Cessna 172SPHUSR05 Pilot Operating Handbook

Cessna 172SPHUSR05 Pilot Operating Handbook

Faa approved airplane flight manual
Table of Contents

Advertisement

Pilot's Operating Handbook
FAA Approved Airplane Flight Manual
THIS PUBLICATION MUST BE
CARRIED IN THE AIRPLANE
AT ALL TIMES.
This publication includes the material required to be furnished to the pilot by FAR Part
23
and constitutes the FAA Approved Airplane Flight Manual.
FAA APPROVAL
PAA APPROveo UNDER FAR 21 SUBPART J
Cessna
The
Date: July 10, 1998
i}
Member of GAMA
and
Aircraft Co
Executiv o Enginee r
The Cessna Aircraft
Company
Model 172S
Serial No.
Registration No.
COPYRIGHT©
The Cessna Aircraft Company
Wichita, Kansas USA
-
Original Issue
-.
Cessna
A Textron Company
1 72 S 927 1
N5308A
1998
8
1998
July

Advertisement

Table of Contents
loading

Summary of Contents for Cessna 172SPHUSR05

  • Page 1 FAA Approved Airplane Flight Manual. FAA APPROVAL PAA APPROveo UNDER FAR 21 SUBPART J Cessna Aircraft Co 1998 COPYRIGHT© Executiv o Enginee r The Cessna Aircraft Company Date: July 10, 1998 Wichita, Kansas USA Member of GAMA 1998 Original Issue July...
  • Page 2 THIS MANUAL WAS PROVIDED FOR THE AIRPLANE IDENTIFIED ON THE TITLE 12/12/02 PAGE SUBSEQUENT REVISIONS SUPPLIED BY CESSNA AIRCRAFT COMPANY MUST BE PROPERLY INSERTED. The Cessna Aircraft Company, Aircraft Division...
  • Page 3 REVISION 1728 MODEL PILOT'S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL REVISION 2004 JULY 172S H S INSERT THE FOLLOWING PAGES INTO THE PILOT'S OPERATING HANDBOOK...
  • Page 5 PUBLICATION PART NUMBER CESSNA MODEL 1 72S Pilot's Operating Handbook FAA Approved Airplane Flight Manual Serial Numbers 172S8001 and On 8 J ul y 1998 Original Issue 5 -19 2004 Revision July PART NUMBER: 1 72SPHUS05 i / ii Revi s i o n 5...
  • Page 7 CESSNA LOG OF EFFECTIVE PAGES MODEL 1 72S LOG OF EFFECTIVE PAGES The following Log of Effecti v e Pages provi d es the date of i s sue for original and revi s ed pages, as well as a li s ting of al l pages i n the POH.
  • Page 8: Table Of Contents

    LOG OF EFFECTIVE PAGES CESSNA MODEL 172S LOG OF EFFECTIVE PAGES (Continued) PAGE DATE PAGE 3-11 ... Revision 4 4-33 ..Revision 4 3-12 ... Revision 4 4-34 ..Revision 4 3-13 ... . July 8/98 Revision 4 4-35 ..
  • Page 9 LOG OF EFFECTIVE PAGES CESSNA MODEL 172S EFFECTIVE PAGES LOG OF (Continued) DATE DATE PAGE PAGE Dec 30/00 7-308 May 30/00 6-16 Dec 30/00 July 8/98 7-31 6-17 Revision 4 7-32 May 30/00 6-18 Revision 4 7-33 May 30/00 6-19...
  • Page 10 CESSNA LOG OF EFFECTIVE PAGES MODEL 172S LOG OF EFFECTIVE PAGES (Continued) DATE 8-20 ... Revision 4 8-21 ... May 30100 8-22 ... May 30100 8-23 ..Revision 4 8-24 ... Revision 4 9-1 /9-2 ..
  • Page 11: Revision

    MODEL 172S PILOT'S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL REVISION 1 2 AUGUST 2003 INSERT THE FOLLOWING PAGES INTO THE PILOT'S OPERATING HANDBOOK...
  • Page 13: Revision 4

    LIST OF TEMPORARY REVISIONS CESSNA MODEL 172R, 172R180, AND 172S PILOT1S OPERATING HANDBOOK FAA APPROVED AIRPLANE FLIGHT MANUAL 16 February 2004 172PHTR...
  • Page 14: Revision 4

    Pi l ot' s Operati n g Handbook and FAA Approved Ai r pl a ne Fli g ht Manual Cessna Model 172R, 172R180, and 172S The followi n g li s t of Temporary Revi s i o ns must be i n corporated i n to the Pilot' s Operating Handbook and FAA Approved Ai r plane Flight Manual unti l the removal i n structi o ns have been compli e d wi t h.
  • Page 15 LIST OF TEMPORARY REVISIONS CESSNA MODEL 172R, 172R180, 172S AIRPLANES NOT INCORPORATING THE NAV III AVIONICS OPTION (G1000) PILOT'S OPERATING HANDBOOK APPROVED AIRPLANE FLIGHT MANUAL 1 0 August 2005 172PHTR...
  • Page 16 Pi l o t's Operating Handbook and FAA Approved Ai r pl a ne Flight Manual Cessna Model 172R, 172R1S0, and 172S Ai r pl a nes not incorporating the Nav III Avi o ni c s Opti o n (G1 000).
  • Page 17: July

    PUBLICATION PART NUMBER CESSNA MODEL 1 72S Pilot's Operating Handbook FAA Approved Airplane Flight Manual Serial Numbers 172S8001 and On Original Issue... July 1998 2003 Revision August PART NUMBER: 1 72SPHUS04 Revision 4 i J ii...
  • Page 19 • Congratulations on your purchase and welcome to Cessna ownership! Your Cessna has been designed and constructed to give you the most in performance, value and comfort. This Pilot's Operating Handbook has been prepared as a guide to help you get the most utility from your airplane.
  • Page 20: Revision

    PERFORMANCE­ CESSNA SPECIFICATIONS MODEL 172S *SPEED: . . 1 26 KNOTS Maxi m um at Sea Level ..Cruise, 75% Power at 8500 FT ... 1 24 KNOTS...
  • Page 21 They are cal c ulated val u es deri v ed from flight tests conducted by The Cessna Ai r craft Company under careful l y documented condi t i o ns and will vary wi t h indi v i d ual ai r planes and numerous factors affecting flight performance.
  • Page 22: July

    The Pi l ot's Operating Handbook in the ai r plane at the time of deli v ery from The Cessna Ai r craft Company contains information appli c able to the Model 172S ai r plane by serial number and regi s tration number shown on the Ti t le Page.
  • Page 23: Revision 4

    It is the responsibility of the owner to maintain this handbook i n a ,current status when it is being used for operational purposes. Owners should contact the i r local Cessna Service Station whenever the revision status of their handbook is in q uestion.
  • Page 24: Revision 4

    COVERAGE/REVISIONS CESSNA MODEL 172S IDENTIFYING REVISED MATERIAL Add itions or revisions to the text in an existing section will be identified by a vertical l ine (revision bar) adjacent to the applicable revised area on the outer margin of the page.
  • Page 25: Revision 4

    CESSNA CONTENTS MODEL 1 72S SECTION GENERAL ......LIMITATIONS EMERGENCY PROCEDURES ....NORMAL PROCEDURES ....PERFORMANCE WEIGHT & BALANCE/EQUIPMENT LIST AIRPLANE &...
  • Page 27 CESSNA SECTION 1 MODEL 1 72S GENERAL Page CONTENTS Three View - Normal Ground Atti t ude 1 -2 Introducti o n ....
  • Page 28 SECTION 1 CESSNA GENERAL MODEL 1 72S 76" MAX 0510T1005 051 OT1 005 Figure 1 -1 . Three Vi e w - Normal Ground Atti t ude (Sheet 1 of 2) 1 -2 Revision 4...
  • Page 29 SECTION 1 CESSNA GENERAL MODEL 1 72S NOTE WING SPAN SHOWN WITH STROBE LIGHTS INSTALLED. NOTE WHEEL BASE LENGTH IS 65". NOTE PROPELLER GROUND CLEARANCE IS 1 1 1/4". NOTE WING AREA I S 1 74 SQUARE FEET. NOTE 5: MINIMUM TURNING RADIUS (* PIVOT POINT TO OUTBOARD WING TIP) IS 27'-5 1/2".
  • Page 30: D Escriptive Data

    FAR Part 23. It al s o contai n s Isupplemental data supplied by Cessna Aircraft Company. Section 1 provi d es basi c data and informati o n of general interest.
  • Page 31: Oil

    SECTION 1 CESSNA MODEL 1 72S GENERAL NOTE Isopropyl al c ohol or diethyl e ne glycol mono methyl ether (DiEGME) may be added to the fuel supply. Addi t i v e concentrati o ns shall not exceed 1 % for i s opropyl al c ohol or 0.1 0% to 0.1 5% for DiEGME.
  • Page 32: Maximum Certificated Weights

    SECTION 1 CESSNA MODEL 1 72S GENERAL Recommended Vi s cosi t y for Temperature Range: MIL-L-6082 MIL-L-22851 or SAE Temperature J1 899 SAE J1 966 Ashl e ss Di s persant Strai g ht SAE Grade Mineral Oil SAE Grade Above 2rC (80°F)
  • Page 33: Standard Airplane Weights

    SECTION 1 CESSNA MODEL 1 72S GENERAL Weight in Baggage Compartment, Normal Category: Baggage Area 1 (Station 82 to 1 08): 1 20 Ibs. See note bel o w. Baggage Area 2 (Stati o n 1 08 to 1 42): 50 Ibs. See note bel o w.
  • Page 34: Symbols, Ab B Reviations A N D Terminology

    SECTION 1 CESSNA GENERAL MODEL 1 72S SYMBOLS, AB B REVIATIONS A N D TERMINOLOGY GENERAL AIRSPEED TERMINOLOGY AND SYMBOLS KCAS i s indicated airspeed Knots Calibrated Airspeed corrected for posi t i o n and instrument error and expressed i n knots. Knots calibrated airspeed i s equal to KT AS in standard atmosphere at sea level.
  • Page 35: Meteorologi C Al Terminol O Gy

    SECTION 1 CESSNA MODEL 1 72S GENERAL METEOROLOGICAL TERMINOLOGY i s the free ai r static Outside Air Temperature temperature. It may be expressed in ei t her degrees Celsius or degrees Fahrenhei t . Standard is 1 5°C at sea level...
  • Page 36: Engine Power Terminology

    SECTION 1 CESSNA GENERAL MODEL 1 72S (Conti n ued) E NGINE POWER TERMINOLOGY Full Throttle full forward (pushed in, full control travel, toward the panel) Al s o known as "full open" throttle. Throttle Closed Throttl e full aft (pulled out, full control travel, away Throttle from the panel).
  • Page 37: Weight And Bal A Nce Terminol O

    CESSNA SECTION 1 MODEL 1 72S GENERAL WEIGHT ANP BALANCE TERMINOLOGY Reference Reference Datum is an imaginary vertical plane from Datum which all horizontal distances are measured for balance purposes. Station Station is a location along the airplane fuselage given in terms of the distance from the reference datum .
  • Page 38 SECTION 1 CESSNA GENERAL MODEL 172S Maximum Ramp Weight Maximum is the maximum weight Ramp approved for ground maneuver, and includes the Weight weight of fuel used for start, taxi and runup. Maximum Maximum Takeoff Weight is the maximum weight Takeoff approved for the start of the takeoff roll.
  • Page 39: Metri C Imperial U.s. Conversion Charts

    CES S NA S ECTIO N 1 M O D E L 1 72S G E N E RAL METRIC / IMPERIAL / U.S. CONVERSION CHARTS The fol lowing charts have been provided to help i nternational operators convert U.S. measurement supplied with the Pilot's Operating Handbook i nto metric and imperial measurements.
  • Page 40: Weight Conversions

    SECTION 1 CESSNA GENE RAL MODEL 1 72S (Kilograms x 2.205 (Pounds x .454 Pounds) Kilograms) KILOGRAMS INTO POUNDS KILOGRAMMES EN LIVRES 2.205 4.409 6.614 8.81 9 1'.023 13.228 1 5.432 17.637 19.842 22.046 24.251 26.456 28.660 30.865 33.069 35.274 37.479...
  • Page 41 SECTION 1 CESSNA GENERAL MODEL 172S (Pounds .454 Kilograms) (Kilograms 2.205 Pounds) POUNDS KILOGRAMS 21 0 1 90 1 80 1 70 1 60 1 50 1 40 1 20 1 10 Units 1 0, 1 00, etc. Figure 1 -2 . Wei g ht Conversi o ns (Sheet 2)
  • Page 42 CESSNA SECTION 1 MODEL 172S GENERAL (Meters 3.281 Feet) (Feet . 3 05 Meters) METERS INTO F E ET METRES EN PIEDS feet feet feet feet feet feet feet feet feet feet - - - 3.281 6.562 9.842 13.123 16.404 19.685 22.956 26.247...
  • Page 43 SECTION 1 CESSNA GENERAL MODEL 172S (Feet .305 Meters) (Meters 3.281 Feet) FEET METERS 1 00 1 80 1 60 1 40 1 20 1 00 Uni t s 1 0, 1 00, etc. Fi g ure 1 -3 . Length Conversions (Sheet 2)
  • Page 44 CESSNA SECTION 1 MODEL 172S GENERAL Inches) (Inches 2.54 Centimeters) (Centimeters .394 CENTIMETERS INTO INCHES CENTIMETRES EN POUCES in . in . - - - 1.181 1.575 1.969 2.362 2.756 3.150 3.543 0.394 0.787 6.299 6.693 7.087 7.480 4.331 4.724 5.118...
  • Page 45: Length Conversi O Ns

    SECTION 1 CESSNA GENERAL MODEL 172S (Inches 2.54 Centimeters) (Centimeters .394 Inches) INCHES CENTIMETERS 1 2' Uni t s 1 0, 1 00, etc. 0585T1028 Fi g ure 1 -4. Length Conversi o ns (Sheet 2 1-1 9 Revi s ion 4...
  • Page 46: Di S Tance Conversi O Ns

    CESSNA SECTION 1 MODEL 172S GENERAL (Statute Miles x1 .609�Kilometers) (Kilometers x.622�Statute Miles) (Statute Miles x.869=Nautical Miles) (Nautical Miles x1 .1 5=Statute Miles) (Nautical Miles x1 .852=Kilometers) (Kilometers x.54=Nautical Miles) NAUTICAL STATUTE MILES KILOMETERS MILES 1 15 1 00 1 00...
  • Page 47: Volume Conversions

    CESSNA SECTION 1 MODEL 172S GENERAL (Imperial Gallons 4.546 Liters) ..- (Liters Imperial Gallons) ..-LlTERS INTO IMPERIAL GALLONS LlTRES EN GALLONS IMPERIAL - - - 0.220 0.440 0.880 1.100 1.540 0.660 1.320 1.760 1.980 2.200 2.420 2.640 2.860 3.080 3.300 3.520...
  • Page 48 CESSNA SECTION 1 MODEL 172S GENERAL (Imperial Gallons 4.4546 Litres) (LUres Imperial Gallons) 1 00 LITERS IMPERIAL GALLONS Units 10, 100, etc. 0585T1032 Figure 1-6. Volume Conversions (Sheet 2 of 3) July 8/98 1-22...
  • Page 49 SECTION 1 CESSNA GENERAL MODEL 172S (Imperial Gallons 1 .2 U.S. Gallons) (U.S. Gallons .833 Imperial Gallons) (U .S. Gallons 3.785 Liters) ... (Liters .264 U.S. Gallons) ..U . S. IMPERIAL LITERS GALLONS GALLONS 1 00 1 20...
  • Page 50: Temperature Conversi O Ns

    S ECTION 1 CESS NA G EN E RAL MODEL 112S TEM P ERATUR E CONVERSIONS x 5/9 ::: ° C e x 9/5 F-32 32 ::: ° F ° c ° c 1 60 ·30 1 80 ·20 - 1 0 -1 0 1 00 1 1 0...
  • Page 51 S: O o C/) < m C/) w" 0" � --L » � """-.I I\.) » "'Tl cO" » §! m r C/) !:: C/) OJ c � » HECTOPASCAlS (MILLIBARS) :O m 9811 99t! 1000 1004 1008 1012 1015 102C 1024 1028...
  • Page 52 CESSNA SECTION 1 MODEL 1 72S GENERAL AVGAS Speci f i c Gravi t y (Li t ers X .72 Kilograms) - (Kilograms X 1 .389 Liters) (Li t ers X 1 .58 Pounds) - (Pounds X .633 Liters) LI T ERS POUNDS...
  • Page 53 CESSNA SECTION 1 MODEL 1 72S GENERAL AV GAS SPECIFIC GRAVI T Y 0.72 GALLONS Fi g ure 1 -1 0. Quick Conversions Revi s i o n 4 1 -27/1 -281...
  • Page 55 CESSNA SECTION 2 LIMI T ATIONS MODEL 1 72S SECTI N 2 LIMITATI NS Page TABLE O F CONTENTS Introducti o n ........
  • Page 57: Secti N

    CESSNA SECTION 2 MODEL 1 72S LIM ITATIONS INTRODUCTION Section 2 incl udes operating l imitations, instrument markings, and basic placards necessary for the safe operation of the airplane, engine, standard systems standard equipment. l i mitations i ncl uded in this section and in Section 9 have been approved by the Federal Aviation Administration .
  • Page 58: Airspeed Limitat Ions

    SECTION 2 C ESSNA LIMITATIONS MODEL 1725 AIRSPEED LIMITAT IONS Airspeed l i mitations and their operational significance are shown in Figu re 2-1. Maneuvering speeds shown apply to normal category operations. The uti lity category maneuvering speed is KIAS at 2200 pounds.
  • Page 59: Airspeed Indicator Markings

    SECTION 2 CESSNA MODEL 1 72S LIMITATIONS AI RSP E E D I N DI CATOR MAR KINGS Airspeed i n dicator markings and their color code significance are shown i n Fi g ure 2-2. KIAS MARKING VALUE SIGNIFICANCE OR RANGE 40 - 85 Full Fl a p Operating Range.
  • Page 60: Powerplant Instrument Marki N Gs

    SECTION 2 CESSNA LIMITATIONS MODEL 1 72S Fuel Grade: See Fuel Limi t ati o ns. Oil Grade (Speci f i c ati o n): MIL-L-6082 or SAE J1 966 Aviati o n Grade Strai g ht Mineral Oil MIL-L-22851 or SAE J1 899 Ashless Di s persant Oil. Oil must compl y wi t h the latest revi s i o n and/or supplement for Textron Lycoming Servi c e Instructi o n No.
  • Page 61: Weight Limits

    CESSNA SECTION 2 MODEL 1 72S LI MITATIONS 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 1 08 : 1 20 Ibs.
  • Page 62: Utility Category

    SECTION 2 CESSNA LI MITATIONS MODEL 172S UTILITY CATEGORY Center of Gravity Range: 35.0 inches aft of datum at 1 950 Ibs. or less, with Forward: straight line variation to 37.5 inches aft of datum at 2200 1bs. Aft: 40.5 inches aft of datum at all weights.
  • Page 63: Utility Category

    CESSNA SECTION 2 MODEL 1 72S LIMITATIONS UTILITY CATEGORY Thi s airpl a ne i s not designed for purel y aerobatic flight. However, in the acquisi t i o n of vari o us certi f icates such as commerci a l pilot and flight instructor, certai n maneuvers are required by the FAA.
  • Page 64: Flight Load Factor Limits

    SECTION 2 CESSNA LIMITATIONS MODEL 1 72S FLIGHT LOAD FACTOR LIMITS NORMA L CATEGORY Flight Load Factors (Maximum Takeoff Weight - 2550 Ibs.): *Flaps Up ..... . . +3.8g, -1 .52g *Flaps Down .
  • Page 65: Fuel Limitations

    SECTION 2 CESSNA MODEL 172S LIMITATIONS FUEL LIMITATIONS Total Fuel: 56 U.S. gallons (2 tanks at 28.0 gallons each). Usabl e Fuel (all flight condi t i o ns): 53.0 U.S. gallons. Unusabl e Fuel: 3.0 U.S. gallons (1 .5 gallons each tank).
  • Page 66: Placards

    SECTION 2 CESSNA LIMI T ATIONS MODEL 1 72S PLACAR DS The foll o wing informati o n must be di s played i n the form of compos­ i t e or indi v i d ual placards. 1 . In full vi e w of the pil o t: (The "DAY-NIGHT-VFR-IFR" entry, shown on the exampl e below, will vary as the ai r pl a ne i s equipped).
  • Page 67 CESSNA SECTION 2 MODEL 1 72S LIMITATIONS 2. On the fuel selector val v e: TAKEOFF BOTH ALL FLIGHT LANDING 53.0 GAL. ATTITUDES FUEL SELECTOR LEFT RIGHT 26.5 GAL. 26.5 GAL. LEVEL LEVEL FLIGHT FLIGHT ONLY ONLY 3. Near fuel tank filler cap: FUEL 1 00LU1 00 MIN.
  • Page 68 CESSNA SECTION 2 LIMI T ATIONS MODEL 1 72S In baggage compartment: 1 20 POUNDS MAXIMUM BAGGAGE FORWARD OF BAGGAGE DOOR LATCH 50 POUNDS MAXIMUM BAGGAGE AFT OF BAGGAGE DOOR LATCH MAXIMUM 1 20 POUNDS COMBINED FOR ADDITIONAL LOADING INSTRUCTIONS...
  • Page 69 CESSNA SECTION 2 MODEL 1 72S LIMI T ATIONS 1 0. On the Upper Right Si d e of the Aft Cabin Parti t i o n: EMERGENCY LOCATOR TRANSMITTER INSTALLED AFT OF THIS PARTITION MUST BE SERVICED IN ACCORDANCE WITH FAR PART 91 .207...
  • Page 71 CESSNA SECTION 3 MODEL 1 72S EMERGENCY PROCEDURES SECTI N 3 E MERG ENCY P R C E O RES Page TABLE O F CONTENTS Introducti o n AIRSPEEDS Airspeeds For Emergency Operation ....3-3 E M E RG ENCY PROCEDU R ES CHECKLIST Engine Failures .
  • Page 72 SECTION 3 CESSNA EMERGENCY PROCEDURES MODEL 1 72S (Conti nued) Page El e ctri c al Power Suppl y System Mal f uncti o ns ... 3-1 1 Ammeter Shows Excessi v e Rate of Charge (Full Scal e Defl e cti o n) .
  • Page 73: Airspeeds For Emergency Operation

    CESSNA SECTION 3 MODEL 1 72S EMERGENCY PROCEDURES INTROD UCTION Section 3 provi d es checkli s t and ampli f i e d procedures for copi n g wi t h emergencies that may occur. Emergenci e s caused by airpl a ne or engi n e mal f unctions are extremely rare if proper prefl i ght inspecti o ns and maintenance are practi c ed.
  • Page 74: Engine Failure During Takeoff Roll

    SECTION 3 CESSNA EMERGENCY PROCEDURES MODEL 1 72S Procedures in the Emergency Procedures Checkl i s t porti o n of this section shown i n type are immediate acti o n i t ems ' which should be commi t ted to memory.
  • Page 75: Engine Failure Duri N G Flight (Restart Procedures)

    CESSNA SECTION 3 MODEL 1 72S EMERGENCY PROCEDURES E N G I N E FAI L U R E D U R ING FLIGHT (Restart Procedu res) Airspeed -- KIAS. Fuel Shutoff Valve -- O N (push ful l i n).
  • Page 76: P Recautionary Landing With Engin E Power

    SECTION 3 CESSNA EMERGENCY PROCEDURES MODEL 1 72S P RECAUTIONARY LANDING WITH ENGIN E POWER Passenger Seat Backs -- MOST UPRIGHT POSITION. 2. Seats and Seat Bel t s ,. - SECURE. 3. Ai r speed -- 65 KIAS. Wi n g Flaps -- 20°.
  • Page 77: Fires

    CESSNA SECTION 3 MODEL 1 72S EMERGENCY PROCEDURES FIR ES D U RING START O N G R O U N D to get a start. whi c h would suck the fl a mes and accumulated fuel into the Ignition Switch -- START, Continue Cranking engine.
  • Page 78: Electri C Al Fire I N Flight

    SECTION 3 CESSNA EMERGENCY PROCEDURES MODEL 1 72S E LECTRICAL F I R E IN FLIGHT Master Switch -- OFF. Vents, Cabi n Air, Heat -- C LOSED. Avionics Master Swi t ch -'- OFF. Fire Exti nguisher -- ACTIVATE.
  • Page 79: Wing Fire

    SECTION 3 CESSNA MODEL 1 72S EMERGENCY PROCEDURES WING FIRE Landi n g/Taxi Light Switches OFF. Navigation Light Switch OFF. Strobe Light Switch OFF. Pitot Heat Switch O FF. NOTE Perform a si d eslip to keep the fl a mes away from the fuel tank and cabin.
  • Page 80: Static Source B Lockag E

    SECTION 3 CESSNA EMERGENCY PROCEDURES MODEL 172S 1 0. Approach at 65 to 75 KI A S dependi n g upon the amount of the accumulati o n. 1 1 . Perform a landing in level atti t ude. STATIC SOURCE B LOCKAG E ( Erroneous I nstrument Readi ng Suspected) 2.
  • Page 81: El E Ctri C Al Power Suppl Y System Mal F Uncti O

    CESSNA SECTION 3 MODEL 1 72S EMERGENCY PROCEDURES ELECTRICAL POWE R S U P PLY SYSTE M MALF U NCTIONS A M M ETER SHOWS EXCESSIVE RATE O F CHARGE (Fu l l Scale Deflection) 1 . Al t ernator -- OFF.
  • Page 82: Vacuum System Failure

    SECTION 3 CESSNA EMERGENCY PROCEDURES MODEL 1 72S VAC U U M SYSTE M FAILU R E Left Vacuum (L VAC) Annunciator or Right Vacuum (VAC R) Annunciator Illuminates. CAUTION VAC U U M WITHIN NORMAL OPERATING LIMITS, FAI L U R E...
  • Page 83: Amplifi E D Emerge Ncy Proc E D U R Es

    CESSNA SECTION 3 MODEL 1 72S EMERGENCY PROCEDURES AMPLIFIED E M R ENCY P R CEDU RES The foll o wing Amplified Emergency Procedures el a borate upon information contained in the Emergency Procedures Checkl i s ts porti o n of this section. These procedures al s o include informati o n...
  • Page 84 CESSNA SECTION 3 MODEL 1 72S EMERGENCY PROCEDURES After an engine failure in fli g ht, the most important course of acti o n is to continue fl y ing the airplane. Best gli d e speed as shown i n Fi g ure 3-1 should be established as quickl y as possible. While gli d ing toward a sui t abl e l a ndi n g area, an effort shoul d be made to identi f y the cause of the failure.
  • Page 85: Forced Landi N Gs

    CESSNA SECTION 3 EMERGENCY PROCEDURES MODEL 1 72S FORC E D LANDINGS If all attempts to restart the engi n e fail and a forced landing i s imminent, sel e ct a sui t able fi e l d and prepare for the l a nding as di s cussed under the Emergency Landi n g Wi t hout Engine Power checkl i s t.
  • Page 86: Fires

    SECTION 3 CESSNA EMERGENCY PROCEDURES MODEL 1 72S At the l a nding fl a re (round-out), the nose down moment resul t i n g from power reduction i s an adverse factor and the ai r pl a ne may land on the nose wheel.
  • Page 87: Emergency Descent Through Clouds

    CESSNA SECTION 3 MODEL 172S EMERGENCY PROCEDURES 3. Check accuracy of the turn by observing the compass heading whi c h shoul d be the reciprocal of the original heading. If necessary, adjust heading primarily wi t h ski d ding moti o ns rather than rolling moti o ns so that the compass wi l l read more accuratel y .
  • Page 88: Recovery From Spi R Al Di V E I N The Clouds

    SECTION 3 CESSNA EMERGENCY PROCEDURES MODEL 1 72S R ECOVERY FROM SPIRAL DIVE IN T H E C LO U DS If a spi r al is encountered in the cl o uds, proceed as follows: Retard throttle to i d l e posi t ion.
  • Page 89: Spins

    SECTION 3 CESSNA MODEL 1 72S EMERGENCY PROCEDURES When using the al t ernate stati c source, refer to the Al t ernate Stati c Source Ai r speed Cal i bration table i n Secti o n 5, Performance, for addi t i o nal information.
  • Page 90: Rough Engi N E Operati O N Or Loss Of Power

    CESSNA SECTION 3 EMERGENCY PROCEDURES MODEL 1 72S ROUGH E NG I N E OP E RATION O R LOSS O F POWER SPARK PLUG FOU LI N G A slight engine roughness in fli g ht may be caused by one or more spark pl u gs becoming fouled by carbon or lead deposi t s.
  • Page 91 Temporary Revision for Cessna Pilot' s Operating Handbook and FAA Approved Airplane Flight Manual Publi c ation Affected: Model 1 72R (172RPHU809), 172R180 (172R180PHU803), 1728 (1728PHU805) Pilot' s Operati n g Handbook and FAA Approved Ai r pl a ne Flight Manual.
  • Page 92 Temporary Revision for Cessna Pilofs Operating Handbook and FAA Approved Ai r pl a ne Flight Manual APPROVE D BY DATE O F APPROVAL 1 72PHTR02...
  • Page 93: Excessi V E Fuel Vapor Indi C Ati O Ns

    SECTION 3 CESSNA MODEL 1 72S EMERGENCY PROCEDURES EXCESSIVE F U E L VAPOR I N DI CATIONS Excessi v e fuel vapor is most li k el y to be generated during ground operations when operati n g at hi g her al t i t udes, in unusually warm temperatures or wi t h more volati l e fuel bl e nds.
  • Page 94: Elect Rical Powe R S Upply Syste M Malfunctions

    SECTION 3 CESSNA EMERGENCY PROCEDURES MODEL 1 72S ELECT RICAL POWE R S UPPLY SYSTE M MALFUNCTIONS Mal f uncti o ns in the el e ctri c al power suppl y system can be detected by peri o di c moni t ori n g of the ammeter and low vol t age lannunciator (VOLTS);...
  • Page 95: Insuffi C I E Nt Rate Of Charge

    CESSNA SECTION 3 MODEL 1 72S EMERGENCY PROCEDURES I NSU FFICI E NT RATE O F CHARGE NOTE The low vol t age annunci a tor (VOLTS) may come on and • ammeter di s charge i n dications may occur during l o w RPM condi t i o ns wi t h an el e ctri c al l o ad on the system, such as during a low RPM taxi.
  • Page 97 SECTION 4 CESSNA NORMAL PROCEDURES MODEL 1 72S S E CTI C E O U RES Page TABLE CONTENTS Introducti o n AIRSPEEDS Ai r speeds For Normal Operation CHECKLIST PROC E D UR ES Preflight Inspecti o n Cabin...
  • Page 99 CESSNA SECTION 4 MODEL 1 72S NORMAL PROCEDURES TABLE OF CONTENTS (Conti nued) Page Landing 4-33 Normal Landing 4-33 Short Fi e l d Landing 4-33 Crosswind Landing 4-34 Balked Landing 4-34 Col d Weather Operati o n 4-34 Winteri z ati o n Ki t...
  • Page 101 SECTION 4 CESSNA MODEL 1 72S NORMAL PROCEDURES I N TROD UCTION Section 4 provi d es checkli s t and ampli f i e d procedures for the conduct of normal operati o n. Normal procedures associ a ted wi t h opti o nal systems can be found in the Supplements, Secti o n 9.
  • Page 102: Preflight Inspecti O N

    SECTION CESSNA NORMAL PROCEDURES MODEL 1 72S NOTE Visually check airpl a ne for general condi t i o n during wal k ­ around inspecti o n. Ai r pl a ne shoul d be parked in a normal ground atti t ude (refer to Fi g ure 1 -1 ) to ensure that fuel drain val v es all o w for accurate sampling.
  • Page 103: Cabin

    CESSNA SECTION 4 NORMAL PROCEDURES MODEL 1 72S CH ECKLIST PROCEDU R ES I NSPECTIO N CABI N 1 . Pi t ot Tube Cover -- REMOVE. Check for pi t ot bl o ckage. 2. Pi l ot' s Operating Handbook -- AVAILABLE IN THE AIRPLANE.
  • Page 104: Empennage

    SECTION 4 CESSNA NORMAL PROCEDURES MODEL 1 72S 1 5. Annunci a tor Panel Test Swi t ch -- RELEASE. Check that ap­ propri a te annunci a tors remain on. N OT E When Master Swi t ch i s turned ON, some annunci a tors wi l l flash for approximatel y 10 seconds before illuminating steadil y .
  • Page 105: Nose

    CESSNA SECTION 4 MODEL 1 72S NORMAL PROCEDURES 2. Main Wheel Tire -- CHECK for proper infl a ti o n and general condi t i o n (weather checks, tread depth and wear, etc ... ). 3. Fuel Tank Sump Qui c k Drain Val v es -- DRAIN at l e ast a...
  • Page 106: @ Left Wing

    SECTION CESSNA NORMAL PROCEDURES MODEL 1728 2. Engine Oil Di p sti c k/Filler Cap -- CHECK oil level, then check di p sti c k/filler cap SECURE. Fill to eight quarts for extended flight. Do not operate with less t han 3.
  • Page 107: Left Wing, Leading Edge

    SECTION 4 CESSNA MODEL 172S NORMAL PROCEDURES LEFT WING Leadi ng Edge 1 . Fuel Tank Vent Opening -- CHECK for bl o ckage. 2. Stall Warning Opening -- CHECK for bl o ckage. To check the system, place a clean handkerchief over the vent opening and appl y sucti o n;...
  • Page 108: Starting Engine (With Battery)

    SECTION CESSNA NORMAL PROCEDURES MODEL 1728 STARTING ENGINE (With Battery) 1 . Throttle -- OPEN 1/4 INCH. 2. Mi x ture -- IDLE CUTOFF. 3. Propeller Area -- CLEAR. Master Swi t ch -- ON. 5. Flashing Beacon -- ON.
  • Page 109 Tem po rary Revision for Cessna Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Publication Affected : Model 1 72R, 1 72R 1 80, and 1 72S Pilot's Operating Handbook and FAA Approved Airplane Flight Manual. incorporating Serial Numbers Affected : Airplanes SB04-24-01 .
  • Page 110 Temporary Revi s i o n for Cessna Pilot' s Operating Handbook and FAA Approved Ai r pl a ne Fli g ht Manual (Conti n ued) STARTI N G E N G I N E NOTE I f engi n e fl o ods (engi n e has been primed too much),...
  • Page 111 CESSNA SECTION 4 NORMAL PROCEDURES MODEL 1 72S E N GI N E (With External Power) 1 . Throttle -- OPEN 114 INCH. 2. Mixture -- IDLE CUTOFF. 3. Propell e r Area -- CLEAR. 4. Master Swi t ch -- OFF.
  • Page 112 SECTION 4 CESSNA NORMAL PROCEDURES MODEL 1 728 b. Taxi and Landing Li g ht Swi t ches -- ON. (to provi d e an ini t i a l electri c al load on the system). c. Engine RPM -- REDUCE to idle.
  • Page 113: Before Takeoff

    CESSNA SECTION NORMAL PROCEDURES MODEL 1 72S B EFOR E TAKEOFF Parking Brake -- SET. Passenger Seat Backs -- MOST UPRIGHT POSITION. Seats and Seat Bel t s -- CHECK SECURE. Cabi n Doors -- CLOSED and LOCKED. Flight Control s -- FREE and CORRECT.
  • Page 114: Short Fi Eld Takeoff

    SECTION CESSNA NORMAL PROCEDURES MODEL 1 72S SHORT FI ELD TAKEOFF Wing Fl a ps Brakes -- APPLY. -- 1 0°. Throttle -- FULL OPEN. Mi x ture -- RICH (above feet, LEAN to obtai n maximum RPM). 3000 Brakes -- RELEASE.
  • Page 115: Landing

    SECTION CESSNA MODEL NORMAL PROCEDURES 1 72S LAN DING NORMAL LAN DING Airspeed KIAS (fl a ps UP). Wing Flaps -- AS DESIRED below KI A S, -- 65-75 bel o w 85 KIAS). (0°- 1 0° 1 1 0 1 0°-30°...
  • Page 116 SECTION CESSNA NORMAL PROCEDURES MODEL 1 72S AMPL I FI E D PROC ED U R ES PREFLIGHT INSPECTION The Preflight Inspecti o n, descri b ed in Fi g ure and adjacent checkli s t, is required pri o r to each flight. If the ai r pl a ne has been in...
  • Page 117 SECTION CESSNA MODEL 1 72S NORMAL PROCEDURES If the airpl a ne has been operated from muddy fi e l d s or in snow or slush, check the main and nose gear wheel fairi n gs for obstructi o ns and cl e anliness.
  • Page 118 CESSNA SECTION 4 NORMAL PROCEDURES MODEL 1 72S Should the engine tend to die after starting, turn on the auxiliary fuel pump temporaril y and adjust the throttle and/or mi x ture as necessary to keep the engine running. I n the event of over priming or fl o oding, turn off the auxiliary fuel pump, open the throttle from 1/2 to full open, and continue cranki n g wi t h the mi x ture full lean.
  • Page 119 CESSNA SECTION MODEL NORMAL PROCEDURES 1 72S L EANING FOR G RO UN D OPE RATIONS For all ground operati o ns, after starting the engine and when the engi n e is running smoothl y : a . set the throttle to RPM.
  • Page 120 SECTION 4 CESSNA NORMAL PROCEDURES MODEL 172S CODE WIN D D I RECTION Strong quartering tail winds require cauti o n. NOTE Avoi d sudden bursts of the throttle and sharp braking when the ai r pl a ne i s i n this si t uati o n.
  • Page 121 CESSNA SECTION MODEL 1 72S NORMAL PROCEDURES BEFORE TAKEOFF WAR M U P If the engi n e i d les (approximatley RPM) and accelerates smoothly, the airplane i s ready for takeoff. Since the engine i s cl o sely cowl e d for effi c i e nt in-flight engine cooling, precauti o ns should be taken to avoid overheating duri n g prolonged engine operati o n on the ground.
  • Page 122 SECTION CESSNA NORMAL PROCEDURES MODEL 1 72S LAN DING LIGHTS If landing li g hts are to be used to enhance the vi s ibili t y of the airpl a ne in the traffi c pattern or enroute, i t i s recommended that onl y the taxi li g ht be used.
  • Page 123 CESSNA SECTION MODEL 1 72S NORMAL PROCEDURES WING F LAP SETTINGS Normal takeoffs are accomplished wi t h wi n g fl a ps 0°-1 0°. Using 1 0° wing fl a ps reduces the ground roll and total di s tance over an obstacl e by approximately 1 0 percent.
  • Page 124 SECTION 4 CESSNA NORMAL PROCEDURES MODEL 1 72S C RUISE Normal crui s e is performed between 45% and 75% power. The engi n e RPM and corresponding fuel consumption for vari o us al t i t udes can be determined by using the data in Secti o n 5.
  • Page 125 SECTION 4 CESSNA NORMAL PROCEDURES MODEL 1 72S 750/ 0 POWER POWER POWER KTAS NMPG KTAS NMPG KTAS NMPG ALTITU D E 1 2.0 1 01 1 2.8 Sea Level 1 14 1 1 .2 1 08 4000 feet 1 1 9 1 1 .7 1 12 1 2.4...
  • Page 126 SECTION 4 CESSNA MODEL 1 72S NORMAL PROCEDURES NOTE The EGT indicator requires several seconds to respond to mi x ture adjustments and changes in exhaust gas temperature. More rapi d changes in EGT indication are nei t her necessary nor desi r able.
  • Page 127 CESSNA SECTION NORMAL PROCEDURES MODEL 1 72S F U EL VAPOR PROC E D UR ES The engine fuel system can become susceptible to fuel vapor formation on the ground during warm weather. Thi s wi" generall y occur when the outside ambient air temperature i s above .
  • Page 128 Cessna 1 72S.
  • Page 129 CESSNA SECTION 4 MODEL 1 72S NORMAL PROCEDURES The normal entry is made from a power off stall. As the stall is approached, the el e vator control shoul d be smoothly pulled to the full aft posi t ion. Just prior to reaching the stall "break", rudder...
  • Page 130 SECTION 4 CESSNA NORMAL PROCEDURES MODEL 1 72S NOTE If di s orientation precludes a visual determinati o n of the direction of rotation, the symboli c airpl a ne in the turn coordinator may be referred to for thi s informati o n.
  • Page 131: Crosswind Landing

    CESSNA SECTION NORMAL PROCEDURES MODEL 1 72S SHORT FIELD LANDING For a short fi e l d landing i n smooth air condi t i o ns, make an approach at 61 KIAS wi t h flaps using enough power to control the gli d e path.
  • Page 132 SECTION 4 CESSNA MODEL 1 72S NORMAL PROCEDURES Speci a l consi d erati o n shoul d be gi v en to the operati o n of the airpl a ne fuel system duri n g the wi n ter season or pri o r to any flight in col d temperatures.
  • Page 133: Winterization Kit

    SECTION CESSNA MODEL 1 72S NORMAL PROCEDURES When using an external power source, the master swi t ch must be in the OFF posi t ion before connecti n g the external power source to the airplane receptacle. See Section Ground Servi c e Plug Recepta­...
  • Page 134: Noise Characteristics And Noise Re D Uction

    SECTION 4 CESSNA NORMAL PROCEDURES MODEL 1 72S Refer to the general warm temperature starti n g informati o n under Starti n g Engine in this secti o n. Avoi d prol o nged engine operation on the ground.
  • Page 135 CESSNA SECTION MODEL PERFORMANCE 1 72S TABL E O F CONTENTS Page Introduction ........Use of Performance Charts ......Sample Problem ......... Takeoff Cruise ........Fuel Required ......... Landing ........Demonstrated Operating Temperature ....Figure Airspeed Calibration - Normal Static Source 5- 1 , Airspeed Calibration - Alternate Static Source ..
  • Page 137: Introduction

    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 138 CESSNA SECTION 5 PERFORMANCE MODEL 172S CRUISE CONDITIONS: 360 Nautical Miles Total distance Pressure altitude 7500 Feet 16°C (16°C Above Standard) Temperature 10 Knot Headwind Expected wind enroute LANDING CONDITIONS: Field pressure altitude 2000 Feet Temperature 25°C 3000 Feet Field length...
  • Page 139: Cruise

    CESSNA SECTION 5 MODEL 1 72S P ERFORMANCE Total d istance t o clear a 50-foot obstacle, zero wi nd 2 1 90 Decrease in total d istance 2 1 90 feet X 1 3% - 285 Corrected total d istance...
  • Page 140: Fuel Required

    S ECTION 5 C ESSNA P ERFORMAN C E MODEL 1 72S F U E L R E QU I RE D The total fuel requ irement for the flight may be esti mated using the performance i nformation i n Figu re 5-7 and Figu re 5-8. For this sample problem, Figu re 5-7 s hows that a cli m b from 2000 feet to 8000 feet requ i res 2 .2 gallons of fue l .
  • Page 141 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: - 10 107 Knot Therefore, the time required for the cruise portion of the trip is: 342 Na uti ca l Mi les 3.
  • Page 142: Landing

    SECTION 5 CESSNA PERFORMANCE MODEL 172S LANDING A procedure similar to takeoff should be used for estimating the landing distance at the destination airport. Figure 5-11 presents landing distance information for the short field technique. The distances corresponding to 2000 feet and 30°C are as follows:...
  • Page 143 CESSNA SECTION 5 MODEL 172S PERFORMANCE AIRSPEED CALIB RATION NORMAL STATIC SOURCE CONDITION: Power required for level flight or maximum power descent. FLAPS KIAS 100 110 120 130 140 150 160 KCAS 107 117 127 137 147 157 FLAPS 10°...
  • Page 144: Airspeed Calibration

    SECTION 5 CESSNA PERFORMANCE MODEL 172S AIRSPEED CALIBRATION ALTERNATE STATIC SOURCE CONDITION: Power required for level flight or maximum power descent. FLAPS KIAS 100 110 120 130 140 150 160 KCAS 105 115 125 134 144 154 FLAPS 10° KIAS...
  • Page 145: Temperature Conversion Chart

    SECTION 5 CESSNA PERFORMANCE MODEL 172S TEMPERATURE CONVERSION CHART I­ DEGREES - CELSIUS Figure 5-2. Temperature Conversion Chart S-11...
  • Page 146: Stall Speeds

    SECTION 5 CESSNA PERFORMANCE MODEL 172S STAll S PEEDS AT 2550 POUNDS Conditions: Power MOST REARWARD CENTER OF GRAVITY ANGLE OF BANK FLAP 0° 30° 45° 60° SETTING KIAS KCAS KIAS KCAS KIAS KCAS KIAS KCAS 10° 30° MOST FORWARD CENTER OF GRAVITY...
  • Page 148 S ECTION 5 C ESSNA P ERFORMANCE MODEL 1 72S S H O RT F I E L D TAKEOF F DISTA N C E AT 2550 POU N DS CONDITIONS: Flaps 1 0° Fu" Throttle Prior to Brake Release Paved, level, dry runway Zero Wind Lift Off:...
  • Page 149 CESSNA SECTION 5 MODEL 172S PERFORMANCE SHORT FIELD TAKEOFF DISTANCE AT 2400 POUNDS COND I Flaps 10° Full Throttle Prior to Brake Release Paved, level, dry runway Zero Wind Lift Off: 48 K I Speed at 50 Ft: 54 K I O°C...
  • Page 150 SECTION 5 CESSNA PERFORMANCE MODEL 172S SHORT FIELD TAKEOFF DISTANCE AT 2200 POUNDS CONDITI ONS: Flaps 10° Full Throttle Prior to Brake Release Paved, level, dry runway Zero Wind Lift Off: 44 KIAS Speed at 50 Ft: 50 KIAS O°C 10°C...
  • Page 151 CESSNA SECTION 5 MODEL 172S PERFORMANCE MAXIMUM RATE-OF-CLIMB AT 2550 POUNDS COND I T IONS: Flaps Up Full Throttle PRESS CLIMB RATE OF CLIMB - FPM SPEED -20°C O°C 20°C 40°C KIAS S.L. 2000 4000 6000 8000 10 , 000...
  • Page 152 SECTION 5 CESSNA PERFORMANCE MODEL 172S TIME, FUEL AND DISTANCE TO CLIMB AT 2550 POUNDS CONDI TI ONS: Flaps Up Full Throttle Standard Temperature FROM SEA LEVEL RATE PRESS CLIMB TIME FUEL SPEED DIST CLIMB USED KIAS S.L. 1000 2000 3000 1 .
  • Page 153 CESSNA SECTION 6 PERFORMANCE MODEL 172S C RUISE PERFORMANCE CONDITIONS: 2660 Pounds Recommended Lean Mixture At All Altitudes (Refer to Section 4, Cruise) 20°C ABOVE 20°C BELOW STANDARD STANDARD TEMP TEMPERATURE STANDARD TEMP KTAS GPH KTAS GPH KTAS GPH 2000 2660 11.1...
  • Page 154 SECTION 5 CESSNA PERFORMANCE MODEL 172S CRUISE PERFORMANCE CONDITIONS: 2550 Pounds Recommended Lean Mixture At All Altitudes (Refer to Section 4 , Cruise) 20°C ABOVE 20°C BELOW STANDARD STANDARD TEMP STANDARD TEMP TEMPERATURE KTAS GPH KTAS GPH KTAS GPH 8000 2700 125 11.1...
  • Page 155 SECTION CESSNA PERFORMANCE MODEL 172S RANGE PROFILE 45 MINUTES RESERVE 53 GALLONS USABLE FUEL CONDITIONS: 2550 Pounds Recommended Lean Mixture for Cruise At All Altitudes Standard Temperature Zero Wind 12,000 10,000 8,000 I­ 1.1.. 6,000 4,000 2,000 RANGE - NAUTICAL MILES...
  • Page 157 CESSNA SECTION 5 MODEL 1 72S PERFORMANCE S H O RT FIE L D LAND I N G DISTANCE AT 2550 POU N DS CONDITIONS: Flaps 30° Power Off Maximum Braking Paved, level, dry runway Zero Wind Speed at 50 Ft: 61 KIAS O°C...
  • Page 159 SECTION 6 CESSNA & WE I G HT BALANCE/EQU I P M E NT LIST MODEL 1 72S SECTI WEIG ANCEl EQUIP ENT LIST TABLE O F CONTENTS Page I ntrodu ction Airplane Weigh i ng Procedu res ......
  • Page 161 C ESSNA SECTION 6 & MODEL 1 72S WE I G HT BALANCE / EQU I P ME NT LIST I NTRODU CTION T h i s section describes the procedure for establish i ng t h e basic empty weight and moment of th e airplane. Sample forms are provided for reference.
  • Page 162 S ECTI ON 6 C ESSNA & WEIGHT BALANC E EQU I P M ENT LIST MODEL 1 72S AIRPLANE WEI G H I N G FORM REFEREN C E DAT U M (FIREWALL FRONT FACE, LOWER PORTION) 0. 0 IT IS THE RESPONSIBILITY OF THE PILOT TO ENSURE THAT THE AIRPLANE IS...
  • Page 163 CESSNA SECTION 6 & MOD EL 1 72S WE IG HT BALANCE / EQU I P M E NT L IST LOCATING CG WITH AIRPLANE ON LANDING GEAR FORMULA for Longitudinal CG: INCHES (NOSE G EAR N ET WEIGHT) (...
  • Page 164 6- 1 . WEIGHT A N D BALAN C E T h e fol lowing i nformation will enable you t o operate you r Cessna withi n the prescribed weight and center of gravity l i m itations. To...
  • Page 165 5: 0 -< o (J) m (J) � -L » ( CONTINUOUS HISTORY OF CHANGES IN STRUCTURE OR EQUIPMENT AFFECTING WEIGHT AND BALANCE ) -..J ." AIRPLA N E M OD EL RUNNING WEIGHT CHANGE ITEM NO. BASIC EMPTY �...
  • Page 166 S ECTION 6 C ESSNA & WE IGHT BALANCE EQU I PM ENT LIST MODEL 1 72S NOTE Loading G raph i nformation for the pi lot, passengers and baggage based seats positioned average occu pants and baggage loaded i n the center of the baggage areas as shown on the Loadi ng Arrangements diagram .
  • Page 167 C ESSNA S ECTION 6 MODEL 1 72S WEIGHT BALANCE EQUI PM ENT LIST & LOADING ARRANGEMENTS Pilot or passenger center of g ravity on adjustable seats positioned for average occupant. Numbers in parentheses indicate forward and aft limits of occupant center of gravity range .
  • Page 168 SECTION CESSNA WEIGHT BALANCE EQUIPMENT LIST MODEL 1728 & CAB I N HEIGHT M EASUREMENTS FIREWALL AFT BAGGAGE AREA DOOR OPENI NG DIMENSIONS WIDTH WIDTH HEIGHT HEIGHT (TOP) (BOTTOM) (FRONT) (REAR) 40 1 / 2 " 3 9 " CABIN DOORS 321/2"...
  • Page 169 C ESSNA SECTION MODEL 1 72S WEIGHT BALANCE EQU IPMENT LIST & CABIN WIDTH MEASUREMENTS REAR DOORPOST BULKHEAD 1 0 20 CABIN 65 . 3 STATIONS (C.G. ARMS) .. LWR WIN DOW LI N E CABI N FLOOR 0585X1 023 Figure Internal Cabin Dimensions (Sheet 2 of 2) 6 - 4 .
  • Page 170 S ECTION CESSNA WEI G HT BALANCE (EQUIPMENT LIST MODEL 1 72S & WEIGHT AND MOMENT TABULATION SAMPLE YOUR ITEM DESCRIPTION AIRPLANE AIRPLANE Moment Moment Weight Weight (Lb-ins. (Lb-ins. (lbs.) (lbs.) 11000) 11000} 1. Basic Empty Weight (Use the data pertaining to...
  • Page 171 CESSNA SECTION 6 & MODEL 1 72S WEIGHT BALANCE 1 EQUIPMENT LIST YOUR YOUR YOUR AIRPLANE AIRPLANE AIRPLANE Moment Moment Moment Weight Weight Weight (Lb-ins. (Lb-ins. (Lb-ins. (Ibs (Ibs.) (Ibs.) 11000) 11000) /1000) 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 172 CESSNA SECTION 6 & MODEL 172S WEIGHT BALANCE EQUIPMENT LIST LOAD MOMENT/1000 (KILOGRAM - MILLIMETERS) 100 150 200 250 300 350 400 175 � « ::::> ...J -- 300 ..:::c 125 ..::r: � � � � LOAD MOMENT/1000 (POUNDS - INCHES)
  • Page 174 CESSNA SECTION 6 & MODEL 172S WEIGHT BALANCE 1 EQUIPMENT LIST 2600 2500 2400 2300 2200 ::r: 2100 � 2000 « 1900 « ...J 1800 1700 1600 1500 AIRPLANE C.G. LOCATION - INCHES AFT OF DATUM (STA. 0.0) 0585C1008 Figure 6 - 8. Center of Gravity Limits...
  • Page 175: Equipment List

    In the EQUIPMENT LIST DESCRIPTION column, each item is assigned a descriptive name to help identify its function. In the REF DRAWING column, a Cessna drawing number is provided which corresponds to the item. NOTE If additional equipment is to be installed, it must...
  • Page 176 SECTION 6 CESSNA WEIGHT BALANCE / EQUIPM E NT LIST M ODEL 1 72S & ITEM EQUIPMENT LIST DESCRIPTION R EF DRAWING INS. PLACARDS AND MARKINGS • PLACARD, OPERATIONAL LIMITATIONS 1 1 -0 1 ·R 0505087-23 43.0 PAINT, OVERALL EXTERIOR 0504051 1 9.2"...
  • Page 178 SECTION 6 CESSNA WEIGHT BALANCE / EQUIPMENT LIST MODEL 1 72S & ITEM EQUIPMENT LIST DESCRIPTION REF DRAWING INS. 25-1 5-S REAR SEAT RESTRAINT SYSTEM, I NERTIA 2000031 -1 1 , - 1 2 90.0 REEL 25-16-0 REAR SEAT RESTRAINT SYSTEM, MANUAL 90.0...
  • Page 179 CESSNA S ECTION 6 MODEL 1 72S WEIGHT BALANCE / EQUIPMENT LIST & ITEM EQUIPMENT LIST DESCRIPTION REF DRAWING INS. LANDING GEAR 32-01 ·R WHEEL BRAKE AND TIRE, 6.00 X 6 MAIN 57.8* 0541200·9,·1 0 34.4" 58.2 - WHEEL ASSY, CLEVELAND (EACH)
  • Page 180 SECTION 6 C ESSNA WEIGHT BALANCE / EQUIPMENT LIST MODEL 1 72S & ITEM EQUIPMENT LIST DESCRIPTION REF DRAWING INS. 34-08-0 GYRO INSTL, REQUIRES 37-01 -S USED 390001 6 1 1 .8" & 3.9" WITH 34-14-0 - A ITITUDE GYRO S3326-1 1 4.0 - HOSES...
  • Page 181 CESSNA SECTION 6 MODEL 1 72S WEIG HT BALANCE / EQUIPMENT LIST & ITEM EQUIPMENT LIST DESCRIPTION REF DRAWING INS. FUSELAGE 53-01 -S REFUELING STEPS AND HANDLE INSTL 051 341 5·2 1 .7 1 6.3 56 · WINDOWS 56-01 -S 5.8"...
  • Page 182 CESSNA SECTION 6 WEIGHT BALANCE / EQUIPMENT LIST MODEL 1 72S & ITEM EQUIPMENT LIST DESCRIPTION REF DRAWING I NS. & 73 - ENGINE FUEL CONTROL EGTIFUEL FLOW INDICATOR S32n-4 73-01 -S - ENGINE I N DICAT I NG 1 .0...
  • Page 183: Revision 4

    CESSNA SECTION 6 & MODEL 1 72S WE I G HT BALANCE / EQU I P M E NT LIST ITEM EQUIPMENT LIST DESCRIPTION REF DRAWING INS. 98-02-A NAV I AVIONICS PKG (NET CHANG E OVE R 3900004-1 21 .3* 21 .5*...
  • Page 185: May 30/00

    C ESSNA S ECTION & MODEL 1 72S AIRPLANE SYSTEMS DESC R I PTION SECTI N & SYSTEMS TABLE O F CONTENTS Page I ntrodu ction Airframe Flight Controls Tri m System I nstru ment Panel 7 -9 7 -9 P i lot Side Panel Layout Center Panel Layout Copilot Side Panel Layout...
  • Page 186: May 30/00

    S ECTION 7 C ESSNA & AIRPLAN E SYSTE MS D ESC R I PTION MODEL 1 72S (Conti nued) Page Engine ........7-1 9 Engine Controls .
  • Page 187: Revision 4

    CESSNA SECTION & MODEL 1 72S A I R P LANE SYSTEMS D ESCR I PTION TABLE OF CONTENTS (Contin ued) Page Lighting Systems ....... . .
  • Page 189 CESSNA S ECTION 7 MODEL 1 72S AIRPLANE SYSTEMS DESCRIPTION & I NTRODUCTION This section provides description and operation of the airplane and its systems. Some equipment described herein is optional and may not be installed in the airplane. Refer to the sUPPlements' Section 9, for details of other optional systems and equipment.
  • Page 190: Flight Controls

    SECTION 7 CESSNA AIRPLANE SYSTEMS DESCRI PTION MODEL 1 72S & 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...
  • Page 191 CESSNA SECTION 7 & MODEL 1 72S AIRPLANE SYSTEMS DESCRIPTION 0585X1017 Figure 7 - 1. Flight Control and Trim Systems (Sheet 1 of 2) July 8/98...
  • Page 192 SECTION 7 CESSNA & AIRPLANE SYSTEMS DESCRIPTION MODEL 172S E LEVATOR CONTROL SYSTEM ... ELEVATOR TRIM CONTROL SYSTEM {.:':!.</.7 / i I ..· ..· · ..· ..
  • Page 193: Revision 4

    SECTION CESSNA & MOD E L 1 72S AIRPLA N E SYSTEMS D ESCR I PTION I N ST R U M E NT PAN E L The i nstrument panel ( Refer to Figu re 7 -2) i s of all-metal...
  • Page 194: Revision 4

    C ESSNA & A I R P LANE SYSTEMS D ESCR I PTION MODEL 1 72S 0585C1 040 Figure 7-2 . Instru ment Panel (Sheet 1 of 2) 7-1 0 Revision 4...
  • Page 195: Revision 4

    CESSNA S ECTION & MOD E L 1 72S A I R P LAN E SYSTEMS D ESC R I PTION Oil Temperature and Oil Hou r Meter Pressure Ind icator Vacuum Gage and Ammeter Glove Box Fuel Quantity Ind icator...
  • Page 196: Revision 4

    SECTION 7 C ESSNA & MODEL 1 72S AI RPLAN E SYSTEMS D ESC R I PTION R H SIDE PAN E L LAYOUT The RH panel contains the hour meter, E L T switc h , and roo m for expansion of i ndicators and other avionics equipment.
  • Page 197: Revision 4

    C ESSNA SECTION & MODEL 1 72S A I RP LANE SYSTE MS D ESC R I PTION WI NG FLAP SYSTEM T h e single-slot type wing flaps (Refer t o Fig u re 7-3), are extended or retracted by positioni ng the wing flap switch l ever on th e i nstrument panel to the desired flap deflection position.
  • Page 198 C ESSNA & SYSTEMS D ESCR I PTION MODEL 1 72S LAN D I NG G EA R SYSTE M The landing gear is of the tricycle type, with a steerable nose wheel and two main wheels. Wheel fairings are standard equ ipment for both the main and nose wheels.
  • Page 199 CESSNA SECTION MODEL 1 728 AI RPLAN E SYSTE MS DESCR IPTION & The rear passengers' seat consists of a fixed, one piece seat bottom and a three-position , reclining back. The recli ning back is adjusted by a lever located below the center of the seat frame. To...
  • Page 200 SECTION 7 CESSNA MODEL 1 72S AIRPLANE SYSTEMS DESCRIPTION & STANDARD INTEGRATED SEATBELTI SHOU LDER HARNESS WITH INTERTIA REEL VERTICAL (HEIG HT) ADJUSTMENT CRANK SEAT BACK ANG LE BUDON FORE AND AFT BUCKLE ADJUSTMENT ... PRESS TO (NON ADJUSTABLE) LEVER...
  • Page 201 C ESSNA SECTION MODEL 1 72S AIRPLANE SYSTEMS DESCRIPTION & A manually adustable seat belt/shoulder harness assembly is available for a" seats. To use the manually adjustable seat belt/shoulder harness, fasten and adjust the seat belt/shoulder harness first. Lengthen the seat belt as required by pulling on the release strap on the belt.
  • Page 202 SECTION 7 CESSNA AIRPLANE SYSTEMS D ESCRIPTION MODEL 1 72S & N OTE Accidental opening of a cabin door in flight due to i mproper 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 , m omentarily shove the door outward slightly, and forcefully close and lock the door.
  • Page 203: Engine

    C ESSNA S ECTION & MODEL 1 72S A I R P LANE SYSTEMS D ESC R I PTION E N G I N E The airplane is powered by a horizontally opposed, fou r cyl inder, overhead valve, air-cooled , fuel-i njected engine with a wet sump lubri cation system .
  • Page 204: Revision 4

    C ESSNA SECTION 7 & AI RPLAN E SYSTEMS D ESC R I PTION MODEL 1 72S Oil pressu re signals are generated fro m an oil pressu re l i ne/transdu cer combination . An oil pressu re line is routed fro m the upper front of the engine case to the rear engine baffle.
  • Page 205: New Engine Break- I N And Operation

    C ESSNA S ECTION & MODEL 1 72S AI RPLANE SYSTEMS DESC R I PTION The EGT system uses a thermocouple in the engine exh aust (tai lpipe) supply voltage proportional exhaust temperature. Th e EGT i ndicator responds to the voltage developed by the thermoco uple .
  • Page 206: Ignition And Starter System

    CESSNA S ECTION 7 & AI RPLAN E SYSTEMS DESC R I PTION MODEL 1 72S I G N ITION A N D STA RTER SYSTEM Engine ignition is provided by two eng ine-driven magnetos , and two spark plugs i n each cyli nder. The right mag neto fires the lower rig ht and upper left spark plugs, and the left magneto fi res the lower left and u pper rig ht spark plugs.
  • Page 207: Exhaust System

    C ESSNA SECTION & MODEL 1 72S AIRPLAN E SYSTEMS D ESCRI PTION EXHAUST SYSTEM Exhaust gas from each cyli nder passes th rough riser assemblies to a m uffler and tai lpipe. O utside air is pulled i n around s h rouds which are constructed aro u nd the o utside of the muffler to form h eating chambers which supply heat to the cabin.
  • Page 208: Fuel D Istribution

    SECTION 7 CESSNA & AI RPLAN E SYSTEMS D ESCR I PTION MODEL 1 72S F U E L F U E L LEVEL TOTAL TOTAL TOTAL USABLE TAN KS (QUANTITY F U E L U N USABLE A L L FLIGHT...
  • Page 209: Fuel I Ndicati Ng

    C ESSNA SECTION & MOD E L 1 72S AI RPLANE SYSTEMS DESC R I PTION F U E L I N DI CATI N G Fuel q uantity is measured by two float type fuel quantity transmitters (one i n each tank) and i ndicated by an electrically operated fuel quantity i ndicator on the left side of the i nstrument panel.
  • Page 210: Fuel Venting

    C ESSNA & AI RPLAN E SYSTEMS D ESC R I PTION MODEL 1 72S F U E L VENTI N G F u e l system venting is essential t o system operation . Blockage of the system wi l l result in decreasing fuel flow and eventual eng i ne stoppage.
  • Page 211: Revision 4

    CESSNA SECTION & MODEL 1 72S AI RPLAN E SYSTEMS D ESC R I PTION FUEL QUANTITY INDICATORS LEFT RIGHT FUEL FUEL TANK TANK ( WITH CHECK VALVE ) FUEL TANK FUEL SHUTOFF - - - VALVE KNO B VENT...
  • Page 213 C ESSNA SECTION & MODEL 1 72S AIRPLAN E SYSTEMS D ESC R I PTION 82113 FUEL QUANTITY INDICATORS FUEL QUANTITY TRANSMITTER R IGHT FUEL TANK S ELECTOR VENT VALVE (WITH CH ECK D RAIN DRAIN VALVE) VALVES VALVES (5 TOTAL) (5 TOTAL) FUEL RETURN...
  • Page 214 S ECTION 7 C ESSNA & AIRPLAN E SYSTEMS DESC R I PTION MODEL 1 72S NOTE When the fuel tanks are 1 /4 fu l l or less, prolonged u ncoordinated flight such as slips or skids can uncover the fuel tank outlets.
  • Page 215: Avionics Master Switch

    SECTION CESSNA & MODEL 1 72S AI RPLA N E SYSTEMS DESC R I PTION 0)- TO GLARESHIELD LT OVERHEAD LTS CABIN COURTESY LTS LTS / 0)"-TO AVN FAN 1 2V POWER ,... AVN FAN 0)-- TO INSTRUMENTS � Q)"- TO GPS ,...
  • Page 216: Revision 4

    C ESSNA SECTION 7 & MODEL 1 72S A I R P LAN E SYSTEMS DESC R I PTION The airplane uses a power d istribution module (J-Box) , located on the left forward side of the firewal l , to house all relays used th roughout the airplane electrical system .
  • Page 217: Revision 4

    C ESSNA SECTION & MOD EL 1 72S AI RPLANE SYSTEMS DESC R I PTION MASTER SWITCH The master switch is a split-rocker type switch l abeled MASTER' and is ON i n the up position and OFF i n the down pos ition . The right h alf of the switch , labeled BAT, controls the battery power to the airplane.
  • Page 218: Revision 4

    C ESSNA SECTION 7 & AI RPLAN E SYSTEMS D ESCR I PTION MODEL 1 72S AVI O N I CS MAST E R SWITCH Electrical power for each Avionics Bus is supplied from a primary Electrical Bus. For airplane serial n u m bers 1 72S800 1 through 1 72S8703, except for certai n non- U .S.
  • Page 219: Low Voltage Annunciation

    C ESSNA SECTION & MOD E L 1 72S AI RPLA N E SYSTE MS DESC R I PTION lOW VOLTAGE AN N U NCIATION The low voltage warning annu nciator is incorporated in the ann unciator panel and activates when voltage fal ls below 24.5 volts. If low voltage is detected, the red ann unciation VOLTS wil l flash for approxi mately 1 0 seconds before i l l u m i nating steadily.
  • Page 220: Revision 4

    CESSNA SECTION 7 & AI RPLAN E SYSTEMS D ESC R I PTION MODEL 1 72S EXTERNAL POW E R RECEPTACL E An external power receptacle is i ntegral to the power distribution mod u le and allows the use of an external electrical power sou rce for cold weather starting, and d u ring lengthy maintenance work on electrical and avionics equ ipment.
  • Page 221: Lighting Systems

    C ESSNA S ECTION & MODEL 1 72S A I RP LA N E SYSTEMS DESC R I PTION LIG HTIN G SYSTEMS EXTER I O R LIG HTI N G Exterior l ighting consists of navigation lights on the wing tips and top of the rudder, a dual l andi ng/taxi l ig ht configuration located i n the l eft wi ng leading edge, a flashing beacon mounted on top o f the vertical fin , and a strobe light on each wing tip.
  • Page 222: Revision 4

    C ESSNA S ECTION 7 & AIRPLAN E SYSTEMS D ESC R I PTION MODEL 1 72S G l areshield lighting is provided by either a fluorescent l ig ht or a series of LED lig hts recessed i nto the lower surface of the glaresh ield .
  • Page 223: Cabin Heating , Ventilating And Defrosti Ng System

    C ESSNA SECTION & MODEL 1 72S A I R P LANE SYSTEMS D ESC R I PTION CABI N H EATI N G , VE NTI LATI NG A N D D EFROSTIN G SYSTEM The temperatu re and volume o f airflow i nto t h e cabin can be reg u lated by manipulation of the push-pu l l CAB I N HT and CAB I N A I R controls (Refer to Fig u re 7-8) .
  • Page 224 C ESSNA SECTION 7 & MODEL 1 72S SYSTEMS D ESC R I PTION H EATE R M U FFLER VALVE S H RO U D CABI N H EAT CONTROL FORWARD FORWARD CAB I N CAB I N LOWER LOWER VENTI LATI N G VENTI LATI N...
  • Page 225: 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 p ressure to the a irspeed indicator and static p ressu re to the airspeed indicator, vertical speed indicator and altim eter. The system is composed of a h eated p itot...
  • Page 226: Airspeed Indicator

    SECTION 7 CESSNA & AIRPLANE SYSTEMS DESCRIPTION MODEL 172S AIRSPEED INDICATOR The airspeed indicator is calibrated in knots. It incorporates a true airspeed window which allows true airspeed to be read off the face of the dial. In addition , the indicator incorporates a window at...
  • Page 227: Alti M Eter

    CESSNA SECTION & MODEL 1 72S AI RPLANE SYSTE MS D ESCRI PTION ALT I M ETE R Airplane altitude is depicted by a barometric type altimeter. A knob n ear the lower left portion of the indicator provides adjustment of th e i nstrument's barometric scale to the current alti meter setting .
  • Page 228 C ESSNA SECTION 7 & MODEL 1 72S SYSTEMS D ESC R I PTION LOW VACUUM VACUUM SWITCHES (CONNECTED TO DISCHARGE ANNUNCIATOR PANEL) MANI FOLD CHECK VALVE DIRECTIONAL INDICATOR 0585C1 0 1 4 Fig ure 7-9. Vacuu m System J u ly 8/98 7-44...
  • Page 229: Low Vacu U M Annunciation

    CESSNA SECTION MODEL & AIRPLANE SYSTEMS DESCRIPTION 1 72S VAC U U M GAG E 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 230: Clock / O.a.t. I Nd Icator

    C ESSNA SECTION 7 & AIRP LAN E SYSTEMS D ESC R I PTION MOD E L 1 72S I C LOCK / O.A.T. I NDI CATO R An i ntegrated clock / O.A.T. / voltmeter is i nstal led in the u pper left side of the i nstru ment panel as standard equ i pment.
  • Page 231: Avionics Su Pport Equi Pment

    CESSNA SECTION & MODEL 1 72S AI RPLA N E SYSTEMS DESC R I PTION AVI O N I CS S U P PO RT EQUI PMENT Avionics operations are supported b y t h e avionics cooling fan , m icrophone a n d headset i nstall ations a n d static d ischarge wicks.
  • Page 232: Static Dischargers

    S ECTION 7 C ESSNA & AIRPLANE SYSTEMS D ESC R I PTION MODEL 1 72S NOTE To ensure audibility and clarity when transmitti ng with the handheld m icrophone, always hold it as closely as possible to the l ips, then key the microphone and speak d i rectly i nto it.
  • Page 233: Cabin Features

    CESSNA S ECTION MODEL 1 72S AIRPLANE SYSTEMS DESCRIPTION & CABIN FEATURES E M ER G EN CY LOCATOR TRANSMITTER (ELT) A remote switch/annunciator is installed on the top center location of the copilot's i nstrument panel for control of the EL T from the flight crew station.
  • Page 234 SECTION 7 CESSNA SYSTEMS DESCRI PTION MODEL 1 72S & WAR N I N G VENTILATE T H E CABI N PROMPTLY AFTER S U C .. CESSFUll EXTIN G U IS H I NG THE FIRE TO RE­ DUCE THE GASES PRODUCED BY THE R MAL DECOMPO SITION.
  • Page 235 United States Airplane Owners I nternational Airplane Owners Publications Airplane File Airplane I nspection Periods FAA Required Inspections Cessna Inspection Programs Cessna Customer Care P rogram Pi lot Conducted Preventive Maintenance Alterations Or Repairs 8-1 0 Ground Handling 8-1 0 Towing...
  • Page 236 SECTION 8 CESSNA HANDLING, SERVIC E MAINTENANCE MODEL 172S & TABLE OF CONTENTS (Continued) Page Capacity of Engine Sump Oil and Oil Filter Change ......8-15...
  • Page 237 Cessna. Other modifications may void warranties on the ai rplane since Cessna has no way of knowing the ful l effect on the overall airplane. Operation of an airplane that has been modified may be a risk to the occupants , and operating procedu res and performance data set forth i n the operating h andbook may no longer be considered accurate for the modified airplane.
  • Page 238: Identification Plate

    . CESSNA OWNE R A DVISO R I ES C essna Owner Advisories are sent to Cessna Aircraft FAA Registered owners of record at no charge to i nform them about mandatory and/or beneficial aircraft service requ i rements and product changes.
  • Page 239: United States Airplane Owners

    Cessna's Product Support Department at (3 1 6) 5 1 7-5800. Fax (3 1 6) 942-9006 or write to The Cessna Aircraft Co mpany, P . O. Box 7706, Wich ita, KS 67277, Dept 75 1 C .
  • Page 240: Airplane File

    Man u al • I llustrated Parts Catalog You r local Cessna Service Station h as a Customer Care Supplies and Publ ications Catalog covering all available items, many of which the Service Station keeps on hand . The Service Station can place an order for any item wh ich is not in stock.
  • Page 241: Airplane I Nspection Periods

    United States should check with their own aviation officials to determine their individual requ irements. Cessna recommends that these items, plus the Pilot's Checklists, Customer Care Program Handbook and Customer Care Card , be carried in the airplane at all times.
  • Page 242: Cessna Inspection Programs

    HANDLING, SERVICE MAINTENANCE MODEL 172S CESSNA INSPECTION PROGRAMS In l ie u of the 100 hour and ann u al inspection req u i rements, an airPlane may be inspected in accordance with a Progressive Care Inspection Program or a PhaseCard I nspection Program. Both...
  • Page 243: Cessna Customer Care P Rogram

    While these important inspections will be performed for you by any Cessna Service Station, in most cases you wil l prefer to have the Cessna Service Station from whom you purchased the airplane accomplish this work.
  • Page 244: Alterations Or Repairs

    A M aintenance M anual must be obtained prior to performing any preventive maintenance to ensure that proper procedu res are fol lowed . You r local Cessna Service Station should be contacted for further information or for required maintenance which m ust be accomplished by appropriately licensed personnel.
  • Page 246: Leveling

    SECTION 8 C ESSNA HANDLING, SERVICE MAINTENANCE MODEL 1 72S & CAUTION DO N OT APPLY PRESSUR E ON THE E LEVATOR HORIZONTAL STABI LIZER SURFACES. WHEN PUSHING ON THE TAI LCONE, ALWAYS APPLY PRESSURE AT A BULKHEAD TO AVOI D BUCKLIN G T H E SKI N .
  • Page 247: Servicing

    , and/or testing at special i ntervals . Since Cessna Service Stations conduct a" service , i nspectio n , a n d test procedu res i n accordance with applicable M ai ntenance Man uals, it is recommended that you contact you r local Cessna...
  • Page 248: Oil

    C ESSNA S ECTION 8 & MODEL 1 72S HAN D L I N G , S E RV I C E MAI NTENANCE Depending on various fl ight operations, you r local Government Aviation Agency may req u i re additional service, i nspections, or tests.
  • Page 249: Capacity Of Engine Sump

    CESSNA SECTION 8 & MODEL 1 72S HAN DLI NG , SERVICE MAI NTENANCE CAPACITY O F ENGINE S U M P The e n g i n e l ubrication system has a total capacity o f 9 q uarts Of oil, with the oil filter accou nting for 1 q uart of that total .
  • Page 250: Fuel Capacity

    C ESSNA S ECTI ON 8 & MOD E L 1 72S HAN D L I N G , S E RV I C E MAINTENANCE F U E L APPROVED F U E l G RA D ES (AN D COlOR� 1 DOLL G rade Aviation Fuel (Blue) .
  • Page 252 SECTION 8 CESSNA HANDLING, SERVICE MAINTENANCE MODEL 1 72S & ,oi-+--r7!" :'�++·t··:·;-� ·!- ���·7u!-t-r·:··T·�·· ·�·r·t·+·r+·T++·. ··�1·1··�· -1�:++ ·+f·+J•· · .. ;. • • • • " • • • • • " • � " • • > � �...
  • Page 253 CESSNA SECTION 8 & MODEL 1 72S HAN D L I NG , SERVICE MAI NTENANCE 2 . An alternate method that may be used is to premix the complete alcohol dosage with so me fuel in a separate clean...
  • Page 254: Fuel Contamination

    Mai ntenance Manual . Only the proper fuel , as reco mmended in this handbook, shou ld be used , and fuel additives should not be used u nless approved by Cessna and the Federal Aviation Ad min istration.
  • Page 255: Landing Gear

    CESSNA S ECTION 8 & MODEL 1 72S HAN DLING, S E RVICE MAI NTENANCE LAN DING G EA R Consult the fol lowi ng table for servici ng i nformation o n the landi ng gear. COM PO N ENT...
  • Page 256: Painted Surfaces

    PAI NTED S U R FACES The pai nted exterior su rfaces of you r new Cessna have a d u rable , long lasting fi nish. Generally, the painted surfaces can be kept bright by washing with water and mild soap, followed by a ri nse with water and drying with cloths or a chamois.
  • Page 257: Propeller Care

    C ESSNA SECTION 8 & MODEL 1 72S HAN D L I N G , SERVICE MAI NTENANCE When the airplane is parked outside i n cold cli mates and it is necessary to remove ice before flight, care should be taken to protect the painted surfaces duri ng i ce removal with chemical liquids.
  • Page 258: I Nterior Care

    S ECTION 8 CESSNA & HAN D L I N G , S E RVICE MAINTENANCE MODEL 1 72S I NTERIOR CARE To remove dust and loose dirt fro m the u pholstery and carpet, clean the i nterior regularly with a vacu u m cleaner.
  • Page 259 SUPPLEMENT REVISION MODEL 172S PILOT'S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL REVISION 10 7 JANUARY 2004 PART NUMBER: 172SUSLOG10 INSERT THE FOLLOWING PAGES INTO THE SUPPLEMENT SECTION OF THE PILOT'S OPERATING HANDBOOK...
  • Page 261 SUPPLEMENTS." THIS APPROVED SUPPLEMENTS" WAS THE LATEST REVISION AS OF THE DATE IT WAS SHIPPED BY CESSNA; HOWEVER, SOME CHANGES MAY HAVE OCCURRED AND THE OWNER SHOULD VERIFY THIS IS THE LATEST, MOST UP-TO-DATE VERSION BY CONTACTING CESSNA CUSTOMER SUPPORT AT (316) 517-5800.
  • Page 262 SECTION 9 CESSNA SUPPLEMENTS MODEL 172S LOG OF APPROVED SUPPLEMENTS SUPP. SUPPLEMENT NAME REVISION EQUIPMENT LEVEL INSTALLED Canadian Supplement Bendix/King KCS-55A Slaved Compass System with KI-525A Horizontal Situation Indicator (HSI) Reserved Bendix/King KAP 140 2 Axis Autopilot Reserved Reserved Reserved...
  • Page 263 CESSNA 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 airplane are observed.
  • Page 265 SUPPLEMENTS" WAS THE LATEST REVISION AS OF THE DATE IT WAS SHIPPED BY CESSNA; HOWEVER, SOME CHANGES MAY HAVE OCCURRED AND THE OWNER SHOULD VERIFY THIS IS THE LATEST, MOST Up· TO·DATE VERSION BY CONTACTING CESSNA CUSTOMER SUPPORT AT (316) 517·5800. REVISION EQUIPMENT SUPP. SUPPLEMENT NAME LEVEL...
  • Page 266 CESSNA SECTION 9 MODEL 17 2S SU PPLEMENTS LOG OF APPROVED SUPPLEMENTS SUPP. SUPPLEMENT NAME REVISION EQUIPMENT LEVEL INSTALLED Canadian Supplement Bendix/King KCS-55A Slaved Compass System with KI-525A Horizontal Situation Indicator (HSI) Reserved Bendix/King KA P 140 2 Axis Autopilot...
  • Page 267 Section Pilot's Operating Handbook and FAA Approved Airplane Flight Manual. FAA APPROVAL J!lAA APPROveO UNDER FAR 21 SUBPART J The Cessna Aircraft Co Extc:utivo EnSInHf 1998 Member of GAMA 8 July 1998 © COPYRIGHT 1998 CESSNA AIRCRAFT COMPANY...
  • Page 268 SECTION 9 - SUPPLEMENTS CESSNA MODEL 172S SUPPLEMENT 1 BENDIX/KING KX 155A VHF NAV/COMM with KI KI209A INDICATOR HEAD 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 269 CESSNA SECT ION 9 - SUPP LEME NTS MODEL 172S SUPPL EMENT 1 - FAA APPRO VED SUPPLEMENT BENDIX/KING KX 155A VHF NAV/COMM with KI 208 or KI 209A INDICATOR HEAD SECTION 1 G ENERAL 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 270 SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 1 - FAA APPROVED MODEL 172S 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 271 CESSNA SECTION 9 SUPPLEMENTS MODEL 172S SUPPLEMENT 1 - FAA APPROVED 122.1 3.00 I I7.bO 39:5b KX 155A VHF NAV/COMM TO INDICATION FROM INDICATION FLAG INDICATION KI 209A INDICATOR 0585C1045 0585C1046 KI 208 INDICATOR HEAD 0585C1047 Figure 1. Bendix/King KX 155A VHF NAV/COMM with KI 208 or...
  • Page 272 CESSNA SECTION 9 - SUPPLEMENTS SUPPLEMENT 1 - FAA APPROVED MODEL 172S NAV FUNCTION DISPLAYS VOR MODE: ACTIVE/BEARING, CDI FORMAT VOR MODE: ACTIVE/BEARING, FLAG DISPLAY 109.50 VOR MODE: ACTIVE "BEARING TO" FUNCTION DISPLAY VOR MODE: ACTIVE/BEARING, FLAG DISPLAY � '-' f- �...
  • Page 273 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 1 - FAA APPROVED 1. OPERATING COMM FREQUENCY DISPLAY -- Displays liT' COMM ACTIVE and COMM STANDBY frequencies with a between them to indicate TRANSMIT and an "R" to indicate RECEIVE modes of operation.
  • Page 274 SECTION 9 SUPPLEMENTS CESSNA SUPPLEMENT 1 - FAA APPROVED MODEL 172S NAV/FREQUENCY TRANSFER BUnON Interchanges the NAV Active and STANDBY frequencies. Depressing the NA V frequency transfer button for 2 seconds or more will cause the display to go into the ACTIVE ENTRY mode.
  • Page 275 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 1 - FAA APPROVED Another push of the mode button will cause the NAV display from ACTIVE/BEARING format ACTIVE/RADIAL format. In the RADIAL mode, the frequency inc/dec knobs channel the ACTIVE frequency window and...
  • Page 276 SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 1 - FAA APPROVED MODEL 172S 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 277 CESSNA SECTION 9 SUPPLEMENTS MODEL 1728 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 278 SECTION 9 SUPPLEMENTS CESSNA SUPPLEMENT 1 - FAA APPROVED MODEL 172S SECTION 2 LIMITATIONS There is no change to the airplane limitations when this avionic equipment is installed. SECTION EMERGENCY PROCEDURES There is no change to the airplane emergency procedures when this avionic equipment is installed.
  • Page 279 CESSNA SECTIO N 9 - SUPPL EMENT S MODEL 172S SUPPLE MENT 1 - FAA APPRO VED 6. Mic Button: a. To transmit -- Press button and speak in microphone. NOTE "TI During COMM transmission, a lighted will appear between the "COMM" and "STBY" displays to indicate that the transceiver is operating in the transmit mode.
  • Page 280: July

    SECTION SUPPLEMENTS CESSNA 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 NA V...
  • Page 281 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 the NA V Transfer Button momentarily exits Pilot configuration mode. The NA V returns to its pre-Pilot Config state with the new brightness and sidetone levels stored in nonvolatile memory.
  • Page 283 A Textron Company Pilot's Operating Handbook and FAA Approved Airplane Flight Manual CESSNA MODEL 172S AIRPLANES 17258001 AND ON SUPPLEMENT 2 BENDIX/KING KT 76C TRANSPONDER WITH BLIND ENCODER SERIAL NO., REGISTRATION NO. This supplement must inserted into Section Pilot's Operating Handbook and FAA Approved Airplane Flight Manual.
  • Page 284 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 285 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 (ATCRB8).
  • Page 286 SECTION 9 SUPPLEMENTS CESSNA SUPPLEMENT 2 FAA APPROVED MODEL 172S 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 11120011.
  • Page 287 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 2 - FAA APPROVED 1200 1. IDENT SUDON (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 288 SECTION 9 SUPPLEMENTS CESSNA SUPPLEMENT 2 - FAA APPROVED MODEL 172S 3. MODE ANNUNCIATORS - Displays the operating mode of the transponde r. 4. REPLY INDICATOR (R) - "R" is illuminated momentarily when the transponder is replying to a valid interrogation and during the 18 ±2 seconds following the initiation of an Ident.
  • Page 289 CESSNA SECTION 9 SUPPLEMENTS MODEL 172S SUPPLEMENT 2 - FAA APPROVED SECTION 2 LIMITATIONS There is no change to the airplane limitations when this avionic equipment is installed. SECTION EMERGENCY PROCEDURES TO TRANSMIT AN EMERGENCY SIGNAL: Mode Selector Knob -- ALT.
  • Page 290 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 AL T also;...
  • Page 291 CESSNA SECTION 9 SUPPLEMENTS MODEL 172S SUPPLEMENT 2 - FAA APPROVED TO PROGRAM VFR CODE: 1. Mode Selector Knob -- SBY. Numeric Keys SELECT desired VFR code. 0-7 - 3. lOT Button -- PRESS AND HOLD. a. VFR Code Button -- PRESS...
  • Page 293 ATextron Pilot's Operating Handbook and FAA Approved Airplane Flight Manual CESSNA MODEL 172S AIRPLANES 172S8001 AND ON SUPPLEMENT BENDIX/KING KMA 26 AUDIO SELECTOR PANEL .. _ _ _ _ _ _ _ _ SERIAL NO REGISTRATION NO., This supplement must be inserted into Section of the Pilot's Operating' Handbook and FAA Approved Airplane Flight Manual.
  • Page 294: May 30/00 July

    S ECTION 9 SUPPLEMENTS CESSNA S UPPLEMENT 3 - APPROVED MODEL 1 72S SUPPLEMENT 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 l isting of all pages i n the Supplement.
  • Page 295 CESSNA SECTION 9 - S UPPLEM E NTS MODEL 1 72S SUPPLE M ENT 3 - FAA APPROVED SUPPLE ENT 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 296 SECTION 9 SUPPLEMENTS CESSNA S UPPLEM E NT 3 - FAA APPROVED MODEL 1 72S INTERCOM .,.. PUSH VOX 1 . M ARKER BEACON ANNUNCIATOR LIGHTS -- The three-light marker beacon receiver built i nto the KMA 26 g ives a visual and aural signal when the ship's antenna passes over a 75 M Hz beacon .
  • Page 297 CESSNA SECTION 9 - S U PP LEME NTS MODEL 1 72S S UPPLEM E NT 3 - FAA APPROVED 3. MARKER B EACON S ENSITIVITY LAM P AND TEST SWITCH --The II MKR " Audio Select button m ust be pushed so that the green ann unciator is illuminated for the marker beacon to receive to provide an audio signal at beacon passage.
  • Page 298 SECTION 9 - SU PPLEME NTS CESSNA S U PPLEM ENT 3 FAA APPROVED MODEL 1 72S 6. SPEAKER S ELECT (PUSH S PKR) SWITCH -- With the Speaker Select Switch pushed in, both headphone and cabin speaker audio wil l be heard . Headphone audio is active ful l­...
  • Page 299 CESSNA SECTION S UPPLEMENTS MODEL 1 72S SUPPLEMENT 3 - FAA APPROVED 1 a. INTERCOM MODE SELECT SWITCH -. Has three modes "ALL" , "CREW " , AND " PI LOT" which are selected with the toggle switch on the lower left side on the faceplate.
  • Page 300 S ECTION 9 S UPPLEMENTS CESSNA SUPPLEMENT 3 - APPROVED MODEL 1 72S 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 fail u re of the audio amplifier in the KMA 26, as evidenced by the inability to transmit in COM 1 , 2 or 3.
  • Page 301 CESSNA SECTIO N 9 - SUPPLEMENTS MODEL 1 72S S UPPLEMENT 3 - APPROVED MARKER BEACON RECEIVER OPERATION: 1 . TEST Position -- HOLD toggle down momentarily to verify all l ights are operational . 2. S ENS Selections -- Select HI sensitivity for airway flying or LO for I LS/LOC approaches.
  • Page 303 FAA APPROVAL 'AA APPROveO UNDER FAR21 SUSPART J AirCfGft Co The Cessna ation Option Manufacturer CE·1 Exteutivo EnQlnn, 2000 Member of GAMA 8 July 1998 COPYRIGHT C> 1998 Revision 30 May 2000 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA 84-1 172SPHUS·S4-01...
  • Page 304 SECTION 9 - S UPPLEMENTS CESSNA SUPPLEM E NT 4 - APPROVED MODEL 1 72S SUPPLE MENT POINTER MODEL 3000 .. 11 OR MODEL 4000-11 EMERGENCY lOCATOR TRANSMITTER (El T) The fol lowing Log of Effective Pages provides the date of issue for original and revised pages, as wel l as a listing of all pages i n the Supplement.
  • Page 305 CESS NA SECTION 9 - S UPPLEMENTS MODEL 1 72S SUPPLEME NT 4 - FAA APPROVED POINTER MODEL 3000 11 OR MODEL 4000 EMERGENCY LOCATOR TRANSMITTER (ELT) SECTION 1 This supplement provides i nformation which must be observed when operating the Pointer Model 3000- 1 1 or Model 4000-1 1 E mergency Locator Transmitter.
  • Page 306 SECTION 9 - SUPP L E M ENTS CESS NA SUPPLEMENT 4 - FAA APPROVED MODEL 1 72S In accordance with FAA regulations, the ELT's battery pack must be replaced after 2 years shelf or service l ife or for any of the following reasons: a.
  • Page 307 CESSNA SECTION 9 - SUPPLEMENTS MODEL 1 728 S U PPLEMENT 4 - FAA APPROVED OFF/RESET -- Deactivates transmitter during handl i ng, fol lowing rescue and to reset the automatic activation function. (The red ann unciator in the center of the remote switch/annunciator should extinguish).
  • Page 308 SECTI O N 9 - S U PPLEMENTS CESSNA SUPPLEMENT 4 - FAA APPROVE D MODEL 1 72S 4. M�STER FUN CTION SELECTOR SWITC H (3-position toggle sWitch): ON -- Activates transmitter i nstantly. Used for test purposes and if " G " switch is i noperative. The ON position bypasses the automatic activation switch.
  • Page 309 CESSNA SECTION 9 - SUPPLEMENTS MODEL 1 72S SUPPLEMENT 4 - FAA APPROVED SECTION 3 EMERGENCY PROCEDURES Before performing a forced landing, especially in remote and mountainous areas, activate the EL T transmitter by positioning the remote switch/annunciator to the ON position. The annunciator i n center of t h e rocker switch should b e i ll uminated.
  • Page 310 SECTION 9 - SUPPLEMENTS CESSNA SUPPLEM E NT 4 - FAA APPROVED MODEL 1 72S SECTION 4 NORMAL PROCEDURES As long as the remote switch/ann u nciator is in the AUTO position and the EL T master function selector switch remains in the AUTO position, the EL T automatically activates when the unit senses longitudinal inertia forces as required in TSO-C9 1 A.
  • Page 313 System is installed, FAA APPROVAL 'AA APPROveO UNDER FAR21 SUBPARTJ AifChll ft Co The Cessna ex.eutivoEng,"Hf 2000 Member of GAMA 8 July 1998 COPYRIGHT CI 1998 Revision 2 - 30 May 2000 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA S5-1 172SPHUS-S5-02...
  • Page 314 SECTION 9 - S UPPLEMENTS CESSNA MODEL 1 72S S U PPLE M E NT 5 APPROVED SUPPLEMENT 5 BENDIX/KING KLN 898 GLOBAL POSITIONING SYSTEM (IFR) The fol lowi ng Log of Effective Pages provides the date of issue for origi nal and revised pages, as well as a l isting of all pages i n the Supplement.
  • Page 315 CESSNA SECTION 9 S UPPLEMENTS MODEL 1 72S SUPPLEM E NT 5 APPROVED SUPPLEMENT 5 BENDIX/KING KLN 89B GLOBAL POSITIONING SYSTEM (IFR) SERVICE BULLETIN CONFIGURATION LIST The fol lowing is a list of Service Bulletins that are applicable to the operation of the airplane, and have been incorporated into this supplement.
  • Page 316 SECTION 9 - SUPPLE M E NTS CESSNA SUPPLE M E NT 5 FAA APPROVED MODEL 1 72S SUPPLEMENT BENDIX/KING KLN 89B GPS NAVIGATION SYSTEM (IFR) SECTION 1 GENERAL WARNING NOT AUTHORIZED I NSTRUME NT APPROACHES U N LESS REVISION...
  • Page 317 CESSNA SECTION 9 - SUPPLEMENTS MODEL 1 72S SUPPLEMENT - FAA APPROVED database card electronic memory containing information on airports, navaids, intersections, SIO's, STAR's, instrument approaches, special use airspace, and other items of interest to the pilot. Every 28 days, Bendix/King receives new d atabase information from Jeppesen Sanderson for the North American database region.
  • Page 318 SECTIO N 9 - SUPPLEMENTS CESSNA SUPPLEM E NT FAA APPROVED MODEL 1 72S NOTE Aircraft using G PS for oceanic I FR operations may use the KLN 898 to replace one of the other approved means of long range navigation . A single KLN 898 GPS i nstal lation may also be used on short oceanic routes which require only one means of long-range navigation.
  • Page 320 SECTION 9 - SUPPLEM E NTS C ES S NA SUPPLEMENT 5 - FAA APPROVED MODEL 1 72S WARNING TURN ANTICIPATION AUTOMATICALLY D ISABLED FOR FAF WAYPOINTS AND THOSE USED EXCLUSIVELY I N SID/STARS WHERE OVERFLIGHT I S REQUIRED. FOR WAYPOINTS SHARED B ETWEEN SID/STARS...
  • Page 321 CESSNA SECTION 9 - SUPPLEMENTS MODEL 1 725 SUPPLEMENT 5 - FAA APPROVED 6. NAV/GPS SWITCH -- Toggles from Nav 1 to G PS and vice versa to control the type of navigation data to be d isplayed on the COl (Course Deviation Indicator). The No.
  • Page 322 S ECTION 9 - S UPPLEMENTS CESSNA SUPPLEMENT 5 FAA APPROVE D MODEL 1 72S SECTION 2 LIMITATIONS 1 . The KLN 89B G PS Pilot's G uide, PIN 006-08786-0000, dated May, 1 995 (or later applicable revision) m ust be available to the flight crew whenever I FR G PS navigation is used.
  • Page 323 CESSNA S ECTION 9 - S UPPLEMENTS MODEL 1 72S S U PPLEMENT 5 - FAA APPROVED 3) APR ACTV mode m ust be ann unciated at the Final Approach Fix. 4) Accomplishment of I LS , LOC, LOC-BC, LOA, SDF, and M LS approaches are not authorized.
  • Page 324 SECTION 9 - SUPPLEMENTS CESSNA S UPPLEM E NT 5 - FAA APPROVED MODEL 1 72S The aircraft must have other approved navigation equipment appropriate to the route of flight i nstalled and operational . SECTION 3 EMERGENCY PROCEDURES There are no changes to the basic airplane emergency procedures when the KLN 898 GPS is installed.
  • Page 325 CESSNA S ECTION 9 - S UPPLEMENTS MODEL 1 72S SUPP LEME NT - FAA APPROVED WAR N I NG PREVENT T H E POSSIBILITY TURN ANTICIPATION CAUSING POTENTIALLY M ISLEADING NAVIGATION WHEN AIRCRAFT IS NOT ON COURSE, VERIFY T H E CDI...
  • Page 326 SECTION 9 SUPPLEME NTS CESSNA SUPPLE M E NT FAA APPROVED MODEL 1 72S APPROACH MODE SEQU ENCING AND RAI M PREDICTION WARNING FAM ILIARITY WITH THE E N ROUTE OPERATION OF THE KlN 89B Will NOT CONSTITUTE P ROFICIENCY APPROACH OPERATIONS.
  • Page 327 C ESSNA S ECTION 9 - SUPPLEMENTS MODEL 1 72S S U PPLEMENT FAA APPROVE D 2. En route, check for RAIM availability at t h e destination airport ETA on the OTH page. N OTE RAI M m ust be available at the FAF in order to fly an i nstrument approach.
  • Page 328 SECTION 9 - SUPPLEMENTS CESSNA SUPPLE M E NT FAA APPROVED MODEL 1 72S NOTE Select H OG mode for DME arc i ntercepts. NAV or APR cou pled DME arc intercepts can result in excessive overshoots (agg ravated by high ground speeds and/or i ntercepts from i nside the arc).
  • Page 329 C ESSNA SECTION 9 S UPPLEM E NTS MODEL 1 72S S U PPLEMENT FAA APPROVED 8. M issed Approach: a. Clim b . b. Navigate to the MAP (in APRARM if APR ACTV is not available). NOTE There is no automatic LEG sequencing at the MAP. c.
  • Page 330 SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT - FAA APPROVED MODEL 1 72S e Waypoint suffixes i n the flight plan: i -- f -- m -- MAP h -- missed approach holding fix. eThe DME arc IAF (arc intercept waypoint) will be on your present...
  • Page 331 CESSNA SECTION 9 S U PPLEMENTS MODEL 1 72S S U PPLEMENT 5 APPROVED The i nstrument approach using the KLN 898 may be essentially automatically started 30 nm out (with a manual baro setting u pdate) or it may require judicious selection of the OBS and LEG modes.
  • Page 333 Direction Finder is instal/ed. FAA APPROVAL f1lAA APPROveO UNDER FAR 21 SUBPART J Aircreft Co The Cess n a ce·, 2000 Member of GAMA 8 July 1998 COPYRIGHT c 1998 Revision 1 30 May 2000 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA 86-1 172SPHUS·Se·01...
  • Page 334 S ECTION 9 - SUPPLEMENTS CESSNA S U PPLEM E NT 6 - APPROVED MODEL 1 72S BENDIX/KING KR 87 AUTOMATIC DIRECTION FINDER (ADF) The following Log of Effective Pages provides the date of issue f or original and revised pages, as well as a listing of all pages i n the Supplement.
  • Page 335 C ESSNA S ECTION 9 - SUPPLEMENTS MODEL 1 72S S U PPLEMENT 6 - FAA APPROVED BENDIX/KING KR 87 AUTOMATIC DIRECTION FINDER (ADF) SECTION 1 GENERAL The Bendix/King Digital ADF is a panel-mounted, digitally tuned automatic d i rection finder . It is designed to provide contin uous 1 - kHz digital tuni ng i n the frequency range of 200-kHz to 1 799-kHz and elim inates the need for mechanical band switching.
  • Page 336 SECTION 9 - S U PPLEMENTS CESSNA S UPPLEMENT 6 FAA APPROVED MODEL 1 72S K R87 TSO A D F 0585C1 043 0585C1 044 Figure 1 . KR 87 Automatic Direction Finder (ADF) (Sheet 1 of 4) 86-4 July 8/98...
  • Page 337 CESSNA S ECTION 9 - SUPPLEMENTS MODEL 1 72S SUPPLE MENT 6 - FAA APPROVED 1 . ANT/ADF M ODE ANNUNCIATOR -- Antenna (ANT) is selected by the "out" position of the ADF button . This mode i mproves the audio reception and is usually used for station identification.
  • Page 338 SECTIO N 9 - SUPPLEMENTS CESSNA SUPPLEM E NT - FAA APPROVED MODEL 1 72S FLIGHT TIM E R E LAPSE D TIM E R MODE ANNU NCIATION -- Either the elapsed time ( ET) or flight time (FL T) mode is annunciated here.
  • Page 339 CES S NA SECTION 9 - SUPPLEMENTS MODEL 1 72S SUPPLEME NT 6 - FAA APPROVED 1 0. FREQUEN CY TRANSFER BUTTON (FRQ) -- The FRQ transfer button when pressed exchanges the active and standby frequencies. The new frequency becomes active an d the former active frequency goes into standby.
  • Page 340 SECTION 9 - S UPPLEM ENTS C ESSNA SUPPLEMENT 6 - FAA APPROVED MODEL 1 728 SECTION 2 LIMITATIONS There is no change to airplane l i mitations when the KR is installed. SECTION 3 EMERGENCY PROCEDURES There are no changes to the basic airplane emergency procedures when the KR ADF is installed .
  • Page 341 CESSNA S ECTION 9 - S UPPLEM E NTS MODEL 1 72S SUPPLEMENT 6 - FAA APPROVED TO OPERATE BFO: OFFNOL Control -- ON. 2. BFO Button -- PRESS on. 3. ADF Selector Buttons (on audio control panel) -- S ET to desired mode.
  • Page 342 S ECTIO N 9 - SUPPLEMENTS CESSNA S U PPLEMENT 6 - FAA APPROVE D MODEL 1 72S TO OPERATE ELAPSED TIME TIMER-COUNT UP MODE: 1 . OFFNOL Control -- ON. 2. FLT/ET Mode Button -- PRESS (once or twice) u ntil ET is annunciated.
  • Page 343 CESSNA SECTION 9 S UPPLEM EN TS MODEL 1 72S S UPPLEM ENT 6 - FAA APPROVED ADF OPERATION N OTES: E RRONEOUS ADF BEARING DUE TO RADIO FREQU ENCY PHENOMENA: In the U.S., the FCC, which assigns AM radio frequencies, occasionally will assign the same frequency to more than one station in an area.
  • Page 344 SECTION 9 SUPPLEMENTS CESSNA SUP PLEM E NT 6 APPROVED MODEL 1 728 SECTION PERFORMANCE There is no change to the airplane performance when this avionic equipment is i nstalled. However, the installation of an external ly mounted antenna or related external antennas, may result i n a m inor reduction in cruise performance.
  • Page 345 ATextron Pilot's Operating Handbook and FAA Approved Airplane Flight Manual CESSNA MODEL 1725 AIRPLANES 172S8001 AND ON SUPPLE ENT 7 BENDIX/KING KAP 140 SINGLE AXIS AUTOPILOT SERIAL NO, REGISTRATION NO, This supplement must be inserted into Section of the Pilot's Operating...
  • Page 346 SECTION 9 - SUPPLEMENTS C ESSNA SUPPLEM E NT 7 - APPROVED MODEL 1 72S SUPPLEMENT 7 BENDIX/KING KAP 140 SINGLE AXIS AUTOPILOT The following Log of Effective Pages provides the date of issue for original and revised pages, as wel l as a l isting of all pages i n the Supplement.
  • Page 347 CESSNA S ECTION 9 - SUPPLEMENTS MODEL 1 72S SUPPLEME NT 7 - APPROVED SERVICE BULLETIN CONFIGURATION LIST The following is a l ist of Service Bulletins that are applicable to the operation of the airplane, and have been i ncorporated i nto this supplement.
  • Page 349 CESSNA SECTION 9 - S UPPLEME NTS MODEL 1 72S SUPPLEMENT 7 - APPROVED SUPPLE ENT BENDIX/KING KAP 140 SINGLE AXIS AUTOPILOT SECTION 1 GENERAL The Bendix/King KAP 1 40 is an all-electric, single-axis (aileronl control) autopilot system that provides lateral and directional control.
  • Page 350 S ECTION 9 - S U PPLEME NTS CESSNA SUPPLEMENT 7 APPROVED MODEL 1 72S The following circuit breakers are used to protect the listed elements of the KAP 1 40 single axis autopilot: LABEL FUNCTIONS AUTO Supplies power to the KC 1 40 P I LOT Computer and the autopilot.
  • Page 351 CESSNA SECTION - SUPPLEMENTS MODEL 172S SUPPLEMENT 7 - FAA APPROVED NAV/COMM 1 CONTROL PANEL HORIZONTAL SITUATION INDICATOR NAVIGATION SOURCE SELECTOR SWITCH CONTROL WHEEL TURN COORDINATOR CIRCUIT BREAKER 05851054 Figure 1 . Bendix/King KAP 140 Autopilot, Operating Controls and Indicators (Sheet 1 of 3)
  • Page 352 SECTION SUPPLEMENTS CESSNA SUPPLEMENT 7 - FAA APPROVED MODEL 1 72S 8SIJ/XIfrJ1S KAP 140 Hf>G 1 . ROLL (R) AXIS ANNUNCIATOR .. - When illuminated, indicates a failure in the roll axis and prevents engagement or disengages the autopilot. 2. AUTOPILOT ENGAGEIDISENGAGE (AP) BUTTON -- When pushed, engages autopilot if all preflight self test conditions are met.
  • Page 353 CESSNA SECTION 9 - SUPPLEMENTS MODEL 1 72S SUPPLEMENT 7 - FAA APPROVED 5. APPROACH (APR) MODE SELECTOR BUTTON -- When pushed, will select the Approach mode. This mode provides automatic beam capture and tracking of VOR, LOC, or GPS signals as selected for presentation on the NAV # 1 COl or HSI (if installed).
  • Page 354 SECTION SUPPLEMENTS CESSNA SUPPLEMENT 7 - FAA APPROVED MODEL 1 72S SECTION 2 LIMITATIONS The following autopilot limitations must be adhered to: 1 . The autopilot must be OFF during takeoff and landing. 2. During autopilot operation, the pilot, with seat belt fastened, must be seated in the left front seat.
  • Page 356 SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 7 - FAA APPROVED MODEL 1 72S Note that the emergency procedure for any malfunction is essen­ tially the same: immediately grasp the control wheel and regain air­ plane control while pressing and the holding the AlP DISC switch down.
  • Page 357 CESSNA SECTION 9 SUPPLEMENTS MODEL 172S SUPPLEMENT 7 - FAA APPROVED 3. Loss of the Directional Gyro (DG) -- The directional gyro does not provide any system valid flag. If the DG fails to function properly the autopilot heading and navigation mode will no function correctly.
  • Page 358 SECTION 9 SUPPLEMENTS CESSNA SUPPLEMENT 7 - FAA APPROVED MODEL 1 72S 6. AlP DISC Switch -- PRESS. Verify that the autopilot disconnects and tone sounds. BEFORE TAKEOFF: Autopilot -- OFF. AUTOPILOT ENGAGEMENT: 1 . AP Button -- PRESS. Note ROL annunciator on. If no other modes are selected the autopilot will operate in the ROL mode.
  • Page 359 CESSNA SECTION 9 SUPPLEMENTS MODEL 172S FAA APPROVED SUPPLEMENT 7 c. Heading Selector Knob -- to agree with ROTATE BUG course. NOTE When NAV is selected, the autopilot will flash HOG for 5 seconds to remind the pilot to reset the HOG bug to the OBS course.
  • Page 360 SECTION 9 SUPPLEMENTS CESSNA SUPPLEMENT 7 - FAA APPROVED MODEL 172S 2) If the D -Bar is less than 2 to 3 dots: the HOG mode will disengage upon selecting NAV mode; the annunciator will illuminate capture/track sequence will automatically begin.
  • Page 361 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 7 - FAA APPROVED 2) If the D-Bar is less than 2 to 3 dots: the HDG mode will dis­ engage upon selecting APR mode; the annunciator will illuminate and the capture/track sequence will automati­...
  • Page 362 SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 7 - FAA APPROVED MODEL 172S 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. If...
  • Page 363 CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 7 - FAA APPROVED 2) If the D-Bar is less than 2 to 3 dots: the HDG mode will dis­ engage upon selecting mode; the annunciator will illuminate and the capture/track sequence will automati­...
  • Page 365 Handbook and FAA Approved Airplane Flight Manual when the Winterization Kit is installed. FAA APPROVAL PAA APPROVeO UNDER FAR SUBPART J The Cessna Aircraft CEo 1 ExtC#lJtivo Engineer Member of GAMA 8 July 1998 © COPYRIGHT 1998 CESSNA AIRCRAFT COMPANY 88-1 WICHITA, KANSAS, USA 172SPHUS·S8·QQ...
  • Page 366 S ECTION 9 - SU PPL EM E NTS C ESSNA SUPPLEMENT 8 - FAA APPROVED MODEL 1 72S SU P P LE M E NT 8 W I NT E R IZATION KIT 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 S upplement.
  • Page 367 CESSNA S ECTION 9 S UPPLEM ENTS MODEL 1 72S S U PPLEM ENT 8 FAA APPROVED S U P P LE M E NT WINTE RIZATION KIT S E CTION 1 G E N E RAL The winterization kit consists o f two cover plates (with placards)
  • Page 368 SECTION 9 SUPPL EM E NTS C ESSNA SUP PL E M ENT 8 FAA A PP ROVED MODEL 1 72S S E CTION 3 E M E R G E N CY P R OC E D U R ES There is no change to the airp lane emergency procedures when the winterization kit is installed.
  • Page 369 Approved Airplane Flight Manual when Davtron Clock/O.A.T. is installed. FAA APPROVAL PAA APPROVeO UNDER FAR SUBPART J Cessna Aircraft exteutivo Engineer 1998 Member of GAMA 8 July 1 998 © COPYRIGHT 1998 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA 89-1 172SPHU8-S9-00...
  • Page 370 SECTION 9 - S U P PL EM E NTS CESSNA MODEL 1 72S SUPPLEM ENT 9 - FAA APPROVE D S U P P L E M E NT 9 DAVT R ON M OD E L 803 C LOCK/O.A.T.
  • Page 371 CESSNA S ECTION 9 S U PPL EM ENTS MODEL 1 72S SU PPL E M ENT 9 FAA APPROVED M NT s u pp DIGITAL C LOCK/O.A.T. S E CTION 1 G E N E RA L The Davtron Model 803 digital clock combines the features of a clock, outside air temperature gauge (O.A.T.) and voltmeter in a...
  • Page 372 SECTION 9 S U PPL EMENTS CESSNA SU PPLEM ENT 9 FAA APPROVED MODEL 1 72S UPPER BUTTON UPPER LCD WINDOW LOWER L C WINDOW 078SC100S SELEC CONTROL BUTTON BUTTON Figure 1 . Clock/OAT Gauge S E CTION 4 N OR M A L P R OC E D U R ES...
  • Page 373 C ESSNA S ECTION 9 SU PPL EM ENTS MODEL 1 72S S UP PL E M ENT 9 FAA APPROVED C L O C K O P ERATIONS The lower portion of the LCD window is dedicated to clock and timing operations.
  • Page 374 SECTION 9 SU PPL EM E NTS C ESSNA SUPPL E M E NT 9 FAA A PP ROVED M O D EL 1 72S SETTIN G FLI G HT TI M E FLASH I N G ALARM S EL ECT button select flight...
  • Page 375 Handbook and FAA Approved Airplane Flight Manual when the Global POSitioning System is installed. FAA APPROVAL 'AAAPPROveOUNDERFAR21SUBPARTJ Cessna AirCfaft Co EncIllivo E/lil llll ' Date: 27 June 2000 Member of GAM 8 July 1998 COPYRIGHT 11:>1998 CESSNA AIRCRAFT COMPANY Revision 1 30 May 2000 WICHITA, KANSAS, USA 810-1 172SPHUS-S10-01...
  • Page 376 SECTION 9 - SUPPLEMENTS CESSNA FAA APPROVED MODEL 172S SUPPLEMENT 10 SUPPLEMENT 10 BENDIX/KING KlN 89 IVFR GLOBAL POSITIONING SYSTEM (GPS) 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 377 CESSNA SECTION 9 UPPLEMENTS MODEL 172S SUPPLEMENT 10 - FAA APPROVED SUPPLEMENT BENDIX/KING KLN 89 VFR GLOBAL POSITIONING SYSTEM (GPS) SECTION 1 GENERAL The Bendix/King KLN 8 9 is a navigation system based on the Global Positioning Satellite network. It contains a database cartridge which may be updated by subscription.
  • Page 378 SECTION 9 - SUPPLEMENTS CESSNA FAA APPROVED SUPPLEMENT 10 MODEL 172S SECTION NORMAL PROCEDURES There is no change to basic airplane normal operating procedures with the KLN 8 9 GPS installed. SECTION 5 PERFORMANCE There is no change to the airplane performance when the KLN 8 9 GPS is installed.
  • Page 379 Handbook and FAA Approved Airplane Flight Manual when used for Canadian Operation. FAA APPROVAL J!AA APPROveo UNDER FAR 21 SUBPART The Cessna Aircraft Executivo Ens,""r Member of GAMA 8 July 1 998 © COPYRIGHT 1998 CESSNA AIRCRAFT COMPANY S12-1 WICHITA, KANSAS, USA 172SPHUS-S 12-00...
  • Page 380 SECTIO N 9 - SUPPLEM E NTS C ESSNA MODEL 1 728 SUPPLEM ENT 1 2 - FAA APPROVED S U P P LE M E N T 1 2 CANADIAN S U PP L E M E NT The fol lowin g Log of Effective Pages provides the date of issue for original and revised pages, as well as a l isting of all pages in the Supplement.
  • Page 381 S U P PL E M E NT CANADIAN S U P P L E M E NT S E CTION 1 G E N E RA L This supplement i s required for Canadian operation of Cessna Model 1 72S. S ECTION 2 LIM ITATIONS The following placard m ust be installed .
  • Page 382 SECTION 9 - SU PPLEM E NTS C ESSNA SUPPLEME NT 1 2 - FAA APPROVED M OD EL 172S S E CTION 3 E M E R G ENCY P R O C E D U R ES There is no change to the airplane emergency procedu res when used for Canadian operation.
  • Page 383 Handbook and FAA Approved Airplane Flight Manual when Horizontal Situation Indicator is installed, FAA APPROVAL 'AA APPROveO UNDER FAR 21 SUBPART J Cessna Aircraft Co ex.cutMtEn8InHf 2000 Member of GAMA 1999 January COPYRIGHT (l 1999 CESSNA AIRCRAFT COMPANY Revision 1 30 May 2000 WICHITA, KANSAS, USA 813-1 172SPHUS-S13-01...
  • Page 384 SECTION 9 - SUPPLEMENTS CESSNA FAA APPROVED SUPPLEMENT 13 MODEL 172S SUPPLEMENT 13 BENDIX/KI NG KCS .. 55A SLAVED COMPASS SYSTEM WITH KI-525A HORIZONTAL SITUATION I NDICATOR (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 385 CESSNA SECTION 9 SUPPLEMENTS MODEL 172S SUPPLEMENT 13 - FAA APPROVED SUPPLEMENT 13 B ENDIX/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. The...
  • Page 386 SECTION 9 - SUPPLEMENTS CESSNA MODEL 172S SUPPLEMENT 1 3 - FAA APPROVED Figure 1. Horizontal Situation Indicator System (Sheet 1 of 2) 1. HORIZONTAL SITUATION INDICATOR ( HSI) -- Provides a pictorial presentation of aircraft deviation relative to VOR/GPS radials and localizer beams.
  • Page 387 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 388 SECTION 9 - SUPPLEMENTS CESSNA MODEL 172S SUPPLEMENT 13 - FAA APPROVED 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 (FREE/SLAVE) COMPASS SLAVE SWITCH -- Selects either the manual or automatic slaving mode for the Compass System.
  • Page 389 CESSNA SECTION 9 - SUPPLEMENTS FAA APPROVED MODEL 172S SUPPLEMENT 1 3 SECTION 2 LIMITATIONS There is no change to the airplane limitations when this instrument is installed. SECTION 3 E MERGENCY PROCEDURES There is no change to the airplane emergency procedures when this instrument is installed.
  • Page 390 SUPP L EMENTS SECTION 9 CESSNA SUPPLEMENT FAA APPROVED MODEL 172S 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.
  • Page 391 Handbook and FAA Approved Airplane Flight Manual when the KAP Axis Autopilot System is installed. FAA APPROVAL I'AA Af'PROVEO UNDER FAR 21 SUBPART J The Cessna Aircraft Co Date: 28 December 1999 Member of GAMA 28 December 1999 COPYRIGHT © 1999...
  • Page 392 S ECTION 9 - SU PPLEM ENTS C ESSNA MOD EL 1 72S SU PPLE M E NT 1 5 - FAA A P P ROVED SUPPLEMENT B E N DIX/KI N G KAP 1 40 2 AXIS AUTO P I LOT U se the Log of Effective Pages to determine the current status of this supplement.
  • Page 393 S ECTION 9 - SU PPLEM ENTS C ESSNA S U P P L E M E NT 1 5 - FAA APPROVED MODEL 1 72S SUPPLEMENT B E N D IX/KI N G KAP 1 40 2 AXIS A U TO P I LOT S E RVIC E B U L LETI N C O N FI G U RATIO N LIST The fol lowing is a list of Service Bulletins that are applicable to the operation of the airplane, and have been incorporated into this...
  • Page 395 C ESSNA S ECTION 9 S U PPLEME NTS MODEL 1 72S S U P P L E M E NT 1 5 - FAA APP ROVED SUPPLEMENT BE N DIX/K I N G KAP 1 40 2 AXIS AUTO P I LOT S ECTI O N 1 G EN E RAL The KAP 1 40, 2 Axis Autopilot provides the pilot with the fol lowing...
  • Page 396 S ECTION 9 - SU P P LE M E NTS C ESSNA MOD E L 1 72S SU P P L E M E NT 1 5 - FAA APPROVE D C. Pitch accelerations i n excess of + 1 . 4g or less than +0.6g only when produced by a failure causing servo runaway.
  • Page 397 C ESSNA S ECTION 9 S U PPLEM ENTS MODEL 1 72S S U PPLEMENT 1 5 - FAA APPROVED NAV/COMM 1 r - - - - .:1!t5g 123.0D 1 nbD l1li' 1I!!,o ;Ji NAVIGATION r - - - - ..J S ELECTOR SWITCH E LEVATOR AND...
  • Page 398 S ECTION 9 - SU P PLEM ENTS C ESSNA MODEL 1 72S S U PPLEM ENT 1 5 - FAA APPROVE D 1 8** BENDIX KING KAP 1 40 WITHOUT ALTITU DE PRES ELECT 1 40 1 . P ITCH AXI S ( P) AN N U NC IATOR...
  • Page 399 C ESSNA S ECTION 9 - S U P PLEM ENTS MOD E L 1 72S S U PPLEM E NT 1 5 - FAA APPROVED 4. H EAD ING ( H OG) MODE SELECTOR B UTTON -- When pushed, wil l 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 H S I (if i nstalled).
  • Page 400 S ECTION 9 - S U P PL E M E NTS C ESSNA S U PPLEM E NT 1 5 - FAA APPROVED MODEL 1 72S 9. VERTICAL S P E ED ( U P/ON) MOD E BUTTONS -- The action of these buttons depends on the vertical mode present when pressed .
  • Page 401 C ESSNA SECTION 9 - S U PPLEMENTS MODEL 1 72S S U P P LE M E NT 1 5 - FAA APPROVED 1 4. O M N I B EARING SELECT (OBS) KNOB -- Selects the des i red course to be tracked by the autopilot. (Note: The H OG bug must also be positioned to the proper cou rse to captu re and track the selected radial or desired track) .
  • Page 402 S ECTION 9 - SU PPLEM ENTS C ESSNA S U PPLEM E NT 1 5 - FAA A P PROVED MOD EL 1 72S BENDIX/KING U I\. r: I AP I n . KAP 140 T .." v LJ il L.
  • Page 403 C ESSNA S ECTION 9 S U PPLEM ENTS MODEL 1 72S S U P P L E M E NT 1 5 - FAA APPROVED 3 . ALTIT U D E ARM (ARM) BUTTON -- When pushed , wil l toggle altitude arm ing on or off.
  • Page 404 S ECTION 9 - SU PPLEM ENTS C ESSNA S U PPLEM ENT 1 5 - FAA A P P ROVED MODEL 1 72S S E CTIO N 2 LIMITATIONS The following autopilot l i m itations m ust be adhered to: 1 .
  • Page 405 C ESSNA S ECTION 9 - S U P PLEM E NTS MOD E L 1 72S S U P P L E M E NT 1 5 - FAA APPROVED S E CTIO N 3 EMERG E N CY P R OC E D U R ES The four step procedure listed under paragraph A should be among the basic airplane emergency procedures that are committed to memory.
  • Page 406 S ECTION 9 SU PPLEM E NTS C ESSNA S U P PLEM ENT 1 5 - FAA APPROVED MOD EL 1 72S AMPLI FIED EMERG ENCY PROCEDURES The following paragraphs are presented to supply additional i nformation for the purpose of providi ng the pilot with a more complete understanding of the recommended cou rse of action for an emergency situation.
  • Page 407 C ESSNA S ECTION 9 - SU PPLEMENTS MODEL 1 72S S U P P L E M E NT 1 5 - FAA APPROVED 3 . Note that the emergency proced u re for any malfu nction is essential ly the sam e : i m mediately g rasp the control wheel and regain airplane control while pressi ng and holding the NP DISCITR I M INT switch down , and retrim the airplane as...
  • Page 408 S ECTION 9 - SU P PLEM ENTS C ESSNA S U P P L E M E NT 1 5 - FAA APPROVE D MOD EL 1 72S - G RASP 2. If annunciation continues , Airplane Control Wheel FIRMLY, disengage the autopilot and check for an out of pitch trim condition.
  • Page 409 C ESSNA S ECTI O N 9 - S U P PLEMENTS MODEL 1 72S S U P P L E M E NT 1 5 - FAA APPROVED 3. Flashing GS -- I ndication of a flagged g lideslope. (GS will rearm automatically if a valid GS signal is received.
  • Page 410 S ECTION 9 - S U P P L E M E NTS C ESSNA S U PPLEM E NT 1 5 - FAA A P P ROVED MODEL 1 72S NOTE The followi ng procedures apply to airplane serials 1 72S800 1 thru 1 72S9 1 29 i ncorporating Honeywell Service Bulletin KC1 40-M 1 , and serials 1 72S9 1 30 and on.
  • Page 411 C ESSNA S ECTION 9 - SU PPLEM E NTS MODEL 1 72S S U P P L E M E NT 1 5 - FAA APPROVED NOTE Upon applying power to the autopilot, the red P warni ng on the face of the autopilot may illuminate indicating that the pitch axis cannot be engaged.
  • Page 412 S ECTION 9 - S U P P L E M E NTS C ESSNA S U P PLEM E NT 1 5 - FAA A P P ROVED MOD EL 1 72S NOTE If red R" light is not observed after holding RH switch for 5 seconds, the trim monitor system has failed.
  • Page 413 C ESSNA S ECTION 9 - SU PPLEM ENTS · MODEL 1 72S S U P P LE M E NT 1 5 - FAA APPROVED 4. FLASHING BARO SETTING (if installed) -- SET proper baro setting manually (or press BARO to accept the present value). 5.
  • Page 414 S ECTION 9 - SU P PLEM ENTS C ESSNA S U PPLEM ENT 1 5 - FAA AP P ROVED MOD E L 1 72S NOTE Autopilot tracking performance will deg raded turbulence. 1 . B E FO R E TAKEOFF: a.
  • Page 415 C ESSNA S ECTION 9 - S U PPLEMENTS : MODEL 1 72S S U P PLEM E NT 1 5 - FAA APPROVED NOTE Avoid autopilot engagement into a climb condition that either cannot be maintained, or is on the perform ance limits of the airplane for its power and weight configuration.
  • Page 416 S ECTION 9 - SU PPLEM ENTS C ESSNA S U PPLE M E NT 1 5 - FAA AP P ROVED MOD EL 1 72S 3. CLI M B OR D ESCE NT: a. BARO setting (if installed) -- CHECK. b.
  • Page 417 C ESSNA S ECTION 9 S U PPLEM ENTS MOD E L 1 72S S U P P L E M E NT 1 5 - FAA APPROVED NOTE Altitude preselect captures are not recommended on non precision approaches to capture the M DA. Glideslope coupling will preclude a preselect altitude capture on an I LS.
  • Page 418 S ECTION 9 - SU PPLEM ENTS CESSNA S U P P LEM ENT 1 5 - FAA APPROVED MODEL 1 72S 5. H EADING HOLD : SET BUG to desired heading. a. Heading Selector Knob b. H OG Mode Selector Button - P R ESS.
  • Page 419 C ESSNA S ECTION 9 - S U P PLEM ENTS MODEL 1 72S S U PPLEM ENT 1 5 - FAA A P PROVED NOTE All angle intercepts compatible with radar vectors may be accomplished by selecting ROL mode PRIOR to pressing the NAV button.
  • Page 420 S ECTION 9 SU P P LE M E NTS C ESSNA S U PPLEM ENT 1 5 - FAA A P P ROVE D MODEL 1 72S 7. APP ROACH (APR) COU PLING : enable glideslope coupling on an I LS and more precise tracking on instru ment approaches) .
  • Page 421 C ESSNA S ECTION 9 - SU PPLEM ENTS MOD E L 1 72S S U P PL E M E NT 1 5 - FAA APPROVED b. When equipped with H S I : 1 ) BARO Setting ( i f installed) - - CHECK. SET to desired cou rse.
  • Page 422 S ECTION 9 - S U PPLEM E NTS C ESSNA S U P PLEM ENT 1 5 - FAA APPROVE D MOD EL 1 72S NOTE When R EV is selected , the autopilot will flash H OG for 5 seconds to remind the pilot to reset the H OG bug to the localizer FRONT COU RS E I NBOU N D heading.
  • Page 423 C ESSNA S ECTION 9 - SU PPLEME NTS MOD EL 1 72S SU PPLEMENT 1 5 - FAA APPROVED a) If the D-Bar is g reater than 2 to 3 dots from center, the autopi lot wil l annunciate REV when the ARM ;...
  • Page 424 S ECTION 9 - SU PPLEM ENTS C ESSNA S U P PLEM E NT 1 5 - FAA APPROVE D MODEL 1 72S 1 0. M ISS E D APP ROACH a. AlP DISCITRIM INTER Switch - PRESS to d isengage AP. b.
  • Page 425 P i l ot's O perat i n g H a n d book a n d FAA Approved A i rplane Fli g ht Man ual CESSNA M O D E L 1 72S A I R PLANES 1 7258372...
  • Page 426 SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 1 9 - FAA APPROVED MODEL 1 728 S U P P L E' M E NT 1 9 B ENDIX/KING KLN 94 GLO BAL POSITIONING SYSTEM ( I F R) 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 427 CESSNA SECTION 9 - SUPPLEMENTS MODEL 1 72S SUPPLEMENT 1 9 - FAA APPROVED M E NT 1 B E N D IX/KIN G K L N 94 G LO BA L POSITI O N I N G SYST E M (I F R)
  • Page 428 C ESSNA SECTION 9 - SUPPLEMENTS SUPPLEMENT 1 9 - FAA APPROVED MODEL 1 72S S U P PL E M E NT B ENDIX/KING KlN 94 GLOB AL POSITIONING SYST E M (IFR) S E CTION G EN ER AL The KLN 94 G PS (Global Positioning System) is a three­...
  • Page 429 C ESSNA S ECTIO N 9 - SUPPLEM ENTS MODEL 1 72S S U PPLE M E NT 1 9 - FAA APPROVED database card e lectronic memory contain ing information on airports, navaids, intersections, D P's, STAR's, instrument approaches, special use airspace, and other items of interest to the pilot.
  • Page 430 SECTIO N 9 - SUPPLE M E NTS C ESSNA SUPPLE M E NT 1 9 - FAA APPROVED MODEL 1 72S NOTE Aircraft using G PS for oceanic I FR operations m ay use the KLN 94 to replace one of the other approved m eans of long ran ge navigation.
  • Page 431 CESSNA SECTIO N 9 - S U PPLEM ENTS MODEL 1 72S SUPPLE M E NT 1 9 - FAA APPROVED 0585C1 042 1 . G PS M ESSAG E (MSG) ANNUNCIATOR LIG HT -- MSG will begin flashing whenever the message p rompt (a large "...
  • Page 432 C ESSNA S ECTION 9 SUPPLEMENTS SU PPLEMENT 1 9 FAA APPROVE D MODEL 1 728 WARN I NG TURN ANTIC IPATION AUTOMATICALLY DISABLED FOR FAF WAYPOINTS AND THOSE USED EXCLUSIVELY DP/STARS WHERE OVERFLI G HT IS REQUIRED. FOR WAYPOINTS SHARED B ETWEEN DP/STARS AND PUBLISHED SEGMENTS R OUTE...
  • Page 433 C ESSNA SECTION 9 - SUPPLEMENTS MODEL 1 72S SUPPLEM ENT 1 9 - FAA APPROVED 6. NAV/GPS SWITCH -- Toggles from Nav 1 to G PS and vice versa to control the type of navigation data to be displayed on the C O l (Cou rse Deviation Indicator).
  • Page 434 CESSNA SECTIO N 9 - SUPPLEMENTS MODEL 1 72S SUPPLE M ENT 1 9 - FAA APPROV E D 1 __ G PS 1 . HSI ANN U NCIATOR LIGHT -- This label is present when the optional HSI is installed.
  • Page 435 C ESSNA S ECTION 9 - SUPPLEM ENTS MODEL 1 72S SUPPLE M E NT 1 9 - FAA APPROVED N OTE Manual COl course centering in O BS mode using the control knob can be d ifficult, especially at long distances.
  • Page 436 SECTIO N 9 - S U PPLEMENTS C ESSNA MODEL 1 72S SU PPLE M E NT 1 9 - FAA APPROVED S E CTION 2 L I M ITATIONS 1 1 . The KLN 94 G PS Pilot's Guide, PIN 006-1 8207-0000, dated September 2000 (or later applicable revision) m ust be available to the flight crew whenever I FR G PS n avigation is used.
  • Page 437 CESSNA S ECTION 9 - SUPPLEM E NTS MODEL 1 72S SUPPLEM E NT 1 9 - FAA APPROVED 3) APR ACTV mode must be annunciated at the Final Ap­ proach Fix. 4) Accomplishment of I LS, LOC, LOC-BC, LDA, SDF, and M LS approaches are not authorized.
  • Page 438 SECTION 9 - SUPPLEMENTS C ESSNA SUPPLE M E NT 1 9 - FAA APPROVE D MODEL 1 72S N OTE Honeywell's Preflight, Version 2.0 or later comp uter based prediction p rogram may be used for the RAI M p rediction. Alternate methods should be submitted for approval in accordance with Advisory Circular AC90-96.
  • Page 439 CESSNA SECTION 9 S U PPLEM ENTS MODEL 1 72S SUPPLE M E NT 1 9 FAA APPROVED S ECTI O N 4 N O R MA L P R O C E D U R E S OPERATION Normal operating procedures are outlined in the KLN 9 4 G PS Pilot's G u ide, PIN 006- 1 8207-0000, dated September 2000 (or later applicable revision) .
  • Page 440 SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 1 9 - FAA APPROVED MODEL 1 72S N OTE The special use airspace alert will automatically be disabled prior to flying an instrument approach to reduce the potential for message congestion. 1 . Prior to arrival, select a STAR if appropriate from the page.
  • Page 441 CESSNA SECTION 9 - SUPPLEMENTS MODEL 1 72S SUPPLEMENT 1 9 - FAA APPROVED At or within nm from the airport: a. Verify automatic annunciation of APRARM. b. Note automatic COl needle scaling change from to ±1 .0 nm over the next seconds.
  • Page 442 CESSNA SECTION 9 - SUPPLEMENTS MODEL 1 72S SUPPLEMENT 1 9 - FAA APPROVED At or before 2 nm from the FAF inbound: a. Select the FAF as the active waypoint, if not accomplished already. b. Select LEG operation. Approaching the FAF inbound (within 2 nm): a.
  • Page 443 CESSNA SECTION 9 - SUPPLEMENTS MODEL 1 72S SUPPLEMENT 1 9 - FAA APPROVED GENERAL NOTES The aeronautical database m ust be up to date for instrument approach operation. Only approach can be in the flight plan at a time.
  • Page 444 SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 1 9 - FAA APPROVED MODEL 1 72S The DME arc IAF identifier may be unfamiliar. Example: D098G where 098 stands for the 0980 radial off the referenced VOR, and G is the seventh letter in the alphabet indicating a 7 DME arc.
  • Page 445 Section Pilot's Operating Handbook and FAA Approved Airplane Flight Manual. FAA APPROVAL Date: Janua ry 9, 2001 Member of GAMA 30 Dece m be r 2000 © COPYRIGHT 2000 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA 172SPHUS-S20-00 820-1...
  • Page 446 SECTION 9 - SUPPLEM E NTS C ESSNA SUPPLEM ENT 20 - FAA APPROVED MODEL 1 72S L E M E NT 20 B E N D IX/KI N G K M A 2 8 A U D I O S E L ECTO R PAN E L 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 447 C ESSNA SECTION 9 - S UPPLEME NTS MODEL 1 72S SUPPLEM ENT 20 - FAA APPROVED L E M NT B E N D I X/KIN G K M A 2 8 A U DI O S E L E CTOR PAN E L S E CTION 1 G E N E RA L The Bendix/Kin g KMA 2 8 Audio Selector Panel i s a combination...
  • Page 448 SECTION 9 - SUPPLEMENTS C ESSNA MODEL 1 72S SU PPLEM ENT 20 - FAA APPROVED N OTE 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 wil l lose one audio channel.
  • Page 449 CESSNA SECTION 9 SUPPLEM ENTS MODEL 1 72S SUPPLE M E NT 20 - FAA APPROVED 1 . MARKER BEACON ANNUNCIATOR LIG HTS -- The three-light marker beacon receiver built into the KMA gives a visual and aural signal when the ship's antenna passes over a 75 MHz beacon.
  • Page 450 SECTION 9 - S U PPLEME NTS C ESSNA SUPPLEMENT 20 - FAA APPROVED MODEL 1 72S 3. RECEIVE AUDIO S ELECT BUTTONS -- Push button audio selection is available for two Communications receivers (IICOM 1 11, IICOM 211), two Navigation receivers (IINAV 1 11 and IINAV 211), the internal Marker Beacon receiver (IIMKW), one DME, one ADF, one additional auxiliary receiver (IIAUXII) and a speaker amplifier (IISPRII).
  • Page 451 CESSNA S ECTION 9 - SU PPLEM ENTS MODEL 1 72S SUPPLE M E NT 20 - FAA APPROVED TELEPHONE MODE (TEL) - The telephone mode is not available on this installation. SPLIT MODE (COM 1 /2 OR COM 211 ) -- Moving the mic selector switch to COM 1 12 places the KMA 28 into "split mode".
  • Page 452 C ESSNA SECTION 9 S U PPLEME NTS MODEL 1 72S SUPPLE MENT 20 - FAA APPROVED 1 0. INTERCOM MODE SELECT (ISO-ALL-CREW) -- A three-position mode switch that allows the pilot to tailor the intercom function to best meet the current cockpit situation.
  • Page 453 C ESSNA SECTION 9 S U PPLEM ENTS MODEL 1 72S SUPPLEME NT 20 - FAA APPROVED 1 1 . VOLUM E CONTROUPOWER SWITCH/EMERGENCY OPERATION KNOB -- The KMA 28 unit is turned on and off by pushin I;J the volume knob.
  • Page 454 C ESSNA SECTION 9 SUPPLEMENTS SU PPLEMENT 20 - FAA APPROVED MODEL 1 72S S E CTION 2 L I M ITATIONS 1 . PUSH O FF/EMG operation is prohibited during normal operations. 2. Use of the Entertainment audio input (and PED) is prohibited during takeoff and landing.
  • Page 455 CESSNA SECTION 9 - SUPPLEM ENTS MODEL 1 72S SUPPLEMENT 20 - FAA APPROVED S E CTION 4 N O R MA L P R O C E D U R ES AUDIO CONTROL SYSTEM OPERATION : 1 . MIC Selector Switch .- Turn to desired transmitter.
  • Page 456 SECTION 9 S U PPLEME NTS C ESSNA SUPPLEME NT 20 - FAA APPROVED MODEL 1 72S N OTE Disconnect the audio cable from the Entertainment audio input jack whenever the PED is not in use. N OTE Passenger briefing should specify that Entertainment audio input (and PED) use is perm itted only during the enroute phase of flight.
  • Page 457 Handbook and FAA Approved Airplane Flight Manual when the KMD Multi­ Function Display is installed. FAA APPROVAL Date: Janua ry 9, 2001 Member of GAMA 3 0 Decem be r 2000 © COPYRIGHT 2000 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA 821 -1 172SPHUS-S21-00...
  • Page 458 SECTION 9 - SUPPLEMENTS C ESSNA SUPPLEMENT 21 - FAA APPROVED MODEL 1 72S S U P P L E M E NT 2 1 B E N D IX/KI N G K M D 550 M U l T I .. FU N CTION DISP LAY 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 459 C ESSNA SECTION 9 - SUPPLEM ENTS MODEL 1 72S SU PPLEM ENT 21 - FAA APPROVED S U P P LE M E NT B EN D IX/KI N G KM D 550 M U l TI ... F U N CTIO N D IS P LAY S ECTI O N 1 G E N E RA L WAR N I NG...
  • Page 460 C ESSNA SECTION 9 SUPPLEMENTS SUPPLE M E NT 21 - FAA APPROVE D MODEL 1 72S N OTE The KMD 550 is designed to be used as a supplemental navigation system . You should always carefully compare indications from you r KMO 550 unit with the information available from all other navigation sources including N OBis, VORis, OMEls, visual sightings, charts, etc.
  • Page 461 CESSNA SECTIO N 9 S U PPLEM ENTS MODEL 1 72S S U PPLE M E NT 21 - FAA APPROVE D 4 --H-I--Iu:J 1 .BRIG HTNESS CONTROL -- Clockwise rotation will increase the brightness of the d isplay. Counter-clockwise rotation decreases the display brightness.
  • Page 462 SECTION 9 SUPPLEMENTS C ESSNA SUPPLEMENT 21 - FAA APPROVED MODEL 1 72S 5. ON/OFF CONTROL -- Rotating clockwise to the nONn position provides power to the KMD 550. Rotating counter-clockwise to the nOFFn position removes power from the u nit. 6.
  • Page 463 CESSNA SECTION 9 - S UPPLEM ENTS MODEL 1 72S SUPPLEMENT 21 - FAA APPROVED OVL Y -- 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 available for overlay.
  • Page 464 SECTION - S UPPLEMENTS C ESSNA SU PPLEMENT 21 - FAA APPROVED MODEL 1 72S STARTUP DISPLAY This display will be seen after power-up. The 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 465 CESSNA SECTION 9 - SUPPLEMENTS MODEL 1 72S SUPPLEMENT 21 - FAA APPROVE D S ECTIO N 3 E M E R G E N CY P RO CE D U R ES There is no change to the airplane emergency procedures when the KMD MUlti-Function Display is installed.
  • Page 467 Handbook and FAA Approved Airplane Flight Manual when the Volt Cabin Power System is installed. FAA A P PROVAL Date: January 9, 2001 Member of GAMA 3 0 Dece m be r 2000 © COPYRIGHT 2000 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA 822- 1 172SPHUS-S22·00...
  • Page 468 SECTION 9 SUPPLEM ENTS CESSNA SU PPLE M E NT 22 - FAA APPROVED MODEL 1 72S S U P P LE M E NT 22 V O LT C A B I N POW E R SYST E M...
  • Page 469 C ESSNA SECTION 9 - SUPPLEM ENTS MODEL 1 72S SUPPLE M E NT 22 - FAA APPROVED S U P P LE M E NT 1 2 V O LT CAB I N POWE R SYST E M S E CTI O N 1 G E N E R A L The 1 2 Volt Cabin Power System provides passenger access to a fixed direct current (DC) voltage for powering portable electronic...
  • Page 470 SECTION 9 - S U PPLEMENTS C ESSNA SUPPLEME NT 22 - FAA APPROVED MODEL 1 72S R ELEASE BUTTON Figu re 2. Mating Plug The mating plug is a plastic 9-pin circular connector with a q uick disconnect push button release (Hypertronics D02PBMRTH-0025 or equivalent) (See Figure 2).
  • Page 471 CESSNA SECTIO N 9 - SUPPLEM ENTS MODEL 1 72S SU PPLE M ENT 22 - FAA APPROVED Power is supplied to the 1 2-volt Cabi n 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 "CABI N...
  • Page 472 SECTION 9 SUPPLEM E NTS C ESSNA SU PPLEME NT 22 - FAA A PPROV E D MODEL 1 72S S E CT I O N 4 N O RM A L P R OC E D U R ES The pilot m ust be familiar with the location of the 1 2 Volt Cabin Power System connector and with the operation of locking and release features common to the connector and power/adapter...
  • Page 473 CESSNA SECTION 9 SUPPLEM ENTS MODEL 1 72S SUPPLE M E NT 22 - FAA A PPROVED N OTE D u ring passenger briefing, it m ust be explained that use of the PED (portable e lectronic device) is not permitted during takeoffs and landings.
  • Page 475 A Textron Company Pilot's Operating Handbook and FAA Approved Ai rplane Fl ight Manual CESSNA MODEL 1725 AI R P LANES 1 72S9063 A N D ON S U PPLEMENT 24 ASTROTECH MODEL TC-2 C LOCKIOATNOLT INDICATOR SERIAL NO., REGISTRATION NO.
  • Page 476 S ECTION 9 - S UPPLEM ENTS C ESSNA S U PPLEMENT 24 - FAA APPROVED MODEL 1 72S S U P P L E M E NT 24 ASTROTECH MODEL TC-2 C lOCK/OATNO lT I N DI CATOR The following Log of Effective Pages provides the date of issue for original and revised pages, as well as a listing of all pages i n the Supplement.
  • Page 477 S ECTION 9 S UPPLEMENTS C ESSNA S UPPLEMENT 24 - FAA APPROVED MODEL 1 728 S U P P L E M ENT DIGITA L C LOCKIOATNOLT I N D I CATOR SECTION 1 GEN ERAL 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 478 S ECTION 9 - S UPPLEM E NTS C ESSNA S U PPLEM ENT 24 - FAA APPROVED MODEL 1 72S UPPER LCD WINDOW LOWER LCD WINDOW 0714R1028 Figure 1 . Astrotech Model TC-2 Clock/OAT Nolt Indicator 1 . OAT NOL T BUTTON - Volts are displayed at power up. When the button is pressed, the display switches to outside air temperature in OF.
  • Page 479 C ESSNA S ECTION 9 - S UP PLEM ENTS MODEL 1 72S S UPPLEMENT 24 - FAA APPROVED SECTION 2 LIMITATIONS There is no change to the airplane limitations when the digital clock/OAT/volt indicator is installed. SECTION 3 E M E R G E N CY PROC E D URES There is no change to the airplane emergency procedures when the clock/OAT/volt indicator is installed .
  • Page 480 S ECTION 9 S U P PLEM ENTS C ESSNA S UPPLEM ENT 24 FAA APPROVED MODEL 1 72S Press the S ET (RES ET) 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.
  • Page 481 Handbook and FAA Approved Airplane Flight Manual when the VHF NAV/COMM with Indicator Head is installed. FAA APPROVAL Dale: 31 January 2002 Member of GAMA 3 1 J a n u a ry 2002 COPYRIGHT " 2002 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA 825-1 172SPHUS·S25·00...
  • Page 482 S ECTI O N 9 - S U PPLEM ENTS CESSNA S U PP L E M E NT 25 APPROVED MODEL 1 72S S U P P L E M E N T 25 B E N DIX/KI N G KX 1 65A V H F NAV/CO M M...
  • Page 483 C ESSNA SECTION 9 - S U PPLEM E NTS MODEL 1 72S S U PPLE M E NT 25 - FAA APPROVED S U P PLE M E NT B E N DIX/KING KX 1 65A V H F NAV/C O M M S E CTIO N 1 G E N ERAL T h e...
  • Page 484 SECTION 9 S U P PLEMENTS C ESSNA MODEL 1 72S SU PPLEMENT 25 - FAA APPROVED The Com m portion incorporates an automatic squelch . override the automatic squelch, the Comm vol ume control knob is pulled out. Push the knob back i n to reactivate the automatic squelch .
  • Page 485 S ECTION 9 S U PP L E ME N TS C ES S NA � MODEL 1 72S S U P PLEMENT 25 - FAA APPROVED NAV F U N CTION DISPLAYS 83276 109. 50 � O 30 VO R M O D E : ACTIVE/BEAR I N G , C D I FORMAT 10�J.
  • Page 486 S ECTI O N 9 - S U PPLEMENTS C ESSNA SU PPLEMENT 25 - FAA APPROVED MODEL 1 72S 1 . OP ERATI N G COMM FREQUENCY D ISPLAY -- Disp lays COMM ACTIVE and COMM STAN DBY frequencies with a "T"...
  • Page 487 CESSNA S ECTI ON 9 - S U PPLEM E NTS S UP P L E M E NT 25 - FAA APPROVED MODEL 1 72S 6 . NAV/FREQU EN CY TRANSFER B U TTON I n terchanges the NAV ACTIVE and STAN DBY frequencies .
  • Page 488 S ECTION 9 - S U PPLEMENTS CESSNA S U P P L E M E NT 25 - FAA APPROVED MODEL 1 72S Another push of the mode button will cause the NAV display from ACTIVE/B EARI N G format ACTIVE/RADIAL format.
  • Page 489 S E CTION 9 - S U PP L E M E NTS CESS NA MODEL 1 72S S U PPLEM E NT 25 - FAA AP P ROVED 1 0. COMM FREQ U E N CY S ELECTO R KNOB (OUTER) -- The outer, larger selector knob is used to change the M Hz portion of the frequency display.
  • Page 490 S ECTION 9 S U PPLEM ENTS C E S S NA S U PPLEMENT 25 - FAA APPROVED M O D E L 1 72S 1 2. COMM F REQUE N CY TRAN S F E R B UTTON I nterchanges the frequ encies U S E STAN DBY...
  • Page 491 S ECTION 9 - S U P P L E M ENTS C ES S NA M O D EL 1 72S S U PPLEMENT 25 APPROVED - FAA S ECTION 3 E M E RG E N CY PROC E D URES There is no change to th e airplane emergency procedures when this avionic equipment is i nstalled .
  • Page 492 SECT I O N 9 - S U P PLEM ENTS C E S S NA S U PPLEM ENT 25 - FAA A P P ROVED MODEL 1 72 S NAVIGATION RECEIVER OPERATI O N : 1 . NAV F requency Selector Knobs - - SELECT desired operati ng frequency in "STBY"...
  • Page 493 CESSNA S ECTI ON 9 - S U P PLEM ENTS S U PP L E M E NT 25 - FAA APPROVED MODEL 1 72S The pilot may adjust two parameters i n the pilot configuration, the display minimum brig htness and sidetone volume leve l .
  • Page 495 WEIGHT & BALANCE AND INSTALLED EQUIPMENT DATA CESSNA AIRCRAFT COMPANY Company SINGLE ENGINE DIVISION A Textron SERIAL & REGISTRATION WEIGHT MOMENT MODEL 172S 172S9271 N5308A (Ibs) (in) (Ib-in) ( calculated) STANDARD EMPTY WEIGHT 1,663.2 40.719 67,724 INSTALLED EQUIPMENT Net Change from standard Aircraft ALTIMETER WITH 20 FT MARKING, DUAL WINDOW, 20000 FT 0.000...
  • Page 496 Airplane Order OPERATIONS CHANGE 1 SHIP TO INVOICE TO 172S9271 Domestic Single Engine Mkt. 319271 DATE CUSTOMER ORDER NO. MODEL Skyhawk SP 09-25-02 LOCK NO. ENGINE NUMBER FORElL.H. AFT/R.H. REGISTRATION SERIAL NO. 10-31-02 WfA- 172S9271 N5308A PROPELLER NUMBER FORElL.H. AFT/R.H. INSTALL EQUIPMENT AS FOLLOWS CHANGE DESCRIPTION...
  • Page 497 SIGNAL AEROSPACE PAGE COMMERCIAL AVIONICS SYSTEMS ATTACHMENT REPORT PRINTED 12/12/2002 CFINAL) 6:02:41 172S9271 A;rcra-Ft: ser;al# 172S9271 work order Number Cessna A;rcra-Ft: Type SEP172MD-2B same �/kc140-7703 package opt:;on DELIVERY Servos Un;t: Part: Se r; 801 Number Descr;pt:;on Number Number 0092 ANTENNA...
  • Page 498 LOAD DATA SHEET H.J.GREA YES AIRCRAFT TYPE: CESSNA 172S AIRCRAFT REG: VH�WGL AIRCRAFT LOADING SYSTEM: CESSNA 172S FLIGHT MANUAL DATE DATE of EXPIRY ISSUE AUTHORISED H.J.GREA YES A V58 21/02/2008 INDEFINITE (CAO 100.7) H J Greaves A V-58 WEIG HT...

This manual is also suitable for:

172s skyhawk

Table of Contents