROM indicator shows FROM OBS Knob TURN to displace course approximately 10 to either side of 0 while holding ID...

Page 232: ......

Page 233: ...tion Operating informa tion for the communication set and for VOR localizer navigation is presented in this supplement Operating information for area navigatfon and for DME is presented in separate su...

Page 234: ...In 5 position enables COM frequency readout to display and COM Fractional MHz Selector to select frequency in 05 MHz steps between 025 and 975 MHz In O position enables COM frequency readout to displ...

Page 235: ...L Used to adjust signal threshold necessary to activate COM receiver audio Clockwise rotation increases background noise decreases squelch action counterclockwise rotation decreases background noise 1...

Page 236: ...OFF position flag indicates unusable signal With usable VOR signal when OFF position disappears indicates whether selected course is TO or FROM station or waypoint With usable localizer signal shows T...

Page 237: ...s and indicators are shown and described in Figure 1 Operating controls for the RN 478A Area Navigation Computer which are used for area navigation and operating controls for the associated Type R 476...

Page 238: ...tone may be selected by placing the AUTO selector switch on audio control panel in either the SPEAKER or PHONE position Adjustment of sidetone may be accomp lished by adjusting the sidetone pot locate...

Page 239: ...nob TURN to displace course approximately 10 to either side of0 while holding ID VOX T switch at T CDI pointer should deflect full scale in direction corresponding to course displace ment OFF TO FROM...

Page 240: ......

Page 241: ...bed in Figure 1 The Cessna 300 ADF can be used for position plotting and homing procedures and for aural reception of amplitude modulated AM signals With the function selector knob at ADF the Cessna 3...

Page 242: ...ise rotation from OFF position applies primary power to receiver further clockwise rotation increases audio level 2 FREQUENCY SELECTORS Knob A selects 100 kHz incre ments of receiver frequency knob B...

Page 243: ...tary on position used during ADF operation to test bearing reliability When held in TEST position slews indicator pointer clockwise when released if bearing is r eliable pointer returns to original be...

Page 244: ...osition as desired 5 VOL Control ADJUST to desired listening level TO OPERATE AS AN AUTOMATIC DIRECTION FINDER 1 OFF VOL Control ON 2 Frequency Selector Knobs SELECT operating frequency 3 ADF SPEAKER...

Page 245: ...hone position 5 VOL Control ADJUST to desired listening level NOTE A 1000 Hz tone is heard in the audio output when a CW signal Morse Code is tuned in properly SECTION 5 PERFORMANCE There is no change...

Page 246: ......

Page 247: ...iated wiring The Channel Selector Knob determines the operating frequency of the transmitter and receiver The frequencies of operation are shown on the frequency chart adjacent to the channel selector...

Page 248: ...s listed in the frequency chart 3 CHANNEL READOUT WINDOW Displays channel selected in frequency chart 4 SENSITIVITY CONTROL Controls the receiver sensitivity for audio gain 5 ANTENNA TUNING METER Indi...

Page 249: ...ing level Frequency Chart SELECT desired operating frequency Channel Selector c DIAL in frequency selected in step 4 SENSITIVITY Control ROTATE clockwise to maximum posi tion NOTE If receiver becomes...

Page 250: ...T SECTION 5 PERFORMANCE There is no change to the airplane performance when this avionic equipment is installed However the installation of an externally mounted antenna or several related external an...

Page 251: ...hannel selector knob determines the operating frequency of the transceiver which has predetermined crystals installed to provide the desired operating frequencies A mode selector control is provided t...

Page 252: ...pondence telephone and ship to shore LSE Optional Selects lower sideband operation not legal in U S Canada and most other countries 4 SQUELCH CONTROL Used to adjust signal threshold necessary to activ...

Page 253: ...EDURES There is no change to the airplani emergency procedures when this avionic equipment is installed SECTION 4 NORMAL PROCEDURES COMMUNICATIONS TRANSCEIVER OPERATION 1 2 3 4 5 6 7 XMTR SEL Switch S...

Page 254: ...b To Receive RELEASE mike button NOTE Voice communications are not available in the LSB mode NOTE Lower sideband LSB mode is not legal in the U S Canada and most other countries SECTION 5 PERFORMANCE...

Page 255: ...ve voltage prevents loss of the preset frequencies when the Nav Com is turned off Both the communications and navigation operating frequen cies are digitally displayed by incandescent readouts on the...

Page 256: ...SECTION 2 LIMITATIONS There is no change to the airplane limitations when this avionic equipment is installed However the pilot should be aware that on many Cessna airplanes equipped with the windshie...

Page 257: ...ERATING HANDBOOK SUPPLEMENT CESSNA 400 NAV COM TYPE RT 485A TYPICAL 300 SERIES INDICATORS TYPICAL 400 SERIES INDICATORS Figure 1 Cessna 400 Nav Com Type RT 485A Operating Controls and Indicators Sheet...

Page 258: ...tion by holding C pushbutton pressed for more than 1 7 seconds This lights each COM and NAV MEMORY pushbutton in turn and displays the corresponding preset frequency in MEMORY 4 NAVIGATION OPERATING F...

Page 259: ...nd the reverse sense switch or autopilot s back course function is engaged and receiver is tuned to a localizer frequency indicates course deviation pointer is reversed 15 COURSE INDEX Indicates selec...

Page 260: ...ber light illuminates when Automatic Radial Centering is in use 23 COURSE CARD Indicates selected VOR course under course index 24 OMNI BEARING SELECTOR OBS Rotates course card to select desired cours...

Page 261: ...s while selecting fractional frequencies or you will activate the MEMORY test function 4 MEMORY 2 and 3 Pushbuttons REPEAT STEPS 2 and 3 using next desired NAV or COM MEMORY to be stored Up to 3 NAV a...

Page 262: ...Frequency Selection SELECT desired operating frequency by either pressing a NAV MEMORY 1 2 or 3 pushbutton to recall a preset frequency or by using NAV frequency selectors 4 NAV VOL Control ADJUST to...

Page 263: ...LF TEST OPERATION 1 2 3 4 5 6 COM OFF VOL Control TURN ON NAV Frequency Selector Switches SELECT usable VOR station signal OBS Knob SET for 0 course at course index course deviation pointer centers or...

Page 264: ...ays start with the last COM MEMORY selected and cycle through the remaining COM and NAV preset frequencies The MEMORY test will always stop on the last selected COM and NAV preset frequencies SECTION...

Page 265: ...OR localizer navigation is presented in this supplement Operating information for area naviga tion and for DME is presented in separate supplements Microprocessor frequency management provides storage...

Page 266: ...ptional IN 1048AC Course Deviation Indicator is installed an Automatic Radial Centering lamp ARC is incorporated in the CDI to alert the pilot that the Automatic Radial Centering feature has been sele...

Page 267: ...ncies may be stored in MEMORY and selected as desired by merely pressing the appropriate COM MEMORY pushbutton to recall the desired operating frequency If electrical power to the set s keep alive cir...

Page 268: ...t s keep alive circuit has not been interrupted upon turn on the set will automatically recall the last NAV MEMORY frequency selected by the MEMORY pushbutton If electrical power is removed from the s...

Page 269: ...TION POINTER Indicates course deviation from selected VOR or RNAV course or localizer centerline 20 OFF TO FROM INDICATOR Operates only with VOR or localizer signal OFF position flag indicates unusabl...

Page 270: ...able 4OR or localizer signal When white flag is in view indicates whether selected course is TO or FROM station With usable localizer signal shows TO 25 AUTOMATIC RADIAL CENTERING ARC LAMP Amber light...

Page 271: ...COM pushbut ton 1 momentarily to alert the memory bank of a forthcoming frequency to be stored 3 FREQUENCY SELECTORS MANUALLY ROTATE correspond ing NAV or COM frequency selectors press C pushbutton as...

Page 272: ...ng the AUTO selector switch on audio control panel in either the SPEAKER or PHONE position Adjustment of sidetone may be accomp lished by adjusting the sidetone pot located inside the audio control pa...

Page 273: ...ive to present the VOR radial the aircraft is on until manually returned to the center detent by the pilot AP CPLD Annunciator CHECK ON if 400B or 400B IFCS autopilot is engaged amber light illuminate...

Page 274: ...reset frequency displayed NOTE If the keep alive circuit has not been interrupted the MEMORY test will always start with the last COM MEMORY selected and cycle through the remaining COM and NAV preset...

Page 275: ...stable waypoint information which enhances autopilot operation The 400 RNAV is coupled to the number 2 Nav Com and includes storage for 3 waypoints Ground speed time to station information to the sele...

Page 276: ...NCE DISPLAY READOUT Depending on position of DSPL Switch displays distance programmed for waypoint 1 or waypoint 2 6 BEARING MINILEVER SWITCHES 4 Select bearing of desired waypoint from VOR DME statio...

Page 277: ...nic equipment is installed SECTION 4 NORMAL PROCEDURES VOR LOC OPERATION VOR NAVIGATION CIRCUITS VERIFICATION TESTS 1 See appropriate Nav Com supplement VOR LOC NAVIGATION As a convenience to the pilo...

Page 278: ...not those being used for navigation This does not affect operation of the unit 6 BEARING Minilever Switches SET to first waypoint bearing 7 DISTANCE Minilever Switches SET to first waypoint distance...

Page 279: ...ntrol Head FLASHES 3 RNAV DSPL and FLY Switches DSPL set to 2 FLY set to 1 a Readout DISPLAYS second waypoint bearing and distance b Fly Display Lamp On RNAV Control Head FLASHES 4 RNAV DSPL and FLY S...

Page 280: ...be tested a BEARING Display READOUT is waypoint bearing b DISTANCE Display READOUT is waypoint distance c Course Indicator RN LAMP lights 7 Course Indicator OBS or ARC SET to waypoint bearing 8 VHF N...

Page 281: ...ront panel The goniometer indicator presents station bearing in degrees of azimuth An automatic pointer stow feature alerts the operator to non ADF operation by slewing the pointer to the 3 00 o clock...

Page 282: ...CESSNA 400 ADF TYPE R 446A PILOT S OPERATING HANDBOOK SUPPLEMENT Figure 1 Cessna 400 ADF Operating Controls and Indicator Sheet 1 of 2 2...

Page 283: ...signals Morse Code to be heard 7 REC Pushed in Selects receive mode set operates as a standard communica tions receiver using sense antenna only NOTE In this position an automatic pointer stow featur...

Page 284: ...l ON 2 REC Pushbutton PUSH in NOTE ADF indicator pointer will stow at a 90 degree position to alert the pilot to non ADF operation 3 PRI Frequency Selectors SELECT desired operating frequency 4 SEC Fr...

Page 285: ...dicates relative magnetic or true bearing to station 8 VOL Control ADJUST to desired listening level NOTE When switching stations place function pushbutton in the REC position Then after station has b...

Page 286: ...d listening level NOTE A 1000 Hz tone is heard in the audio outputwhen CW signal Morse Code is tuned in properly SECTION 5 PERFORMANCE There is no change to the airplane performance when this avionic...

Page 287: ...tains all of the operating controls and displays and a remotely mounted RTA 476A Receiver Transmitter The RTA 476A transmits interrogating pulse pairs on 200 channels between 1041 MHz and 1150 MHz it...

Page 288: ...ound speed 3 DME MODE SELECTOR SWITCH Selects DME operating mode as follows RNAV Selects area navigation operation selects display of nautical miles distance to selected RNAV waypoint NAV 1 Selects DM...

Page 289: ...s as follows a With GS TTS Switch set to GS displays ground speedcomponenttoorfrom station in knots aircraft must be flying directly to or from the VOR DME station for true ground speed indication b W...

Page 290: ...d Therefore the sys tem does not provide independent operation ofthe DME for reception of the DME Morse Code identifier 4 GS TTS Switch SET as desired 5 TEST ON OFF Switch HOLD to TEST a Distance to S...

Page 291: ...ection On 152 series airplanes a HI LO sensitivity selector switch is provided with a separate press to test button This system provides visual and aural indications of 75 MHz ILS marker beacon signal...

Page 292: ...PERATING HANDBOOK TYPE R 402A SUPPLEMENT TYPICAL INSTALLATION ON ALL 152 MODEL SERIES TYPICAL INSTALLATION ON ALL MODELS EXCEPT 152 MODEL SERIES Figure 1 Cessna 400 Marker Beacon Operating Controls an...

Page 293: ...In the LO position Up receiver sensitivity is positioned for LS approaches In the HI position Down receiver sensitivity is positioned for airway flying 5 SPEAKER PHONE SWITCH Selects speaker or phone...

Page 294: ...sired listening level 2 LO HI SENS Switch SELECT HI position for airway flying or LO position for ILS approaches 3 SPKR PHONE Switch SELECT speaker or phone audio 4 TEST Switch PRESS and ensure that m...

Page 295: ...ting pulse signals on 1030 MHz and transmits coded pulse train reply signals on 1090 MHz It is capable of replying to Mode A aircraft identification and Mode C altitude reporting interrogations on a s...

Page 296: ...CESSNA 400 TRANSPONDER AND ENCODING ALTIMETER PILOT S OPERATING HANDBOOK SUPPLEMENT Figure 1 Cessna 400 Transponder and Encoding Altimeter Operating Controls Sheet 1 of 2 2...

Page 297: ...transponder to gen erate a self interrogating signa l to provide a check of transponder operation Reply Lamp will glow steadily to verify self test operation 6 REPLY CODE SELECTOR SWITCHES 4 Select a...

Page 298: ...ontroller s display TO TRANSMIT A SIGNAL REPRESENTING LOSS OF ALL COMMUNICATIONS WHEN IN A CO TROLLED ENVIRONMENT 1 Function Switch ON 2 Reply Code Selector Switches SELECT 7700 operating code for 1 m...

Page 299: ...on encoding altimeter 2 Altitude Encoder Altimeter Setting Knob SET IN assigned local altimeter setting 3 Reply Code Selector Switches SELECT assigned code 4 Function Switch ALT NOTE When directed by...

Page 300: ...ht with full brilliance regardless of DIM control setting 4 TEST Button RELEASE for normal operation SECTION 5 PERFORMANCE There is no change to the airplane performance when this avionic equipment is...

Page 301: ...r frequenc y is selected on the NAV receiver the associated glide slope frequenc y is selected automati cally Operation of the Cessna 400 Glide Slope system is controlled by the associated navigation...

Page 302: ...equipment The flag disappears when a re liable glide slope signal is being received Spurious glide slope signals may exist in the area of the localizer back course approach which can cause the glide...

Page 303: ...equency Select Knobs SELECT desired localizer frequency glide slope frequency is automatically selected 2 NAV COM ID T Switch SELECT ID position to disconnect filter from audio circuit 3 NAV VOL Contr...

Page 304: ......

Page 305: ...m radios When dual Nav Com radios are installed the HSI is coupled to the number 1NAV COM and a standard 300 or 400 series VOR LOC course deviation indicator is coupled to the number 2 NAV COM This sy...

Page 306: ...also displays glide slope deviations and gives heading reference with respect to magnetic north when compass card is set to agree with compass 2 OMNI BEARING POINTER Indicates selected VOR course or l...

Page 307: ...ted sets compass card 6 to agree with magnetic compass The omni bearing pointer 2 heading bug 14 and deviation bar 15 rotate with the compass card 6 NOTE The compass card 6 must be reset periodically...

Page 308: ...o the autopilot to reverse for back course operation 17 BACK COURSE REVERSE SENSE REV SNS LOC 1 OR LOC 2 SELECTOR SWITCH With AP switch ON on 400A or 400B Autopilot control units and either LOC 1 or L...

Page 309: ...aches to retain this pictorial presentation When the HSI system is installed with a Cessna 300A Type AF 395A Cessna 400A Type AF 530A or Cessna 400B Type IF 550A Autopilot a back course indicator ligh...

Page 310: ......

Page 311: ...orizontal Situation Indicator HSI a SA 832A remote slaving accessory without course datum or an alternate SA 832B with course datum and a remote VOR LOC converter which is only installed without a RNA...

Page 312: ...and localizer beams It also displays glide slope deviations and gives heading reference with respect to magnetic north 2 OMNI BEARING POINTER Indicates selected VOR course or localizer course on comp...

Page 313: ...ET Positions heading bug on compass card 16 by rotating the PUSH A CARD SET knob Pushing in and rotating the PUSH A CARD SET knob sets the compass card The bug 7 rotates with the compass card 10 11 12...

Page 314: ...everse However selection of back course opera tion will always cause the localizer signal to the autopilot to reverse for back course operation 18 BACK COURSE REVERSE SENSE REV SNS LOC 1 OR LOC 2 SELE...

Page 315: ...pilot or Cessna 400B Type IF 550A Autopilot a back course indica tor light labeled BC is mounted adjacent to the HSI and will illuminate amber when the reverse sense REV SNS switch mounted in upper po...

Page 316: ......

Page 317: ...itude alerter Type AA 801A is an accessory unit used with the Cessna 800 encoding altimeter to supply a preselected altitude capture signal to arm the altitude hold function of the Integrated Flight C...

Page 318: ...de alerter are shown in Figure 2 The altitude capture function is selected by a white pushbutton switch ARM which energizes the preselector logic circuits For altitude capture function operation the I...

Page 319: ...ppears in 10 000 foot window 3 ZERO TO THOUSAND FOOT ALTITUDE DISPLAY DIAL Calibrated in 10 numerical graduations which represent increments of 100 feet the subdivisions of each graduation represent i...

Page 320: ...gaged remains lighted until altitude is captured CPLD Green Lamp Lights when airplane reaches selected altitude and Integrated Flight Control System altitude hold mode is automatically engaged 3 ALTIT...

Page 321: ...METER OPERATION r 1 Baroset Knob TURN as necessary to set readout to local altimeter setting 2 Power off Warning Flag VERIFY that flag is not in view I WARNING I Do not attempt to use altimeter indica...

Page 322: ...ea level and pressure presents a below 100 foot situation then preset lowest obtainable altitude above 100 feet on altimeter and perform the upper range of the test specified in steps 5 and 6 Followin...

Page 323: ...ght 6 Turn baroset knob to reset altimeter as required 7 Turn off power switches Power off warning flag appears and all indicator lamps go out ALTITUDE CAPTURE OPERATING NOTES CAUTION The altitude ale...

Page 324: ...e is being held 4 If the altitude hold is manually selected on the flight directormode selector prior to automatic altitude capture the ARMD lamp will go out the CPLD lamp will not light and the captu...

Page 325: ...turn coordina tor gyro The computer amplifier electronically computes the necessary correction and signals the actuator to move the ailerons to maintain the airplane in the commanded lateral attitude...

Page 326: ...PILOT TYPE AF 295B NAV 1 NAV 2 CDI INDICATORS TURN COORDINATOR PILOT S OPERATING HANDBOOK SUPPLEMENT AILERON ACTUATOR COMPUTER AMPLIFIER Figure 1 Cessna 200A Autopilot Operating Controls and Indicator...

Page 327: ...itivity position push button out response to NAV signal is dampened for smoother tracking of enroute VOR r adials it also smooths out effect of course scalloping during NAV opera tion 8 BACK CRS PUSHB...

Page 328: ...itch OFF SECTION 3 EMERGENCY PROCEDURES TO OVERRIDE THE AUTOPILOT 1 Airplane Control Wheel ROTATE as required to override autopi lot NOTE The servo may be overpowered at anytime without dam age TO TUR...

Page 329: ...0 185 U206 and TU206 Series Models COMMAND TURNS 1 PULL TURN Knob CENTER PULL out and ROTATE DIRECTION HOLD 1 PULL TURN Knob CENTER and PULL out 2 Autopilot TRIM Control ADJUST for zero turn rate 3 Ai...

Page 330: ...e station or more than 3 minutes from intercept use a manual intercept procedure NAV TRACKING VOR LOC 1 NAV TRK Button PUSH when CDI centers and airplane is within 5 of course heading 2 HI SENS BUTTON...

Page 331: ...cted heading are sensed by the direction al gyro The computer amplifier electronically computes the necessary correction and signals the actuator to move the ailerons to maintain the airplane in the c...

Page 332: ...LOT TYPE AF 395A NAV 1 NAV 2 CDI INDICATORS 2 TURN COORDINATOR PILOT S OPERATING HANDBOOK SUPPLEMENT AILERON j_ I I I I COMPUTER AMPLIFIER Figure 1 Cessna 300A Autopilot Operating Controls and Indicat...

Page 333: ...to NAV signal to provide more precise operation during localizer approach In low sensitivity position push button out response to NAV signal is dampened for smoother tracking of enroute VOR radials it...

Page 334: ...ch OFF SECTION 3 EMERGENCY PROCEDURES TO OVERRIDE THE AUTOPILOT 1 Airplane Control Wheel ROTATE as required to override autopi lot NOTE The servo may be overpowered at any time without dam age TO TURN...

Page 335: ...S on 180 185 U206 and TU206 Series Models COMMAND TURNS 1 PULL TURN Knob CENTER PULL out and ROTATE HEADING SELECT 1 Directional Gyro SET to airplane magnetic heading 2 Heading Selector Knob ROTATE bu...

Page 336: ...y selected the CDI on selected nav radio will be reversed even when the autopilot switch is OFF 9 PULL TURN Knob PUSH NOTE Airplane will automatically turn to a 45 intercept angle NAV TRACKING VOR LOC...

Page 337: ...00 autopilot system consist of a control unit mounted in either the lower center stack of the instrument panel or lower console a panel mounted vacuum driven unslaved direc tional gyro and an aileron...

Page 338: ...CESSNA 400 AUTOPILOT TYPE AF 420A A P NAY 1 PILOT S OPERATING HANDBOOK SUPPLEMENT 19 Figure 1 Cessna 400 Autopilot Type AF 420A Sheet 1 of 3 2...

Page 339: ...e PITCH control from level flight detent disen gages the altitude hold circuit LATERAL TRIM Used when PULL TURN control knob is pulled out and in detent to trim aircraft for wing level attitude AIRCRA...

Page 340: ...visual indication of aircraft heading and also provides electrical heading infor mation to the autopilot The slaved DG eliminates the need to manually compen sate for precessional errors in the gyro...

Page 341: ...le Altitude Loss with Autopilot Malfunction REFER to Autopilot Limitations Placard on instrument panel of airplane SECTION 3 EMERGENCY PROCEDURES IN CASE OF AUTOPILOT MALFUNCTION 1 Airplane Control Wh...

Page 342: ...h ALT ON COMMAND TURNS 1 PULL TURN Knob PULL and ROTATE CLIMB OR DESCENT 1 Aircraft Power and Trim ADJUST 2 PITCH Control Wheel Rotate UP or DOWN 3 Lateral Trim Lever ADJUST to level wings 4 PITCH Tri...

Page 343: ...CDI 5 Function Switch SET to OMNI INTERCEPT 6 PULL TURN Knob PUSH NOTE Airplane will automatically intercept at 45 and then track the selected omni course 7 Function Switch SET to TRK for VOR station...

Page 344: ......

Page 345: ...y side in the lower center stack of the instrument panel a panel mounted vacuum driven unslaved directional gyro and an attitude gyro a remote mounted acceleration sensor with a built in G switch an a...

Page 346: ...airplane pitches down at more than a normal rate from normal flight attitude The operational capability of the disengage function should be tested before takeoff by pressing the TEST EA FLT button loc...

Page 347: ...rse operation for either autopilot or manual flight Except when a horizontal situation indicator is installed selecting back course REV SNS LOC 1 LOC 2 causes reversal of the Course Deviation Indicato...

Page 348: ...TING HANDBOOK SUPPLEMENT 4 CONTROL UNIT G 519A 1 HORIZON GYRO G 502A NON SLAVED DG STANDARD NON SLAVED Y G 519A 1 HORIZON GYRO IG 832C NON SLAVED HSI OPTIONAL NON SLAVED GYRO SYSTEM Figure 1 Cessna 40...

Page 349: ...AUTOPILOT TYPE AF 550A G 519A 1 HORIZON GYRO G 504A SLAVED DG OPTIONAL SLAVED GYRO SYSTEM G 519A 1 HORIZON GYRO IG 832A SLAVED HSI OPTIONAL SLAVED GYRO SYSTEM CONTROL WHEEL SWITCHES Figure 1 Cessna 40...

Page 350: ...flight the altitude control will smoothly level the _ airplane and return it to the altitude existing when ALT hold switch was pressed __ 6 8 ACCESSORY UNIT Provides the pilot w ith an automatic autop...

Page 351: ...titude 15 SYMBOLIC AIRCRAFT Serves as a stationary symbol of the aircraft Aircraft pitch and roll attitudes are displayed by the relationship between the fixed symbolic aircraft and the movable backgr...

Page 352: ...red gyro speed being low 28 NAV FLAG Flag is in view when the NAV receiver signal is inadequate 29 COURSE DEVIATION BAR Bar is center portion of omni bearing pointer and moves laterally to pictorially...

Page 353: ...installed with a 300 Series Radio or 400 Series Radios without course datum 40 SLAVING OFF WARNING FLAG When out ofview indicates adequate slaving voltage When in view indicates absent or low slaving...

Page 354: ...anual overpower 2 AUTOPILOT DISENGAGE Switch on Control Wheel PULL OFF NOTE This action automatically trips autopilot ON OFF switch OFF If electrical malfunction still persists turn avionics power swi...

Page 355: ...ker Switch PUSH OFF 2 REV SNS LOC 1 LOC 2 Switch on Autopilot Accessory Unit OFF IN FLIGHT WINGS LEVELING 1 Airplane Elevator and Rudder Trim ADJUST 2 PULL TURN Knob CENTER and PULL OUT 3 AP ON OFF RO...

Page 356: ...ULL OUT 2 APNAV 1 NAV2SelectorSwitch onAutopilotAccessoryUnit SET to desired VOR receiver 3 Nav Indicator OBS or Course Selector Knob on HSI SET VOR course 4 HDG Knob on DG or CARD SET Knob on HSI 300...

Page 357: ...e Deviation Indicator When the optional Horizontal Situation Indicator is installed operation of the HSI needle is unaffected by the selection of LOC 1 or LOC 2 However selection of LOC 1 or LOC 2 cor...

Page 358: ...approach only 15 Landing Gear EXTEND by outer marker NOTE Airspeed should be reduced to 115 KIAS prior to operation of the gear if operating in the altitude hold mode 16 AUTOPILOT DISENGAGE SWITCH on...

Page 359: ...ies the airplane to center the two command bars to follow the calculated flight path determined by the computer In this way climbs descents or turns are easily and accurately executed A Horizontal Sit...

Page 360: ...al in either the roll or pitch actuators the thermostatic switch opens and disengages the autopilot to remove power from the actuator After approximately 10 minutes the switch automatically resets to...

Page 361: ...PILOT S OPERATING HANDBOOK SUPPLEMENT CESSNA 400B IFCS TYPE IF 550A Figure 1 Cessna 400B IFCS Type IF 550A Sheet 1 of 6 3...

Page 362: ...ht R or left L When turned disconnects heading HDG or navigation NAV modes selected on Mode Selector 4 LATERAL TRIM CONTROL TRIM When TURN knob is centered with no lateral modes engaged and the airpla...

Page 363: ...led to the Integrated Flight Control System by pressing the NAV 1 NAV 2 pushbutton The NAV 1 NAV 2 annunciator will illuminate green to show NAV 1 when engaged By pressing NAV 1 NAV 2 a second time th...

Page 364: ...ontal Situation Indicator HSI A new heading may be selected at anytime and will result in airplane turning to new heading with maximum bank angle of 25 HDG mode will cancel GA mode and HDG annunciator...

Page 365: ...G BUG Indicates selected heading relative to the compass card 40 32 TO FROM INDICATOR FLAG Indicates direction of VOR station relative to selected course 33 HEADING SELECTOR AND CARD SET KNOB PUSH CAR...

Page 366: ...removes all electrical power from the system Autopilot will remain OFF until primary AP ON OFF switch is turned ON even though the switch is spring loaded to return to ON when released The AUTOPILOT D...

Page 367: ...Mode Maximum Speed for Flap and Gear Operation 115 KIAS SECTION 3 EMERGENCY PROCEDURES IN CASE OF AUTOPILOT MALFUNCTION 1 Airplane Control Wheel OPERATE as required to manually override the autopilot...

Page 368: ...lector e Airplane Control Wheel HOLD to reduce movement f Autopilot Disconnect TEST Prior To EA FLT Button PUSH and HOLD g Verify the following 1 Flight Director Indicator OBSERVE command bars are vis...

Page 369: ...autopilot ON OFF switch must be engaged for a short time maximum of 30 seconds before the ALT switch can be engaged COMMAND TURNS 1 TURN Knob ROTATE as desired CLIMB OR DESCENT 1 ALT Rocker Switch DI...

Page 370: ...ADJUST to approach speed 95 to 115 KIAS 3 Rudder Trim ADJUST as required 4 MODE SELECTOR NAV 1 NAV 2 Button PUSH for NAV 1 receiver 12 5 MODE SELECTOR NAV 1 NAV 2 Annunciator CHECK correct NAV ON gree...

Page 371: ...mode 15 AUTOPILOT DISENGAGE Switch Control Wheel OFF before landing or extending flaps more than 10 16 Wing Flaps EXTEND as REQUIRED after landing is assured MISSED APPROACH 1 Control Wheel GA Switch...

Page 372: ...ECTOR FD Button PUSH ON and observe that command bars appear on FD Indicator 3 MODE SELECTOR FD Annunciator CHECK ON green light illuminated NOTE If pitch command bar is not aligned in pitch with the...

Page 373: ...d HSI Course Selector Knob or OBS on CDI SET desi red VOR course MODE SELECTOR NAV Button PUSH MODE SELECTOR NAV Annunciator CHECK ON green light illuminated Control Wheel OPERATE as necessary to sati...

Page 374: ...r ALT engaged is not required to capture glide slope 12 MODE SELECTOR ALT Button OFF at final approach fix if localizer approach only Use pitch trim wheel to establish proper command attitude 13 Contr...

Page 375: ...SUPPLEMENT CESSNA 400B IFCS TYPE IF 550A 8 Control Wheel OPERATE as necessary to satisfy command signals SECTION 5 PERFORMANCE There is no change to the airplane performance when this avionic equipmen...

Page 376: ...i...

Page 377: ...tration of heavy weather and its usually associated turbulence Internally generated range marks appear as evenly spaced concentric circular arcs on the display to assist in determining distance from w...

Page 378: ...determine operability of system Energizes Transmitter Selects 5 nautical mile range presentation with 1 mile range marks Energizes Transmitter Selects 10 nautical mile range presentation with 2 mile r...

Page 379: ...second If a dark hole remains the same intensity while in the WxA mode then this area of the display does not represent a contour or storm cell 3 ANTENNA TILT CONTROL Electronically adjusts the radar...

Page 380: ...h positions Function Switch Position TEST 5 10 20 40 80 160 Mode Selector Switch Position MAP GAIN Wx WxA Range Range Mks Spacing 40 10 5 1 10 2 20 4 40 10 80 20 160 40 Mode Readout MAP Wx WxA Footnot...

Page 381: ...e radiation and improper use or exposure may cause serious bodily injury DO NOT OPERATE THIS EQUIPMENT UNTIL YOU HAVE READ AND CAREFULLY FOLLOWED THE FOLLOWING SAFETY PRECAUTIONS AND INSTRUC TIONS SAF...

Page 382: ...ding band small to appear on units with a five band display and not appear on units with a four band display The four and five band displays are as follows Nearest is light shading appears on five ban...

Page 383: ...alphanumeric area of the display TILT Control 4 to minimize ground return BRT Control ADJUST as required Antenna Tilt Control TILT UP degrees and DOWN degrees in small increments Close in ground targe...

Page 384: ...DJUST as required for ambient light conditions 4 Antenna Tilt Control 4 to 6 approximate minimum angle relative to horizon without ground return NOTE If airplane is climbing or descending tilt angles...

Page 385: ...T as required 4 Antenna Tilt Control ADJUST for clearest display SECTION 5 PERFORMANCE There is a slight reduction in cruise speed performance with the radar pod installed which varies from approximat...

Page 386: ......

Page 387: ...playback with a tape speed of 4 76 cm sec Any standard size monural or stereo cassette may be used in the player Cassettes are automatically activated when inserted in tape receptacle with tape play s...

Page 388: ...CASSETTE AM FM STEREO TYPE C 114A PILOT S OPERATING HANDBOOK SUPPLEMENT Figure 1 Cassette Player AM FM Radio Operating Controls Sheet 1 of 3 2...

Page 389: ...e as desired 7 TAPE RECEPTACLE Insert cassette with tape play side to the right Top numbered side will play Either monural or stereo standard cassettes may be used 8 TAPE EJECT AND FAST FORWARD PUSHBU...

Page 390: ...nes with 1 4 inch stereo type plugs 15 EARPHONE IDENTIFICATION MONOGRAMS L R Located on left L and right R earphones Audio in left or cord earphone is regulated by LEFT lever on Headphone VOLUME CONTR...

Page 391: ...phone Extension Adjustment Levers ADJUST to comforta ble listening position 3 Stereo Mono Selector Switch SELECT desired monural AM or stereo FM position on Headphone VOLUME CONTROL Box 4 Headphone LE...

Page 392: ...Control ADJUST to desired audio setting CASSETTE PLAYER OPERATION 6 1 Tape Receptacle INSERT CASSETTE with tape play side to right and adjust listening controls on unit and headphones Player will play...

Page 393: ...alfway and release c To Cancel Fast Forward RELEASE BUTTON or if in lock position PUSH BUTTON in slightly and release SECTION 5 PERFORMANCE There is no change to the airplane performance when this avi...

Page 394: ...__ f...

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