Redarc R-12-700S Especificações

CESSNA INTRODUCTIONMODEL 172R NAV III GFC 700 AFCSU.S.NOTICEAT THE TIME OF ISSUANCE, THIS INFORMATIONMANUAL WAS AN EXACT DUPLICATE OF THEOFFICI

SECTION 3 CESSNAEMERGENCY PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.ROUGH ENGINE OPERATION OR LOSS OF POWER(Continued)ENGINE-DRIVEN FUEL PUMP FAILU

CESSNA SECTION 3MODEL 172R NAV III EMERGENCY PROCEDURES GFC 700 AFCSU.S.ROUGH ENGINE OPERATION OR LOSS OF POWER(Continued)LOW OIL PRESSUREIf t

SECTION 3 CESSNAEMERGENCY PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.ELECTRICAL POWER SUPPLY SYSTEMMALFUNCTIONSMalfunctions in the electrical power

CESSNA SECTION 3MODEL 172R NAV III EMERGENCY PROCEDURES GFC 700 AFCSU.S.ELECTRICAL POWER SUPPLY SYSTEMMALFUNCTIONS (Continued)INSUFFICIENT RAT

SECTION 3 CESSNAEMERGENCY PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.ELECTRICAL POWER SUPPLY SYSTEMMALFUNCTIONS (Continued)INSUFFICIENT RATE OF CHAR

CESSNA SECTION 3MODEL 172R NAV III EMERGENCY PROCEDURES GFC 700 AFCSU.S.HIGH CARBON MONOXIDE (CO) LEVELANNUNCIATIONCarbon monoxide (CO) is a c

CESSNA SECTION 4MODEL 172R NAV III NORMAL PROCEDURES GFC 700 AFCSU.S.NORMAL PROCEDURESTABLE OF CONTENTSPageIntroduction . . . . . . . . . . .

SECTION 4 CESSNANORMAL PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.TABLE OF CONTENTS (Continued)PageAMPLIFIED NORMAL PROCEDURES. . . . . . . . . . .

CESSNA SECTION 4MODEL 172R NAV III NORMAL PROCEDURES GFC 700 AFCSU.S.INTRODUCTIONSection 4 provides procedures and amplified instructions for

CESSNA SECTION 1MODEL 172R NAV III GENERAL GFC 700 AFCSU.S.THREE VIEW - NORMAL GROUND ATTITUDEFigure 1-1 (Sheet 1 of 2)1-3172RPHBUS-00

SECTION 4 CESSNANORMAL PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.NORMAL PROCEDURESPREFLIGHT INSPECTION NOTEVisually check airplane for general cond

CESSNA SECTION 4MODEL 172R NAV III NORMAL PROCEDURES GFC 700 AFCSU.S.PREFLIGHT INSPECTION (Continued)1 CABIN1. Pitot Tube Cover - REMOVE (che

SECTION 4 CESSNANORMAL PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.PREFLIGHT INSPECTION (Continued)1 CABIN (Continued)17. AVIONICS Switch (BUS 1) -

CESSNA SECTION 4MODEL 172R NAV III NORMAL PROCEDURES GFC 700 AFCSU.S.PREFLIGHT INSPECTION (Continued)4 RIGHT WING1. Wing Tiedown - DISCONNECT

SECTION 4 CESSNANORMAL PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.PREFLIGHT INSPECTION (Continued)5 NOSE1. Fuel Strainer Quick Drain Valve (located

CESSNA SECTION 4MODEL 172R NAV III NORMAL PROCEDURES GFC 700 AFCSU.S.PREFLIGHT INSPECTION (Continued)5 NOSE (Continued)3. Engine Cooling Air

SECTION 4 CESSNANORMAL PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.PREFLIGHT INSPECTION (Continued)7 LEFT WING1. Wing Tiedown - DISCONNECT2. Fuel Qu

CESSNA SECTION 4MODEL 172R NAV III NORMAL PROCEDURES GFC 700 AFCSU.S.BEFORE STARTING ENGINE1. Preflight Inspection - COMPLETE2. Passenger Brie

SECTION 4 CESSNANORMAL PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.STARTING ENGINE (With Battery)1. Throttle Control - OPEN 1/4 INCH2. Mixture Contro

CESSNA SECTION 4MODEL 172R NAV III NORMAL PROCEDURES GFC 700 AFCSU.S.STARTING ENGINE (With Battery) (Continued)17. Oil Pressure - CHECK (verif

SECTION 1 CESSNAGENERAL MODEL 172R NAV IIIGFC 700 AFCSU.S.THREE VIEW - NORMAL GROUND ATTITUDE NOTE• Wing span shown with standard strobe lights instal

SECTION 4 CESSNANORMAL PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.STARTING ENGINE (With External Power) (Continued)17. Mixture Control - SET to FULL

CESSNA SECTION 4MODEL 172R NAV III NORMAL PROCEDURES GFC 700 AFCSU.S.STARTING ENGINE (With External Power) (Continued)WARNINGIF M BATT AMMETER

SECTION 4 CESSNANORMAL PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.BEFORE TAKEOFF (Continued)15. A/P TRIM DISC Button - PRESS (if installed)(verify a

CESSNA SECTION 4MODEL 172R NAV III NORMAL PROCEDURES GFC 700 AFCSU.S.BEFORE TAKEOFF (Continued)27. CDI Softkey - SELECT NAV SOURCECAUTIONTHE G

SECTION 4 CESSNANORMAL PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.TAKEOFFNORMAL TAKEOFF1. Wing Flaps - UP - 10° (10° preferred)2. Throttle Control -

CESSNA SECTION 4MODEL 172R NAV III NORMAL PROCEDURES GFC 700 AFCSU.S.ENROUTE CLIMB1. Airspeed - 70 - 85 KIAS2. Throttle Control - FULL (push f

SECTION 4 CESSNANORMAL PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.DESCENT1. Power - AS DESIRED2. Mixture - ADJUST (if necessary to make engine run s

CESSNA SECTION 4MODEL 172R NAV III NORMAL PROCEDURES GFC 700 AFCSU.S.BEFORE LANDING1. Pilot and Passenger Seat Backs - MOST UPRIGHT POSITION2.

SECTION 4 CESSNANORMAL PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.LANDING (Continued)BALKED LANDING1. Throttle Control - FULL (push full in)2. Wing

CESSNA SECTION 4MODEL 172R NAV III NORMAL PROCEDURES GFC 700 AFCSU.S.AMPLIFIED NORMAL PROCEDURESPREFLIGHT INSPECTIONThe preflight inspection,

CESSNA SECTION 1MODEL 172R NAV III GENERAL GFC 700 AFCSU.S.INTRODUCTIONThis POH contains 9 sections, and includes the material required to bef

SECTION 4 CESSNANORMAL PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.PREFLIGHT INSPECTION (Continued)Outside storage for long periods may result in dus

CESSNA SECTION 4MODEL 172R NAV III NORMAL PROCEDURES GFC 700 AFCSU.S.STARTING ENGINEIn cooler weather, the engine compartment temperature drop

SECTION 4 CESSNANORMAL PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.STARTING ENGINE (Continued)RECOMMENDED STARTER DUTY CYCLEOperate the starter motor

CESSNA SECTION 4MODEL 172R NAV III NORMAL PROCEDURES GFC 700 AFCSU.S.TAXIINGWhen taxiing, it is important that speed and use of brakes be held

SECTION 4 CESSNANORMAL PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.TAXIING (Continued)TAXIING DIAGRAM NOTEStrong quartering tail winds require cautio

CESSNA SECTION 4MODEL 172R NAV III NORMAL PROCEDURES GFC 700 AFCSU.S.BEFORE TAKEOFFWARM UPIf the engine idles, with the throttle against the i

SECTION 4 CESSNANORMAL PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.BEFORE TAKEOFF (Continued)ELEVATOR TRIMThe elevator trim tab is in the takeoff pos

CESSNA SECTION 4MODEL 172R NAV III NORMAL PROCEDURES GFC 700 AFCSU.S.TAKEOFF (Continued)WING FLAP SETTINGSNormal takeoffs use wing flaps UP -

SECTION 4 CESSNANORMAL PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.ENROUTE CLIMBNormal enroute climbs are performed with flaps up, at full throttle a

CESSNA SECTION 4MODEL 172R NAV III NORMAL PROCEDURES GFC 700 AFCSU.S.CRUISENormal cruise is performed between 60% and 80% power. The engineRPM

SECTION 1 CESSNAGENERAL MODEL 172R NAV IIIGFC 700 AFCSU.S.DESCRIPTIVE DATA (Continued)FUELWARNINGUSE OF UNAPPROVED FUELS MAY RESULT INDAMAGE TO THE EN

SECTION 4 CESSNANORMAL PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.CRUISE (Continued)CRUISE PERFORMANCE TABLECONDITIONS:Standard Conditions Zero Wind

CESSNA SECTION 4MODEL 172R NAV III NORMAL PROCEDURES GFC 700 AFCSU.S.CRUISE (Continued)LEANING USING EXHAUST GAS TEMPERATURE (EGT)The cruise p

SECTION 4 CESSNANORMAL PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.CRUISE (Continued)LEANING USING EXHAUST GAS TEMPERATURE (EGT)(Continued)To aid in

CESSNA SECTION 4MODEL 172R NAV III NORMAL PROCEDURES GFC 700 AFCSU.S.CRUISE (Continued)LEANING USING EXHAUST GAS TEMPERATURE (EGT)(Continued)E

SECTION 4 CESSNANORMAL PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.CRUISE (Continued)FUEL SAVINGS PROCEDURES FOR FLIGHT TRAININGOPERATIONSFor best fu

CESSNA SECTION 4MODEL 172R NAV III NORMAL PROCEDURES GFC 700 AFCSU.S.CRUISE (Continued)FUEL VAPOR PROCEDURESThe engine fuel system can cause f

SECTION 4 CESSNANORMAL PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.CRUISE (Continued)FUEL VAPOR PROCEDURES (Continued)In addition to the previous pro

CESSNA SECTION 4MODEL 172R NAV III NORMAL PROCEDURES GFC 700 AFCSU.S.SPINS (Continued)It is recommended that entries be accomplished at high e

SECTION 4 CESSNANORMAL PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.SPINS (Continued)Regardless of how many turns the spin is held or how it is entere

CESSNA SECTION 4MODEL 172R NAV III NORMAL PROCEDURES GFC 700 AFCSU.S.LANDINGNORMAL LANDINGNormal landing approaches can be made with power on

CESSNA SECTION 1MODEL 172R NAV III GENERAL GFC 700 AFCSU.S.DESCRIPTIVE DATA (Continued)OILOIL SPECIFICATIONMIL-L-6082 or SAE J1966 Aviation Gr

SECTION 4 CESSNANORMAL PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.LANDING (Continued)CROSSWIND LANDINGWhen landing in a strong crosswind, use the mi

CESSNA SECTION 4MODEL 172R NAV III NORMAL PROCEDURES GFC 700 AFCSU.S.COLD WEATHER OPERATIONSSpecial consideration should be given to the opera

SECTION 4 CESSNANORMAL PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.COLD WEATHER OPERATION (Continued)STARTINGWhen air temperatures are below 20°F (-6

CESSNA SECTION 4MODEL 172R NAV III NORMAL PROCEDURES GFC 700 AFCSU.S.COLD WEATHER OPERATION (Continued)STARTING (Continued)Cold weather starti

SECTION 4 CESSNANORMAL PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.HOT WEATHER OPERATIONSRefer to the general warm temperature starting information u

CESSNA SECTION 5MODEL 172R NAV III PERFORMANCE GFC 700 AFCSU.S.PERFORMANCE TABLE OF CONTENTSPageIntroduction . . . . . . . . . . . . . . . . .

CESSNA SECTION 5MODEL 172R NAV III PERFORMANCE GFC 700 AFCSU.S.INTRODUCTIONPerformance data charts on the following pages are presented so tha

SECTION 5 CESSNAPERFORMANCE MODEL 172R NAV IIIGFC 700 AFCSU.S.SAMPLE PROBLEMThe following sample flight problem utilizes information from thevarious c

CESSNA SECTION 5MODEL 172R NAV III PERFORMANCE GFC 700 AFCSU.S.SAMPLE PROBLEM (Continued)TAKEOFFThe takeoff distance chart, Figure 5-5, should

SECTION 1 CESSNAGENERAL MODEL 172R NAV IIIGFC 700 AFCSU.S.DESCRIPTIVE DATA (Continued)MAXIMUM CERTIFICATED WEIGHTSRamp Weight:Normal Category . . . .

SECTION 5 CESSNAPERFORMANCE MODEL 172R NAV IIIGFC 700 AFCSU.S.SAMPLE PROBLEM (Continued)CRUISEThe cruising altitude should be selected based on a cons

CESSNA SECTION 5MODEL 172R NAV III PERFORMANCE GFC 700 AFCSU.S.SAMPLE PROBLEM (Continued)FUEL REQUIREDThe total fuel requirement for the fligh

SECTION 5 CESSNAPERFORMANCE MODEL 172R NAV IIIGFC 700 AFCSU.S.SAMPLE PROBLEM (Continued)FUEL REQUIRED (Continued)With an expected 10 knot head wind, t

CESSNA SECTION 5MODEL 172R NAV III PERFORMANCE GFC 700 AFCSU.S.SAMPLE PROBLEM (Continued)LANDINGA procedure similar to takeoff should be used

SECTION 5 CESSNAPERFORMANCE MODEL 172R NAV IIIGFC 700 AFCSU.S.AIRSPEED CALIBRATION NORMAL STATIC SOURCECONDITIONS: Power required for level flight or

CESSNA SECTION 5MODEL 172R NAV III PERFORMANCE GFC 700 AFCSU.S.AIRSPEED CALIBRATION ALTERNATE STATIC SOURCEHEATER OFF, VENTS AND WINDOWS CLOSE

SECTION 5 CESSNAPERFORMANCE MODEL 172R NAV IIIGFC 700 AFCSU.S.TEMPERATURE CONVERSION CHARTFigure 5-2172RPHBUS-005-12

CESSNA SECTION 5MODEL 172R NAV III PERFORMANCE GFC 700 AFCSU.S.STALL SPEED AT 2450 POUNDSCONDITIONS:Power IDLEMOST REARWARD CENTER OF GRAVITYM

SECTION 5 CESSNAPERFORMANCE MODEL 172R NAV IIIGFC 700 AFCSU.S.CROSSWIND COMPONENT NOTEMaximum demonstrated crosswind velocity is 15 knots (nota limita

CESSNA SECTION 5MODEL 172R NAV III PERFORMANCE GFC 700 AFCSU.S.SHORT FIELD TAKEOFF DISTANCE AT 2450 POUNDSCONDITIONS:Flaps 10°Full Throttle pr

CESSNA SECTION 1MODEL 172R NAV III GENERAL GFC 700 AFCSU.S.DESCRIPTIVE DATA (Continued)STANDARD AIRPLANE WEIGHTSStandard Empty Weight . . . .

SECTION 5 CESSNAPERFORMANCE MODEL 172R NAV IIIGFC 700 AFCSU.S.MAXIMUM RATE OF CLIMB AT 2450 POUNDSCONDITIONS:Flaps UPFull Throttle NOTEMixture leaned

CESSNA SECTION 5MODEL 172R NAV III PERFORMANCE GFC 700 AFCSU.S.TIME, FUEL AND DISTANCE TO CLIMBAT 2450 POUNDSCONDITIONS:Flaps UPFull ThrottleS

SECTION 5 CESSNAPERFORMANCE MODEL 172R NAV IIIGFC 700 AFCSU.S.CRUISE PERFORMANCECONDITIONS:2450 PoundsRecommended Lean Mixture. NOTE• Maximum cruise p

CESSNA SECTION 5MODEL 172R NAV III PERFORMANCE GFC 700 AFCSU.S.CRUISE PERFORMANCECONDITIONS:2450 PoundsRecommended Lean Mixture. NOTE• Maximum

SECTION 5 CESSNAPERFORMANCE MODEL 172R NAV IIIGFC 700 AFCSU.S.RANGE PROFILE45 MINUTES RESERVE53 GALLONS USABLE FUELCONDITIONS:2450 Pounds Standard Tem

CESSNA SECTION 5MODEL 172R NAV III PERFORMANCE GFC 700 AFCSU.S.ENDURANCE PROFILE45 MINUTES RESERVE53 GALLONS USABLE FUELCONDITIONS:2450 Pounds

SECTION 5 CESSNAPERFORMANCE MODEL 172R NAV IIIGFC 700 AFCSU.S.SHORT FIELD LANDING DISTANCE AT 2450 POUNDSCONDITIONS:Flaps FULL Zero WindPower IDLE Pa

CESSNA SECTION 6MODEL 172R NAV III WEIGHT AND BALANCE/ GFC 700 AFCS EQUIPMENT LISTU.S.WEIGHT AND BALANCE/EQUIPMENT LISTTABLE OF CONTENTSPageIn

CESSNA SECTION 6MODEL 172R NAV III WEIGHT AND BALANCE/ GFC 700 AFCS EQUIPMENT LISTU.S.INTRODUCTIONThis section describes the procedure for est

SECTION 1 CESSNAGENERAL MODEL 172R NAV IIIGFC 700 AFCSU.S.SYMBOLS, ABBREVIATIONS AND TERMINOLOGYGENERAL AIRSPEED TERMINOLOGY AND SYMBOLSKCAS Knots Cal

SECTION 6 CESSNAWEIGHT AND BALANCE/ MODEL 172R NAV IIIEQUIPMENT LIST GFC 700 AFCSU.S.AIRPLANE WEIGHING PROCEDURES (Continued)2. Level:a. Place scales

CESSNA SECTION 6MODEL 172R NAV III WEIGHT AND BALANCE/ GFC 700 AFCS EQUIPMENT LISTU.S.AIRPLANE WEIGHING FORMFigure 6-1 (Sheet 1 of 2)172RPHBUS

SECTION 6 CESSNAWEIGHT AND BALANCE/ MODEL 172R NAV IIIEQUIPMENT LIST GFC 700 AFCSU.S.AIRPLANE WEIGHING FORMFigure 6-1 (Sheet 2)172RPHBUS-006-6

CESSNA SECTION 6MODEL 172R NAV III WEIGHT AND BALANCE/ GFC 700 AFCS EQUIPMENT LISTU.S.SAMPLE WEIGHT AND BALANCE RECORDFigure 6-2172RPHBUS-006-

SECTION 6 CESSNAWEIGHT AND BALANCE/ MODEL 172R NAV IIIEQUIPMENT LIST GFC 700 AFCSU.S.WEIGHT AND BALANCEThe following information will enable you to op

CESSNA SECTION 6MODEL 172R NAV III WEIGHT AND BALANCE/ GFC 700 AFCS EQUIPMENT LISTU.S.WEIGHT AND BALANCE (Continued)BAGGAGE TIEDOWNA nylon bag

SECTION 6 CESSNAWEIGHT AND BALANCE/ MODEL 172R NAV IIIEQUIPMENT LIST GFC 700 AFCSU.S.SAMPLE LOADING PROBLEMITEM DESCRIPTIONWEIGHT AND MOMENT TABULATIO

CESSNA SECTION 6MODEL 172R NAV III WEIGHT AND BALANCE/ GFC 700 AFCS EQUIPMENT LISTU.S.SAMPLE LOADING PROBLEM NOTEWhen several loading configur

SECTION 6 CESSNAWEIGHT AND BALANCE/ MODEL 172R NAV IIIEQUIPMENT LIST GFC 700 AFCSU.S.LOADING GRAPH NOTELine representing adjustable seats shows the pi

CESSNA SECTION 6MODEL 172R NAV III WEIGHT AND BALANCE/ GFC 700 AFCS EQUIPMENT LISTU.S.LOADING ARRANGEMENTS*Pilot and front seat passenger cent

CESSNA SECTION 1MODEL 172R NAV III GENERAL GFC 700 AFCSU.S.SYMBOLS, ABBREVIATIONS AND TERMINOLOGY(Continued)METEOROLOGICAL TERMINOLOGYOAT Outs

SECTION 6 CESSNAWEIGHT AND BALANCE/ MODEL 172R NAV IIIEQUIPMENT LIST GFC 700 AFCSU.S.INTERNAL CABIN DIMENSIONS NOTE• Maximum allowable floor loading i

CESSNA SECTION 6MODEL 172R NAV III WEIGHT AND BALANCE/ GFC 700 AFCS EQUIPMENT LISTU.S.CENTER OF GRAVITY MOMENT ENVELOPEFigure 6-7172RPHBUS-006

SECTION 6 CESSNAWEIGHT AND BALANCE/ MODEL 172R NAV IIIEQUIPMENT LIST GFC 700 AFCSU.S.CENTER OF GRAVITY LIMITSFigure 6-8172RPHBUS-006-16

CESSNA SECTION 6MODEL 172R NAV III WEIGHT AND BALANCE/ GFC 700 AFCS EQUIPMENT LISTU.S.COMPREHENSIVE EQUIPMENT LISTFigure 6-9 is a comprehensiv

CESSNA SECTION 6MODEL 172R NAV III WEIGHT AND BALANCE/ GFC 700 AFCS EQUIPMENT LISTU.S.Figure 6-9 (Sheet 1 of 6)ITEM NO EQUIPMENT LIST DESCRIPT

SECTION 6 CESSNAWEIGHT AND BALANCE/ MODEL 172R NAV IIIEQUIPMENT LIST GFC 700 AFCSU.S.Figure 6-9 (Sheet 2)ITEM NO EQUIPMENT LIST DESCRIPTIONREF DRAWING

CESSNA SECTION 6MODEL 172R NAV III WEIGHT AND BALANCE/ GFC 700 AFCS EQUIPMENT LISTU.S.Figure 6-9 (Sheet 3)ITEM NO EQUIPMENT LIST DESCRIPTIONRE

SECTION 6 CESSNAWEIGHT AND BALANCE/ MODEL 172R NAV IIIEQUIPMENT LIST GFC 700 AFCSU.S.Figure 6-9 (Sheet 4)ITEM NO EQUIPMENT LIST DESCRIPTIONREF DRAWING

CESSNA SECTION 6MODEL 172R NAV III WEIGHT AND BALANCE/ GFC 700 AFCS EQUIPMENT LISTU.S.Figure 6-9 (Sheet 5)ITEM NO EQUIPMENT LIST DESCRIPTIONRE

INTRODUCTION CESSNAMODEL 172R NAV IIIGFC 700 AFCSU.S.PERFORMANCE - SPECIFICATIONS*SPEED:Maximum at Sea Level . . . . . . . . . . . . . . . . . . . .

SECTION 1 CESSNAGENERAL MODEL 172R NAV IIIGFC 700 AFCSU.S.SYMBOLS, ABBREVIATIONS AND TERMINOLOGY(Continued)ENGINE POWER TERMINOLOGY (Continued)RichMix

SECTION 6 CESSNAWEIGHT AND BALANCE/ MODEL 172R NAV IIIEQUIPMENT LIST GFC 700 AFCSU.S.Figure 6-9 (Sheet 6)ITEM NO EQUIPMENT LIST DESCRIPTIONREF DRAWING

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.AIRPLANE AND SYSTEMS DESCRIPTIONTABLE OF CONTENTSPageIntrod

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.TABLE OF CONTENTS (Continued)PageCylinder Head Temperature . . . .

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.TABLE OF CONTENTS (Continued)PageLighting Systems . . . . .

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.INTRODUCTIONThis section provides description and operation

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.AIRFRAME (Continued)The rudder is constructed of a formed leading ed

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.FLIGHT CONTROLSThe airplane's flight control system, R

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.FLIGHT CONTROLS AND TRIM SYSTEMFigure 7-1 (Sheet 1 of 2)172RPHBUS-00

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.FLIGHT CONTROLS AND TRIM SYSTEMSFigure 7-1 (Sheet 2)172RPHB

CESSNA SECTION 1MODEL 172R NAV III GENERAL GFC 700 AFCSU.S.SYMBOLS, ABBREVIATIONS AND TERMINOLOGY(Continued)AIRPLANE PERFORMANCE AND FLIGHT PL

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.INSTRUMENT PANELThe instrument panel, Refer to Figure 7-2, is of all

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.INSTRUMENT PANEL (Continued)PILOT PANEL LAYOUT (Continued)S

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.INSTRUMENT PANEL (Continued)CENTER PANEL LAYOUT (Continued)The stand

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.INSTRUMENT PANEL (Continued)RIGHT PANEL LAYOUTThe Emergency

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.INSTRUMENT PANELFigure 7-2172RPHBUS-007-14

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.INSTRUMENT PANEL1. MASTER Switch (ALT and BAT)2. STBY BATT

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.FLIGHT INSTRUMENTSThe G1000 Integrated Cockpit System primary flight

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.FLIGHT INSTRUMENTS (Continued)ATTITUDE INDICATORThe G1000 a

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.FLIGHT INSTRUMENTS (Continued)AIRSPEED INDICATORThe G1000 vertical t

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.FLIGHT INSTRUMENTS (Continued)HORIZONTAL SITUATION INDICATO

SECTION 1 CESSNAGENERAL MODEL 172R NAV IIIGFC 700 AFCSU.S.SYMBOLS, ABBREVIATIONS AND TERMINOLOGY(Continued)WEIGHT AND BALANCE TERMINOLOGYReference Dat

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.FLIGHT INSTRUMENTS (Continued)HORIZONTAL SITUATION INDICATOR (Contin

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.GROUND CONTROLEffective ground control while taxiing is acc

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.WING FLAP SYSTEMThe single slot type wing flaps, Refer to Figure 7-3

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.LANDING GEAR SYSTEMThe landing gear is of the tricycle type

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.SEATSThe seating arrangement consists of two vertically adjusting cr

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.INTEGRATED SEAT BELT/SHOULDER HARNESSAll seat positions are

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.INTEGRATED SEAT BELT/SHOULDER HARNESSFigure 7-4172RPHBUS-007-26

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.ENTRANCE DOORS AND CABIN WINDOWSEntry to and exit from the

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.ENTRANCE DOORS AND CABIN WINDOWS(Continued)Exit from the airplane is

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.ENGINEThe airplane is powered by a direct drive, horizontal

CESSNA SECTION 1MODEL 172R NAV III GENERAL GFC 700 AFCSU.S.SYMBOLS, ABBREVIATIONS AND TERMINOLOGY(Continued)WEIGHT AND BALANCE TERMINOLOGY (Co

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.ENGINE (Continued)ENGINE INSTRUMENTSThe G1000 Engine Indication Syst

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.ENGINE (Continued)ENGINE INSTRUMENTS (Continued)RPM (TACHOM

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.ENGINE (Continued)ENGINE INSTRUMENTS (Continued)FUEL FLOWFuel flow i

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.ENGINE (Continued)ENGINE INSTRUMENTS (Continued)OIL PRESSUR

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.ENGINE (Continued)ENGINE INSTRUMENTS (Continued)CYLINDER HEAD TEMPER

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.ENGINE (Continued)NEW ENGINE BREAK-IN AND OPERATIONThe engi

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.ENGINE (Continued)IGNITION AND STARTER SYSTEM Engine ignition is pro

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.ENGINE (Continued)EXHAUST SYSTEMExhaust gas from each cylin

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.FUEL SYSTEMThe airplane fuel system, Refer to Figure 7-6, consists o

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.FUEL SYSTEM (Continued)FUEL DISTRIBUTIONFuel flows by gravi

SECTION 1 CESSNAGENERAL MODEL 172R NAV IIIGFC 700 AFCSU.S.METRIC/IMPERIAL/U.S. CONVERSION CHARTSThe following charts have been provided to help intern

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.FUEL SYSTEM (Continued)FUEL INDICATING SYSTEM (Continued)The fuel qu

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.FUEL SYSTEM (Continued)FUEL CALCULATIONS NOTEFuel calculati

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.FUEL SYSTEM (Continued)Figure 7-6172RPHBUS-007-42

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.FUEL SYSTEM (Continued)AUXILIARY FUEL PUMP OPERATIONThe aux

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.FUEL SYSTEM (Continued)FUEL RETURN SYSTEMA fuel return system was in

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.FUEL SYSTEM (Continued)FUEL SELECTOR VALVEThe fuel selector

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.FUEL SYSTEM (Continued)FUEL DRAIN VALVESThe fuel system is equipped

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.ELECTRICAL SYSTEMThe airplane is equipped with a 28-volt di

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.ELECTRICAL SYSTEM (Continued)Figure 7-7 (Sheet 1 of 3)172RPHBUS-007-

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.ELECTRICAL SYSTEM (Continued)Figure 7-7 (Sheet 2)172RPHBUS-

CESSNA SECTION 1MODEL 172R NAV III GENERAL GFC 700 AFCSU.S.WEIGHT CONVERSIONSFigure 1-2 (Sheet 1 of 2)1-17172RPHBUS-00

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.ELECTRICAL SYSTEM (Continued)Figure 7-7 (Sheet 3)172RPHBUS-007-50

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.ELECTRICAL SYSTEM (Continued)G1000 ANNUNCIATOR PANELAll sys

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.ELECTRICAL SYSTEM (Continued)STANDBY BATTERY SWITCHThe STBY BATT mas

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.ELECTRICAL SYSTEM (Continued)ELECTRICAL SYSTEM MONITORING A

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.ELECTRICAL SYSTEM (Continued)ELECTRICAL SYSTEM MONITORING ANDANNUNCI

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.ELECTRICAL SYSTEM (Continued)ELECTRICAL SYSTEM MONITORING A

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.ELECTRICAL SYSTEM (Continued)ELECTRICAL SYSTEM MONITORING ANDANNUNCI

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.ELECTRICAL SYSTEM (Continued)CIRCUIT BREAKERS AND FUSESIndi

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.ELECTRICAL SYSTEM (Continued)EXTERNAL POWER RECEPTACLEA external pow

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.LIGHTING SYSTEMSEXTERIOR LIGHTINGExterior lighting consists

SECTION 1 CESSNAGENERAL MODEL 172R NAV IIIGFC 700 AFCSU.S.WEIGHT CONVERSIONSFigure 1-2 (Sheet 2)172RPHBUS-001-18

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.LIGHTING SYSTEMS (Continued)INTERIOR LIGHTINGInterior lighting is co

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.LIGHTING SYSTEMS (Continued)INTERIOR LIGHTING (Continued)Av

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.CABIN HEATING, VENTILATING AND DEFROSTINGSYSTEMThe temperature and v

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.CABIN HEATING, VENTILATION AND DEFROSTING SYSTEMFigure 7-81

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.PITOT-STATIC SYSTEM AND INSTRUMENTSThe pitot-static system uses a he

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.VACUUM SYSTEM AND INSTRUMENTSThe vacuum system, Refer to Fi

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.VACUUM SYSTEMFigure 7-9172RPHBUS-007-66

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.CLOCK/O.A.T. INDICATORA numerical time or clock window, bas

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.STANDARD AVIONICSThe Garmin G1000 Avionics System is an integrated f

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.STANDARD AVIONICS (Continued)AUDIO PANEL (GMA)The audio pan

CESSNA SECTION 1MODEL 172R NAV III GENERAL GFC 700 AFCSU.S.LENGTH CONVERSIONSFigure 1-3 (Sheet 1 of 4)1-19172RPHBUS-00

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.STANDARD AVIONICS (Continued)AIR DATA COMPUTER (GDC)The Air Data Com

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.STANDARD AVIONICS (Continued)GFC 700 AUTOMATIC FLIGHT CONTR

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.GFC 700 SYSTEM SCHEMATICFigure 7-10172RPHBUS-007-72

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.AVIONICS SUPPORT EQUIPMENTAvionics cooling fans, antennas,

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.AVIONICS SUPPORT EQUIPMENT (Continued)ANTENNASTwo dual-mode VHF COM/

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.AVIONICS SUPPORT EQUIPMENT (Continued)MICROPHONE AND HEADSE

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.AVIONICS SUPPORT EQUIPMENT (Continued)AUXILIARY AUDIO INPUT JACKAn a

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.AVIONICS SUPPORT EQUIPMENT (Continued)12V POWER OUTLETA pow

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.AVIONICS SUPPORT EQUIPMENT (Continued)STATIC DISCHARGERSStatic disch

CESSNA SECTION 7MODEL 172R NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCSU.S.CABIN FEATURESEMERGENCY LOCATOR TRANSMITTER (ELT)Refer to S

SECTION 1 CESSNAGENERAL MODEL 172R NAV IIIGFC 700 AFCSU.S.LENGTH CONVERSIONSFigure 1-3 (Sheet 2)172RPHBUS-001-20

SECTION 7 CESSNAAIRPLANE AND SYSTEM DESCRIPTION MODEL 172R NAV IIIGFC 700 AFCSU.S.CABIN FEATURES (Continued)CARBON MONOXIDE DETECTION SYSTEMThe carbon

CESSNA SECTION 8MODEL 172R NAV III AIRPLANE HANDLING, SERVICE GFC 700 AFCS AND MAINTENANCEU.S.AIRPLANE HANDLING, SERVICE AND MAINTENANCETABLE

SECTION 8 CESSNAAIRPLANE HANDLING, SERVICE MODEL 172R NAV IIIAND MAINTENANCE GFC 700 AFCSU.S.TABLE OF CONTENTS (Continued)PageFuel . . . . . . . . .

CESSNA SECTION 8MODEL 172R NAV III AIRPLANE HANDLING, SERVICE GFC 700 AFCS AND MAINTENANCEU.S.INTRODUCTIONThis section contains factory recomm

SECTION 8 CESSNAAIRPLANE HANDLING, SERVICE MODEL 172R NAV IIIAND MAINTENANCE GFC 700 AFCSU.S.IDENTIFICATION PLATEAll correspondence regarding your air

CESSNA SECTION 8MODEL 172R NAV III AIRPLANE HANDLING, SERVICE GFC 700 AFCS AND MAINTENANCEU.S.PUBLICATIONS Various publications and flight ope

SECTION 8 CESSNAAIRPLANE HANDLING, SERVICE MODEL 172R NAV IIIAND MAINTENANCE GFC 700 AFCSU.S.AIRPLANE FILEThere are miscellaneous data, information an

CESSNA SECTION 8MODEL 172R NAV III AIRPLANE HANDLING, SERVICE GFC 700 AFCS AND MAINTENANCEU.S.AIRPLANE INSPECTION PERIODSFAA REQUIRED INSPECTI

SECTION 8 CESSNAAIRPLANE HANDLING, SERVICE MODEL 172R NAV IIIAND MAINTENANCE GFC 700 AFCSU.S.AIRPLANE INSPECTION PERIODS (Continued)CESSNA CUSTOMER CA

CESSNA SECTION 8MODEL 172R NAV III AIRPLANE HANDLING, SERVICE GFC 700 AFCS AND MAINTENANCEU.S.ALTERATIONS OR REPAIRSIt is essential that the F

CESSNA SECTION 1MODEL 172R NAV III GENERAL GFC 700 AFCSU.S.LENGTH CONVERSIONSFigure 1-3 (Sheet 3)1-21172RPHBUS-00

SECTION 8 CESSNAAIRPLANE HANDLING, SERVICE MODEL 172R NAV IIIAND MAINTENANCE GFC 700 AFCSU.S.GROUND HANDLING (Continued)TIEDOWNProper tiedown procedur

CESSNA SECTION 8MODEL 172R NAV III AIRPLANE HANDLING, SERVICE GFC 700 AFCS AND MAINTENANCEU.S.GROUND HANDLING (Continued)JACKING (Continued)To

SECTION 8 CESSNAAIRPLANE HANDLING, SERVICE MODEL 172R NAV IIIAND MAINTENANCE GFC 700 AFCSU.S.GROUND HANDLING (Continued)FLYABLE STORAGE (Continued)If

CESSNA SECTION 8MODEL 172R NAV III AIRPLANE HANDLING, SERVICE GFC 700 AFCS AND MAINTENANCEU.S.OILOIL SPECIFICATIONMIL-L-6082 or SAE J1966 Avia

SECTION 8 CESSNAAIRPLANE HANDLING, SERVICE MODEL 172R NAV IIIAND MAINTENANCE GFC 700 AFCSU.S.OIL (Continued)CAPACITY OF ENGINE SUMPThe engine has a to

CESSNA SECTION 8MODEL 172R NAV III AIRPLANE HANDLING, SERVICE GFC 700 AFCS AND MAINTENANCEU.S.FUELAPPROVED FUEL GRADES (AND COLORS)100LL Grade

SECTION 8 CESSNAAIRPLANE HANDLING, SERVICE MODEL 172R NAV IIIAND MAINTENANCE GFC 700 AFCSU.S.FUEL (Continued)FUEL ADDITIVESStrict adherence to recomme

CESSNA SECTION 8MODEL 172R NAV III AIRPLANE HANDLING, SERVICE GFC 700 AFCS AND MAINTENANCEU.S.FUEL (Continued)FUEL ADDITIVES (Continued)Alcoho

SECTION 8 CESSNAAIRPLANE HANDLING, SERVICE MODEL 172R NAV IIIAND MAINTENANCE GFC 700 AFCSU.S.FUEL MIXING RATIOFigure 8-1172RPHBUS-008-18

CESSNA SECTION 8MODEL 172R NAV III AIRPLANE HANDLING, SERVICE GFC 700 AFCS AND MAINTENANCEU.S.FUEL (Continued)FUEL ADDITIVES (Continued)Diethy

CESSNA INTRODUCTIONMODEL 172R NAV III GFC 700 AFCSU.S.PERFORMANCE - SPECIFICATIONS (Continued)STANDARD EMPTY WEIGHT. . . . . . . . . . . . . .

SECTION 1 CESSNAGENERAL MODEL 172R NAV IIIGFC 700 AFCSU.S.LENGTH CONVERSIONSFigure 1-3 (Sheet 4)172RPHBUS-001-22

SECTION 8 CESSNAAIRPLANE HANDLING, SERVICE MODEL 172R NAV IIIAND MAINTENANCE GFC 700 AFCSU.S.FUEL (Continued)FUEL CONTAMINATIONFuel contamination is u

CESSNA SECTION 8MODEL 172R NAV III AIRPLANE HANDLING, SERVICE GFC 700 AFCS AND MAINTENANCEU.S.LANDING GEARConsult the following table for serv

SECTION 8 CESSNAAIRPLANE HANDLING, SERVICE MODEL 172R NAV IIIAND MAINTENANCE GFC 700 AFCSU.S.CLEANING AND CAREWINDSHIELD AND WINDOWSThe plastic windsh

CESSNA SECTION 8MODEL 172R NAV III AIRPLANE HANDLING, SERVICE GFC 700 AFCS AND MAINTENANCEU.S.CLEANING AND CARE (Continued)PAINTED SURFACESThe

SECTION 8 CESSNAAIRPLANE HANDLING, SERVICE MODEL 172R NAV IIIAND MAINTENANCE GFC 700 AFCSU.S.CLEANING AND CARE (Continued)PROPELLER CAREPreflight insp

CESSNA SECTION 8MODEL 172R NAV III AIRPLANE HANDLING, SERVICE GFC 700 AFCS AND MAINTENANCEU.S.CLEANING AND CARE (Continued)INTERIOR CARETo rem

CESSNA SECTION 9MODEL 172R NAV III SUPPLEMENTS GFC 700 AFCSU.S.FAA APPROVEDSUPPLEMENTSINTRODUCTIONThe supplements in this section contain amen

CESSNA SECTION 9MODEL 172R NAV III SUPPLEMENTS GFC 700 AFCSU.S.LOG OF APPROVED SUPPLEMENTS NOTEIT IS THE AIRPLANE OWNER'S RESPONSIBILITY

CESSNA SECTION 1MODEL 172R NAV III GENERAL GFC 700 AFCSU.S.DISTANCE CONVERSIONSFigure 1-41-23172RPHBUS-00

U.S.CESSNA MODEL 172RNAV III AVIONICS OPTION - GFC 700 AFCSSerials 17281497 and OnSUPPLEMENT 1ARTEX ME406EMERGENCY LOCATOR TRANSMITTER (ELT)This suppl

SECTION 9 - SUPPLEMENTS CESSNASUPPLEMENT 1 MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDSUPPLEMENT 1ARTEX ME406 EMERGENCY LOCATOR TRANSMITTER(ELT)Use

CESSNA SECTION 9 - SUPPLEMENTSMODEL 172R NAV III SUPPLEMENT 1 GFC 700 AFCSU.S.FAA APPROVEDSERVICE BULLETIN CONFIGURATION LISTThe following is

SECTION 9 - SUPPLEMENTS CESSNASUPPLEMENT 1 MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDARTEX ME406 EMERGENCY LOCATORTRANSMITTER (ELT)GENERALThe Arte

CESSNA SECTION 9 - SUPPLEMENTSMODEL 172R NAV III SUPPLEMENT 1 GFC 700 AFCSU.S.FAA APPROVEDARTEX ME406 ELT CONTROL PANEL 1. ELT PANEL SWITCH (2

SECTION 9 - SUPPLEMENTS CESSNASUPPLEMENT 1 MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDOPERATING LIMITATIONSThere are no additional airplane operati

CESSNA SECTION 9 - SUPPLEMENTSMODEL 172R NAV III SUPPLEMENT 1 GFC 700 AFCSU.S.FAA APPROVEDEMERGENCY PROCEDURESIf a forced landing is necessary

SECTION 9 - SUPPLEMENTS CESSNASUPPLEMENT 1 MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDNORMAL PROCEDURESWhen operating in a remote area or over haza

U.S.CESSNA MODEL 172RNAV III AVIONICS OPTION - GFC 700 AFCSSerials 17281497 and OnSUPPLEMENT 2ARTEX C406-NEMERGENCY LOCATOR TRANSMITTER (ELT)This supp

SECTION 1 CESSNAGENERAL MODEL 172R NAV IIIGFC 700 AFCSU.S.VOLUME CONVERSIONSFigure 1-5 (Sheet 1 of 3)1-24172RPHBUS-00

SECTION 9 - SUPPLEMENTS CESSNASUPPLEMENT 2 MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDSUPPLEMENT 2ARTEX C406-N EMERGENCY LOCATOR TRANSMITTER(ELT)Us

CESSNA SECTION 9 - SUPPLEMENTSMODEL 172R NAV III SUPPLEMENT 2 GFC 700 AFCSU.S.FAA APPROVEDSERVICE BULLETIN CONFIGURATION LISTThe following is

SECTION 9 - SUPPLEMENTS CESSNASUPPLEMENT 2 MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDARTEX C406-N EMERGENCY LOCATORTRANSMITTER (ELT)GENERALThe Art

CESSNA SECTION 9 - SUPPLEMENTSMODEL 172R NAV III SUPPLEMENT 2 GFC 700 AFCSU.S.FAA APPROVEDARTEX C406-N ELT CONTROL PANEL 1. ELT PANEL SWITCH

SECTION 9 - SUPPLEMENTS CESSNASUPPLEMENT 2 MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDOPERATING LIMITATIONSThere are no additional airplane operati

CESSNA SECTION 9 - SUPPLEMENTSMODEL 172R NAV III SUPPLEMENT 2 GFC 700 AFCSU.S.FAA APPROVEDEMERGENCY PROCEDURESIf a forced landing is necessar

SECTION 9 - SUPPLEMENTS CESSNASUPPLEMENT 2 MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDNORMAL PROCEDURESWhen operating in a remote area or over haza

U.S.CESSNA MODEL 172RNAV III AVIONICS OPTION - GFC 700 AFCSSerials 17281497 and OnSUPPLEMENT 3BENDIX/KING KR87AUTOMATIC DIRECTION FINDER (ADF)This sup

SECTION 9 - SUPPLEMENTS CESSNASUPPLEMENT 3 MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDSUPPLEMENT 3BENDIX/KING KR87 AUTOMATIC DIRECTIONFINDER (ADF)U

CESSNA SECTION 9 - SUPPLEMENTSMODEL 172R NAV III SUPPLEMENT 3 GFC 700 AFCSU.S.FAA APPROVEDSERVICE BULLETIN CONFIGURATION LISTThe following is

CESSNA SECTION 1MODEL 172R NAV III GENERAL GFC 700 AFCSU.S.VOLUME CONVERSIONSFigure 1-5 (Sheet 2)1-25172RPHBUS-00

SECTION 9 - SUPPLEMENTS CESSNASUPPLEMENT 3 MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDBENDIX/KING KR87 AUTOMATIC DIRECTIONFINDER (ADF)GENERALThe Be

CESSNA SECTION 9 - SUPPLEMENTSMODEL 172R NAV III SUPPLEMENT 3 GFC 700 AFCSU.S.FAA APPROVEDBENDIX/KING KR87 AUTOMATIC DIRECTION FINDER (ADF)Fig

SECTION 9 - SUPPLEMENTS CESSNASUPPLEMENT 3 MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDGENERAL (Continued)1. ANT/ADF MODE ANNUNCIATOR - Antenna (ANT

CESSNA SECTION 9 - SUPPLEMENTSMODEL 172R NAV III SUPPLEMENT 3 GFC 700 AFCSU.S.FAA APPROVEDGENERAL (Continued)6. FREQUENCY SELECT KNOBS - Selec

SECTION 9 - SUPPLEMENTS CESSNASUPPLEMENT 3 MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDOPERATING LIMITATIONSRefer to Section 2 of the Pilot's O

CESSNA SECTION 9 - SUPPLEMENTSMODEL 172R NAV III SUPPLEMENT 3 GFC 700 AFCSU.S.FAA APPROVEDNORMAL PROCEDURES (Continued)ADF TEST (PREFLIGHT or

SECTION 9 - SUPPLEMENTS CESSNASUPPLEMENT 3 MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDNORMAL PROCEDURES (Continued)TO OPERATE ELAPSED TIME TIMER-CO

CESSNA SECTION 9 - SUPPLEMENTSMODEL 172R NAV III SUPPLEMENT 3 GFC 700 AFCSU.S.FAA APPROVEDNORMAL PROCEDURES (Continued)TO OPERATE ELAPSED TIME

SECTION 9 - SUPPLEMENTS CESSNASUPPLEMENT 3 MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDNORMAL PROCEDURES (Continued)ADF OPERATION NOTES: (Continued)

U.S.CESSNA MODEL 172RNAV III AVIONICS OPTION - GFC 700 AFCSSerials 17281497 and OnSUPPLEMENT 4WINTERIZATION KITThis supplement must be inserted into S

SECTION 1 CESSNAGENERAL MODEL 172R NAV IIIGFC 700 AFCSU.S.VOLUME CONVERSIONSFigure 1-5 (Sheet 3)1-26172RPHBUS-00

SECTION 9 - SUPPLEMENTS CESSNASUPPLEMENT 4 MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDSUPPLEMENT 4WINTERIZATION KITUse the Log of Effective Pages t

CESSNA SECTION 9 - SUPPLEMENTSMODEL 172R NAV III SUPPLEMENT 4 GFC 700 AFCSU.S.FAA APPROVEDSERVICE BULLETIN CONFIGURATION LISTThe following is

SECTION 9 - SUPPLEMENTS CESSNASUPPLEMENT 4 MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDWINTERIZATION KITGENERALThe winterization kit consists of two

CESSNA SECTION 9 - SUPPLEMENTSMODEL 172R NAV III SUPPLEMENT 4 GFC 700 AFCSU.S.FAA APPROVEDOPERATING LIMITATIONSThe following information must

SECTION 9 - SUPPLEMENTS CESSNASUPPLEMENT 4 MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDEMERGENCY PROCEDURESThere is no change to the airplane emerge

U.S.CESSNA MODEL 172RNAV III AVIONICS OPTION - GFC 700 AFCSSerials 17281497 and OnSUPPLEMENT 5JAR-OPS OPERATIONAL ELIGIBILITYThis supplement must be i

SECTION 9 - SUPPLEMENTS CESSNASUPPLEMENT 5 MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDSUPPLEMENT 5JAR-OPS OPERATIONAL ELIGIBILITYUse the Log of Eff

CESSNA SECTION 9 - SUPPLEMENTSMODEL 172R NAV III SUPPLEMENT 5 GFC 700 AFCSU.S.FAA APPROVEDSERVICE BULLETIN CONFIGURATION LISTThe following is

SECTION 9 - SUPPLEMENTS CESSNASUPPLEMENT 5 MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDJAR-OPS OPERATIONAL ELIGIBILITYGENERALOPERATIONAL ELIGIBILITY

CESSNA SECTION 9 - SUPPLEMENTSMODEL 172R NAV III SUPPLEMENT 5 GFC 700 AFCSU.S.FAA APPROVEDGENERAL (Continued)SSR MODE S ENHANCED SURVEILLANCEO

CESSNA SECTION 1MODEL 172R NAV III GENERAL GFC 700 AFCSU.S.TEMPERATURE CONVERSIONSFigure 1-61-27172RPHBUS-00

SECTION 1 CESSNAGENERAL MODEL 172R NAV IIIGFC 700 AFCSU.S.PRESSURE CONVERSIONHECTOPASCALS TO INCHES OF MERCURYFigure 1-7172RPHBUS-001-28

CESSNA SECTION 1MODEL 172R NAV III GENERAL GFC 700 AFCSU.S.VOLUME TO WEIGHT CONVERSIONFigure 1-8172RPHBUS-00 1-29

SECTION 1 CESSNAGENERAL MODEL 172R NAV IIIGFC 700 AFCSU.S.QUICK CONVERSIONSFigure 1-9172RPHBUS-001-30

CESSNA SECTION 2MODEL 172R NAV III OPERATING LIMITATIONS GFC 700 AFCSU.S.FAA APPROVEDOPERATING LIMITATIONSTABLE OF CONTENTSPageIntroduction .

CESSNA SECTION 2MODEL 172R NAV III OPERATING LIMITATIONS GFC 700 AFCSU.S.FAA APPROVEDINTRODUCTIONSection 2 includes operating limitations, in

SECTION 2 CESSNAOPERATING LIMITATIONS MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDAIRSPEED LIMITATIONSAirspeed limitations and their operational sig

CESSNA SECTION 2MODEL 172R NAV III OPERATING LIMITATIONS GFC 700 AFCSU.S.FAA APPROVEDAIRSPEED INDICATOR MARKINGSAirspeed indicator markings a

SECTION 2 CESSNAOPERATING LIMITATIONS MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDPOWERPLANT LIMITATIONSEngine Manufacturer: Textron LycomingEngine

CESSNA SECTION 2MODEL 172R NAV III OPERATING LIMITATIONS GFC 700 AFCSU.S.FAA APPROVEDPOWERPLANT INSTRUMENT MARKINGSPowerplant instrument mark

SECTION 2 CESSNAOPERATING LIMITATIONS MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDWEIGHT LIMITSNORMAL CATEGORYMaximum Ramp Weight: . . . . . . . . .

CESSNA SECTION 2MODEL 172R NAV III OPERATING LIMITATIONS GFC 700 AFCSU.S.FAA APPROVEDCENTER OF GRAVITY LIMITSNORMAL CATEGORYCenter Of Gravity

SECTION 2 CESSNAOPERATING LIMITATIONS MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDMANEUVER LIMITSNORMAL CATEGORYThis airplane is certificated in bot

CESSNA SECTION 2MODEL 172R NAV III OPERATING LIMITATIONS GFC 700 AFCSU.S.FAA APPROVEDMANEUVER LIMITS (Continued) UTILITY CATEGORY (Continued)

CESSNA INTRODUCTIONMODEL 172R NAV III GFC 700 AFCSU.S.v/viOriginal IssueCessna Aircraft CompanyModel 172RNAV III AVIONICS OPTION - GFC 700 AFCS

SECTION 2 CESSNAOPERATING LIMITATIONS MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDKINDS OF OPERATIONS LIMITSThe Cessna 172R Nav III airplane is appr

CESSNA SECTION 2MODEL 172R NAV III OPERATING LIMITATIONS GFC 700 AFCSU.S.FAA APPROVEDKINDS OF OPERATIONS EQUIPMENT LIST NOTE1. The European

SECTION 2 CESSNAOPERATING LIMITATIONS MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDKINDS OF OPERATIONS EQUIPMENT LIST (Continued)(Continued Next Page

CESSNA SECTION 2MODEL 172R NAV III OPERATING LIMITATIONS GFC 700 AFCSU.S.FAA APPROVEDKINDS OF OPERATIONS EQUIPMENT LIST (Continued)NOTE2. PFD

SECTION 2 CESSNAOPERATING LIMITATIONS MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDKINDS OF OPERATIONS EQUIPMENT LIST (Continued)(Continued Next Page

CESSNA SECTION 2MODEL 172R NAV III OPERATING LIMITATIONS GFC 700 AFCSU.S.FAA APPROVEDKINDS OF OPERATIONS EQUIPMENT LIST (Continued)System, In

SECTION 2 CESSNAOPERATING LIMITATIONS MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDFUEL LIMITATIONSTotal Fuel: . . . . . . . . . . . . . . . . . . .

CESSNA SECTION 2MODEL 172R NAV III OPERATING LIMITATIONS GFC 700 AFCSU.S.FAA APPROVEDSYSTEM LIMITATIONSAUX AUDIO SYSTEMUse of the AUX AUDIO I

SECTION 2 CESSNAOPERATING LIMITATIONS MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDG1000 LIMITATIONSThe current Garmin G1000 Cockpit Reference Guide

CESSNA SECTION 2MODEL 172R NAV III OPERATING LIMITATIONS GFC 700 AFCSU.S.FAA APPROVEDG1000 LIMITATIONS (Continued)The COM 1/2 (split COM) fun

SECTION 2 CESSNAOPERATING LIMITATIONS MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDG1000 LIMITATIONS (Continued)TERRAIN AWARENESS AND WARNING SYSTEM

CESSNA SECTION 2MODEL 172R NAV III OPERATING LIMITATIONS GFC 700 AFCSU.S.FAA APPROVEDPLACARDSThe following information must be displayed in t

SECTION 2 CESSNAOPERATING LIMITATIONS MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDPLACARDS (Continued)3. On the fuel selector valve:4. Near both fue

CESSNA SECTION 2MODEL 172R NAV III OPERATING LIMITATIONS GFC 700 AFCSU.S.FAA APPROVEDPLACARDS (Continued)5. On flap control indicator:6. In b

SECTION 2 CESSNAOPERATING LIMITATIONS MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDPLACARDS (Continued)7. A calibration card must be provided to indi

CESSNA SECTION 2MODEL 172R NAV III OPERATING LIMITATIONS GFC 700 AFCSU.S.FAA APPROVEDPLACARDS (Continued)10. Silk-screened on the upper right

SECTION 2 CESSNAOPERATING LIMITATIONS MODEL 172R NAV IIIGFC 700 AFCSU.S.FAA APPROVEDPLACARDS (Continued)13. On the center overhead flood light control

CESSNA SECTION 3MODEL 172R NAV III EMERGENCY PROCEDURES GFC 700 AFCSU.S.EMERGENCY PROCEDURESTABLE OF CONTENTSPageIntroduction . . . . . . . .

SECTION 3 CESSNAEMERGENCY PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.TABLE OF CONTENTS (Continued)PageABNORMAL LANDINGS. . . . . . . . . . . . . . .

CESSNA SECTION 3MODEL 172R NAV III EMERGENCY PROCEDURES GFC 700 AFCSU.S.TABLE OF CONTENTS (Continued)PageAMPLIFIED EMERGENCY PROCEDURES. . . .

CESSNA INTRODUCTIONMODEL 172R NAV III GFC 700 AFCSU.S.TABLE OF CONTENTSSECTIONGENERAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

CESSNA SECTION 3MODEL 172R NAV III EMERGENCY PROCEDURES GFC 700 AFCSU.S.INTRODUCTIONSection 3 provides checklist and amplified procedures for

SECTION 3 CESSNAEMERGENCY PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.EMERGENCY PROCEDURESProcedures in the Emergency Procedures Checklist portion of

CESSNA SECTION 3MODEL 172R NAV III EMERGENCY PROCEDURES GFC 700 AFCSU.S.ENGINE FAILURES (Continued)ENGINE FAILURE DURING FLIGHT (Restart Proce

SECTION 3 CESSNAEMERGENCY PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.FORCED LANDINGSEMERGENCY LANDING WITHOUT ENGINE POWER1. Pilot and Passenger Sea

CESSNA SECTION 3MODEL 172R NAV III EMERGENCY PROCEDURES GFC 700 AFCSU.S.FORCED LANDINGS (Continued)DITCHING1. Radio - TRANSMIT MAYDAY on 121.5

SECTION 3 CESSNAEMERGENCY PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.FIRESDURING START ON GROUND1. MAGNETOS Switch - START (continue cranking to sta

CESSNA SECTION 3MODEL 172R NAV III EMERGENCY PROCEDURES GFC 700 AFCSU.S.FIRES (Continued)ENGINE FIRE IN FLIGHT1. Mixture Control - IDLE CUTOFF

SECTION 3 CESSNAEMERGENCY PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.FIRES (Continued)ELECTRICAL FIRE IN FLIGHT (Continued)IF FIRE HAS BEEN EXTINGUI

CESSNA SECTION 3MODEL 172R NAV III EMERGENCY PROCEDURES GFC 700 AFCSU.S.FIRES (Continued)WING FIRE1. LAND and TAXI Light Switches - OFF2. NAV

SECTION 3 CESSNAEMERGENCY PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.ICINGINADVERTENT ICING ENCOUNTER DURING FLIGHT1. PITOT HEAT Switch - ON2. Turn

CESSNA SECTION 3MODEL 172R NAV III EMERGENCY PROCEDURES GFC 700 AFCSU.S.STATIC SOURCE BLOCKAGE(ERRONEOUS INSTRUMENT READING SUSPECTED)1. ALT S

SECTION 3 CESSNAEMERGENCY PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.ABNORMAL LANDINGSLANDING WITH A FLAT MAIN TIRE1. Approach - NORMAL2. Wing Flaps

CESSNA SECTION 3MODEL 172R NAV III EMERGENCY PROCEDURES GFC 700 AFCSU.S.ELECTRICAL POWER SUPPLY SYSTEMMALFUNCTIONSHIGH VOLTS ANNUNCIATOR COMES

SECTION 3 CESSNAEMERGENCY PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.ELECTRICAL POWER SUPPLY SYSTEMMALFUNCTIONS (Continued)HIGH VOLTS ANNUNCIATOR CO

CESSNA SECTION 3MODEL 172R NAV III EMERGENCY PROCEDURES GFC 700 AFCSU.S.ELECTRICAL POWER SUPPLY SYSTEMMALFUNCTIONS (Continued)LOW VOLTS ANNUNC

SECTION 3 CESSNAEMERGENCY PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS(Continued)IF LOW VOLTS ANNUNCIATOR

CESSNA SECTION 3MODEL 172R NAV III EMERGENCY PROCEDURES GFC 700 AFCSU.S.AIR DATA SYSTEM FAILURERED X - PFD AIRSPEED INDICATOR1. ADC/AHRS Circu

SECTION 3 CESSNAEMERGENCY PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.AUTOPILOT OR ELECTRIC TRIM FAILURE (if installed)AP OR PTRM ANNUNCIATOR(S) COME

CESSNA SECTION 3MODEL 172R NAV III EMERGENCY PROCEDURES GFC 700 AFCSU.S.DISPLAY COOLING ADVISORYPFD1 COOLING OR MFD1 COOLING ANNUNCIATOR(S)COM

CESSNA SECTION 1MODEL 172R NAV III GENERAL GFC 700 AFCSU.S.GENERALTABLE OF CONTENTSPageThree View - Normal Ground Attitude . . . . . . . . . .

SECTION 3 CESSNAEMERGENCY PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.HIGH CARBON MONOXIDE (CO) LEVEL ADVISORYCO LVL HIGH ANNUNCIATOR COMES ON1. CABI

CESSNA SECTION 3MODEL 172R NAV III EMERGENCY PROCEDURES GFC 700 AFCSU.S.AMPLIFIED EMERGENCY PROCEDURESThe following Amplified Emergency Proced

SECTION 3 CESSNAEMERGENCY PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.MAXIMUM GLIDEFigure 3-1172RPHBUS-003-26

CESSNA SECTION 3MODEL 172R NAV III EMERGENCY PROCEDURES GFC 700 AFCSU.S.FORCED LANDINGSIf all attempts to restart the engine fail and a forced

SECTION 3 CESSNAEMERGENCY PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.LANDING WITHOUT ELEVATOR CONTROLTrim for horizontal flight with an airspeed of

CESSNA SECTION 3MODEL 172R NAV III EMERGENCY PROCEDURES GFC 700 AFCSU.S.EMERGENCY OPERATION IN CLOUDS If the engine-driven vacuum pump fails i

SECTION 3 CESSNAEMERGENCY PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.EMERGENCY OPERATION IN CLOUDS (Continued)EMERGENCY DESCENT THROUGH CLOUDS (AHRS

CESSNA SECTION 3MODEL 172R NAV III EMERGENCY PROCEDURES GFC 700 AFCSU.S.EMERGENCY OPERATION IN CLOUDS (Continued)RECOVERY FROM SPIRAL DIVE IN

SECTION 3 CESSNAEMERGENCY PROCEDURES MODEL 172R NAV IIIGFC 700 AFCSU.S.STATIC SOURCE BLOCKEDIf erroneous readings of the static source instruments (ai

CESSNA SECTION 3MODEL 172R NAV III EMERGENCY PROCEDURES GFC 700 AFCSU.S.ROUGH ENGINE OPERATION OR LOSS OF POWERSPARK PLUG FOULINGA slight engi