Download
Share
Print this page
Cessna 172S Pilot Operating Handbook
  1. Manuals
  2. Brands
  3. Cessna Manuals
  4. Aircrafts
  5. 172S Skyhawk
  6. Pilot operating handbook
Cessna 172S Pilot Operating Handbook

Cessna 172S Pilot Operating Handbook

Hide thumbs Also See for 172S:

Advertisement

Quick Links

Download this manual
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

Advertisement

loading

Related Manuals for Cessna 172S

Summary of Contents for Cessna 172S

  • Page 1 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 3 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 4 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 5 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 7 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 8 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 9 A Textron Company Pilot's Operating Handbook and FAA Approved Airplane Flight Manual CESSNA MODEL 172S AIRPLANES 17258001 AND ON SUPPLEMENT 1 BENDIX/KING KX 155A VHF NAV/COMM with KI 208 or KI 209A INDICATOR HEAD SERIAL NO., REGISTRAT ION NO. This...
  • Page 10 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 11 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 12 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 13 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 14 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 15 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 16 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 17 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 18 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 19 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 20 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 21 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 22 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 23 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 25 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 26 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 27 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 28 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 29 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 30 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 31 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 32 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 33 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 35 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 36 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 37 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 38 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 39 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 40 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 41 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 42 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 43 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 45 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 46 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 47 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 48 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 49 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 50 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 51 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 52 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 55 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 56 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 57 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 58 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 59 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 60 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 62 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 63 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 64 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 65 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 66 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 67 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 68 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 69 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 70 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 71 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 72 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 73 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 75 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 76 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 77 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 78 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 79 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 80 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 81 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 82 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 83 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 84 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 85 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 86 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 87 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 88 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 89 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 91 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 92 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 93 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 94 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 95 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 96 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 98 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 99 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 100 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 101 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 102 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 103 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 104 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 105 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 107 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 108 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 109 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 110 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 111 Pilot's O p eratin g Hand book a n d FAA Approved Airplane Flig ht Manual CES S N A M O D E L 172S AIR P LA N ES 1 7258001 A N D O N S U P P L E M E NT 9 DAVTRON MODE L 803 C L OCK/O.A.T.
  • Page 112 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 113 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 114 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 115 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 116 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 117 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 118 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 119 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 120 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 121 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 122 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 123 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 124 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 125 A Textron Pilot's Operating Handbook and FAA Approved Airplane Flight Manual SSNA MODEL 172S AIRPLANES 17208113 AND ON SUPPLEMENT 13 BENDIX/KING KCS-55A SLAVED COMPASS SYSTEM WITH KI-525A HORIZONTAL SITUATION INDICATOR (HSI) SERIAL NO, REGISTRATION NO, This supplement must be inserted into Section...
  • Page 126 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 127 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 128 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 129 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 130 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 131 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 132 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 133 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 134 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 135 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 137 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 138 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 139 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 140 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 141 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 142 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 143 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 144 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 145 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 146 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 147 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 148 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 149 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 150 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 151 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 152 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 153 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 154 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 155 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 156 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 157 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 158 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 159 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 160 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 161 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 162 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 163 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 164 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 165 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 166 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 167 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 168 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 169 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 170 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 171 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 172 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 173 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 174 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 175 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 176 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 177 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 178 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 179 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 180 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 181 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 182 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 183 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 184 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 185 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 186 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 187 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 188 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 189 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 190 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 191 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 192 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 193 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 194 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 195 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 196 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 197 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 198 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 199 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 200 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 201 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 202 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 203 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 204 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 205 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 206 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 207 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 209 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 210 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 211 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 212 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 213 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 214 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 215 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 217 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 218 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 219 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 220 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 221 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 222 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 223 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 224 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 225 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 226 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 227 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 228 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 229 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 230 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 231 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 232 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 233 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 234 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 235 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 .

This manual is also suitable for:

172suslog10