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Textron Cessna 172S Skyhawk SP Information Manual

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Page 2 CESSNA INTRODUCTION. ' D r MODEL 172S NOTICE AT tHE TIME OF ISSUANCE, THIS INFORMATION MANUAL WAS AN' EXACT DUPLICATE OF. THE OFFICIAL PILOT'S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE, FLIGHT MANUAL AND ISTO BE USED FOR GENERAL PURPOSES ONLY. WILL .
Page 3 CESSNA INTRODUCTION MODEL 172S PERFORMANCE - SPECIFICATIONS " 'SPEED: 126 KNOTS Maximum at Sea Level" " , , ' 124 KNOTS- Cruise, 75%'Power at 8500 Feet. ' :' CRUISE: Recommended lean mixture with fuel allowance for' engine start, taxi, takeoff, climb and 45 minutes reserve. 75%' Power at 8500 Feet.
Page 4 14.7 POWER lOADING: lbs/HP 14.2 FUEL CAPACITY 56 GAllONS Oil CAPACITY 8 QUARTS ENGINE: Textron lycoming IO-360-l2A 180 BHP at 2700 RPM PROPEllER: Fixed Pitch, Diameter 76 INCHES NOTE 'Speed performance is shown for an airplane equipped with speed...
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Page 6 CESSNA INTRODUCTION MODEL 172S cessna Company II Tf!l'tron hE?>. Information Manual SKYHAVVK Membcr of GAMA Cessna Aircraft Company Model172S THIS MANUAL INCORPORATES INFORMATION ISSUED IN THE PILOT'S OPERATING HANDBOOK APPROVED AIRPLANE FLIGHT MANUAL AT REVISION 5 DATED 19 JULY 2004 (PART NUMBER 172SPHUS05) .
Page 8 CESSNA INTRODUCTION MODEL 172S TABLE OF CONTENTS SECTION GENERAL LIMITATIONS EMERGENCYPROCEDURES NORMAL PROCEDURES PERFORMANCE " WEIGHT AND BALANCE/EQUIPMENT LIST AIRPLANE AND SYSTEMS DESCRIPTION HANDLING, SERVICE AND MAINTENANCE SUPPLEMENTS Revision 5 . vii/viii U.S.
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Page 10 CESSNA SECTION 1 MODEL 172S GENERAL SECTION 1 GENERAL TABLE OF CONTENTS Page Three View - Normal Ground Attitude _..Introduction __ . _..Descriptive Data .. , _, . , ..Engine , .
Page 11 CESSNA SECTION 1 MODEL 172S GENERAL -------,--1 36'-1" ,,"M" '~/'.' 0510T1005 0510T1005 Figure 1-1.Three View - Normal Ground Ir" Attitude (Sheet 1 of 2) Revision 4...
Page 12 CESSNA SECTION 1 MODEL 172S GENERAL ---------27'-2" ---------' NOTE 1: WING SPAN SHOWN WITH STROBE LIGHTS INSTALLED. NOTE 2: WHEEL BASE LENGTH IS 65". NOTE 3: PROPELLER GROUND CLEARANCE IS 11 1/4". NOTE 4: WING AREA IS 174 SQUARE FEET .. NOTE 5: MINIMUM TURNING RADIUS (' PIVOT POINT TO OUTBOARD WING TIP) IS 27'-51/2".
Page 13 DESCRIPTIVE DATA ENGINE Number of Engines: 1. Engine Manufacturer: Textron Lycoming. Engine Model Number: IO-360-L2A. Engine Type:, .Normally aspirated, direct drive, air-cooled,. horizontally opposed, fuel injected, four cylinder engine with 360 cu. in. displacement.
Page 14 MIL-L-22851 or SAE J1899 Aviation Grade Ashless Dispersantl Oil: Oil conforming to the latest revision and/or supplements Textron Lycoming Service Instruction NO.1 014, must be used after first 50 hours or once oil consumption has stabilized. Revision 4...
Page 15 CESSNA SECTION 1 MODEL 172S GENERAL Recommended Viscosity for Temperature Range: MIL-L-6082 MIL-L-22851 or SAE Temperature J1899 Ashless Dispersant SAE J1966 SAE Grade Straight Mineral Oil SAE Grade 15W-50,20W-50or 60 Above27'e (80'F) . 50 40 or 50 Above 16'e (60'F) -l'e (30'F) to 32'e (gO' F ) 30,40 or 20W-40 e (O'F)to 21'e (70'F)
Page 16 CESSNA SECTION 1 MODEL 172S GENERAL Weight in Baggage Compartment, Normal Category: Baggage Area 1 (Station 82 t01 08): . 120 Ibs. See note below. Baggage Area 2 (Station 108 to 142): 50 Ibs. See note below. NOTE .The maximum combined weight capacity for Baggage Area 1 and Baggage Area 2 is 120 Ibs.
Page 17 CESSNA SECTION,1 MODEL172S GENERAL SYMBOLS, ABBREVIATIONS AND TERMINOLOGY GENERAL AIRSPEED TERMINOLOGY AND SYMBOLS KCAS Knots Calibrated Airspeed is indicated airspeed corrected position. and instrument error expressed in knots. Knots calibrated airspeed is equal to KTAS in standard atmosphere at sea level. KIAS Knots Indicated Airspeed...
Page 18 CESSNA SECTION 1 MODEL 172S GENERAL METEOROLOGICAL TERMINOLOGY Outside Temperature is the. free air static temperature.,W may'be expressed in either degrees 'Celsius or degrees Fahrenheit Standard Standard Temperature is 15°C at sea level Temperature pressure altitude and decreases by 2°C for each 1000 feet of altitude.
Page 19 CESSNA SECTION 1 MODEL 172S GENERAL ENGINE POWER TERMINOLOGY (Continued) Throttle full forward (pushed in, full control travel, Full toward the panel) Also known a's "full open" throttle. Throttle Throttle full aft (pulled out; full control travel, away Closed from the panel). Also known as the throttle "idle"...
Page 20 CESSNA SECTION 1 MODEL 172S GENERAL WEIGHT AND BALANCE TERMINOLOGY Reference Reference Datum is an imaginary vertical plane from Datum which horizontal distances measured balance pu rposes. Station Station is a location along the airplane fuselage given in terms of the distance from the reference datum. is the horizontal distance from the reference datum to the center of gravity (C.G.) of an item.
Page 21 CESSNA SECTION 1 MODEL 172S GENERAL WEIGHT AND BALANCE TERMINOLOGY (Continued) Maximum Ramp Weight is the maximum weight Maximum approved for ground maneuver, and includes the Ramp weight of fuel used for start, taxi and runup. Weight . Maximum Takeoff Weight is the maximum weight Maximum approved for the start of the takeoff roll:'...
Page 22 CESSNA SECTION 1 MODEL 172S GENERAL METRIC I IMPERIAL I U.S. CONVERSION CHARTS The following charts have been provided to help international operators convert U.S. measurement supplied with the Pilot's Operating Handbook into metric and imperial measurements. The standard followed for measurement units shown, is.
Page 23 CESSNA SECTION 1 MODEL 172S GENERAL (Pounds x .454 Kilograms) (Kilograms x 2.205 Pounds) KILOGRAMS INTO POUNDS KILOGRAMMES EN L1VRES 17.637 19.842 15.432 13.228 6.614 8.819 11.023 4.409 2.205 37.479 39.683 41.888 33.069 28.660 30.865 35.274 26.456 10 22.046 24.251 63.934 61.729 59.525...
Page 24 CESSNA SECTION 1 MODEL 172S GENERAL (Kilograms x 2.205 Pounds) (pounds.x .454 ~ Kilograms) POUNDS KILOGRAMS .150 . 50 Units x 10, 100, etc .. 0585T102 Figure 1.2. Weight Conversions (Sheet 2) • Revision 4 1.15...
Page 25 CESSNA SECTION 1 MODEL 172S GENERAL (Feet x .305 Meters) (Meters x 3.281 Feet) METERS. INTO FEET . METRES EN PIEDS feet feet feet feet feet feet feet teet feet feet 26.247 29.528 19.685 22.956 13.123 16.404 3.281 6.562 9.842 59.055 49.212 52.493...
Page 26 CESSNA SECTION 1 MODEL 172S GENERAL (Meters x 3.281 Feet) (Feet x .305 Meters) FEET . METERS .100 Units x 10, 100, etc. . Figure 1-3 : Length Conversions (Sheet 2) Revision 4 1-17...
Page 27 CESSNA SECTION 1 MODEL.172S GENERAL (Inches x 2.54 Centimeters) (Centimeters x .394 = Inches) CENTIMETERS iNTO INCHES CENTIMETRES EN POUCES 3.543 3.150 1.575 1.969 2.756 0.787 1.181 2.362 0.394 7.480 6.693 7.087 5.906 6.299 5.118 5.512 3.937 4.724 4.331 11.417 11.024 10.236 10.630...
Page 28 CESSNA SECTION l' MODEL 172S GENERAL (Centimeters x .394 ,; Inches) (Inches x 2.54 Centimeters) INCHES CENTIMETERS Units x 10, 100, etc. 0585T1028 Figure 1-4. Length Conversions (Sheet 2) Revision 4 1-19...
Page 30 CESSNA SECTION 1 MODEL 172S GENERAL (Imperial Gallons x 4.546 Liters) (Liters x .22 Imperial Gallons) LITERS INTO IMPERIAL GALLONS L1TRES EN GALLONS IMPERIAL 0.220 0.440 0.660 0.880 1.100 1.320 1.760 1.540 1.980 2.200 2.860 2.420 3.080 2.640 3.300 3.520 3.740 3.960 4.180...
Page 31 CESSNA SECTION 1 MODEL 172S GENERAL (Imperial Gallons x 4.4546 Litres) (Lilres x .22 Imperial Gallons) LITERS. IMPERIAL. GALLONS 280. 180 . Units x 10, 100, etc. 0585T1032 Figure 1-6. Volume Conversions (Sheet 2 of 3) " July 8198 1-22...
Page 32 CESSNA SECTION 1 MODEL 172S GENERAL (Imperial Gallons x 1.2 U.S. Gallons) (U.S. Gallons x .833 Imperial Gallons) (U.S. Gallons x 3.785 Liters) (Liters x .264 U.S. Gallons) . U. S. IMPERIAL LITERS GALLONS 100 120 GALLONS 100 45 .55 Units x 10, 100, etc.
Page 33 CESSNA SECTION 1 MODEL 172S GENERAL TEMPERATURE CONVERSIONS 'Cx9/5+32= (' F-32) x 5/9 °C 240" 1000 1020 1040 0585Tl034 Figure 1-7. Temperature Conversions July 8/98 1-24...
Page 34 CESSNA SECTION 2 MODEL 172S LIMITATIONS SECTION 2 LIMITATIONS TABLE OF CONTENTS Page Introduction Airspeed Limitations Airspeed Indicator Markings .....•..Powerplant Limitations Powerplant Instrument Markings Weight Limits Normal Category Utility Category Center Of Gravity Limits Normal Category Utility Category Maneuver Limits Normal Category .
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Page 36 CESSNA SECTION 2 MODEL 172S LIMITATIONS INTRODUCTION Section 2 includes operating limitations, instrument markings, and basic placards necessary for the safe operation of the airpiane, engine, standard systems standard equipment. limitations included in this section and in Section 9 have been approved by the Federal Aviation Administration.
Page 37 CESSNA SECTION 2 MODEL 172S LIMITATIONS AIRSPEED LIMITATIONS Airspeed limitations and their operational significance are shown in Figure 2.1. Maneuvering speeds shown apply to normal category operations. "The utility category maneuvering speed is 98 KIAS at 2200 pounds. REMARKS KCAS KIAS SPEED SYMBOL Do not exceed this...
Page 38 Red Line Maximum speed for all operations. POWERPLANT LIMITATIONS Engine Manufacturer: Textron Lycoming. Engine Model Number: 10-360-L2A. Maximum Power: 180 BHP rating. Engine Operating Limits for Takeoff and Continuous Operations: Maximum Engine Speed: 2700 RPM.
Page 39 SAE J1966 Aviation Grade Straight Mineral Oil or Mll-l-22851 or SAE J1899 Ashless Dispersant Oil. Oil must comply with the latest revision and/or supplement for Textron lycoming Service Instruction NO.1 014. Propeller Manufacturer: McCauley Propeller Systems. Propeller Model Number: 1A170E/JHA7660. Propeller Diameter Maximum 76 inches.
Page 40 CESSNA SECTION 2 MODEL 172S LIMITATIONS WEIGHT LIMITS NORMAL CATEGORY Maximum Ramp Weight: 2558 Ibs. Maximum Takeoff Weight: 2550 Ibs. Maximum landing Weight: 2550 Ibs. Maximum Weight in Baggage Compartment: Baggage Area 1 - Station 82 to 108: 120 Ibs. Baggage Area 2 - Station 108 to 142: 50 Ibs.
Page 41 CESSNA SECTION 2 MODEL 172S LIMITATIONS UTILITY CATEGORY Center of Gravity Range: Forward: 35.0 inches aft of datum at 1950 Ibs. or less, with straight line variation to 37.5 inches aft of datum at 22001bs. Aft: 40.5 inches aft of datum at all weights . Reference Datum: Lower portion of front face of firewall.
Page 42 CESSNA SECTION 2 MODEL 172S LIMITATIONS UTILITY CATEGORY This airplane is not designed for purely aerobatic flight. HOwever, in the acquisition of various certificates such as commercial pilot and flight instructor, certain maneuvers are required by the FAA. All of these maneuvers are permitted in this airplane when operated in the utility category.
Page 43 . CESSNA SECTION 2 MODEL172S LIMITATIONS FLIGHT LOAD FACTOR LIMITS NORMAL CATEGORY Flight Load Factors (Maximum Takeoff Weight - 2550 Ibs.): *Flaps Up +3:8g, -1.52g *Flaps Down +3.0g 'The design load factors are 150% of the above, and.in all cases, the structure meets or exceeds design loads.
Page 44 CESSNA SECTION 2 MODEL 172S LIMITATIONS FUEL LIMITATIONS Total Fuel: 56 U.S. gallons (2 tanks at 28.0 gallons each). Usable Fuel (all flight conditions): 53.0 U.S gallons. Unusable Fuel: 3.0 U.S. gallons (1.5 gallons each tank). NOTE To ensure maximum fuel capacity and minimize cross-...
Page 45 CESSNA SECTION 2 MODEL 172S LIMITATIONS' PLACARDS The following information must be displayed in the form of compos- ite or individual placards. 1. In full view of the pilot: (The "DAY-NIGHT-VFR-IFR" entry, shown on the example below, will vary as the airplane is equipped).
Page 46 CESSNA SECTION 2 MODEL 172S LIMITATIONS On the fuel selector valve: TAKEOFF BOTH ALL FLIGHT LANDING 53.0 GAL. ATIITUDES FUEL SELECTOR LEFT RIGHT 26.5 GAL. 26.5 GAL. LEVEL LEVEL FLIGHT FLIGHT ONLY ONLY Near fuel tank filler cap: FUEL 100LU1 00 MIN. GRADE AVIATION GASOLINE CAP.
Page 47 CESSNA SECTION 2 MODEL 172S LIMITATIONS In baggage compartment: 120 POUNDS MAXIMUM BAGGAGE FORWARD OF BAGGAGE DOOR LATCH 50 POUNDS MAXIMUM BAGGAGE AFT OF BAGGAGE DOOR LATCH MAXIMUM 120 POUNDS COMBINED FOR ADDITIONAL LOADING INSTRUCTIONS. SEE WEIGHT AND BALANCE DATA A calibration card must be provided to indicate the accuracy of the magnetic compass in 30°...
Page 48 CESSNA SECTION 2 MODEL 172S LIMITATIONS On the Upper Right Side of the Aft Cabin Partition: EMERGENCY LOCATOR TRANSMIITER INSTALLED AFT OF THIS PARTITION MUST BE SERVICED IN ACCORDANCE WITH FAR PART 91.207 On forward face of firewall adjacent to the battery: CAUTION 24 VOLTS D.C.
Page 49 .'.," ..•,.-c.i...
Page 50 CESSNA SECTION 3 MODEL 172S EMERGENCY PROCEDURES SECTION 3 EMERGENCY PROCEDURES TABLE OF CONTENTS Page Introduction ........AIRSPEEDS Airspeeds For Emergency Operation EMERGENCY PROCEDURES CHECKLIST Engine Failures . 3-4 Engine Failure During Takeoff Roll 'Engine Failure Immediately After Takeoff Engine Failure During Flight (Restart Procedures) 3-51 Forced Landings Emergency Landing Without Engine Power...
Page 51 CESSNA SECTION 3 MODEL 172S EMERGENCY PROCEDURES TABLE OF CONTENTS (Continued) <. Page • • Electrical Power Supply System Malfunctions 3-11 Ammeter Shows Excessive Rate of Charge (Full Scale Deflection) :....3-11 Low Voltage Annunciator (VOLTS) Illuminates During Flight' (Ammeter Indicates Discharge) 3-11 Vacuum System Failure 3-12...
Page 52 CESSNA SECTION 3 MODEL 172S EMERGENCY PROCEDURES INTRODUCTION Section 3 provides checklist and amplified procedures for coping with emergencies that may occur. Emergencies caused by airplane or engine malfunctions extremely rare. if proper preflight .inspections maintenance practiced. Enroute weather emergencies can be minimized or eliminated by careful...
Page 53 CESSNA SECTION 3 MODEL 172S EMERGENCY PROCEDURES EMERGENCY PROCEDURES CHECKLIST Procedures in the Emergency Procedures Checklist portion of this section shown in bold facEld type are immediate action items which should be committed to memory. ENGINE FAILURES ENGINE FAILURE DURING TAKEOFF ROLL 1.
Page 54 CESSNA SECTION 3 MODEL 172S EMERGENCY PROCEDURES ENGINE FAILURE DURING FLIGHT (Restart Procedures) 1. Airspeed •• 68 KIAS. 2. Fuel Shutoff Valve •• ON (push full in). 3. Fuel Selector Valve •• BOTH. 4. Auxiliary Fuel Pump Switch •• ON. 5.
Page 55 CESSNA SECTION 3 MODEL 172S EMERGENCY PROCEDURES PRECAUTIONARY LANDING WITH ENGINE POWER' 1. Passenger Seat Backs .. MOST UPRIGHT POSITION. 2. Seats and Seat Belts .- SECURE.' 3. Airspeed -- 65 KIAS. 4. Wing Flaps -- 20°.. 5. Selected Field -- FLY. OVER, noting terrain and obstructions, then retract flaps upon reaching a safe altitude and airspeed.
Page 56 CESSNA SECTION 3 MODEL 172S EMERGENCY PROCEDURES FIRES DURING START ON GROUND 1. Ignition Switch •• START, Continue Cranking to get a start. which would suck the flames and accumulated. fuel into the engine. If engine starts: 2. Power -- 1800 RPM for a few minutes. 3.
Page 57 CESSNA SECTION 3 MODEL 172S EMERGENCY PROCEDURES ELECTRICAL FIRE IN FLIGHT 1. lIIiaster Switch •• OFF. 2. Vents, Cabin Air, Heat •• CLOSED. 3. Fire Extinguisher •• ACTIVATE. 4. Avionics Master Switch .- OFF. 5. All Other Switches (except ignition switch) -- OFF. WARNING AFTER DISCHARGING FIRE EXTINGUISHER AND'...
Page 58 CESSNA SECTION 3 MODEL 172S EMERGENCY PROCEDURES WING FIRE 1. LandinglTaxi Light Switches -. OFF, 2. Navigation Light Switch _. OFF. 3, Strobe Light Switch -- OFF. 4. Pitot Heat Switch -- OFF. NOTE Perform a sideslip to keep the. flames away from the fuel tank and cabin.
Page 59 CESSNA SECTION 3 MODEL 172S EMERGENCY PROCEDURES 10. Approach at 65 to 75 KIAS depending upon th~ amount of the accumulation. 'C" • 11. Perform a landing in level attitude. STATIC SOURCE BLOCKAGE (Erroneous Instrument Reading Suspected) Static Pressure Alternate Source Valve •• PULL ON. 2.
Page 60 CESSNA SECTION 3 MODEL 172S EMERGENCY PROCEDURES ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS AMMETER SHOWS EXCESSIVE RATE OF CHARGE (Full Scale Deflection) 1. Alternator -- OFF .. CAUTION WITH THE ALTERNATOR SIDE OF. THE MASTER SWITCH OFF, COMPASS DEVIATIONS OF AS MUCH AS 25°...
Page 61 CESSNA SECTION 3 MODEL 172S EMERGENCY PROCEDURES SYSTE'M VACUUM FAILlJRE' Right Vacuum (VAC Left Vacuum (L VAC) Annunciator Annunciator Illuminates. CAUTION. VACUUM WITHIN NORMAL OPERATING LIMITS, FAILURE OCCURRED VACUUM SYSTEM PARTIAL PANEL PROCEDURES REQUIRED FOR CONTINUED FLIGHT. :':. 1. Vacuum Gage,"...
Page 62 CESSNA SECTION 3 MODEL 172S EMERGENCY PROCEDURES AMPLIFIED EMERGENCY PROCEDURES The following Amplified Emergency Procedures elaborate upon information contained in the Emergency Procedures Checklists portion of this section. These procedures also include information not readily adaptable to a checklist format, and material to which a pilot could not be expected to refer' in resolution of a specific...
Page 63 CESSNA SECTION 3' MODEL 172S EMERGENCY PROCEDURES After an engine failure in flight, ,the most important course of action is to continue flying the airplane. Best glide speed as shown in Figure 3-1 should be established as quickly as possible. While gliding toward a suitable landing area, an effort should be made to identify the cause of the failure.
Page 64 CESSNA SECTION 3 MODEL 172S EMERGENCY PROCEDURES FORCED LANDINGS If all attempts to restart the engine fail and a forced landing is imminent, select a suitable field and prepare for the landing as discussed under the Emergency Landing Without Engine Power checklist.
Page 65 CESSNA SECTION 3 MODEL 172S EMERGENCY PROCEDURES ' , \ . At the landing flare (round-out), the nose down moment resulting from power reduction is an adverse factor and the airplane may land on the nose wheel. Consequently, at flare, the elevator trim control should be adjusted toward the full nose up position and the power adjusted so that the airplane will rotate to the horizontal attitude for touchdown, Close the throttle at touchdown,...
Page 66 CESSNA SECTION 3 MODEL 172S EMERGENCY PROCEDURES 3. Check accuracy of the turn by observing the compass heading which should be the reciprocal of the original heading. 4. If necessary, adjust heading primarily with skidding motions rather than rolling motions so that the compass will read more accurately.
Page 67 CESSNA SECTION 3 MODEL 172S EMERGENCY PROCEDURES RECOVERY FROM SPIRAL DIVE IN THE CLOUDS If a spiral'isencountered in the clouds; proceed as follows: 1. Retard throttle to idle position. 2. Stop the turn by using coordinated aileron and rudder control to align the symbolic airplane in the turn coordinator with the horizon reference line.
Page 68 CESSNA SECTION 3 MODEL 172S EMERGENCY PROCEDURES When using the alternate static source, refer to the Alternate Static Source Airspeed Calibration table in Section 5, Performance, for additional information. Maximum airspeed and altimeter variation from normal is 4 knots and 30 feet over the normal operating range with the window(s) Closed.
Page 69 CESSNA , SECTION 3 MODEL 172S EMERGENCY PROCEDURES ROUGH ENGINE OPERATION OR LOSS OF POWER SPARK PLUG FOULING A slight engine roughness in flight maybe caused by one or mo're spark plugs becoming fouled by carbon or lead deposits, This may be verified by turning the ignition switch momentarily from BOTH to either L or R position, An obvious power loss in single...
Page 70 CESSNA SECTION 3 MODEL 172S EMERGENCY PROCEDURES EXCESSIVE FUEL VAPOR INDICATIONS Excessive fuel vapor is.most likely to be generated during groun operations when operating at higher altitudes, in unusually war temperatures or with ,more volatile fuel blends. Operation at or nea Idle RPM (low fuel flow) for extended periods will increase th chances of fuel vapor generation.
Page 71 CESSNA SECTION 3 MODEL 172S EMERGENCY PROCEDURES ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS Malfunctions in the electrical power supply. system can be detected by periodic monitoring of the ammeter and low vottage lannunciator (VOLTS); however, the cause of these malfunctions is usually difficult to determine.
Page 72 CESSNA SECTION MODEL 172S EMERGENCY PROCEDURES INSUFFICIENT RATE OF CHARGE NOTE The low voltage annunciator (VOLTS) may come on and • ammeter discharge indications may occur during low RPM conditions with an electrical load on the system, such as during taxi.
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Page 74 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES SECTION 4 NORMAL PROCEDURES TABLE OF CONTENTS Page. Introduction AIRSPEEDS. Airspeeds For Normal Operation CHECKLIST PROCEDURES Preflight Inspection Cabin ;......Empennage Right Wing, Trailing Edge Right Wing 4-8' Nose ........Left Wing 4-10 Left Wing, Leading Edge...
Page 75 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES ~". ",' TABLE OF CONTENTS,(Continued) ;." • .~#-,~. Page . i .. ~ .• ?.•.. ' :.;.~" . ..,. .. ~.~ . . .4-17 Landing 4-17 Normal Landing 4-17 Short Field Landing 4-17 Balked Landing 4-17 After Landing...
Page 76 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES TABLE OF CONTENTS (Continued) Page Landing _.. _ _. _ _. _..4-33 Normal Landing . _. _ _. _. _ __..4-33 Short Field Landing __.
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Page 78 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES INTRODUCTION Section 4 provides checklist and amplified procedures for the conduct of normal operation. Normal procedures associated with optional systems can be found in the Supplements, Section 9. AIRSPEEDS AIRSPEEDS FOR NORMAL OPERATION Unless otherwise noted, the following speeds are based on a maximum weight of 2550 pounds and may be used for any lesser weight.
Page 79 s6crioN 4 OElSSNA NDRMALpROC~DUR~S MObi::L 1725 NOTE VisuaUy cHeck. airpi(ln8, lot genetal, condition, dUring Walk; aroUM ihspectioit Airplane. sHoUld be paiKecl iii a iiO/IMI groUha altitude, (rMer to FigUre ,.1) to, ensUre Ihat I~el arain . ValVes alloW, for, aceUrale sampling, ,Hse of tna. refUeling steps ana ,assist"...
Page 80 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES CHECKLIST PROCEDURES PREFLIGHT INSPECTION G)CABIN 1. Pitot Tube Cover -- REMOVE. Check for pitot blockage. 2. Pilot's Operating Handbook -- AVAILABLE IN THE AIRPLANE. 3. Airplane Weight and Balance -- CHECKED. 4. Parking Brake -- SET. 5.
Page 81 CESSNA SECTION 4 MODEL1728 NORMAL PROCEDURES 15. Annunciator ,Panel Test Switch :- H!=LEASE'; Check that ap- propriate annunciators remain on. ." 11>, When Master Switch is turned ON, some annunciators will flash for approximately. 10 .seconds before illuminating. steadily. When panel TST switch is toggled up and held in position, all remaining lights will flash until the switch is released.
Page 82 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES 2. Main Wheel Tire -- CHECK for proper inflation and general condition (weather checks, tread depth and wear, etc ...). 3. Fuel Tank Sump Quick Drain Valves -- DRAIN at least a cupful of fuel (using sampler cup) from each sump location to check for water, sediment, and proper fuel grade before each flight and after each refueling.
Page 83 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES 2. Engine Oil Dipstick/Filler Cap -- CHECK oil level, then check dipstick/filler cap SECURE. Do not operate with less than five quarts. Fill to eight qu-arts for extended flight. 3. Engine Cooling Air Inlets -- CLEAR of obstructions. 4.
Page 84 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES LEFT WING Leading Edge 1. Fuel Tank Vent Opening -- CHECK for blockage.. 2. Stall Warning Opening -- CHECK for blockage. To check the system, place a clean handkerchief over the vent opening apply suction;...
Page 85 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES STARTING ENGINE (With Battery) 1. Throllie -- OPEN 1/4 INCH: 2. Mixture --.IDLE CUTOFF .. 3. Propeller Area ._-CLEAR: 4. Master Switch -- ON. 5. Flashing Beacon -- ON. NOTE If engine is warm, omit priming procedure of steps 6, 7 and 8 below.
Page 86 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES STARTING ENGINE (With External Power) 1. Throttle -- OPEN 1/4 INCH. 2. Mixture -- IDLE CUTOFF. 3. Propeller Area -- CLEAR. 4. Master Switch -- OFF. 5. External Power -- CONNECT to airplane receptacle. 6.
Page 87 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES b. Taxi and Landing Light Switches -- ON. (to provide an initial electrical load on the system):' c. Engine RPM -- REDUCE to idle .. (Minimum alternator output occurs at idle.) • d. Master Switch -- ON (with taxi and landing lights switched on)..
Page 88 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES BEFORE TAKEOFF 1. Parking Brake -- SET. 2. Passenger Seat Backs -- MOST UPRIGHT POSITION. 3. Seats and Seat Belts -- CHECK SECURE. 4. Cabin Doors -- CLOSED and LOCKED. 5. Flight Controls -- FREE and CORRECT. 6.
Page 89 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES ...;.- SHORT FIELD TAKEOFF 1. Wing Flaps -- 10°. 2. Brakes --.APPLY. 3. Throttle ~- FULL OPEN. 4. Mixture -- RICH (above .3000 feet, LEAN obtain maximum RPM). 5. Brakes -- RELEASE. 6. Elevator Control -- SLIGHTLY TAIL LOW. - . 7.
Page 90 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES LANDING NORMAL LANDING 1. Airspeed -- 65-75 KIAS (flaps UP). 2. Wing Flaps --AS DESIRED (0°_10° below 110 KIAS, 10°-30° below 85 KIAS). 3. Airspeed -- 60-70 KIAS (flaps DOWN). 4. Touchdown -- MAIN WHEELS FIRST. 5: Landing Roll -- LOWER NOSE WHEEL GENTLY.
Page 91 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES AMPLIFIED PROCEDURES PREFLIGHT INSPECTION - The Prefiight Inspection, described in Figure 4-1 'and adjacent checklist, is required prior to each flight If the airplane has been in extended storage, has had recent major maintenance, or has been operated from marginal...
Page 92 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES If the airplane has been operated from muddy fields or in snow or slush, check the main and nose gear wheel fairings for obstructions and cleanliness. Operation from a gravel or cinder field will require extra attention to propeller tips and abrasion on leading edges of the horizontal tail.
Page 93 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES Should the engine tend to die after starting, turn on the auxiliary fuel pump temporarily and adjust the throttle and/or mixture as event 'necessary to keep the engine running. In the of over priming or flooding, turn off the auxiliary fuel pump;...
Page 94 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES LEANING FOR GROUND OPERATIONS 1. For all ground operations, after starting the engine and whe the engine is running smoothly: a. set the throttle to 1200 RPM. b. lean the mixture for maximum RPM. set the throttle to ah RPM appropriate operatio.ns (800 to 1000 RPM re"commended).
Page 95 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES ."...•. "..•.. ,.",Iti .•. ' ..i•••••• ,;..#I. .::;:;:::::::::::::~~: . ;.;.; :.: i..•• ""';"""ii" ,.,.,' , t .. i ' •.•••.••••.•.•. ..•••• ,' ••••••••••••• t..ttt:;@:it ..•..•..•..i . •. ~ . •. i.!.;.,.?.~::.:.:.:~::::::: •.•...
Page 96 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES BEFORE TAKEOFF WARMUP If the engine idles (approximatley 600 RPM) and accelerates smoothly, the airplane is ready for takeoff. Since the engine is closely cowled for efficient in-flight engine cooling, precautions should be taken to avoid overheating during prolonged engine operation on the ground.
Page 97 CESSNA SECTION 4 MODEL'172S NORMAL PROCEDURES " LANDING LIGHTS If landing lights are to be used to enhance the visibility of the airplane in the traffic pattern or enroute, it is recommended that only the taxi light be used, This will extend the service life of the landing light appreciably, TAKEOFF POWER CHECK...
Page 98 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES WING FLAP SETTINGS Normal takeoffs are accomplished with wing flaps 0°_10°. Using 10° wing flaps reduces the ground roll and total distance over an obstacle by approximately 10 percent. Flap deflections greaterl than 10° are not approved for takeoff.
Page 99 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES CRUISE Normal cruise .is performed between 45% and 75% power. The engine corresponding fuel .consumption for various altitudes can be determined by using the data in Section 5. NOTE • Cruising should be. done at 75% power as much as practicable until a total of 50 hours has accumulated or oil...
Page 100 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES 75% POWER . 55% POWER 65% POWER ALTITUDE KTAS NMPG KTAS NMPG KTAS NMPG Sea Level 11.2 12.0 12.8 4000 feet 11.7 12.4 13.2 8000 feet 12.2 12.9 13.6 Figure 4-3. Cruise Performance Table LEANING WITH AN EGT INDICATOR At or below 75% power...
Page 101 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES NOTE indicator requires several seconds. to respond to mixture adjustments and changes exhaust gas temperature. More rapid changes in EGT indication are neither necessary nor desirable. Determining peak EGT and setting the desired mixture should take approximately one minute when the adjustments are made sufficiently...
Page 102 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES FUEL VAPOR PROCEDURES The engine fuel system can become susceptible to fuel vapor formation on the ground during warm weather. This will generally occur when the outside ambient air temperature is above 80"F.1 The situation is further aggravated by the fact that the engine fuel flows are lower at idie and taxi engine speeds.
Page 103 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES ..STALLS -,,', <" ,The stall characteristics are conventional and aural warning is provided by a stall warring horn which .sou~ds between 5 and 10 knots above the stall in all configurations . .
Page 104 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES The normal entry is made from. a power off stall. As the stall is approached, the elevator control should be smoothly pulled to the full aft position. Just prior to reaching the stall "break", rudder control in the desired direction of the spin rotation should be applied so that full rudder deflection is reached almost simultaneously with...
Page 105 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES NOTE . If disorientation precludes, a 'visual determination of the direction of rotation, the symbolic airplane in 'the turn Coordinator may be referred to for this information. Variations in basic airplane rigging or in weight and balance due installed equipment right...
Page 106 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES SHORT FIELD LANDING For a short .field landing in smooth air conditions, make an approach at 61 KIAS with 30° flaps using enough power to control the glide path. (Slightly higher approach speeds should be used under turbulent air conditions.) After all approach obstacles...
Page 107 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES COLD WEATHER OPERATION Special consideration should be given to the operation of the airplane tuel system during the winter season or prior to any tlight in cold temperatures, Proper preflight draining of the tuel, system is especially important and will eliminate any free water, accumulation, The use of additives such as isopropyl alcohol or diethylene glycol monomethyl ether may also be desirable, Hefer to Section 8 for...
Page 108 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES When using an external power source, the master switch must be in the OFF position before connecting the external power source to the airplane receptacle. See Section 7, Ground Service Plug Recepta- cle for external power source operations. Cold weather starting procedures are the same as the normal starting procedures.
Page 109 CESSNA SECTION 4 MODEL 172S NORMAL PROCEDURES HOT WEATHER OPERATION Refer to the general warm temperature starting information under Starting Engine in this section. Avoid prolonged engine operation on the ground. . " NOISE CHARACTERISTICS. AND NOISE REDUCTION "The certificated nois~ level for the Model 172S at 2550 pounds maximum weight is 75.1 dB(A).
Page 110 CESSNA SECTION 5 MODEL 172S PERFORMANCE SECTIONS PERFORMANCE TABLE OF CONTENTS Page Introduction Use of Performance Charts Sample Problem Takeoff Cruise 'Fuel Required Landing Demonstrated Operating Temperature Figure 5-1, Airspeed Calibration - Normal Static Source Airspeed Calibration - Alternate Static Source 5-10 Figure 5-2, Temperature Conversion Chart 5-11...
Page 111 .:;: \ .. ,t ..1...
Page 112 CESSNA SECTION 5 MODEL 172S PERFORMANCE INTRODUCTION Performance data charts on the following pages are presented so that you may know what to expect from the airplane under various conditions, and also, to facilitate the planning of flights in detail and with reasonable accuracy.
Page 113 CESSNA SECTION 5 MeDEL 172S PERFORMANCE CRUISE CONDITIONS: 360 Nautical Miles Total distance 7500 Feei .Pressure altitude 16°C (16°C Above Standard). Temperature , 10 Knot Headwind Expected wind enroute LANDING CONDITIONS: 2000 Feet 'Field pressure altitude 25°C Temperature, ' 3000 Feet Field length TAKEOFF The takeoff distance chart,.
Page 114 CESSNA SECTION 5 MODEL 172S PERFORMANCE Total distance to clear a 50-foot obstacle, zero wind 2190 . Decrease in total distance (2190 feet X 13%) Corrected total distance to clear 50-foot 'obstacle 1905 Feet CRUISE The. cruising altitude. should selected based consideration of.
Page 115 CESSNA SECTION 5 MODEL'172S PERFORMANCE FUEL REQUIRED The total fuel requirement for th'e flight may be estimated using the performance information in Figure 5-7 and Figure 5-8. For this sample problem, Figure 5-7 shows that a climb from 2000 feet to 8000 feet requires 2.2 gallons of fuel.
Page 116 CESSNA SECTION 5 MODEL 172S PERFORMANCE The resultant cruise distance is: Total distance Climb distance Cruise distance 342 nm . With an expected 10 knot headwind, the ground speed for cruise is predicted to be: 107 Knots Therefore, the time required for the cruise portion of the trip is: 342 Nautical Miles 3.2 Hours , 107 Knots...
Page 117 CI::SSNA SECTION 5 MODEL 172S PERFORMANCE LANDING A procedure similar to takeoff should be useiUor 'estimating the landing distance at the destination airport, Figure 5-11 presents landing distance information for,. the short field technique. distanCes corresponding to 2000 feet and 30°C are as follows: Ground roll .650 Feet Total distance to clear a 50-foot obstacle...
Page 118 CESSNA SECTION 5 MODEL 172S PERFORMANCE AIRSPEED CALIBRATION NORMAL STATIC SOURCE CONDITION: Power required-for level flight or maximum power descent FLAPS - UP - KIAS 10011012013014 150 160 KCAS 10711712713 7 147 1'57 FLAPS 10° 70- 80 KIAS 100 110 - - - -" KCAS 109----- FLAPS...
Page 119 CESSNA SECTION 5 MODEL 172S PERFORMANCE 'AIRSPEED CALIBRATION ALTERNATE STATIC SOURCE CONDITION: Power required for level flight or maximum power descent. FLAPS 50 60 70 80 90 100110120130140150160 KIAS 56 62 68 76 85 95 105 115 125 134 144154, KCAS FLAPS , 10.
Page 120 CESSNA SECTION 5 MODEL 172S PERFORMANCE TEMPERATURE CONVERSION CHART tPf1-1t~4+ UJ 60 "~Trn~rfn.~r ~ !+:: . . "~::r H--H--H.++y.J .. q .. ! .. +H--;.t1--: .t.i..i" --:_;..!.~. i'f. <D 20 q -.. .+.+ ..1. .--f- :.1. :. DEGREES - CELSIUS Figure 5-2.
Page 121 . CESSNA SECTION.5 MODEL 172S PERFORMANCE STALL SPEEDS AT 2550 POUNDS Conditions: Power Off MOST REARWARD CENTER OF GRAVITY ANGLE OF BANK FLAP SETIING KIAS KCAS KIAS KCAS KIAS KCAS KIAS KCAS MOST FORWARD CENTER OF GRAVITY ANGLE OF-BANK FLAP SETIING KIAS KCAS KIAS KCAS KIAS KCAS KIAS KCAS NOTES:...
Page 122 CESSNA SECTION 5 MODEL 172S PERFORMANCE WIND COMPONENTS NOTE: Maximum demonstrated crosswind velocity is 15 knots (not a limItation). (/)~ 1-« Z:I: :lii NOTE Maximum demonstrated crosswind component' knots (not a. limitation). 0585C1003 Figure 5-4. Crosswind Components -Revision 4 5-13...
Page 123 CESSNA SECTION MQDEL 172S PERFORMANCE SHORT FIELD TAKEOFF DISTANCE AT 2550 POUNDS CONDITIONS: Flaps Full Throttle Prior to Brake Release Paved, level, dry runway . Zero Wind Litt Off: 51 KIAS Speed at 50 Ft: 56 KIAS , 30 0 ( 40 0 ( 20 0 ( 100(...
Page 124 CESSNA ,SECTION 5 MODEl: 172S PERFORMANCE SHORT FIELD TAKEOFF DISTANCE AT,2400 POUNDS CONDITIONS: Flaps 10° Full Throttle Prior to Brake' Release . Paved, level, dry runway Zero Wind Lift Off: 48 KIAS Speed at KIAS 1DoC, . 3DoC 2DoC 4DoC ' Grnd Total Grnd Total Grnd Total'...
Page 125 CESSNA SECTION 5 MODEL172S, PERFORMANCE SHORT FIELD TAKEOFF DISTANCE ,;AT 2200 POUNDS CONDITIONS: ',' Flaps 10 Full Throttle Prior to Brake Release Paved, level, dry runway Zero Wind Lift Off: 44 KIAS Speed at 50 Ft: 50 KIAS 40°C 30°C 20°C 10°C Grnd Total...
Page 126 CESSNA SECTION 5 MODEL 172S PERFORMANCE MAXIMUMRATE"OF-CLIMB AT 2550 POUNDS CONDITIONS: Flaps Up Full Throttle CLIMB, PRESS RATE OF CLIMB -FPM ' SPEED KIAS -20°C O°C, 20°C 40°C ,S.L. 2000 • 560 4000 6000 390 ' 8000 285 , 10,000 12,000 NOTE: maxi":,um...
Page 127 CESSNA SECTION 5. MODEL 172S PERFORMANCE TIME, FUEL AND DISTANCE TO CLIMB AT 2550 POUNDS . CONDITIONS: Flaps Up Full Throttle Standard Temperature. FROM SEA LEVEL RATE' PRESS CLIMB FUEL TIME SPEED DIST CLIMB USED KIAS' 74 . 1000 2000. .1.2 3000 4000'...
Page 128 CESSNA SECTION MODEL 172S PERFORMANCE CRUISE PERFORMANCE CONDITIONS: 2550 Pounds Recommended Lean Mixture At All' Altitudes(Refer to Section 4, Cruise) 20'( BELOW STANDARD 20'(ABOVE PRESS STANDARD TEMP TEMPERATURE STANDARD TEMP . ALT KTAS KTAS KTAS 2000 2550 117 11.1 77 118 10.5 2500 115 10.6...
Page 129 CESSNA SECTION 5 MODEL 172S PERFORMANCE CRUISE PERFORMANCE CONDITIONS: 2550 Pounds Recommended Lean Mixture At All Altitudes (Refer to Section 4, Cruise) 20'(ABOVE STANDARD 20'( BELOW STANDARD TEMP PRESS TEMPERATURE STANDARD'TEMP KTAS KTAS KTAS FT ' • 10.4 11.1 2700 ~OOO 10,5 2650...
Page 130 CESSNA SECTION 5 MODEL 172S PERFORMANCE '.RANGE PROFILE 45 MINUTES RESERVE 53 GALLONS USABLE FUEL CONDITIONS: 2550 Pounds Recommended Lean Mixture for. Cruise At All Attitudes Standard Temperature Zero Wind 12,000 10,000 8,000 6,000 4,000 NOTES: This chart allows for the fuel used for engine 'start, taxi, takeoff and climb, ,and the distance during climb.
Page 131 CESSNA SECTION 5 MODEL ,172S . PERFORMANCE ENDURANCE PROFILE 45 MINUTES RESERVE 53 GALLONS USABLE FUEL CONDITIONS: 2550 Pounds Recommended Lean Mixture for Cruise At All Altitudes Standard Temperature 12000 10000 8000 w 6000 :> 4000 « 2000 +1-++: ENDURANCE - HOURS NOTE: This chart allows for the fuel used for engine start, taxi, takeoff and climb, and the time during climb.
Page 132 CESSNA SECTION 5 MODEL 172S PERFORMANCE SHORT FIELD LANDING DISTANCE AT 2550 POUNDS CONDITIONS: Flaps 30 Power Off Maximum Braking Paved, level, dry runway Zero Wind Speed at 50 Ft: 61 KIAS lD.( 2D.( 3D.( 4D.( Grnd Total Grnd Total Total Grnd Grnd Total Grnd...
Page 134 CESSNA SECTION 6 MODEL 172S WEIGHT & BALANCE/EQUIPMENT LIST SECTION 6 WEIGHT & BALANCE/ EQUIPMENT LIST TABLE OF CONTENTS Page Introduction ....Airplane Weighing Procedures. .
Page 136 . CESSNA _SECTION MODEL 172S WEIGHT & BALANCE / EQUIPMENT LIST INTRODUCTION This section describes the procedure for establishing the basic empty weight and moment of the airplane. Sample forms are provided for reference. Procedures for calculating the weight and moment for various operations are also provided.
Page 137 CESSNA SECTION 6 MODEL 172S WEIGHT & BALANCE / EQUIPMENT LIST AIRPLANE WEIGHING FORM REFERENCE DATUM (FIREWALL FRONT FACE, NOTE LOWER PORTION) STA 0.0 IT IS THE RESPONSIBILITY OF THE PILOT TO ENSURE THAT THE AIRPLANE IS LOADED PROPERLY. .58.80 25.90 ~ 100 ::::;...
Page 138 CESSNA SECTION 6 MODEL 172S WEIGHT & BALANCE IEQUIPMENT LIST LOCATING CG WITH AIRPLANE ON LANDING GEAR FORMULA lor Longitu.dinat CG: INCHES (NOSE GEAR NET WEIGHT)( (X) ~ (A)~ ------ AFT OF NOSE AND MAIN LANDING GEAR WEIGHT TOTALED ( DATUM MEASURING A AND B MEASURE...
Page 139 CESSNA SECTION 6 MODEL 172S WEIGHT & BALANCE EQUIPMENT LIST 3. Weighing: a. Weigh airplane in a closed hangarto avoid errors caused by air currents. b. With the airplane level and brakes released, record the weight shown on each scale. Deduct the tare, if any, from each reading.
Page 140 • • •• • -----.,.--.....------~ :;;::0 '< o(f) SAMPLE WEIGHT AND BALANCE RECORD Q.> m(f) <D ~:t> (CONTINUOUS HISTORY OF CHANGES IN STRUCTURE OR EQUIPMENT AFFECTING WEIGHT AND BALANCE) " ",' " "" AIRPLANE MODEL ISERIAL NO. IPAGE NUMBER RUNNING WEIGHT CHANGE ITEM NO.
Page 141 CESSNA SECTION 6 MODEL 172S WEIGHT&BALANCE EQUIPMENT LIST NOTE Loading Graph information for the pilot, passengers baggage based seats positioned average occupants and baggage loaded in the center of the baggage areas as shown on the Loading Arrangements diagram. For loadings which may differ from these, the Sample Loading Problem lists fuselage stations for these items to indicate their forward and aft C.G.
Page 142 CESSNA SECTION 6 MODEL 172S WEIGHT & BALANCE / EQUIPMENT LIST LOADING ARRANGEMENTS Pilot or passenger center ot gravity on adjustable seats positioned tor average occupant Numbers in parentheses indicate forward and aft limits of occupant center .of gravity range. Arm measured to the center of the areas shown.
Page 143 CESSNA SECTION 6 MODEL 172S WEIGHT & BALANCE EQUIPMENT LIST FIREWALL :41" 48" 10'/4" 1----1-- __ J 65.3 AFT BAGGAGE AREA DOOR OPENING DIMENSIONS HEIGHT HEIGHT WIDTH WIDTH (REAR) (FRONT) (BOTTOM) (TOP) '40112" 39" 32112" CABIN DOORS 37" 15 1 /.' 22"...
Page 144 CESSNA SECTION 6' MODEL 172S WEIGHT & BALANCE EQUIPMENT LIST CABIN WIDTH MEASUREMENTS •• INSTRUMENT PANEL REAR DOOR POST BULKHEAD l------" .142 r-r--\Ir-~/ ,:\-___ '7!!;f/'" .. /2" 1" "1 035" 03312 039'/2" 037'/ 2 211/2" • * 34" *29 ' /2" *25"...
Page 145 CESSNA SECTION 6 MODEL 172S WEIGHT & BALANCE / EQUIPMENT LIST WEIGHT AND MOMENT TABULATION YOUR SAMPLE AIRPLANE ITEM DESCRIPTION AIRPLANE Moment Moment Weight Weight (Lb-ins. (Lb-ins. (Ibs.) (Ibs.) /1000) /1000) 1. Basic Empty Weight (Use data pertaining your airplane presently equipped.
Page 146 CESSNA SECTION 6 MODEL 172S WEIGHT & BALANCE tEQUIPMENT LIST YOUR YOUR YOUR AIRPLANE AIRPLANE AIRPLANE Moment Moment Moment Weight Weight Weight (Lb-ins. (Lb-ins. (Lb-ins. (Ibs.) (Ibs.) (Ibs.) 11OOO) 11OOO) 11OOO) NOTE When several loading configurations are representative of your operations, it may be useful to fill out one or more of the above columns so specific loadings are available at a glance.
Page 147 CESSNA SECTION 6 MODEL 172S WEIGHT & BALANCE / EQUIPMENT LIST LOAD MOMENT/1000 (KILOGRAM - MILLIMETERS) 150. 200 250 300 350 400 175 ~ « £1 w 250 -t-i--l--:--j- --:---t.-t- LOADING GRAPH 100. (POUNDS -INCHES) LOAD MOMENTil000 NOTE: LINE REPRESENTING ADJUSTABLE SEATS SHOWS THE PILOT OR PASSENGER CENTER OF GRAVITY ON ADJUSTABLE SEATS POSITIONED FORAN AVERAGE OCCUPANT.
Page 148 CI::SSNA SECTION 6 MODEL 172S WEIGHT& BALANCE / EQUIPMENT LiSt 2500 1700 D585C1007 Figure 6-7. Center of Gravity Moment Envelope July 8/98 6-15...
Page 149 CESSNA SECTION 6 MODEL 172S WEIGHT.& BALANCE / EQLJIPMENT LIST 2600 2500 2400 2300 '" « ' " ~ 2200 2100 ' " « 2000 •• •• 1900 « « 1800 1700 1600 1500 35 36 37 38 40 41 42 43 44 45 46 47 48 AIRPLANE...
Page 150 CESSNA SECTION 6 MODEL.172S WEIGHT & BALANCE / EQUIPMENT LIST COMPREHENSIVE EQUIPMENT LIST The .following figure (Figure 6-9) is a comprehensive list of all, Cessna equipment which is available for the Model 1725 airplane. This comprehensive equipment list provides the following inlormalion in column form: In the ITEM NO column, each item is assigned a coded number.
Page 151 CESSNA SECTION 6 MODEL 172S WEIGHT & BALANCE 1 EQUIPMENT LIST ITEM REF DRAWING EQUIPMENT LIST DESCRIPTION . lBS INS. 11 • PLACARDS AND MARKINGS 43.0 0505087-23 PLACARD, OPERATIONAL LIMITATIONS 11.01-R 19.2. 95.4. 0504051 PAINT, OVERALL EXTERIOR 11-02-5 93.6 870-003 18.4 - OVERALL WHITE 135.9...
Page 152 CESSNA SECTION 6 MODEL 172S WEIGHT & BALANCE / EQUIPMENT LIST ITEM EQUIPMENT LIST DESCRIPTION . REF DRAWING INS. 23-03.A NAV/COM #2 INSTAllATION. WITH G.8. 17." KX 155A NAV/COM WITH GliDESLQPE 069-01032-0101 12.5 - KI209A INDICATOR WITH GLiDESLOPE 066-03056-0003 13.9 - NAV ANTENNA WITH G.8.
Page 153 CESSNA SECTION 6 MODEL 172S WEIGHT BALANCE 1 EQUIPMENT LIST & ITEM REF DRAWING EQUIPMENT LIST DESCRIPTION INS. 90.0 000031 11,-12 REAR SEAT RESTRAINT SYSTEM, INERTIA 2515-8 REEL 90.0 2000031-11,-12 AEAR SEAT RESTRAINT SYSTEM, MANUAL 25-16-0 ADJUST 21.0 0514230-1 PADDED GLARESHIElD 25.17.S 32.8 0514166-2...
Page 154 CESSNA SECTION 6 MODEL 172S WEIGHT & BALANCE IEQUIPMENT LIST ITEM EQUIPMENT LIST DESCRIPTION REF DRAWING INS. 32. LANDING GEAR 32-01-R WHEEL BRAKE, AND TIRE, 6.00 X 6 MAIN 57.S' 0541200-9,-10 34.4' . WHEEL ABBY, CLEVELAND (EACH) C163001-Q1Q4 58.2 - BRAKE ABBY, CLEVELAND (EACH) C163030-1111 54.5...
Page 155 CESSNA SECTION 6 MODEL 172S WEIGHT BALANCE EQUIPMENT LIST & ITEM REF DRAWING EQUIPMENT LIST DESCRIPTION INS. 11.B~ 3.9" 3900016 GYRO INSTl, REQUIRES 37 01-$ USED & 34-08-0 WITH 34-14.Q 14.0 $3326-1 . ATIlTUOE GYRO 10.0 900016 . HOSES & MSIC HAROWARE 15.8 83291-1 TURN COORDINATOR INDICATOR...
Page 156 CESSNA SECTION 6 MODEL 172S WEIGHT & BALANCE / EQUIPMENT LIST ITEM EQUIPMENT LIST DESCRIPTION REF DRAWING INS: 53 • FUSElAG 53-01-8 REFUELING STEPS AND HANDLE INSTl 0513415-2 16.3 56-WINDOWS WINDOW - RIGHT HAND DOOR, 56-01-8 5.8~ 48.5' 0517001~40 OPENABlE 56-02-$ WINDOW - LEFT HAND DOOR,...
Page 157 CESSNA SECTION 6 MODEL 172S WEIGHT & BALANCE 1 EQUIPMENT LIST ITEM REF O-AAWING EQUIPMENT LIST DESCRIPTION INS. 73 • ENGINE FUEL CONTROL & 53277-4 73-01-$ EGT/FUEl FLOW INDICATOR ENGINE INDICATING 12.1 S3329.5 RECORDING TACHOMETER INSTALLATION 77-01-R 78 - EXHAUST .20.0' 16.3* 9954100-1...
Page 158 CESSNA SECTION 6 MODEL 172S WEIGHT & BALANCE 1 EQUIPMENT LIST ITEM EQUIPMENT LIST DESCRIPTION REF DRAWING INS. 98-02-A NAV I AVIONICS PKG (NET CHANGE OVER 3900004-1 21.3" 21.5" STANDARD AVIONICS PKG) - 34-10-A -GPS INSTALLATION 15.3 3930408-1 - 23-D3-A ~NAVICOM INSTL WITH G.S. 3930408-1 17,1 - 34-09-A -ADF INSTALLATION...
Page 160 CESSNA SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION SECTION 7 AIRPLANE,&SYSTEMS DESCRIPTION TABLE OF CONTENTS , Page Introduction '.' ... . . Airframe Flight Controls 7-6 . . .Trim System Instrument Panel Pilot Side Panel Layout .Center Panel Layout...
Page 161 CESSNA SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION TABLE OF CONTENTS (Continued) Page 7-19 Engine 7-19 Engine Controls 7.19 Engine Instruments 7-21 New Engine Break-In And Operation 7.21 Engine Lubrication System 7-22 Ignition And Starter System 7-22 Air Induction System 7.23 Exhaust System 7-23...
Page 162: Table Of Contents
CESSNA SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION TABLE OF CONTENTS (Continued) Page Lighting Systems """'......7-37 Exterior Lighting ,....7-37 Interior Lighting 7-37 Cabin Heating, Ventilating And Defrosting System ..7-39 Pitot-Static System And Instruments '....
Page 164 CESSNA SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION INTRODUCTION This section provides description and operation of the airpiane and its systems. Some equipment described herein is optional and may not be installed in the airplane. Refer to the sUPPlements'l Section 9, for details of other optional systems and equipment.
Page 165 CESSNA SECTION 7 MODEL 172S AIRPLANE SYSTEMS DESCRIPTION & The empennage (tail assembly) consists of a conventional verti- cal stabilizer, rudder, horizontal stabilizer, and elevator. The vertical stabilizer consists of a spar, formed sheet metal ribs and reinforce- ments, a wraparound skin panel, formed leading edge skin and a .
Page 166 CESSNA SECTION-7 MODEL 172S &- AIRPLANE SYSTEMS DESCRIPTION AILERON CONTROL SYSTEM 0585X1017 Figure 7-1_ Flight Control and Trim Systems (Sheet 1 of 2) July 8/98...
Page 167 CESSNA SECTION 7 MODEL'172S AIRPLANE & SYSTEMS DESCRIPTION ELEVATOR TRIM CONTROL SYSTEM 0585X1018 Figure 7-1. Flight Control and Trim Systems (Sheet 2 of 2) July 8/98...
Page 168 CESSNA SECTION-7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION INSTRUMENT PANEL The instrument panel. (Refer to Figure 7-2) is of all;metal construction, and is designed in segments to allow related groups of instruments, switches and controls to be removed without removing the entire panel.
Page 169 CESSNA SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION 18 19.20 i-C}] 0585C1040 •.• Figure 7-2. Instrument Panel (Sheet 1 of 2) Revision 4 7-10...
Page 170 CESSNA SECTION MODEL 1'72S AIRPLANE &'SY.STEMS DESCRIPTION Oil Temperature and Oil Hour Meter Pr~ssure Indicator Vacuum Gage and Ammeter Glove Box . 3. Fuel Quantity lridicato', 25: Cabin Heat Control EGT/Fuel Flow Indicator 26. Cabin Air Control Digital Clock I O.A.T. Flap Switch and.
Page 171 CESSNA SECTION 7. MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION RHSIDE PANEL LAYOUT EL T The RH panel contains the hour meter, switch, and room for expansion of indicators and other avionics equipment Below this sub panel are .the glove box, cabin heat and cabin air controls, and wing flap switch.
Page 172 CESSNA SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION WING FLAP SYSTEM The single-slot type wing flaps (Refer to Figure 7-3), are extended or retracted by positioning the wing flap switch lever on the instrument panel to the desired flap deflection position. The switch lever is moved up or down in a slotted panel that provides mechanical stops at the 10°, 20°...
Page 173 CESSNA SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION LANDING GEAR SYSTEM The landing gear is of the tricycle type, with a steerable nose wheel and two main wheels. Wheel fairings are standard equipment for both the main and nose wheels. Shock absorption is provided by the tubular spring steel main landing gear struts and the airloil nose gear shock strut.
Page 174 CESSNA SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION The rear passengers' seat consists of fixed, one piece seat bottom and a three-position, reclining back. The reclining back is adjusted by a lever located below the center of the seat frame. adjust the seat back, raise the lever, position the seat back to the .
Page 175 CESSNA SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION VERTICAL (HEIGHT) ADJUSTMENT CRANK SEAT SACK ANGLE SUDON FORE AND AFT BUCKLE ADJUSTMENT PRESSTO (NON ADJUSTABLE) LEVER RELEASE AVAILABLE MANUAL (PUSH SUDON) ADJUSTMENT ? /' PUSH SUDON ~~E:~E RELEASE •• (LATCH) 0514T1004 .
Page 176 CESSNA SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION A manually adustable seat belt/shoulder harness assembly available for all seats. To use the manually adjustable seat belt/shoulder harness, fasten and adjuslthe seat belt/shoulder harness first. Lengthen the seat belt as required by pulling on the 'release strap oli the belt. Snap the connecting link firmly into the buckle, then adjust to length.
Page 177 • CESSNA SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION NOTE . Accidental opening of a cabin door in flight due to improper . closing does not constitute a'need to land the airplane. The best procedure is to set up the airplane in a trimmed condition at approximately 75 KIAS, momentarily shove the...
Page 178 CESSNA SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION ENGINE The airplane is powered by a horizontally opposed,~ four cylinder, overhead valve, air-cooled,'.tueHnjected, engine with a wet sump lubrication system. The. engine is a Lycoming. Model IO-360-L2A and is rated at. .180 horsepower at 2700 RPM. Major accessories 'include a starter and belt driven alternator mounted on the tront of the engine, and dual magnetos, dual vacuum pumps, and a full flow oil filter mounted on the' rear of the engine accessory case ..
Page 179 CESSNA SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION pressure signals generated from pressur~ line/transducer combination. An oil pressure line is routed from the upper front 'of the engine case to the rear engine baffle. At the .baffle, the .oil pressure line is connected to a transducer.
Page 180 CESSNA SECTION 7 MODEL 172S . AIRPLANE & SYSTEMS DESCRIPTION The EGT system 'uses a thermocouple in the engine exhaust (tailpipe) supply voltage proportional exhaust temperature. The 'EGT indicator responds to the voltage developed by the thermocouple. As the mixture is leaned (from full rich), the .
Page 181 CESSNA SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION IGNITION AND STARTER SYSTEM Engine ignition is provided by two engine-driven magnetos, and 'two spark plugs in each cylinder.'The right magneto fires the lower , right and upper left spark plugs, and the left magneto fire's the lower , left and upper right spark plugs, Normal operation is conducted with Iboth magnetos due to the more complete burning of ,th!'l _fuellair...
Page 182 CESSNA SECTION 7 MODEL 172S AIRPLANE_&.SYSTEMS DESCRIPTION EXHAUST SYSTEM . Exhaust gas. from each cylinder passes through ri~er assemblies to a muffler and tailpipe. Outside air is pulled in, around shrouds which are constructed around the outside of the muffler to form heating chambers which supply heat to ihe cabin.
Page 183 CESSNA SECTION? MODEL 172S AIRPLANE &.$YSTEMS DESCRIPTION TOTAL USABLE . TOTAL TOTAL FUEL LEVEL FUEL ALL FLIGHT UNUSABLE (QUANTITY . FUEL TANKS . CONDITIONS EACH TANK) 53.0 Full (28.0) , 56.0" : 11 Figure 7-5. Fuel Quantity Data in U.S. Gallons FUEL DISTRIBUTION .
Page 184 CESSNA SECTION.? MODEL 172S .AIRPLANE & SYSTEMS DESCRIPTION FUEL INDICATING Fuel quantity is measured by two float type fuel quantity transmitters (one in each .tank) and indicated by an. electrically operated fuel quantity indicator on the left side of the instrument panel.
Page 185 -;;"1- ,CESSNA SECTION 7 MODEL 172S AIRPLANE SYSTt:MS DESCRIPTION & FUEL VENTING Fuel system venting is essential to ,system operation, Blockage' 'of the system will result in decreasing fuel flow and eventual engine stoppage, Venting is' accomplished by an interconnecting :Iine from the right fuel tank to the left ..tank.
Page 186 CESSNA SECTION 7 MODEL 172S. AIRPLANE & SYSTEMS DESCRIPTION i;-, FUEL QUANTITY INDICATORS LEFT RIGHT FUEL FUEL TANK TANK VENT - (WITH CHECK VALVE) oRAlN VALVES (5 TOTAL) FUEL SHUTOFF~ VAlVEKNOB LEGEND 1;.. ;:;;;:<:1':'"1 FUEL SUPPLY VENT MECHANICAL LINKAGE ELECTRICAL CONNECTION Figure 7-6.
Page 187 . ~ .. " j,--:...
Page 188 CESSNA SECTION 7 MODEL 172S . AIRPLANE & SYSTEMS DESCRIPTION 82113 FUEL QUANTITY INDICATORS FUEL FUEL QUANTITY, QUANTITY TRANSMITTER TRANSMITTER LEFT RIGHT. FUEL FUEL TANK TANK VENT (WITH CHECK DRAIN- VALVE) VALVES (5TQTAL) FUEl RETURN fUEL RESERVOIR DRAIN PLUG AUXILIARY FUEL PUMP SWITCH.
Page 189 CESSNA SEGTIGN7 MODEL 172S AI RPLANE&' SYSTEMS-DESCRIPTION NOTE When .the fuel .tanks 1/4' 'full" or . less, prolonged' uncoordinated flight such as slips or skids can uncover the fuel tank outlets. Therefore, if operating' with one fuel tank dry or if operating on LEFT or RI~HT tank when 1/4 full or less, do not allow the airplane to remain- in uncoordinated flight for periods in excess of 30 seconds.
Page 190 CESSNA SECTION 7 MODEl: 172S AIRPLANE & SYSTEMSDESCRIPTION BRAKE SYSTEM The airplane has a single-disc, hydraulically actuated brake on each. main landing gear wheel. Each brake is connected, by a hydraulic line, to a master cylinder attached to each of the pilot's rudder pedals.
Page 191 CESSNA SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION • 'j • • ~ • < r---------- ,ACU, ANNUNCIATOR . PANEL LOW VOLT,: RELD GROUND . SENSE POwE;R IN ALI INPUT, 'BUS 2 FUSE OR CIS - ALTERNATOR I • Ill, AMME}ER ~~gE'1...
Page 192 CESSNA SECTION MODEL 172S AIRPLANE & SYSTEMS-DESCRIPTION Figure 7-7. Electrical Schematic (Serials 172S8001.lhru 172S8703) (Sheet 2 of 2) Dec 30/00 7-30A...
Page 193 CESSNA SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION -ACU- ANNUNCIATOR PANEL LQWVOlT FIELD • GROUND SENSE POWER IN ALl-.INPUT BUS 2 FUSE OR CIB ,ALTERNATOR ,II, AMMETER BUS 1 FUSE ORC/B I'GNrTlO SWITCH MAGNETOS . ','1. TO CLOCK " BAT/ALT MASTER -7m...,--...
Page 194 CESSNA SECTION 7 . MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION TO GLARESHIELD LT CABIN OVERHEAD LTS COU RTESY LTS TSI . PWR 12V POWER O)~TO AVN FAN . .,..AVN FAN TO INSTRUMENTS O)~TOGPS ~ NST AND IGNITION :J GPS MFD ••...
Page 195 CESSNA SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION The airplane uses a power 'distributicintncidule '(J.Box), located _to',' on the left forward side of the firewall, hciuse' all relays used. throughout the airplane electrical system: ,In addition, the alternator control unit and the external power. connector are .housed within the, module, ',,',' •...
Page 196 CESSNA SECTION MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION MASTER SWITCH • The master switch is a split-rocker type switch labeled MASTER,. and is ON in' the up ..position and OFF in the down. position. The right half of ,the switch, labeled BAT, controls.the battery power to the airplane.
Page 197 CESSNA SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION AVIONICS MASTER SWITCH Electrical power for each Avionics .gus is supplied from a primary Electrical Bus. For airplane serial numbers 172S8001 through 172S8703, except for certain non-U.S. certified airplanes, both Avionics Buses are.
Page 198 >CESSNA SECTION 7 MODEL,172S . AIRPLANE & SYSTEMSDESCRIPTION" LOW VOLTAGE ANNUNCIATION ..The low 'voltage warning annunciator.is ..i ncorporated in' thel annunciator. panel and activates when voltage .falls below 24.5 volts. If low.voltage is detected; the red .annunciation VOL 1S will flash for approximately 10 ..seconds before illuminating' steadily.
Page 199 CESSNA SECTION MODEL 172S , AIRPLANE & SYSTEMS DESCRIPTION EXTERNAL POWER RECEPTACLE" " "~' 'An external power receptacle'is integral to the power distribution module and allows the use of an external electrical power source'for cold weather sta[ling" and' during lengthy maintenance work, on electrical and avionics equipment:.' T he receptacle is located on the leftside of the .engine cowling, just forward of the firewall and, midway up the ,side.
Page 200: Lighting Systems
CESSNA SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION LIGHTING SYSTEMS EXTERIOR LIGHTING Exterior lighting consists of navigation lights on the wing tips and top of the rudder, a dual landing/taxi light configuration located in the left wing leading edge, a flashing beacon mounted on top of the vertical fin, and a strobe light on each wing tip.
Page 201 CESSNA ,SECTION MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION Glareshield lighting is provo ided by either fluorescent light or a series of LED lights recessed into the lower surface of the glareshield. This light is controlled by rotating the GLARESHIELD LT dimmer, located below the nav indicators. Rotating the dimmer clockwise increases light...
Page 202: Cabin Heating, Ventilating And Defrosting System
CESSNA SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION CABIN HEATING, VENTILATING AND DEFROSTING SYSTEM The temperature and volume of airflow into the cabin can be regulated by manipulation of the push-pull CABIN HT and CABIN AIR controls (Refer to Figure 7-8). Both controls are the double- button locking type and permit intermediate settings.
Page 203 CESSNA SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION EXHAUST HEATER MUFFLER VALVE SHROUD CABIN AIR CONTROL CABIN HEAT CONTROL DEFROSTER OUTLETS (2 FORWARD FORWARD CABIN CABIN LOWER LOWER VENTILATING VENTILATIN AIR OUTLET AIR OUTLET RAM AIR REAR CABIN VENTILATING AIR OUTLETS (2) RAM AIR FLOW VENTILATING...
Page 204: Pitot-Static System And Instruments
CESSNA SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION PITOT-STATIC SYSTEM AND INSTRUMENTS The pitot-static system. supplies ram air pressure to the airspeed indicator and static pressure to the airspeed indicator; vertical speed indicator and altimeter. The system is composed of a heatedpitot tube.
Page 205: Vertical Speed Indicator
" 6~SSNA fvlOD~L172S INDloAToR AiRSP~~D " . rne airspeed iHi:iiealpr caiiBFfHe~ k~bl~,,it incofpofa~~s ifUe alrspe.ea alloWS alrspeell t6 Be off tne WindoW,WHich ,true reai:i iMorporates /:iial, ,Inaaallioni tHelfi~lcalof 'WlndoW iKe ,twelVe, o'clock posltiM WHich i:iisplilYs pressUre allllUl:le a temperalUre scale," "...
Page 206: Altimeter
CESSNA - SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION ALTIMETER Airplane altitude is depicted by a barometric type altimeter. A knob near the lower left portion of the indicator provides adjustment of the instrument's barometric scale to the current altimeter setting. VACUUM SYSTEM AND INSTRUMENTS The vacuum system...
Page 207 . CESSNA SECTION 7 MODEL 172S AIRPLANE SYSTEMS DESCRIPTION & CODE INLET.AIR LOW VACUUM . ,VACUUM SWITCHES (CONNECTED TO DISCHARGE .. . ANNUNCIATOR PANEL) .•. MANIFOLD CHECK VALVE. VACUUM SYSTEM . .~. AIR FILTER ATIITUDE INDICATOR DIRECTIONAL INDICATOR 0585C1014 Figure 7-9. Vacuum System July 8/98 7-44...
Page 208: Vacuum Gauge
CESSNA SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION VACUUM GAGE The vacuum gage is part of the vacuum gage/ammeter, located. on the lower left corner of the instrument panel. It is calibrated in inches of mercury and indicates vacuum air available for operation of the attitude and directional indicators.
Page 209: Clock / O.a.t.lndicator
CESSNA SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION .ClOCK / O.A.T. INDICATOR An integrated clock I OAT.' I voltmeter iS,instalied in the upper left 'side, of, the instrumimt,pariel as standard equipmentF6r comPlete description and' operating instructions, refer' to S~pplements, Section 9. ,", STAll WARNING SYSTEM.
Page 210: Avionics Support Equipment
CESSNA SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION AVIONICS SUPPORT EQUIPMENT Avionics operations are supported by the avionics cooling fan, microphone and headset installations.and static discharge wicks, AVIONICS COOLING FAN An avionics cooling fan is installed on the .Ieft side. of the interior firewall.
Page 211: Static Dischargers
CESSNA SECTION 7 MODEL 172S AIRPLANE SYSTEMS DESCRIPTION & NOTE To ensure audibility and clarity when transmitting with the handheld microphone, always hold it as closely as possible to the lips, then key the microphone and speak directly into it. Avoid covering opening on back side of microphone for optimum noise canceling.
Page 212: Cabin Features
CESSNA SECTION 7 MODEL 172S AIRPLANE & SYSTEMS DESCRIPTION CABIN FEATURES EMERGENCY lOCATOR TRANSMlnER (ElT) A remoteswiti:h/annunciator is' installed on. the . top center location of the copilot's' iristrument'panel for control 'of the ELT from the flight crew station, The annunciator, which is, in the~center of rocker switch, illuminates...
Page 213 CESSNA SECTION 7 MODEL 172S AIRPLANE SYSTEMS DESCRIPTION & " WARNING VENTILATE CABIN PROMPTLY AFTER SUCCESSFULLY EXTINGUISHING THE FIRE TO REDUCE THE GASES PRODUCED BY THERMAL ' • DECOMPOSITION. 3. Antic!pate' approximately eight. s ..ecorids of "~ischarge duration. •. Fire extinguishers-should be recharged - bya qualified fire...
Page 214 CESSNA SECTION.S MODEL 172S HANDLING, SERVICE & MAINTENANCE SECTION 8 AIRPLANE HANDLING, SERVICE & MAINTENANCE . TABLE OF CONTENTS Page Introduction Identification Plate :...... Cessna Owner Advisories ,..United States Airplane Owners : ..International Airplane Owners . Publications Airplane File Airplane Inspection Periods FAA Required Inspections...
Page 215: Table Of Contents Page
CESSNA SECTION 8 MODEL 172S HANDlING;SERVICE & MAINTENANCE TABLE OF CONTENTS (Continued) Page " Capacity of Engine Sump "',', ... ,.,', ... ,' 8-15 Oil and Oil Filler Change ","",.,.,',.,., .. ,",' 8-15 Fuel ,.,', ... ,""",.,.,.,., .. ,""',.,.,',.,. 8-16 .
Page 216: Introduction
CESSNA SECTION 8 MODEL 172S HANDLING, SERVICE & MAINTENANCE INTRODUCTION This section contains factory recommended procedures proper ground handling and routine care and servicing of your airplane. also identifies certain inspection maintenancEJi requirements which must be followed if your airplane is to retain that new airplane performance and dependability.
Page 217: Identification Plate
CESSNA SECTION 8 MODEL 172S HANDLING, SERVICE &'MAINTENANCE • IDENTIFICATION PLATE " All correspondence regarding yourairplarie should include' the Serial Number. The Serial Number, Model' Number; Production 'Certificate Number (PC) and Type Certificate Number (TC) can be found' on the ,Identification Plate, located on the aft left tailcone. A secondary Identification Plate is installed'oli the lower part of the left forward doorpost' on: earlier' serial number airplanes.
Page 218: United States Airplane Owners
CESSNA SECTION 8 MODEL 172S HANDLING, SERVICE& MAINTENANCE UNITED STATES AIRPLANE OWNERS If your airplane is registered in the U. S., appropriate Cessna Owner Advisories will.be m'ailed to you automatically according to the latest aircraft registration name and address which you have provided to the FAA.
Page 219: Airplane File
CESSNA SECTION 8 MODEL 172S HANDLING, SERVICE g, MAINTENANCE The following additional publications, plus many other' supplies that are applicable to your airplane, are available from your local Cessna Service Station. • Infotmation Manual (contains Pilot's Operating Handbook Information)" MaintenanCe .
Page 220: Airplane Inspection Periods
CESSNA SECTION 8 MODEL 172S HANDLING, SERVICE & MAINTENANCE To be carried in the airplane at all times: 1. Current .'Pilot's Operating Handbook FAA 'Appro~edl Airplane Flight Manual. 2. Weight and Balance, and associated papers (latest copy of the -Repair and Alteration Form, FAA Form.337, applicable) ..
Page 221: Cessna Inspection Programs
CESSNA SECTION 8 MODE~172S HANDLING, SERVICE MAINTENANCE & CESSNA INSPECTION PROGRAMS In lieu of the 100 hour and annual inspection requirements, an airPlane may. be ins. p ected in accordance with a Progressive Care Inspection Program or a PhaseCard Inspection Program. Both •...
Page 222: Cessna Customer Care Program
CESSNA SECTION 8 MODEL 172S HANDLING, SERVICE & MAINTENANCE CESSNA CUSTOMER CARE PROGRAM Specific benefits and provisions of the Cessna Warranty plus other important benefits. for you are contained' in your Customer Care Program Handbook supplied with your airplane. The customerl Care Program Handbook should be thoroughly reviewed and kept in the airplane at all times.
Page 223: . Alterationsor Repairs
CESSNA SECTION 8 MODEL 172S HANDLING, SERVICE & MAINTENANCE A Maintenance Manual must be obtained prior to performing any preventive maintenance to ensure that proper procedures Ifollowed. Your local Cessna Service Station should be contacted for further _information or for required maintenance.
Page 224: Parking
CESSNA SECTION 8 MODEL 172S HANDLING, SERVICE & MAINTENANCE ... ~""'. PARKING When parking the airplane, head into the wind and set the parking brake. Do not set the parking brake during cold weatherl when accumulated moisture may freeze the. brakes, or when the brakes are overheated.
Page 225: Leveling
CESSNA SECTION 8 MODEL 172S HANDLING, SERVICE & MAINTENANCE CAUTION DO NOT APpLY PRESSURE ON THE ELEVATOR, HORIZONTAL STABILIZER SURFACES. WHEN PUSHING ON THE TAILCONE, ALWAYS APPLY PRESSURE AT A BULKHEAD ~O AVOID BUCKLING THE SKIN .. If nose gear maintenance is required, the nose wheel may be raised off the ground by pressing down on a tailcone bulkhead, just forward of.
Page 226 CESSNA SECTION 8 MODEL 172S HANDLING, SERVICE & MAINTENANCE WARNING MAXIMUM SAFETY, CHECK THAT IGNITION SWITCH IS OFF, THE THROTILE CLOSED, THE MIXTURE CONTROL IS IN THE IDLE CUT OFF POSITION, AND THE AIRPLANE SECURED BEFORE ROTATING PROPELLER BY HAND; DO NOT STAND WITHIN THE ARC OF THE PROPELLER BLADES WHILE TURNING THE PROPELLER.
Page 227: Oil
MIL-L-22851 or SAE J1899 Aviation Grade Ashless Dispersant Oil: Oil conforming to Textron Lycoming Service Instruction 1014, and all. revision and supplements thereto, must be used after first 50 hours, or when oil consumption has stabilized. RECOMMENDED VISCOSITY FOR TEMPERATURE...
Page 228 CESSNA SECTION 8 MODEL 172S HANDLING, SERVICE & MAINTENANCE CAPACITY OF ENGINE SUMP The engine lubrication system has a total capacity of 9.quarts Ofl oil, with the oil filter accounting for 1 quart of that total. The engine oil sump (crankcase) has a capacity of 8 quarts: The engine' must not be operated with less than 5 quarts in the sump.
Page 229 CESSNA SECTION 8 MODEL 172S HANDLING, SERVICE & MAINTENANCE FUEL APPROVED FUEL GRADES (AND COLORS) 1OOLL'Grade Aviation Fuel (Blue). 100 Grade Aviation Fuel (Green). NOTE Isopropyl alcohol or diethylene glycol monomethyl ether (DiEGME) may be added to the fuel supply in quantities not to exceed 1% (alcohol) or 0.15% (DiEGME) of total volume.
Page 230 CESSNA SECTION 8 MODEL 172S HANDLING, SERVICE & MAINTENANCE One exception to this can be encountered when operating under the combined effect of: (1) use of certain fuels, with (2) high humidity conditions on the ground (3) followed by flight at high altitude and low temperature.
Page 231: May.30100
CESSNA SECTION 8 MODEL 172S HANDLING, SERVICE & MAINTENANCE ~1~:q-~t;4+-t4-t-:; : :.=-t' : -H~'!" ~;; :++-,: :.fj-'h: -H--t" "j ••• ! : !-H--!-f ;: : : ;-H.+ ' 4+' .. +f-!-.' ,i . - j.++J_ +H-+ t\--J--H+.H+ "+"j" ' . t-i-.ti :ttt.t+-t.-.-i.i ..
Page 232 CESSNA SECTION'S MODEL 172S HANDLlNG,.SERVICE & MAINTENANCE 2. An alternate method that may be used is to premix the complete alcohol dosage with some fuel in a separate clean "container" (approximately gallon' capacity) then transferring this mixture to the tank prior tothe.fuel operation. Diethylene glycol monomethyl ether (DiEGME) compound must be carefully mixed with the fuel in concentrations between 0.10%...
Page 233 CESSNA SECTION 8 MODEL 172S HANDLING, SERVICE & MAINTENANCE FUEL CONTAMINATION Fuel contamination is usually the result of foreign material present in the fuel system, and may consist of water, rust, sand, dirt, microbes or bacterial growth. In addition, additives that are not compatible with fuel or fuel system components can cause the fuel to become contaminated.
Page 234 CESSNA SECTION 8 MODEL 172S HANDLING, SERVICE & MAINTENANCE LANDING GEAR Consult the following table for servicing information on the .Ianding gear. COMPONENT SERVICING CRITERIA Nose Wheel (5.00-5, 6-Ply Rated Tire) 45.0 PSI Main Wheel (6.00-6, 6-Ply Rated Tire) 38.0 PSI Brakes MIL-H-5606' Nose Gear Shock Strut...
Page 235 CESSNA SECTION 8 MODEL 172S HANDLING, SERVICE & MAINTENANCE Follow by carefully washing with a mild detergent and plenty of water. Rinse thoroughly, then dry with a clean moist chamois. Do not rub the plastic with a dry cloth since this builds up an electrostatic...
Page 236 CESSNA SECTION 8 . MODEL 172S HANDLING, SERVICE & MAINTENANCE When the airplane is parked outside in cold climates and .it is necessary to remove ice before flight, care should be taken to protect the painted surfaces during ice removal with chemical liquids.
Page 237 CESSNA SECTION 8 MODEL 172S HANDLING, SERVICE & MAINTENANCE INTERIOR CARE To remove dust .and loose dirt .from the upholstery and carpet, clean the. interior regularly with a vacuum cleaner. Blot up 'any spilled liquid promptly with .cleansingtissue or' rags. Do not pat the spot;...
Page 238 CESSNA SECTION 9 MODEL 172S SUPPLEMENTS SUPPLEMENTS INTRODUCTION The supplements in this section contain expanded operational procedures for both standard and optional equipment installed in the .airplane. Operators should refer to each supplement to ensure that all limitations and procedures appropriate for their.
Page 240 CESSNA SECTION 9 MODEL 172S SUPPLEMENTS LOG OF APPROVED SUPPLEMENTS NOTE. IT IS THE AIRPL.ANE OWNER'S RESPONSIBILITY TO MAKE SURE THAT HE OR SHE HAS THE LATEST REVISION TO EACH SUPPLEMENT OF A PILOT'S OPERATING HANDBOOK AND THE LATEST. ISSUED "LOG OF APPROVED SUPPLEMENTS."...
Page 241 CESSNA SECTioN 9 MODEL 172S SUPPLEMENTS LOG OF APPROVED SUPPLEMENTS EQUIPMENT REVISION SUPPLEMENT NAME - SUPP. LEVEL- INSTALLED NO .. 12 _ Canadian Supplement: .•. Bendix/King KCS-55A Slaved Compass System with KI-525A • Horizontal Situation Indicator " (HSI) Reserved Bendix/King KAP 140 Axis .Autopilot Bendix/King KT 73 Mode S Transponder...
Page 242 ATexlron Company Pilot's Operating Handbook and .' FAA Approved Airplane Flight Manual CESSNA'MODEl172S AIRPLANES 17258001 AND ON SUPPLEMENT 1 BENDIX/KING KX 155A . VHF NAV/COMM with KI 208 or KI209A INDICATOR HEAD .", SERIAL NO .. ~__'_ REGISTRATION NO .. "-_ This supplement...
Page 243 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 1 - FAA APPROVED SUPPLEMENT 1 BENDIX/KING KX 155A VHF NAV/COMM with KI KI 209A INDICATOR HEAD The fDllDwing LDg of Effective' Pages prDvides the date Df issue fDr original and revised pages, as well asa listing 'Df all pages in . the Supplement.
Page 244 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 1 - FAA APPROVED SUPPLEMENT BENDIX/KING KX 155A VHF NAV/COMM with KI208 KI209A INDICATOR HEAD SECTION 1 GENERAL • The Bendix/King KX 155A VHF Nav/Comm, shown in Figure 1, consists of a panel-mounted receiver-transmitter and a KI 208 or KI 209A Indicator.
Page 245 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 1 - FAA APPROVED The Comm portion incorporates an automatic squelch. override the automatic squelch, ,the Comm volume control knob is pulled out. Push the knob back in to reactivate the automatic squelch.
Page 246 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 1 - FAA APPROVED -/22.1 1 Il.bO " 39:51!:J 3.00 • .cOMM. STBY STBY. PULL OBS 10 .9 • KX15~~VHF NAV/CC?MM ••• TO INDICATION ••. FROM INDICATioN •• ~ @I FLAG INDICATION "...
Page 247 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 1 - FAA APPROVED NAV FUNCTION DISPLAYS /09.EO --1\_- VOR MODE: ACTIVE/BEARING, CDI FORMAT I~~.~g ~ _~_~_~n) VOR MODE: ACTIVE/BEARING, FLAG DISPLAY . 109.50 VOR MODE: ACTIVE "BEARING TO" FUNCTION DISPLAY 109.50 VOR MODE: ACTIVE/BEARING, FLAG DISPLAY ..
Page 248 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 1 - FAA APPROVED 1. OPERATING COMM FREQUENCY DISPLAY Displays COMM ACTIVE and COMM STANDBY frequencies with a "T" between them to indicate TRANSMIT and an "R" to indicate RECEIVE modes of operation. 2.
Page 249 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 1 - FAA APPROVED 6. NAVIFREQUENCY TRANSFER BUTTON Interchanges the NAV Active and' STANDBY frequencies. Depressing the NAV frequency transfer button for 2 .seconds or more will cause the display to go into the ACTIVE ENTRY mode.
Page 250 CESSNA SEc;;TION 9 - SUPPLEMENTS' MODEL 172S SUPPLEMENT 1 - FAA APPROVED Another push of the mode button will cause the NAV display from the _ ACTIVE/BEARING . format .. to ACTIVE/RADIAL format. In the RADIAL.mode, the frequency inc/dec knobs challnel the ACTIVE frequency window...
Page 251 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 1 - FAA APPROVED 9. COMM FREQUENCY SELECTOR KNOB (INNER) -- This smaller knob is designed to change the indicated frequency in .. steps of 50-kHz when it is pushed in,. and in 25-kHz steps .when it is pulled out.
Page 252 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 1 - FAA APPROVED 12. COMM FREQUENCY TRANSFER BUTTON Interchanges the frequencies in the USE and STANDBY displays. To tune the radio to the desired operating frequency. the desired frequency must be entered into the standby display and then the transfer button must be pushed.
Page 253 . CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 1 - FAA APPROVED SECTION LIMITATIONS There is no change to the airplane limitations when this avionic equipment is insta!led. SECTION EMERGENCY PROCEDURES There is no change to the airplane emergency procedures when this avionic equipment is installed.
Page 254 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 1 - FAA APPROVED 6. Mic Button: a. To transmit -- Press button and speak in microphone. NOTE During COMM transmission, a lighted "T" will appear between the "COMM" and "STBY" displays to indicate that the transceiver is operating in the transmit mode.
Page 255 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 1 - FAA APPROVED GLiDESlOPE OPERATION The glideslope receiver is automatically channeled when a localizer frequency is selected. A separate warning flag is provided to indicate usable signal conditions. PilOT CONFIGURATION This mode can be. accessed by pressing and holding the NAV Mode Button for more than 2 seconds and then pressing the Nav Frequency Transfer Button Tor an additional 2 seconds, while continuing to hold the NAV Mode Button.
Page 256 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 1 - FAA APPROVED Subsequent presses of the MODE button sequences through SWRV, BRIM, SIDE, and then back to SWRV. Pressing Transfer Button momentarily exits Pilot configuration mode. The NAV returns to its pre-Pilot Config state with the new brightness and sidetone levels stored in nonvolatile memory.
Page 257 ~ill...
Page 258 ATextron Company .Pilot's Operating Handbook and FAA Approved Airplane Flight Manual CESSNA MODEL 172S AIRPLANES 11258001 AND ON SUPPLEMENT 2 BENDIX/KING KT 76C TRANSPONDER WITH BLIND ENCODER SERIAL NO .. _ ~~~~ REGISTRATION NO .. This supplement must be inserted into Section 9 of the...
Page 259 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 2 - FAA APPROVED SUPPLEMENT 2 BENDIX/KING KT 76C TRANSPONDER with BLIND ENCODER -" The following Log of Effective Pages provides the date of issue for original and revised pages, as well as a listing'of all pages in the Supplement.
Page 260 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 2 - FAA APPROVED SUPPLEMENT BENDIX/KING KT 76C TRANPONDER with BLIND ENCODER SECTION 1 GENERAL The Bendix/King Transponder (Type KT 76C), shown in Figure 1, is the airborne component of an Air Traffic Control Radar Beacon System (ATCRBS).
Page 261 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 2 - FAA APPROVED A VFR programming sequence, described in Section 4, allows the pilot to preprogram any single code such as "1200" into the KT 76C. Pressing the VFR button instantly returns the KT 76C to the preprogrammed code without having to manually enter "1200".
Page 262 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 2 - FAA APPROVED /200 [Q]mrnrnrnmrnITl \.~--- ----------_/ 1. IDENT BUnON (lOT) - When depressed, selects special identifier pulse to be transmitted with transponder reply to effect immediate identification of the airplane on the ground controller's' display.
Page 263 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 2 - FAA APPROVED 3. MODE ANNUNCIATORS - Displays the operating mode of the transponder. 4. REPLY INDICATOR (R) - "R" is illuminated momentarily when the transponder is replying to a valid interrogation and during the 18 :t2 seconds following the initiation of an Ident.
Page 264 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 2 - FAA APPROVED SECTION LIMITATIONS There is no change to the airplane limitations when this avionic equipment is installed. SECTION EMERGENCY PROCEDURES TO TRANSMIT AN EMERGENCY SIGNAL: 1. Mode Selector Knob -- ALT. 2.
Page 265 SECTION 9- SUPPLEMENTS CESSNA SUPPLEMENT 2 - FAA APPROVED MODEL 172S 2. Mode Selector Knob -- ON. NOTES • During normal operation with Mode Selector Knob in ON position, reply indicator flashes, indicating transponder replies to interrogations. • Mode A reply codes 'are transmitted in ALT also; however, Mode C codes are suppressed when the Mode Selector Knob is positioned to ON.
Page 266 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 2 - FAA APPROVED TO PROGRAM VFR CODE: 1. Mode Selector Knob -- SBY. 2. Numeric Keys 0-7 -- SELECT desired VFR code. 3. lOT Button -- PRESS AND HOLD. a. VFR Code Button -- PRESS (while still holding lOT button) place code nonvolatile...
Page 268 A le)(lron Company Pilot's Operating Handbook and FAA Approved Airplane Flight Manual CESSNA MODEL 1725 AIRPLANES 172S8001 AND ON SUPPLEMENT 3 BENDIX/KING KMA 26 AUDIO SELECTOR PANEL SERIAL NO. __ REGISTRATION This supplement must be inserted into Section '9 of the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual.
Page 269 SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 3 - FAA APPROVED MODEL 172S SUPPLEMENT 3 BENDIX/KING KMA 26 AUDIO SELECTOR PANEL The following Log of Effective Pages provides the date of issue for original and revised pages, as well as a listing of all pages in the Supplement.
Page 270 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 3- FAA APPROVED SUPPLEMENT BENDIX/KING KMA 26 AUDIO SELECTOR PANEL . SECTION 1 GENERAL The Bendix/King KMA 26 Audio Selector Panel is a combination audio amplifier, an audio distribution panel intercom, and a marker beacon receiver.
Page 271 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 3 - FAA APPROVED "" '" '""0 !COMi1 ~ fNAV2] INAV1I laO: INTERCOM t==J B EJ B PUSH .. : :; ~ [~I[~][~I ~ ' PUSH SPKR 1. MARKER BEACON ANNUNCIATOR LIGHTS -- Thethree-light marker beacon receiver built into the KMA 26 gives a visual.
Page 272 CESSNA SECTION 9 ~SUPPLEMENTS MODEL 172S SUPPLEMENT 3 - FAA APPROVED 3 MARKER BEACON SENSITIVITY LAMP AND TEST SWITCH --The "MKR" Audio. Select button must be pushed so that the green annunciator is illuminated for the marker beacon to receive to provide an audio signal at beacon passage. When this switch...
Page 273 SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 3 - FAA APPROVED MODEL 172S 6. SPEAKER SELECT (PUSH SPKR) SWITCH -- With Speaker Select Switch pushed in, both headphone and cabin speaker audio will be heard .. Headphone audio is active full- time.
Page 274 CESSNA SECTION 9 - SUPPLEMENTS' MODEL 172S SUPPLEMENT 3 - FAA APPROVED 10. INTERCOM MODE SELECT SWITCH -- Has three modes "ALL", "CREW", AND "PILOT" which are 'selected with the toggle switch on the lower left side on the faceplate. In the "ALL"...
Page 275 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 3 - FAA APPROVED SECTION 2 LIMITATIONS There is no change to the airplane limitations when this avionic equipment is installed. SECTION 3 EMERGENCY PROCEDURES In the event of a failure cif the audio amplifier in the KMA 26, as evidenced by the inability to transmit in COM 1, 2 or 3.
Page 276 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 3 - FAA APPROVED MARKER BEACON RECEIVER OPERATION: 1. TEST Position -- HOLD toggle down momentarily to verify all lights are operational. 2. SENS Selections -- Select HI sensitivity for airway flying or LO for ILS/LOC approaches.
Page 278 Cessna A Textron Company Pilot's Operating Hand~ook and FAA Approved Airplane Flight Manual CESSNA MODEL 1725 AIRPLANES 17258001 AND ON SUPPLEMENT 4 POINTER MODEL 3000-11 OR MODEL 4000-11 EMERGENCY LOCATOR ~RANSMITTER SERIAL NO .. _ _ REGISTRATION This supplement must be inserted into Section 9 of the Pilot's Operating...
Page 279 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 4 - FAA APPROVED SUPPLEMENT 4 POINTER MODEL 3000-11 OR MODEL 4000-11 EMERGENCY LOCATOR TRANSMITTER (ELT) ." Use the Log of Effective Pages to determine the current status of this supplement. Pages affected by the current revision are indicated by an asterisk (*j"preceeding the page number.
Page 280 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 4 - FAA APPROVED SUPPLEMENT 4 POINTER MODEL 3000-11 OR MODEL 4000-11 EMERGENCY LOCATOR TRANSMITTER (ELT) SECTION 1 GENERAL This supplement provides information which must be observed when operating the Pointer Model 3000-11 or Model 4000-11 Emergency Locator Transmitter.
Page 281 CESSNA. SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 4 - FAA APPROVED In accordance with FAA regulations, the ELT's battery pack must be replaced after 2 years shelf or service life or for any of the following reasons: a. After the transmitter has been used in an emergency situation .
Page 282 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 4 - FAA APPROVED OFF/RESET -' b~activatestransmitter during handling, following rescue and to reset the automatic activation function. (The red annunciator in the center of the remote switch/annunciator should extinguish). 5. REMOTE SWITCH/ANNUNCIATOR (3-position rocker switch): ON -- Remotely activates the transmitter for test or emergency...
Page 283 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 4 - F.AAAPPROVED 4. MASTER FUNCTION SELECTOR SWITCH (3-position toggle switch): ON -- Activates transmitter instantly. Used for test .purposes and if "G" switch is inoperative. ON position bypasses the' automatic activation switch.
Page 284 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 4 - FAA APPROVED SECTION 3 EMERGENCY PROCEDURES Before performing a forced landing, especially in remote" and mountainous areas, activate the ELT transmitter by positioning the remote switch/annunciator to the ON position. The annunciator in center of the rocker switch should be illuminated.
Page 285 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S . SUPPLEMENT 4 - FAA APPROVED SECTION 4 NORMAL PROCEDURES As long as the remote switch/annunciator is in the AUTO position and the ELT master function selector switch remains in the AUTO position, the ELT automatically activates when the unit. senses longitudinal inertia forces as required in TSO-C91 A.
Page 286 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 4 - FAA APPROVED 7. Place the ELT master function selector.switch in the OFF/RESET position. 8. Reposition ELT master function selector switch to AUTO. 9. Reconnect antenna cable to ELT. WARNING A TEST WITH THE ANTENNA CONNECTED...
Page 287 • ',> • , "...
Page 288 ATextron Company Pilot's Operating Handbook and FAA Approved Airplane Flighi Manual CESSNA MODEl172S AIRPLANES 172S8001 AND ON SUPPLEMENT 5 BENDIX/KING KLN 89B GLOBAL POSITIONING SYSTEM (IFR) .• SERIAL ttO .. REGISTRATION This'supple"ment must be inserted into Section 9 of the Pilot's Operating Handbook and -FAA Approved Airplane Flight Manual when the Global Positioning...
Page 289 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 5 - FAA APPROVED SUPPLEMENT 5 BENDIX/KING KLN 89B GLOBAL POSITIONING SYSTEM (IFR) The following Log of Effective Pages provides the date of issue for original and revised pages, as well as a listing of all pages in the Supplement.
Page 290 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 5 - FAA APPROVED SUPPLEMENT 5 BENDIX/KING KLN 89B GLOBAL POSITIONING SYSTEM (IFR) SERVICE BULLETIN CONFIGURATION LIST The following is a list of Service Bulletins that are applicable to the operation of the airplane, and have been incorporated into this supplement.
Page 291 CESSNA SI::CTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 5 - FAA APPROVED SUPPLEMENT BENDIX/KING KLN 89B GPS NAVIGATION SYSTEM (IFR) SECTION 1 GENERAL WARNING IS NOT AUTHORIZED INSTRUMENT APPROACHES UNLESS OPERATIONAL REVISION STATUS UPGRADED TO "ORS 02" OR LATER, AS READ ON- THE POWER-ON PAGE, AND THE HOST SOFTWARE IS UPGRADED TO "HOST '00880- 0004"...
Page 292 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 5 - FAA APPROVED database card electronic memory containing information airports, navaids, intersections, SID's, STAR's, instrument approaches, special use airspace, and other items of interest to the pilot. Every 28 days, Bendix/King receives new database information from Jeppesen Sanderson for the North American database region.
Page 293 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 5 - FAA APPROVED NOTE Aircraft using GPS for oceanic IFR operations may use the KLN 89B to replace one of the other approved means of long range navigation. A single KLN 89B GPS installation may also be used on short.
Page 294 CESSNA SECTION 9 - SUPPLEMENTS MODEL172S SUPPLEMENT 5 - FAA APPROVED 0585C1042 (MSG) 1. GPS MESSAGE ANNUNCIATOR LIGHT -- will begin flashing whenever the message prompt (a large "M" on the lett side of the screen) on the KLN 898 GPS unit begins flashing to alert the pilot that a message is waiting.
Page 295 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 5 - FAA APPROVED j\WARNING TURN ANTICIPATION" AUTOMATICALLY DISABLED FOR FAF WAYPOINTS AND THOSE USED EXCLUSIVELY IN SID/STARS WHERE OVERFLIGHT IS REQUIRED. FOR WAYPOINTS SHARED BETWEEN SID/STARS PUBLISHED EN ROUTE SEGMENTS (REQUIRING OVERFLIGHT.
Page 296 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 5 - FAA APPROVED 6. NAV/GPS SWITCH -- Toggles from Nav 1 to GPS and vice versa to control the type of navigation data to be displayed on the COl (Course Deviation Indicator). The No.
Page 297 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 5 - FAA APPROVED SECTION LIMITATIONS 1. The KLN 89B GPS Pilot's Guide, PIN 006-08786-0000, dated May, 1995 (or later applicable revision) must be available to the flight crew whenever IFR GPS navigation is used. Operational Revision Status (ORS) of the Pilot's Guide must match the ORS level annunciated on the Self Test page.
Page 298 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 5 - FAA APPROVED 3) APR ACTV mode must be annunciated at the Final Approach Fix. 4) Accomplishment of ILS, LOC,' LOC-BC, LDA, SDF, and • MLS approaches are not authorized. 5) When an alternate airport is required by the applicable operating rules, it must be served by an approach based on other than GPS or Loran-C navigation.
Page 299 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 5 - FAA APPROVED f. The aircraft must have other approved navigation equipment appropriate to the route of flight installed and operational. SECTION EMERGENCY PROCEDURES There are no changes to the basic airplane emergency procedures when the KlN 89B GPS is installed.
Page 300 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 5 - FAA APPROVED WARNING PREVENT THE POSSIBILITY OF TURN ANTICIPATION ,CAUSING POTENTIALLY MISLEADING NAVIGATION WHEN AIRCRAFT IS NOT ONCOURSE,.vERIFY THE COl COURSE- AND COl NEEDLE PRESENTATION IS PROPER PRIOR "TO TAKEOFF AND DO NOT SWITCH FROM OBS TO LEG WITH GREATER THAN 1 NM CROSS TRACK ERROR (XTK);...
Page 301 CESSNA SECTION 9- SUPPLEMENTS MODEL 172S, SUPPLEMENT 5 - FAA APPROVED APPROACH MODE SEQUENCING AND RAIM PREDICTION AWARNIN!3 FAMILIARITY WITH THE EN'ROUTE OPERATION OF THE'KLN89B WILL' NOT CONSTITUTE PROFICIENCY IN' APPROACH OPERATIONS. APPROACH OPERATIONS SHOULD NOT BE ATIEMPTED . IN, ,(INSTRUMENT METEOROLOGICAL CONDITIONS) PRIOR TO ATIAINING...
Page 302 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 5 - FAA APPROVED 2. En route, check for RAIM availability at the destination airport ETA on the OTH 3 page. NOTE RAIM must be available at the FAF in order to fly an instrument approach.
Page 303 CESSNA SECTION 9 - SUPPLEMENTS MODEll72S SUPPLEMENT 5 - FAA APPROVED NOTE Select HOG mode for DME arc intercepts. NAV or APR coupled intercepts result excessive overshoots (aggravated by high ground speeds and/or intercepts from inside the arc). >. WARNING "...
Page 304 CESSNA SECTION 9- SUPPLEMENTS' MODEL 172S SUPPLEMENT 5 - FAA APPROVED 8. Missed Approach: a. Climb. b. Navigate to the MAP (in APRARM if APR ACTV is not available). NOTE There is no automatic LEG sequencing at the MAP. 'c. After 'climbing in accorda'nce with the published missed approach procedure, press the Direct To button, verify or change the desired holding fix and press ENT.
Page 305 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 5 - FAA APPROVED • Waypoint suffixes in the flight plan: i -- f -- m -- MAP h -- missed approach holding fix, .The DME arc IAF (arc intercept waypoint) will be on your present position radial off the arc VOR when you load the IAF into the flight plan, or the beginning of the arc if currently on a radial beyond the arc limit.
Page 306 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 5 - FAA APPROVED < • The instrument approach using the KLN 89B may be essentially • automatically started 30 nm out (with a manual baro setting update) or it may require judicious selection of the OBS and LEG modes, •...
Page 307 • " ..:.. 'f':fC-"~~ '" •• < "...
Page 308 Cessna . ATenron Company. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual CESSNA MODEl172S .AIRPLANES 17258001 AND ON SUPPLEMENT 6 BENDIX/KING KR87 AUTOMATIC DIRECTION FINDER (ADF) SERIAlNO._~~ REGISTRATION NO.~ This suppleme'nt must be inserted into Section 9 of the Pilot's Operating Handbook and FAA Approved...
Page 309 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 6 - FAA APPROVED SUPPLEMENT 6 BENDIX/KING KR 87 AUTOMATIC DIRECTION FINDER (ADF) The following Log of Effective Pages pro~ides the date of issue for original and revised pages, as.well as a.listing of all pages in the Supplement.
Page 310 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 6 - FAA APPROVED '~SUPPLEMENT BENDIX/KING KR 87 AUTOMATIC DIRECTION FINDER (ADF) SECTION 1 GENERAL The Bendix/King Digital ADF is a panel-mounted. digitally tuned automatic direction finder. It is designed to provide continuous kHz digital tuning in the frequency 'range of 200-kHz to 1799-kHz and eliminates the need for mechanical...
Page 311 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 6 - FAA APPROVED < ADF KR87 TSO 1211 0585Cl043 0585Cl044 Figure 1. KR 87 Automatic Direction Finder (ADF) (5heet 1of 4) 56-4 JUly 8/98...
Page 312 CESSNA SECTION 9 . SUPPLEMENTS MODEL 172S SUPPLEMENT 6 - FAA APPROVED 1. ANT/ADF MODE ANNUNCIATOR' Antenna (ANT) selected by the "out" position of the ADF button. This mode improves the audio reception and is usually used for station identification. The bearing pointer is deactivated and will park in the 90°...
Page 313 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 6 - FAA APPROVED < 5. FLIGHT. TIMER ELAPSED TIMER MODE ANNUNCIATION -- Either the elapsed time (ET) or flight time (FL T) mode is annunciated here. 6. FREQUENCY SELECT KNOBS --. SeleCts, the standby frequency when FRQ is displayed...
Page 314 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 6 - FAA APPROVED 10. FREOUENCY TRANSFER BUTTON (FRO) -- The transfer button when pressed exchanges the active standby.frequencies. The new frequency becomes active and .the former active frequency goes into standby. 11.
Page 315 CESSNA SECTION 9 - SUPPLEMENtS MODEL: 172S SUPPLEMENT 6 - FAA APPROVED SECTION 2 , LIMITATIONS There is no change to airplane limitations when the K'R 87 ADF is installed, SECTION 3 EMERGENCY PROCEDURES There changes to the basic airplane emergency procedures when the KR 87 ADF is installed, SECTION 4...
Page 316 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 6 - FAA APPROVED TO OPERATE BFO: 1. OFFNOL Control -- ON. 2. BFO Button -- PRESS on. 3. ADF Selector Buttons (on audio control panel) -- SET to desired mode.' 4. VOL Control -- ADJUST to desired listening level. NOTE A 1OOO.Hztone and Morse Code identifier is heard in the audio output when a CW signal is received.
Page 317 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 6 - FAA APPROVED TO OPERATE ELAPSED TIME TIMER.COUNTUPMODE:'" 1, OFFNOL Control -- ON. 2, FL Mode Button -- PRESS (once'.or twice) until ET is TIET annunciated. 3, SETIRST Button -- PRESS momentarily to reset elapsed timer to zero, ,.' NOTE The Standby Frequency which is in memory while Flight...
Page 318 CESSNA SECTION 9 - SUPPLEMENTS MODEL.172S SUPPLEMENT 6 - FAA APPROVED ADF OPERATION NOTES: ERRONEOUS ADF BEARING DUE TO RADIO FREQUENCY PHENOMENA: the U,S., the FCC, which assigns. AM radio frequencies, occasionally, will assign, the same frequency to more than one station in an area, Certain conditions, such as Night Effect, may cause signals from such stations to overlap, This should be taken into consideration when using AM broadcast station for navigation,...
Page 319 CESSNA S.ECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 6 - FAA APPROVED <r" ' • 'i:". . SECTION •• PERFORMANCE There is no change to. the airplane performance when this avionic equipment is installed. However, the .installation, of an externally mounted antenna or related external antennas, may result in a minor reduction in cruise performance.
Page 320 Cessna A Textron C<lmpany .Pilot's Operating Handbook and FAA Approved Airplane Flight Manual CESSNA MODEL 1725 . AIRPLANES 172S8001 AND ON SUPPLl~:MENt 7 BENDIX/KING KAP 140 SINGLE AXIS AUTOPILOT SERIALNO •• REGIS1RATIONNO .. _ _ . This supplement must be' inserted into Section -9 of the,'Pilat's...
Page 321 SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 7 - FAA APPROVED MODEL 1725 SUPPLEMENT 7 BENDIX/KING KAP 140 SINGLE AXIS AUTOPILOT Use the LOg, . ot. Effective Pages t,o,determine th,e current .status ot this supplement. • Pages affected by 1he current revision indicated by'an asterisk (*) preceeding the page number.
Page 322 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 7 - FAA APPROVED SUPPLEMENT 7 BENDIX/KING KAP 140 SINGLE AXIS AUTOPILOT SERVICE BULLETIN CONFIGURATION LIST The following is a list of Service Bulletins that are applicable to the operation of the airplane, and have been incorporated into this supplement.
Page 323 • •••• '" "...
Page 324 CESSNA . SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 7 - FAA APPROVED SUPPLEMENT 7 BENDIX/KING KAP 140 .SINGLE AXIS AUTOPILOT SECTION 1 GENERAL " The Bendix/King KAPl40is an all-electric, single-axis ,(aileron control) autopilot system that provides lateral and directional control. Components are a computer, a turn coordinator, an aileron actuator, a course deviation indicator, and a directional indicator or HSI (if...
Page 325 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 7 - FAA APPROVED The following circuit breakers are used to protect the listed elements ~f the KAP 140 single axis autopilot: FUNCTIONS LABEL Supplies power to the KC 140 AUTO Computer and the autopilot PilOT Supplies power...
Page 326 " CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 7 - FAA APPROVED NAVlCOM'" 1 ••• CONTROL PANEL "" ••• !!ill ;. "'"'''' " " HORIZONTAL SITUATION " " INDICATOR " " NAVIGATION SOURCE SELECTOR SWITCH CONTROL WHEEL TURN COORDINATOR ACTUATOR AUTOPILOT COMPUTER...
Page 327 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 7- FAA APPROVED K AP 140 HI> G "- t-:' ,'I ' ".r • L ROLL (R) AXIS ANNUNCIATOR --When illuminated, indicates a tailure in the roll axis' and 'prevents. engagement diseQgages the autopilot.', .
Page 328 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 7 - FAA APPROVED 4. NAVIGATION (NAV) MODE SELECTOR BUnON -- When pushed, will select the Navigation mode. This mode provides automatic beam capture and tracking ot VOR, LOC, or GPS signa.lsas selected for presentation on the NAV#1CDI or HSI (if installed).
Page 329 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT7 - FAA APPROVED 11.WARN Power to the autopilot disconnect horn. CIS -- ...T 2. AUTOPILOT ENGAGE An~unciatioh" lIiuminates . . whenever theautopilol is engaged. Flashes during pflot initiated or auto'maticdisengagement. * ,Airplane serials 172S8001 thru 172S9128 not incorporating Honeywell Service Bulletin KCI40-Ml."...
Page 330 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 7 - FAA APPROVED. SECTION 3 EMERGENCY PROCEDURES The two step procedure listed under paragraph 1 should be among the basic airplane emergency procedures that are committed to memory. It is important that the pilot be proficient in accomplishing both steps without reference to this manual.
Page 331 . 6iissNA Mob~L1Y2S I:MER<3ENGY AMPliFiED PRoCEDURES ,',- ' -' THe loiioWing p'aragrapHs_are presentea. to ~UpplY aatlitional " inlormaHon for,lhe ,pUfpO,se 61 proVioingihe, Pilo,Wi,fl a, mqre complete Unaeri';tanoingof the recommended coUrse of action for ali emergency siiUatibH, AWA~NiNG ATtEMpT NbT. RE-ENbA<3E,.THE AUTOpiLOT _ fbLLOWiNG., AUtopilOT MALFUNoTiON .
Page 332 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 7-FAA'APPROVED NOTE An exception to this is HDG annunciation which will flash for 5 seconds along with steady NAVARM, APRARM, ,REVARM annunciation to remind the pilo.t to set the HDG bug for course datum use, . 1,' Flashing HDG -- Indicates a failed heading.
Page 333 CESSNA SECTION 9 - SUPPLEMENTS MODEL.172S SUPPLEMENT 7 - FAA APPROVED SECTION 4 NORMAL PROCEDURES PREFLIGHT W.ERFORMPRIOR TO EACH FLIGHT» 1. GYROS -- Allow time for the turn coordinator to come up to speed, as evidenced by the turn coordinator ,flag being pulled from view.
Page 334 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 7 - FAA APPROVED AUTOPILOT ENGAGEMENT: AP Button -- PRESS. Note ROL annunciator on. If no other modes are selected the autopilot will operate in the ROL mode. NOTE Aircraft heading change mode turbulence.
Page 335 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 7 - FAA APPROVED NOTE All angle intercepts compatible with radar vectors may be accomplished. by selecting ROL mode PRIOR to pressing the NAV button. The HOG bug must still be positioned to agree with the OBS course to provide course datum to the autopilot when using a DG (Directional Gyro).
Page 336 CESSNA SECTION 9 - SUPPLEMENTS MODEL 1'72S, SUPPLEMENT 7 - FAA APPROVED APPROACH (APR) COUPLING: (To enable glideslope coupling on an ILS and more precise tracking on instrument approaches). 1. When equipped with DG: Knob -- desired approach course. (For NAV #1 OBS SELECT a localizer, set it to serve as a memory aid.)
Page 337 CESSNA SECTION 9 - SUPPLEMENTS MODEL172S SUPPLEMENTt - r-AA APPROVED 2) If the CDI needle is less than 2 to 3 dots from center, the HDG mode will' disengage upon selecting APR mode; the APR annunciator will, illuminate and the'capture/track sequence will automatically begin.
Page 338 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 7 - FAA APPROVED NOTE • When REV is selected, the autopilot will flash HDG • for 5 seconds to remind the pilot to reset the HDG bug to the localizer FRONT COURSE INBOUND heading.
Page 339 CESSNA SECTION SUPPLEMENTS MODEL 172S SUPPLEMENT 7 - FAA APPROVED 2) If the D-Bar is less than 2 to 3 dots from center, the HOG mode will disengage upon selecting REV mode; the REV :annunciator will illuminate capture/track '. sequence will automatically begin. d.
Page 340 Cessna A Textron Compall)' pilot"s Operating Handbook and FAA Approved Airplane Flight Manual CESSNA MODEL 1725 AIRPLANES 17258001 AND ON SUPPLEMENT 8 WINTERIZATION KIT SERIAL NO. REGISTRATION NO._. This supplement must be inserted 'into Section 9 of the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual when the Winterization is installed.
Page 341 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 8 - FAA APPROVED SUPPLEMENT 8 WINTERIZATION KIT The Iollowing Log of !=ffective Pages provides the date at issue for original and revised pages, as well as a listing of all pages in the Supplement.
Page 342 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 8 - FAA APPROVED SUPPLEMENT WINTERIZATION KIT SECTION 1 GENERAL The winterization kit consists of tWD cover plates (with placards) which attach tD the air intakes in the cowling nose cap, a piacard silk screened Dn the instrument...
Page 343 SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 8 - FAA APPROVED MODEL 172S SECTION EMERGENCY PROCEDURES There is no change to the airplane emergency procedures when the winterization kit is installed. SECTION 4 NORMAL PROCEDURES There is no change to the airplane normal procedures when the winterization kit is installed.
Page 344 ATex1ron C<Jmpany Pilot's Operating Handbook and FAA Approved Airplane Flight Manual CESSNAMODEl172S AIRPLANES 172S8001 AND ON SUPPLEMENT 9 DAVTRON MODEL 803 CLOCK/O.A.T. SERIALNO. REG~RAnDNNO. This supplement must be inserted into Section 9 of the Pilot's Operating Handbook Approved Airplane Flight Manual when Davtron...
Page 345 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 9 - FAA APPROVED SUPPLEMENT 9 DAVTRON MODEL 803 CLOCK/O.A.T. The following Log of Effective Pages provides the date of issue for original and revised pages, as well as a listing of all pages in the Supplement Pages which' are affected by the current revision ~ill carry the date of tha! revisi~n...
Page 346 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 9 - FAA APPROVED SUPPLEMENT DIGITAL CLOCK/O.A.T. SECTION 1 GENERAL The Davtron Model 803 digital clock combines the features of a clock, outside air temperature gauge (OAT.) and. voltmeter in a single unit. The unit is designed for ease of operation with the use of three buttons.
Page 347 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 9 - FAA APPROVED UPPER BUTTON • UPPER LCD OAT. WINDOW 2LJ.OE LOWER sq:sq. WINDOW FTS! CONTROL 0785C1005 SELEC CONTROL BUTTON BUTTON Figure 1. Clock/OAT G,!uge SECTION 4 NORMALPRqCEDURES TEST MODE The unit may.be tested'by holding'the5ELECT button 'down for three seconds.
Page 348 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 9 - FAA APPROVED CLOCK OPERATIONS The lower portion of the LCD window is dedicated to clock and timing operations. Pushing the SELECT button will sequence the window from universal time (UT) to local time (LT) to flight time (FT) to elapsed time (ET), and back again to universal time.
Page 349 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENt 9 - FAA APPROVED SETTING FLIGHT TIME FLASHING ALARM ' SELECT button select flight ,time (FT), Simultaneously press both the SELECT and,the CONTROL buttons to enter the set mode, The tens of ~ours digil will start flashing. The set operation is the same as for UT.' When actual flight time equals the alarm time, the display will flash.
Page 350 ATextron Company Pilot's Operating Handbookand FAA Approved Airplane Flight Manual CESSNA MODEL 172S AIRPLANES 172S8001 AND ON SUPPLEMENT 10 ,BENDIX/KING KLN 89 VFR GLOBAL POSITIONING SYSTEM. (GPS) SERIAL NO. REGISTRATION NO. This supplement must be inserted into Section 9 of the Pilot's Ope;ating Handbook and FAA Approved Airplane Flight Manual when the Global Positioning SyS:t~m is installed.
Page 351 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 10 - FAA APPROVED SUPPLEMENT 10 BENDIX/KING KLN89 IVFR'GLOBAL POSITIONING SYSTEM (GPS) The following Log 'of Effective Pages provides the dai'e of issue for original and revised pages, as well as a listing of all pages in the Supplement.
Page 352 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 10- FAA APPROVED SUPPLEMENT BENDIX/KING KLN 89 .VFR GLOBAL POSITIONING SYSTEM (GPS) SECTION 1 GENERAL The BendiX/King KLN 89 is a navigation system based on the Global Positioning Satellite network. It contains a database cartridge which updated by subscription.
Page 353 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 10 - FAA APPROVED SECTION NORMAL PROCEDURES There. change basic airplane normal operating procedures with the KLN 89 GPS installed. SECTION PERFORMANCE" There is no change to the airplane performance when the KLN 89 GPS is installed.
Page 354 ATextron Company Pilot's Operating Handbook and FAA Approved Airplane Flight Manual CESSNA MODEL 1725 AIRPLANES 172S8001 AND ON SUPPLEMENT 12 -CANADIAN SUPPLEMENT SERIAL NO REGISlRAllON NO This supplement must be inserted into Section 9 of the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual when used for Canadian Operation.
Page 355 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 12 - FAA APPROVED SUPPLEMENT 12 CANADIAN SUPPLEMENT The fallowing Log of Effective Pages provides the date of issue for original and revised pages, as well a listing of all pages in the Supplement Pages which are affected...
Page 356 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 12 - FAA APPROVED SUPPLEMENT . CANADIAN SUPPLEMENT SECTION 1 GENERAL This supplement is required for Canadian operation of Cessna Model 172S. SECTION LIMITATIONS The following placard must be installed. 1. Near the fuel tank filler cap: FUEL 100LU 100 MIN.
Page 357 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 12 - FAA APPROVED .SECTION EMERGENCY PROCEDURES There is no change to the airplane 'emergency procedures when used for Canadian operation. SECTION 4 NORMAL PROCEDURES There change basic airplane normal operating procedures when used for Canadian.operation. SECTION PERFORMANCE \.
Page 358 ATextron Company Pilot's Operating Handbook and FAA Approved Airplane Flight Manual CESSNA MODEL 1725 AIRPLANES 17208113 AND ON SUPPLEMENT 13 BENDIX/KING KCS-55A SLAVED COMPASS SYSTEM _WITH KI.525A HORIZONTAL SllUATION INDICATOR (HSI) SERIAL NO ---- REGISTRATION NO .. This supplement must be inserted into Section.
Page 359 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 13-FAAAPPROVED SUPPLEMENT 13 BENDIX/KING KCS-55A SLAVED COMPASS SYSTEM WITH KI-525A HORIZONTAL SITUATION INDICATOR (HSI) The following Log of Effective.Pages provides the date of issue for original and revised pages, as well as a listing of all pages in the Supplement.
Page 360 CESSNA SECTiON 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 13 - FAA APPROVED SUPPLEMENT 13 BENDIX/KING KCS-55A SLAVED COMPASS SYSTEM WITH KI-525A HORIZONTAL SITUATION INDICATOR (HSI) SECTION 1 GENERAL The Bendix/King KCS-55A Slaved Compass System with KI- 525A HSI Indicator.is an additional navigation indicator option. KCS-55A compass system...
Page 361 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 13 - FAA APPROVED Figure 1. Horizontal Situation Indicator S'ystem (Sheet 10f 2) HORIZONTAL SITUATION INDICATOR (HSI) -- Provides .pictorial presentation of aircraf1 deviation relative to VOR/GPS radials and localizer beams. It also displays glide slope deviations gives...
Page 362 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 13 - FAA APPROVED 6. TO/FROM INDICATOR -- Indicates direction of VOR station relative. to the selected course. Displays TO when a LOC frequency is selected. 7. DUAL GLIDE SLOPE POINTERS -- Displays deviation of airplane from an ILS glideslope.
Page 363 SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 13 - FAA APPROVED MODEL 172S Figure 2. KA-51 B Slaving Accessory and Compensator Unit 1. KA-51B SLAVING ACCESSORY AND COMPENSATOR UNIT -- Controls the KCS-55A Compass System. 2. MANUAUAUTOMATIC(FREEISLAVE) COMPASS SLAVE SWITCH -- Selects either the manual or automatic slaving mode for the Compass System.
Page 364 CESSNA SECTION 9 , SUPPLEMENTS MODEL 172S SUPPLEMENT 13 - FAA APPROVED SECTION 2 .LIMITATIONS There is no change to the airplane limitations when this instrument is installed. SECTION 3 EMERGENCY PROCEDURES There is no change to the airplane emergency procedures when this instrument is installed.
Page 365 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 13 - FAA APPROVED For normal procedures with autopilots, refer to the Autopilot Supplements in the Supplement section of this handbook. description of course datum and autopilot procedures for course datum are incorporated in the appropriate autopilot supplements. SECTION PERFORMANCE There...
Page 366 Cessna A TelClron Company Pilot's Operating Handbook and FAA Approved Airplane Flight Manual CESSNA MODEL 172S AIRPLANES 172S8348 AND ON SUPPLEMENT 15 BENDIX/KING KAP 140 2 AXIS AUTOPILOT SERIAL NO, REGISTRATION This supplement must be inserted into' Section 9 of the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual when the KAP 140 2 Axis Autopilot System is installed.
Page 367 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 15 - FAA APPROVED SUPPLEMENT 15 BENDIX/KING KAP 140 2 AXIS AUTOPILOT Use the Log Effective Pages to determine" the 'current status this supplement.. Pages affected ,by,' ,the current revision < indicated by an asterisk preceeding the page number, 't:' "...
Page 368 CESSNA SECTION 9 - SUPPLEMENTS MODEl172S SUPPLEMENTJ5 - FAA APPROVED SUPPLEMENT 15 BENDIX/KING KAP 140 2 AXIS AUTOPILOT SERVICE BULLETIN CONFIGURATION LIST The following is a list of Service Bulletins that are applicable to the operation of the airplane, and have been incorporated into this supplement.
Page 369 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 15 - FAA APPROVED SUPPLEMENT 15 BENDIX/KING KAP 140 2 AXIS AUTOPILOT SECTION 1 ..GENERAL IThe KAP 140 2 Axis Autopilot provides the pilot with the following features:' Vertical Speed mode.(VS); Altitude', hold (ALT);...
Page 370 CESSNA SECTION 9 - SUPPLEMENTS MODEL172S SUPPLEMENT 15 - FAA APPROVED Activation of AlP DISCfTRIM INT control wheel switch will also disconnect the autopilot. The AVIONICS MASTER switch supplies power to the avionics bus ,bar of the radio circuit breakers and the autopilot circuit breaker. The AVIONICS MASTER switch also serves as an emergency , AP/MET shutoff.
Page 371 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 15 - FAA APPROVED NAVICOMM1 CONTRO. WHEEL r---- ..TURN COORDINATOR WARN 07851026 Figure 1. Bendix/King KAP 1402 Axis Autopilot Schematic (Serials 172S8348 thru 172S9422) (Sheet 1 of 2) Revision 5...
Page 372 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 15 -fAA APPROVED .• :-.: . .. NAV/COMM 1 r---- NAVIGATION r----...I SOURCE SELECTOR SWITCH lECTR1CA WA.RN URN COORDINATOR ROLL STEERING C I B 07851026 Figure.1 ..Bendix/King KAP 140 2.Axis Autopilot Schematic (Serials 172S9423 and On) (Sheet 2) Revision 5...
Page 373 CESSNA SECTION 9 - SUPPLEMENTS' MODEL172S SUPPLEMENT 15 - FAA APPROVED 18** H~GIAPIRLT 5[1[1 KAP 140 WITHOUT ALTITUDE PRESELECT 1. PITCH AXIS, ANNUNCIATOR When illuminated, indicates failure of pitch axis and will either disengage the . autopilot or not allow engagement of the pitch axis, turbulent air,...
Page 374 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 15-FAAAPPROVED 4. HEADING (HDG) MODE SELECTOR BUTTON -- When pushed, will select the Heading mode, which commands the airplane to turn to and maintain the heading selected by the heading bug on the Directional Gyro or HSI (if installed). new heading may be selected at any time and will result in the airplane turning to the new heading.
Page 375 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 15 - FAA APPROVED 9. VERTICAL SPEED (UP/DN) MODE BUnONS -- The action of these buttons depends on the vertical mode present when pressed. If VS mode is active (AP plus any lateral mode) and the UP button is pressed, the autopilot...
Page 376 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 15 - FAA APPROVED 14. OMNI BEARING SELECT (OBS) KNOB -- Selects the desired . course to be tracked by the autopilot. (Note: The HOG bug. must 'also be positioned to the proper course to capture and track the selected radial or desired track) .
Page 377 CESSNA SECTION SUPPLEMENTS MODEL 172S SUPPLEMENT 15 - FAA APPROVED BENDIX KING C6EJ ' 'REV" IALTI KAp 140 WITH ALTITUDE PRESELECT NOTE 'Numbered items apply to the KAP 140 with Altitude Preselect. Other 'controls and indicators shown are the same as those on the KAP 140 without Altitude Preselect (refer to Figure 2), 1, ROTARY KNOBS -- Used to set the altitude alerter reference altitude;...
Page 378 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 15 - FAA APPROVED 3. ALTITUDE ARM (ARM) BUnON -, When pushed, will toggle altitude arming on or off. When ALT ARM is annunciated, the autopilot will capture the altitude alerter displayed altitude (provided the airplane is climbing or descending in VS to'theR displayed altitude).
Page 379 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 15 - FAA APPROVED SECTION 2 LIMITATIONS The fell.owing autepilet Iimitatiens must be adhered te: 1. The entire preflighrtest precedure .outlined under Sectien 4, paragraph A .of this supplement, including steps 1through 7, must be successfully cempleted prier te each flight.
Page 380 CESSNA SECTION .;1- SUPPLEMENTS MODEL 172S SUPPLEMENT 15 - FAA APPROVED SECTION EMERGENCY PROCEDURES . The four step proc~dure (steps A thru D) listed under paragraph 1 should be among the basic airplane emergency procedures that are committed to memory. It is important thatthe pilorbe prolicient in...
Page 381 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 15 - FAA APPROVED AMPLIFIED EMERGENCY PROCEDURES following paragraphs presented to supply additional information for the purpose of providing the. pilot with a more complete understanding of the' recommended course of action for an emergency situation, , 1.
Page 382 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 15 - FAA APPROVED 3. Note that the. emergency procedure for any malfunction essentially the same: immediately grasp the control wheel and regain airplane control while pressing and holding the AlP DISCITRIM INT switch down, and retrim the airplane needed.
Page 383 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT15-FAAAPPROVED 2. If annunciation continues, Airplane Control Wheel -- GRASP FIRMLY, disengage the autopilot and check for an out of pitch trim condition. Manually retrim as required. 3. AUTOPILOT OPERATION -- CONTINUE if satisfied that the out of trim indication was temporary.
Page 384 CESSNA SECTiON 9-:,SUPPLEMENTS MODEU72S SUPPlEMENT 15 - FAA APPROVED 3. Flashing GS -- Indication of a tlagged glideslope. (GS will rearm automatically if a valid GS signal'is received.) ,:;.;". NOTE • To continue tracking the localizer, observe the • appropriate minimums for...a nonpreclslon,...
Page 385 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 15 - FAA APPROVED NOTE The following 'procedures apply to airplane serials 172S8348 thru 172S9128 incorporating Honeywell Service Bulletin KC140-M1, and serials 172S9129 and on. The following voice messages will be annunciated as conditions warrant: 1.
Page 386 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 15 . FAA APPROVED -NOTE Upon applying, power to the autopilot, the red P warning on the face of the autopilot may illuminate 'indicating tharthe pitch axis Gannot be engaged. This' condition should temporary, lasting...
Page 387 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 15 - FAA APPROVED NOTE If red light is not observed after holding RH switch for 5 seconds, the trim monitor system has failed. flight continued AUTOPILOT Circuit Breaker is pulled to the OFF position until repairs can be made.
Page 388 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 15- FAA APPROVED 4. FLASHING BARO SETTING (if installed) _. SET proper baro setting manually (or press BARO to accept the prese~t value). 5. AUTOPILOT -- ENGAGE by pressing', or pressing holding" AP button.
Page 389 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 15 - FAA APPROVED NOTE Autopilot tracking performance will degraded turbulence, 172S Serial. number 172S9423' Roll Steering functionality enables the GPS navigation computer to control the autopilot and automatically perform course changes (turns), and intercept the course to the next active waypoint (when GPS is...
Page 390 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 15 - FAA APPROVED 1. BEFORE TAKEOFF: a. AlP DISCfTRIM INT Switch -- PRESS. b. BARO setting (if installed) -- CHECK. CAUTION CONTINUE TO SET MANUALLY THROUGHOUT THE FLIGHT EACH TIME THE ALTIMETER BARO SETIING REQUIRES...
Page 391 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 15 - FAA APPROVED NOTE . Avoid autopilot engagement into a Climb condition that either cannot be maintained, or is on the performance limits of the airplane for its power and .weight configuration. c.
Page 392 .CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 15 - FAA APPROVED 3. CLIMB OR DESCENT: a. BARO setting (if installed) -- CHECK. b. Using Vertical Trim: 1) VERTICAL SPEED Control -- PRESS either the UP or DN button to select aircraft vertical speed within the +1500 1-2000.ft.
Page 393 CESSNA SECTION 9 SUPPLEMENTS' rv10DEL172S SUPPLEMENT 15 FAA APPROVED NOTE Altitude preselect captures are not recommended on nonprecision approaches capture MDA. Glideslope coupling will preclude a preselect altitude capture on an ILS . .~ b. Altitude (ALT) Hold Button: 1) AL T Hold Selector Button PRESS.
Page 394 CESSNA SI::CTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 15 - FAA APPROVED 5. HEADING HOLD: a. Heading Selector Knob -- SET BUG to desired heading. b. HOG Mode Selector Button -- PRESS. Note HOG mode annunciator Autopilot will automatically turn the airplane to the selected heading.
Page 395 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 15 - FAA APPROVED a) If the CDI needle is greater than 2 to 3 dots from center, the autopilot will annunciate NAVARM. When the computed capture'point is reached the ARM annunciator .will go out and the selected .course will .be au.tomatically captured and tracked.
Page 396 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 15 - FAA APPROVED When Roll Steering is in operation, adjusting or changing position of the heading bug or the course pointer will have no effec on heading or course. It is recommended that both the heading bug and the course pointer (or NO.
Page 397 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 15 - FAA APPROVED NOTE • When APR is selected, the autopilot will flash HDG for 5. seconds to remind the pilot to reset the HDG bug to the approach course .. If HDG mode was in use at the time of APR button selection,' a 45°...
Page 398 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 15 - FAA APPROVED 4) APR Mode Selector Button .- PRESS. a) If the D-Bar is greater than.2 to 3 dots from center, the autopilot will annunciate APRARM; when the computed capture point reached annunciator will go.
Page 399 CESSNA SECTION 9 - SUPPLEMENTS MODEL.172S SUPPLEMENT 15 - FAAAPPROVED NOTE • When REV is selected, the autopilot will flash HOG for 5 seconds to remind the pilot to reset the HOG bug to the localizer FRONT COURSE INBOUND heading. If heading mode was in use at the time of REV button selection, a 45°...
Page 400 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 15 - FAA APPROVED a) If the D-Bar is greater than 2 to 3 dots from center, the autopilot will annunciate REVARM; when computed capture point reached annunciator will go out and the selected back course will be automatically captured and tracked.
Page 401 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 15" FAA AP~ROVED 10. MISSED APPROACH a. AlP DISCITRIM INTER Switch - PRESS to disengage AP. b. MISSED APPROACH - EXECUTE. c. If autopilot is desired: 1) Elevator Trim -- VERIFY or SET. 2) Airspeed and Rate of Climb -~STABILIZED ..
Page 402 Cessna A Textron Company Pilot's Operating Handbook . and FAA Approved Airplane Flight Manual CESSNA MODEL 1725 AIRPLANES 172S8001 AND ON SUPPLEMENT BENDIX/KING KT 73 MODE S TRANSPONDER SERIAL REGISTRATION NO .. This supplement must be inserted into Section 9 of the...
Page 403 CESSNA SECTION 9 • SUPPLEMENTS MODEL 172S SUPPLEMENT 16 SUPPLEMENT 16 BENDIX/KING KT 73 MODE S TRANSPONDER Use the Log of Effective Pages to determine the current status of this supplement. ,Pages affected by the current revision are indicated by an asterisk (*) preceding the page numbeL Date "...
Page 404 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 16 SERVICE BULLETIN CONFIGURATION LIST The following is a list of Service Bulletins that are applicable to the operation of the airplane, and have been incorporated into this supplement. This list contains only those Service Bulletins that are currently active.
Page 406 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 16 . SUPPLEMENT ..,. • BENDIX/KING KT 73 MODE TRANPONDER SECTION 1 . GENERAL The Bendix/King Mode S Transponder (KT 73), shown in Figure S16-1, is the airborne component of the Air Traffic Control Radar Beacon System (ATCRBS).
Page 407 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 16 GENERAL (Continued) BENDIX/KING KT 73 MODE S TRANSPONDER '''''''' FL042 1200R IIDTI ••• II!1N:l1X1KI~ • 011BTl Figure S16-1 1. IDENT BUTTON (lOT) - When pushed, a pulse is transmitted for identification of the airplane on ATC radar display. will be displayed steadily and R will flash for approximately 18 seconds when the Function Selector Knob is set to GND, ON, or ALT.
Page 408 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 16 GENERAL (Continued) 4. REPLY INDICATOR (R) - The R will illuminate on the display panel when the transponder is replying to a valid interrogation during the following conditions: 1. Twice per second with valid interrogation on the ground in Mode S (GND).
Page 409 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 16 GENERAL (Continued) TST - Self-test function. The transmitter is disabled. display segments will come on for a minimum of 4 seconds. If no faults have been detected "TEST OK" will be displayed. Refer to the KT 73 Transponder section of the...
Page 410 CESSNA SECTION.9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 16 SECTION LIMITATIONS' There is no change to the airplane limitations when this' ~vionic equipment is installed.. " SECTION 3 EMERGENCY PROCEDURES TO TRANSMIT AN EMERGENCY SIGNAL 1. Mode Selector Switch - ALT, 2, Transponder Code Selector Knobs -SELECT 7700 operating code.
Page 411 CESSNA SECTION 9 • SUPPLEMENTS MODEL 172S SUPPLEMENT 16 NORMAL PROCEDURES (Continued) TO TRANSMIT MODE AlS (AIRPLANE IDENTIFICATION) CODES IN FLIGHT 1. Transponder Code Selector Knobs - SET assigned code. 2. Mode Selector Switch. ON. NOTE • During normal operation with Mode Selector Switch in ON position, reply indicator flashes, indicating transponder replies to interrogations.
Page 412 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 16 NORMAL PROCEDURES (Continued) TO SELF-TEST TRANSPONDER OPERATION 1. Mode Selector Switch - TST. 2. Check all displays come on. 3. TEST OK displayed. If not refer to the KT 73 Transponder section of the Bendix/King Silver Crown Plus Pilot's Guide.
Page 414 Pilot's Operating Handbook and FAA Approved Airplane Flight.Manual CESSNA MODEL 172S ""'" .,. A IRPLANES 17258372 ANDON" .•. .-.\ SUPPLEMENT 19 BENDIX/KING KLN 94 GLOBAL POSITIONING SYSTEM (IFR) > SERIAL NO. REGISTRATION This supplement must be inserted into Section 9 of the Pilot's Operating Handbook and FAA Approved Airplane Flight, Manual when the Global Positioning...
Page 415 . CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 19-FAAAPPROVED SUPPLEMENT 19 BENDIX/KING KLN 94 GLOBAL POSITIONING SYSTEM (IFR) to .. Use the Log of Effective Pages determine the current status of his supplement. .Pages affected by the current revision indicated by"an asterisk preceding the page number.
Page 416 CESSNA SECTION 9,- .SUPPLEMENTS MODEL 172S SUPPLEMENT 19 - FAA APPROVED .SUPPLEMENT 19 BENDIX/KING KLN94 GLOBAL POSITIONING SYSTEM (IFR) SERVICE BULLETIN CONFIGURATION LIST The following is a list of Service Bulletins that are applicable to the operation of the airplane, and have been incorporated into this supplement.
Page 417 CESSNA SECTION 9 - SUPPLEMENTS. MODEL 172S SUPPLEMENT 19 - FAA APPROVED SUPPLEMENT19 BENDIX/KING KLN 94 .- , GLOBAL POSITIONING SYSTEM (IFR). SECTION 1 GENERAL The KLN 94 Global Positioning System (GPS) is a three- dimensional precision navigation system based on 24 earth orbiting satellites.
Page 418 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 19 -FAA APPROVED Every. 28 days, Bendix/King receives new aeronautical database information from Jeppesen Sanderson for each database region. This information is'processed and downloaded onto the database cards. Bendix/King makes these database .card 'updates available to KLN 94 GPS users.
Page 419 CESSNA SECTION9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 19 - FAA APPROVED NOTE .• Airplanes using GPS for oceanic IFR operations may use the KLN 94. to replace one of the other approved means of long range navigation. A single KLN 94 GPS installation may also be used on short oceanic routes which require only one means of long-range navigation.
Page 420 CESSNA SECTION 9 -SUPPLEMENTS MODELJ72S SUPPLEMENT 19 -FAA APPROVED 0585Cl042 1, GPS MESSAGE (MSG) ANNUNCIATOR LIGHT -- MSG will begin flashing' whenever the'message prompt (a large "M" on the left 'side of the screen) on'the KLN 94 GPS unit begins flashing to alert the pilot that a message is waiting.
Page 421 CESSNA SECTION 9 SUPPLEMENTS MODEL 172S SUPPLEMENT 19 FAA APPROVED WARNING TURN. ANTICIPATION AUTOMATICALLY DISABLED FOR FAF WAYPOINTS AND THOSE USED 'EXCLUSIVELY DP/STARS WHERE OVERFLIGHT IS REQUIRED. FOR WAYPOINTS SHARED BETWEEN DP/STARS AND.PUBLISHED EN ROUTE SEGMENTS (REQUIRING OVERFLIGHT DP/STARS), PROPER SELECTION ON THE PRESENTED WAY POINT...
Page 422 CESSNA SECTION 9 . SUPPlEMENTS MODEL 172S SUPPLEMENT 19. FAA APPROVED -6. NAV/GPS SWITCH -. Toggles from Nav 1 to GPS and vice versa to control the type of navigation data to be displayed on the Course Deviation Indicator (COl). The NO.1 COl Omni Bearing Selector (OBS) provides analog course input to the KLN 94 in OBS mode when the NAV/GPS switch/annunciator...
Page 423 CESSNA -" SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT .19 - FAA APPROVED HSI . 1. HSI ANNUNCIATOR LIGHT -- This label is present when the optional HSI' is installed. The HSI course pointer provides 'course datum to the autopilot. 2.
Page 424 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 19 - FAA APPROVED NOTE • Manual CDI course centering in OBS mode using the control knob can be difficult, especially at long distances. Centering Course Deviation Indicator (CDI) needle can best be accomplished by pressing the Direct-To button and then manually setting the No.
Page 425 SECTION 9 . SUPPLEMENTS CESSNA MODEL 172S SUPPLEMENT 19 - FAA APPROVED SECTION LIMITATIONS 1. The KLN 94 GPS Pilot's Guide, PIN 006-18207-0000, dated September 2000 (or later applicable revision) must be available to the flight crew whenever IFR GPS navigation is used.
Page 426 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 19 - FAA APPROVED 3) APR ACTV mode must be annunciated at the Final Approach Fix. 4) Accomplishment of ILS, LaC,. LOC-BC, LDA, SDF, and MLS approaches are not authorized. 5) When an alternate airport is. required by the applicable operating rules, it must be served by an approach based on other than GPS or Loran-C navigation, 6) The KLN 94 can only be used for approach guidance if...
Page 427 .CESSNA SECTION SUPPLEMENTS MODEL 172S SUPPLEMENT 19, FAA APPROVED NOTE Honeywell's Preflight, Version 2.0. or later computer based prediction program may be used lor the RAIM prediction. Altl;)rnate methods should be submitted lor approval in accordance with Advisory Circular AC 90-96.' g.
Page 428 CESSNA . SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 19 - FAA APPROVED SECTION 4 NORMAL PROCEDURES OPERATION Normal operating procedures are outliri,ed in the KLN 94 GPS Pilot's Guide, PIN 006'18207-0000, dated September 2000 (or later applicable revision). A KLN 94 Quick Reference, PIN 006-18228- 0000, dated August 2000 (or later applicable revision) containing an approach sequence, operating tips and approach related messages is intended as well for cockpit use by the pilot familiar with KLN 94...
Page 429 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S 19 - SUPPLEMENT FAA APPROVED 04." Roll Steering is the default, operating mode for the autoflight system when all of the following conditions are met: 1, The autopilot is engaged in NAV or ApR mode 2, GPS is selected as the autopilot navigation source .3, The GPS navigation computer is executing an active flight plan...
Page 430 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 19 - FAA,APPROVED NOTE The .special use airspace alert will automatically be disabled prior to flying an instrument approach to reduce the potential for message congestion, Roll Steering will operate' . on . instrument approflch .
Page 431 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 19 - FAA APPROVED 3. Al or within 30 nm from the airport: a. Verify automatic' annunciation of APRARM. b. Note automatic CDI needle scaling change from :f:5.0 nm to :f: 1.0nm over the next 30 seconds. c.
Page 432 CESSNA SECTION 9- SUPPLEMENTS MODEL 172$ SUPPLEMENT 19 - FAA APPROVED 5. At or before 2 nm from the FAF inbound: .a. Selectthe FAF as the active waypoint, if not accomplished already. b. Select LEG operation. 6. Approaching the.FAF inbound (within 2 nm): a.
Page 433 CESSNA SECTION'9- SUPPLEMENTS MODEl172S SUPPLEMENT 19 - FAA APPROVED GENERAL NOTES •• The aeronautical database must be up to date for ,instrument approach operation, • Only one approach can be in the flight plan at a time. • Checking RAIM prediction for your approach while enroute using the AUX 3 page is recommended.
Page 434 CESSNA. SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 19 - FAA APPROVED • The DME arc IAF identifier may be unfamiliar. Example: D098G where 098 stands for the 098 radial off the referenced VOR, andG is the'seventh letter in the alphabet indicating a 7 DME arc.
Page 436 Pilot's Operating Handbook and FAA Approved Airplane Flight Manual. CESSNA MODEL 172S AIRPLANES 172S8704AND SUPPLEMENT 20 BENDIX/KING KMA 28 AUDIO SELECTOR PANEL SERIAL NO. REGISTllATlON NO .. This'supplement must b!3 ,inserted into Section 9 Of the 'Pill?l's Operating Handbook and FAA Approv~ ~irp!ane Flight Manual.
Page 437 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 20 - FAA APPROVED ..SUPPLEMENT 20 BENDIX/KING KMA 28 AUDIO SELECTOR PANEL The following Log of Effective Pages provides the date of issue. for original and revised pages, as well as a listing of all pages in . the Supplement Pages' which.
Page 438 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENt 20 - FAA APPROVED SUPPLEMENT . BENDIX/KING KMA 28 AUDIO SELEC)"OR PANEL SECTION 1 GENERAL The Bendix/King .KMA 28 Audio Selector Panel is a combination audio selector panel, cabin intercom, audio amplifier and marker 'beacon receiver.
Page 439 CESSNA SECTION 9 -SUPPLEMENTS .. MODEL 172S SUPPLEMENT 20 -FAA APPROVED "NOTE' '~, ;-' ',<.,t I", • In this stereo 'installation, 'all headset locations are wired' in parallel. If a monaural headset is plugged in at any location, one intercom.channel will be shorted, Although no damage to the intercom will result, all stereo headset users will lose one audio channel.
Page 440 CESSNA ,SECTION 9 -.SUPPLEMENTS MODEL 172S SUPPLEMENT20 - FAAAPPROVED 9 .8 1. MARKER' BEACON. ANNUNCIATOR L1GHTS'- The three-light marker beacon. receiver built into the KMA 28 gives a visual and aural signal when the ship's' antenna .passes over a 75 MHz .beacon. The biue, amber, and white lighis on the.
Page 441 CESSNA SECTION SUPPLEMENTS MODEL 172S' SUPPLEMENT 20 - FAA APPROVED 3. RECEIVE AUDIO SELECT BUDONS.. Push button audio selection is available for two Communications receivers ("COM 1", "COM 2"), two Navigation receivers ("NAV I" and "NAV 2"), the internal Marker Beacon receiver ("MKR"), one DME, one ADF, one additional auxiliary receiver ("AUX") and a speaker amplifier ("SPR").
Page 442 -CESSNA SECTION 9 " SUPPLEMENTS MODEL,172S .SI3PPLEMENT 20.' FAAAPPROVED TELEPHONE MODE ,(TEL) . The telephone mode is not available on this installation. - - SPLIT MODE- (COM 1/2 OR COM 2/1) .• Moving the mic selector switch to COM 1/2 places the KMA 28- into "split mode". This places the pilot on Com 1 and the 'copilot on Com 2: Switching to COM 2/1 will reverse information _regarding...
Page 443 CESSNA SECTION g':SUPPLEMENTS MODEL 172S . SUPPLEMENT 20 - FAA APPROVED 1a.INTERCOM MODE SELECT (ISO-ALL 'CREW) .. A three.position mode switch that allows the pilot to tailor the intercom function to. best meet the ~urrent cockpit situation. ISO .. (Up PoSition) 'The pilot is isolated from the intercom and is' connected only to the aircraft radio system.
Page 444 CESSNA SECTION 9 - SUPPLEMENTS MODEL.: 1 72S SUPPLEMENT 20 - FAA APPROVED 11.VOLUME CONTROUPOWER SWITCH/EMERGENCY OPERATION KNOB -- The KMA 28 unit is turned on. and off by pushin~ the volume knob. In the OFF.or EMG (Emergency) position, the pilot 's connected directly to Com 1.
Page 445 CESSNA SECTiON 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 20 - FAA APPROVED SECTION 2 .LIMITATIONS 1. PUSH OFF/EMG operation is prohibited during normal operations. 2. Use of the Entertainment audio input (and PED) is prohibited during takeoff and landing. 3. Use 01 the Entertainment audio input (and PED) is prohibited under .IFR unless the operator .01 the aircraft has determined that the use of the 12 VDC power supply and the connected portable electronic device(s) will not cause.
Page 446 CESSNA SECTION 9 - SUPPLEMENTS 'MODEL'172S SUPPLEMENT 20 ' FAA APPROVED SECTION 4 NORMAL PROCEDURES AUDIO CONTROL SYSTEM'OPERATION: 11" 1, MIC Selector Switch -- Turn to desired transmitter, 2,SPEAKER and.Audio~elect Button(s) ,-- ,SELECT desired receiver(s), NOTES Rotation of the MIC selector,switch,selec1s the 'Com audio automatically.
Page 447 CESSNA SECTION 9 - SUPPLEMENTS SUPPLEMENT 20 - FAA APPROVED MODEL 172S ~ ~'NOTE":~ ~"'-+.;:r • .' ••.. ' .••..•.•.. , -~ ~::(~- Disconnect the audio cable from the' Entertainment audio input jack whenever the PED is not.in use. ,-." NOTE "...
Page 448 ATe.J:tron Ccmpany Pilot's Operating Handbook and FAA Approved Airplane Flight Manual CESSNA MODEL 172S AIRPLANES 17258704 AND ON • SUPPLEMENT 21 BENDIX/KING KMD 550 . MULTI-FUNCTION DISPLAY SERIALNO. REGISTRATION NO. This supplement ,must be inserted into Section 9 of the Pilot's Operating Handbook and.
Page 449 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 21 -FAA APPROVED SUPPLEMENT 21 . BENDIX/KING KMD 550 MULTI-FUNCTION DISPLAY The following Log of Effective Pages provides the date of issue .fororiginal and revised pages, as well as a listing of all pages in the Supplement.
Page 450 CESSNA SECTION 9 - SUPPLEMENTS MODEL172S 21 - SUPPLEMENT FAA ApPROVEO' . SUPPLEMENT . BENDIX/KING KMD 550 MULTI-FUNCTION DISPLAY. SECTION 1 GENERAL WARNING NEVER REMOVE THE DATABASE CARD WHilE .THE UNIT.IS . SWITCHED ON AND NEVER ATTEMPT TO SWITCH ,:THE UNIT-ON WHEN .THERE IS NO DATABASE CARD INSTAllED.
Page 451 CESSNA SECTION SUPPLEMENTS MODEL172S SUPPLEMENT 21 - FAA APPROVED .• NOTE " '!" -~,;," ", The KMD 550 is designed to be used as a supplemental navigation system.' You. should always carefully compare indications' from your KMD' 550: unit with the information available from all other 'navigation,sources including NDB's, VOR's, DME's, visual sightings, charts, etc.
Page 452 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 21 - FAA APPROVED 1.BRIGHTNESS CONTROL -- Clockwise rotation will increase the brightness of the display. Counter-clockwise rotation decreases the display brightness. 2. DATABASE CARD -- The database card contains the aeronautical and topographical database for the KMD 550. Updated database cards are available by subscription every 28 days.
Page 453 CESSNA SECTION 9'- SUPPLEMENTS MODEL 172S SUPPLEMENT 21 - FAA APPROVED 5. ON/OFF CONTROL -- Rotating clockwise to the "ON" position provides power to the KMD 550, Rotating counter-clockwise to the "OFF" position removes power from the unit. 6. FUNCTION SELECT INDICATORS -- When a function key is pressed, the Function Select Indicator above it will illuminate to show that this function is presently being displayed.
Page 454 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 21 - FAA APPROVED OVLY -- Pressing the Overlay Key allows data from more than once source to be displayed simultaneously on the screen. Soft labels will indicate which data sources are availabie for overlay. 10: SOFT LABELS -- Soft Labels are located to.
Page 455 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 21 - FAA APPROVED STARTUP DISPLAY This display will be seen after power-up. ,he Stormscope logo will be present if a Stormscope is installed and enabled. The self- test results are also displayed. Pressing the OK soft key will show the next display.
Page 456 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 21 - FAA APPROVED SECTION 3 EMERGENCY PROCEDURES There is no change to the airplane emergency procedures when the KMD 550 Multi-Function Display is installed. SECTION 4 NORMAL PROCEDURES There is no change to the airplane normal procedures when the KMD 550 Multi-Function Display is installed.
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Page 458 ATextroll Company Pilot's Operating Handbook and FAA Approved Airplane Flight Manual CESSNA MODEl172S AIRPLANES 17258704 AND ON SUPPLEMENT 22 12 VOLT CABIN POWER SYSTEM SEAIAlNO REGISTRATION This supplement must be inserted into Section 9 of the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual when the 12 Volt Cabin Power System is installed.
Page 459 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 22 - FAA APPROVED SUPPLEMENT 22 12 VOLT CABIN POWER SYSTEM The following Log of Effective Pages provides the.date of issue - ~for original and revised pages, as well as listing of all pages in the Supplement".
Page 460 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 22 -FAA APPROVED SUPPLEMENT. 12 VOLT CABIN POWER SYSTEM SECTION 1 GENERAL The 12 Volt Cabin Power System provides passenger access to a fixed direct current (DC) voltage for powering portable electronic devices (PED).
Page 461 CESSNA SECTION 9- SUPPLEMENTS MODEL 172S SUPPLEMENT 22 - FAA APPROVED RELEASE BUnON .,.. .~ "-. ~:r'~ ;. Figure 2: Maiing Plug " The mating plug'is a pla~tic 9opin'~ircularconnector with aq'uick disconnect push button release (btypertronics.D02PBMRTH-0025 or equivalent) (See Figure 2). Adapter cable assemblies are available thai feature the ARINC628.
Page 462 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT.22 - FAA APPROVED Power is supplied to the 12-volt Cabin Power System from a DC to DC power converter located in the tailcone of the aircraft. The power converter receives 28. VDC power from the "CABIN LTS/PWR"...
Page 463 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 22 - FAA APPROVED SECTION 4" NORMAL PROCEDURES The pilot must be familiar with the location' of the 12 Volt Cabin Power System connector and with the operation' of locking and release features common to the connector...
Page 464 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 22 - FAA APPROVED NOTE During passenger briefing, it must be explained that use of the PED (portable electronic device) is not permitted during takeoffs and landings. NOTE Disconnect the power/adapter cable from the Cabin Power System connector whenever the PED .(portable electronic device) is not in use.
Page 466 A Textron Company Pilot's Operating Handbook and FAA Approved Airplane Flight Manual CESSNA'MODEL 172S AIRPLANES 17259063 AND ON SUPPLEMENT 24 ASTROTECH MODEL TC.2 CLOCKIOATNOLT INDICATOR SERIAL NO.,--,-_--,-_--,- REGISTRATION NO., This supplement must 'be inserted into Section 9 of the Pilot's Operating...
Page 467 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 24 - FAA APPROVED SUPPLEMENT 24 ASTROTECH MODEL TC-2 CLOCK/OATIVOLT INDICATOR The following Log of Effective Pages provides the date of issue for original .and revised pages, as well as a listing of all pages in Supplement.' Pages which...
Page 468 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 24 - FAA APPROVED SUPPLEMENT DIGITAL ClOCK/OATNOl T INDICATOR SECTION 1 GENERAL The Astrotech Model TC-2 digital clock combines the features of a clock, outside air temperature _gauge (OAT) and voltmeter in a single unit.
Page 469 CESSNA SECTION 9 - SUPPLEMENTS SUPPLEMENT 24 - FAA APPROVED. MODEL 172S UPPER LCD <, " WINDOW LOWER LCD WINDOW 071~R1CZl! Figure 1. Astrotech Model TC-2 ClockiOATNolt Indicator 1. OATIVOLT SUDaN - Volts are displayed at power up. When the button is pressed, the display switches to outside air temperature in of.
Page 470 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 24 - FAA APPROVED 2'; . .,' . SECTION LIMITATIONS. There is no change to the airplane limitations when the digital clock/OATNolt indicator is installed. SECTION 3 EMERGENCY PROCEDURES There is no change to the airplane emergency procedures when the clock/OATNolt indicator is installed.
Page 471 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 24 - FAA APPROVED Press the SET (RESET) button and the left two digits will flash, these are the hour digits .. Press the ADV (ST/SP) button to change to the current hour. Press the SET (RESET) button and the right two digits will flash;...
Page 472 A Textron Company Pilot's Operating Handbook and FAA Approved Airplane Flight Manual CESSNA MODEL 172S AIRPLANES 172S9063 AND ON ". SUPPLEMENT 25 BENDIX/KING KX 165A VHF NAV/COMM SERIAL NO., REGISTRATION This supplement must be inserted into Section 9 of the Pilot's.
Page 473 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 25 - FAA APPROVED SUPPLEMENT 25 aENDIX/KING KX 165A VHF NAV/COMM - _The following Log of Effective Pages provides the date of issue for original and revised pages, as well as a listing of all pages in Supplement.
Page 474 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT25 - FAA APPROVED SUPPLEMENT BENDIX/KING KX 165A VHF NAV/COMM SECTION 1 . GENERAL The KX 165AVHF Nav/Comm Transceiver is very similar to the KX 155A VHF Nav/Comm Transceiver except, the KX 165A has a built in VOR/LOC converter, enabling it to directly drive a horizontal situation indicator (HSI).
Page 475 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT25 - FAA APPROVED The Comm portion incorporates an automatic squelch. override the automatic squelch, the Comm volume control knob is pulled out. Push the knob back in to reactivate the automatic squelch. A "T"...
Page 476 CESSNA SECTION SUPPLEMENTS MODEL 172S SUPPLEMENT 25 - FAA APPROVED NAV FUNCTION DISPLAYS 9.50 ~030 VOR MODE: ACTIVE/BEARING, COl FORMAT 109.50 FLRG . VOR MODE: ACTIV8BEARING, FLAG DISPLAY VORE MODE: ACTIVE "BEARING TO" FUNCTION DISPLAY VOR MODE: ACTIVE/BEARING, FLAG DISPLAY I/O- 90 LOCALIZER MODE: FREQUENCY/COl FORMAT...
Page 477 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 25 - FAA APPROVED 1. OPERATING COMM FREQUENCY DISPLAY -- Displays COMM ACTIVE and COMM STANDBY frequencies with a "T" between them to indicate TRANSMIT and an "R" to indicate RECEIVE modes of operation. 2.
Page 478 CESSNA SECTION 9 ' SUPPLEMENTS MODEL 172S SUPPLEMENT 25 - FAA APPROVED 6. NAV/FREQUENCY TRANSFER BUnON )0)-- Interchanges the NAV ACTIVE and STANDBY frequencies. Depressing the NAV frequency transfer button for 2 seconds - or more will cause the display to go into the ACTIVE _ENTRY mode.
Page 479 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 25 - FAA APPROVED Another push of the mode button will cause the NAV display from ACTIVE/BEARING format ACTIVE/RADIAUormat. In the RADIAL mode, the frequency inc/dec knobs channel the ACTIVE frequency window and depressing the frequency transfer button will cause.
Page 480 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 25 - FAA APPROVED 10. COMM FREQUENCY SELECTOR KNOB (OUTER) -- The . outer, larger selector knob is used to change the MHz portion of the frequency display. At either band-edge of the 118-136 MHz' frequency spectrum, an offscale rotation will wrap the...
Page 481 CESSNA SECTION 9 - SUPPLEMENTS MODEL172S SUPPLEMENT 25 - FAA APPROVED 12. COMM FREQUENCY TRANSFER BUnON )0)-- Interchanges the frequencies in the- USE and STANDBY displays. To tune the radio to the desired operating frequency, the desired frequency must be entered into the standby display and then the COMM TRANSFER button.
Page 482 CESSNA SECTION 9 . SUPPLEMENTS MODEL 172S SUPPLEMENT 25 . FAA APPROVED SECTION 3 EMERGENCY 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 frequency selected.
Page 483 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 25 - FAA APPROVED NAVIGATION RECEIVER OPERATION: ':0. 1. NAV Frequency Selector Knobs -- SELECT desired operating frequency in "STBY" display. 2. NAV TRANSFER BUTTON-- PRESS to transfer desired frequency from the "STBY" display into the "NAV" display, 3.
Page 484 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 25 - FAA APPROVED The pilot may adjust two parameters in the pilot configuration, the display minimum brightness and sidetone volume level. Minimum Brightness (BRIM) will have a range of 0-255. The dimmest is 0 and the brightest is 255.
Page 486 CeSSri8 A Textron Company Pilot's Operating Handbook and FAA Approved Airplane Flight Manual CESSNA MODEL 172S AIRPLANES 172S9569 AND ON SUPPLEMENT 26 BENDIX/KING KDR 510 FLIGHT INFORMATION SERVICES (FIS) SERIAL NO .• ------- REGISTRATION This supplement must be into Section 9 6f the Pilot's Operating. Handbook...
Page 487 CESSNA, SECTION 9 - SUPPLEMENTS MODEL 1;,2S SUPPLEMENT26 - FAA APPROVED SUPPLEMENT 26 BENDIX/KING KDR 510 FLIGHT INFORMATION SERVICES (FIS) Use the Log' of Effective Pages to determi~ -the current status of this supplement. ,Pages affected by the ",current ~revision are indicated by an asterisk preceding the page number.
Page 488 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 26 - FAA APPROVED SUPPLEMENT 26 BENDIX/KING KDR 510 FLIGHT INFORMATION SERVICES (FIS) SERVICE BULLETIN CONFIGURATION LIST The following is a list of Service Bulletins that are applicable to the operation of the airplane, and been incorporated into this have supplement.
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Page 490 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLi=:MENT26 - FAA APPROVED SUPPLEMENT BENDIX/KING KDR 510 FLIGHT INFORMATION SERVICES (FIS) SECTION 1 GENERAL. Bendix/King KDR 510 Flight Information Services (FIS) installation provides weather information and other, flight advisory information to pilots to enhance situational awareness, The services rely on a network of ground based VHF...
Page 491 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 26 - FAA APPROVED ". SECTION 3 " .EMERGENCY.PROCEDURES No additio'nal emergency procedures are required when the KDR 510 Flight Information Services (FIS) equipment is installed in the airplane. .: ' SECTION 4 NORMAL PROCEDURES Press the WX .function select key of the KMD 550 multi-function display to toggle through weather related systems installed on the...

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