Information Manual 172S NAV I/NAV II Skyhawk SP

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For Training Purposes Only For Training Purposes Only For Training Purposes Only CESSNA SECTION 9 MODEL 172S NAV I/NAV II SUPPLEMENTS KAP 140 AUTOPILOT U.S. LOG OF APPROVED SUPPLEMENTS NOTE It is the airplane owner's responsibility to make sure that he or she has the latest revision to each supplement of a Pilot's Operating Handbook, and the latest issued "Log Of Approved Supplements". this "Log Of Approved Supplements" was the latest version 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 Propeller Aircraft Customer Services at (316) 517-5800. (Continued Next Page) Supplement Number Name Revision Level Equipment Installed 1 Bendix/King KX 155A VHF NAV/ COMM with KI 208 or KI 209A Indicator Head 0 2 Bendix/King KT 76C Transponder with Blind Encoder 0 3 Bendix/King KMA 26 Audio Selector Panel 1 4 Pointer Model 3000-11 or Model 4000-11 Emergency Locator Transmitter (ELT) 2 5 Bendix/King KLN 89B Global Positioning System (IFR) 2 6 Bendix/King KR 87 Automatic Direction Finder (ADF) 1 7 Bendix/King KAP 140 Single Axis Autopilot 2 8 Winterization Kit 0 9 Davtron Model 803 Clock/OAT 0 10 Bendix/King KLN 89 VFR Global Positioning System (GPS) 1 11 Brazilian Certified Airplanes 0 8 May 2012 172SPHUSLOG-14 Log 1 For Training Purposes Only SECTION 9 CESSNA SUPPLEMENTS MODEL 172S NAV I/NAV II KAP 140 AUTOPILOT U.S. LOG OF APPROVED SUPPLEMENTS Supplement Number Name Revision Level Equipment Installed 12 Canadian Supplement 0 13 Bendix/King KCS-55A Slaved Compass System with KI-525A Horizontal Situation Indicator (HSI) 1 14 Argentine Certified Airplanes 0 15 Bendix/King KAP 140 2 Axis Autopilot 5 16 Bendix/King KT 73 Mode S Transponder 0 17 Reserved 18 Ukrainian Certified Airplanes 0 19 Bendix/King KLN 94 Global Positioning System (IFR) 4 20 Bendix/King KMA 28 Audio Selector Panel 0 21 Bendix/King KMD 550 Multi- Function Display 0 22 12 Volt Cabin Power System 0 23 Reserved 24 Astrotech Model TC-2 Clock/OAT/ Volt Indicator 0 25 Bendix/King KX 165A VHF NAV/ COMM 0 26 Bendix/King KDR 510 Flight Information Services (FIS) 0 8 May 2012 Log 2 172SPHUSLOG-13 For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training 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Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only U.S. CESSNA MODEL 172S NAV I/NAV II AVIONICS OPTION Serials 172S8001 thru 172S10431 SUPPLEMENT 11 BRAZILIAN CERTIFIED AIRPLANES This supplement must be inserted into Section 9 of the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual when used for Brazilian Certified Airplanes and is approved by the U.S. Federal Aviation Administration (FAA) on behalf of the “Agência Nacional de Aviação Civil” (ANAC) for Brazilian Registered Airplanes, in accordance with the “Regulamento Brasileiro de Homologação Aeronáutica” (RBHA) Part 21, Section 21.29. SERIAL NO. REGISTRATION NO. 172SPHUS-S11-00 COPYRIGHT © 2009 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA S11-1 8 JUNE 2009 For Training Purposes Only SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 11 MODEL 172S NAV I/NAV II U.S. FAA APPROVED SUPPLEMENT 11 BRAZILIAN CERTIFIED AIRPLANES Use the Log of Effective Pages to determine the current status of this supplement. Pages affected by the current revision are indicated by an asterisk (*) preceding the page number. LOG OF EFFECTIVE PAGES Supplement Status Date Original Issue 8 June 2009 Page Number Page Status Revision Number S11-1 thru S11-6 Original 0 172SPHUS-S11-01 S11-2 For Training Purposes Only CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S NAV I/NAV II SUPPLEMENT 11 U.S. FAA APPROVED SERVICE BULLETIN CONFIGURATION LIST The following is a list of Service Bulletins that are applicable to the operation of the airplane, and have been incorporated into this supplement. This list contains only those Service Bulletins that are currently active. Number Title Airplane Serial Effectivity Revision Incorporated Incorporated in Airplane 172SPHUS-S11-00 S11-3 For Training Purposes Only SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 11 MODEL 172S NAV I/NAV II U.S. FAA APPROVED GENERAL This supplement is required for Brazilian operation of Cessna Model 172S airplanes equipped with the Nav I/Nav II avionics option. OPERATING LIMITATIONS There is no change to the airplane operating limitations when used for Brazilian Certified Airplanes. EMERGENCY PROCEDURES There is no change to the airplane emergency procedures when used for Brazilian Certified Airplanes. NORMAL PROCEDURES There is no change to the airplane normal procedures when used for Brazilian Certified Airplanes. PERFORMANCE There is no change to the airplane performance when used for Brazilian Certified Airplanes. 172SPHUS-S11-00 S11-4 For Training Purposes Only CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S NAV I/NAV II SUPPLEMENT 11 U.S. FAA APPROVED LOG OF ANAC APPROVED SUPPLEMENTS The following list contains ANAC accepted supplements. Refer to Log of Approved Supplements in the basic Pilot's Operating Handbook and FAA Approved Airplane Flight Manual for revision status. (Continued Next Page) Supplement Number Name Equipment Installed 1 Bendix/King KX 155A VHF NAV/COMM with KI 208 or KI 209A Indicator Head _____________ 2 Bendix/King KT 76C Transponder with Blind Encoder _____________ 3 Bendix/King KMA 26 Audio Selector Panel _____________ 4 Pointer Model 3000-11 or Model 4000-11 Emergency Locator Transmitter (ELT) _____________ 5 Bendix/King KLN 89B Global Positioning System (GPS) _____________ 6 Bendix/King KR 87 Automatic Direction Finder (ADF) _____________ 7 Bendix/King KAP 140 Single Axis Autopilot _____________ 8 Winterization Kit _____________ 9 Davtron Model 803 Clock/OAT _____________ 10 Bendix/King KLN 89 Global Positioning System (GPS) _____________ 11 Brazilian Certified Airplanes _____________ 12 Reserved _____________ 13 Bendix/King KCS-55A Slaved Compass System with KI-525A Horizontal Situation Indicator (HSI) _____________ 14 Reserved _____________ 15 Bendix/King KAP 140 2 Axis Autopilot _____________ 16 Bendix/King KT 73 Mode S Transponder _____________ 17 Reserved _____________ 172SPHUS-S11-00 S11-5 For Training Purposes Only SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 11 MODEL 172S NAV I/NAV II U.S. FAA APPROVED LOG OF ANAC APPROVED SUPPLEMENTS Supplement Number Name Equipment Installed 18 Reserved _____________ 19 Bendix/King KLN 94 Global Positioning System _____________ 20 Bendix/King KMA 28 Audio Selector Panel _____________ 21 Bendix/King KMD 550 Multi-Function Display _____________ 22 12 Volt Cabin Power System _____________ 23 Reserved _____________ 24 Astrotech Model TC-2 Clock/OAT/Volt Indicator _____________ 25 Bendix/King KX 165A VHF NAV/COM _____________ 26 Bendix/King KDR 510 Flight Information Services (FIS) _____________ 172SPHUS-S11-00 S11-6 For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only U.S. CESSNA MODEL 172S SERIALS 172S8001 and On SUPPLEMENT 14 ARGENTINE CERTIFIED AIRPLANES This supplement must be inserted into Section 9 of the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual when used for Argentine Certified Airplanes. This Airplane Flight Manual Supplement is approved in accordance with Section 21.29 of DNAR 21 for Argentine registered airplanes and is approved by the US Federal Aviation Administration (FAA) on behalf of the Dirección Nacional de Aeronavegabilidad (D.N.A.). SERIAL NO. REGISTRATION NO. 172SPHUS-S14-00 COPYRIGHT © 2008 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA S14-1 8 SEPTEMBER 2008 For Training Purposes Only SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 14 MODEL 172S U.S. FAA APPROVED SUPPLEMENT 14 ARGENTINE CERTIFIED AIRPLANES Use the Log of Effective Pages to determine the current status of this supplement. Pages affected by the current revision are indicated by an asterisk (*) preceding the page number. LOG OF EFFECTIVE PAGES Supplement Status Date Original Issue 8 September 2008 Page Number Page Status Revision Number S14-1 thru S14-14 Original 0 172SPHUS-S14-00 S14-2 For Training Purposes Only CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 14 U.S. FAA APPROVED SERVICE BULLETIN CONFIGURATION LIST The following is a list of Service Bulletins that are applicable to the operation of the airplane, and have been incorporated into this supplement. This list contains only those Service Bulletins that are currently active. Number Title Airplane Serial Effectivity Revision Incorporated Incorporated in Airplane 172SPHUS-S14-00 S14-3 For Training Purposes Only SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 14 MODEL 172S U.S. FAA APPROVED GENERAL This supplement is required for Argentine operation of Cessna Model 172S airplanes. The information herein supplements the information of the basic Pilot's Operating Handbook and FAA Approved Airplane Flight Manual. For limitations, procedures and performance information not contained in the supplement, consult the basic FAA Approved Airplane Flight Manual. OPERATING LIMITATIONS GLOBAL POSITIONING SYSTEM (G.P.S.) If the GPS is installed: Pilot is not authorized to use the Global Positioning System (GPS) for precision approach and landing. EMERGENCY LOCATOR TRANSMITTER (E.L.T.) The Emergency Locator Transmitter (ELT) must comply with RAAC 91.207. KINDS OF OPERATIONS LIMITS The necessary equipment for the different kind of operations must comply with the applicable regulations for Argentina. 172SPHUS-S14-00 S14-4 For Training Purposes Only CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 14 U.S. FAA APPROVED PLACARDS The following information must be displayed in the form of composite or individual placards. 1. In full view of the pilot: (The "DAY-NIGHT-VFR-IFR" entry, shown on the example below, will vary as the airplane is equipped). (Continued Next Page) The markings and placards installed in this airplane contain operating limitations which must be complied with when operating this airplane in the Normal Category. Other operating limitations which must be complied with when operating this airplane in this category or in the Utility Category are contained in the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual. Normal Category - No acrobatic maneuvers, including spins, approved. Utility Category - No acrobatic maneuvers approved, except those listed in the Pilot's Operating Handbook. Baggage compartment and rear seat must not be occupied. Spin Recovery - Opposite rudder-forward elevator-neutralize controls. Flight into known icing conditions prohibited. This airplane is certified for the following flight operations as of date of original airworthiness certificate: DAY - NIGHT - VFR- IFR Las marcas y placas instaladas en este avión contienen limitaciones operativas que deben ser cumplidas al operar este avión en la Categoría Normal. En el Manual de Operaciones del Piloto y en el Manual de Vuelo del Avión aprobado por la DNA están contenidas otras limitaciones operativas que se deben cumplir al operar el avión en esta categoría o en la categoría utilitarios. Categoría Normal - No están aprobadas las maniobras acrobáticas, incluido tirabuzón. Categoría Utilitarios - No están aprobadas las maniobras acrobáticas, excepto aquellas que se encuentran en el Manual de Operaciones del Piloto. No se deben ocupar los compartimentos para equipaje ni los asientos traseros. Salida de tirabuzón - Timón contrario, elevador hacia delante, centrar los comandos. Está prohibido el vuelo en condiciones conocidas de formación de hielo. Este avión está certificado para las siguientes operaciones de vuelo a partir de la fecha del certificado de aeronavegabilidad original: DÍA - NOCHE - VFR- IFR 172SPHUS-S14-00 S14-5 For Training Purposes Only SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 14 MODEL 172S U.S. FAA APPROVED PLACARDS (Continued) 2. On the fuel selector valve: (Continued Next Page) DESPEGUE AMBOS TODAS LAS ALTITUDES ATERRIZAJE 200 LTS. DE VUELO SELECTOR DE COMBUSTIBLE IZQUIERDA DERECHA 100 LTS. 100 LTS. VUELO HORIZONTAL VUELO HORIZONTAL SOLAMENTE SOLAMENTE 172SPHUS-S14-00 S14-6 For Training Purposes Only CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 14 U.S. FAA APPROVED PLACARDS (Continued) 3. Near both fuel tank filler caps: 4. On flap control indicator: (Continued Next Page) FUEL 100LL/100 MIN. GRADE AVIATION GASOLINE CAP. 26.5 U.S. GAL. USABLE CAP. 17.5 U.S. GAL. USABLE TO BOTTOM OF FILLER INDICATOR TAB. NAFTA DE AVIACIÓN GRADO 100LL/100 MIN. CAP. 100 LTS (26.5 GALONES ESTADOUNIDENSES) CAP. UTILIZABLE DE 66 LTS (17.5 GALONES ESTADOUNIDENSES) UTILIZABLE HASTA LA PARTE INFERIOR DE LA ALETA INDICADORA DE LLENADO. 0o to 10o 110 KIAS (Partial flap range with blue color code; also, mechanical detent at 10o.) 10o to 30o 85 KIAS (White color code; also, mechanical detent at 20o.) 0o a 10o 110 KIAS (Alcance del movimiento parcial del flap con código de color azul; detención mecánica en la posición 10º.) 10o a 30o 85 KIAS (Código de color blanco, detención mecánica a 20º.) 172SPHUS-S14-00 S14-7 For Training Purposes Only SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 14 MODEL 172S U.S. FAA APPROVED PLACARDS (Continued) 5. In baggage compartment: 6. A calibration card must be provided to indicate the accuracy of the magnetic compass in 30° increments. Se debe proporcionar una tarjeta de calibración para indicar la precisión de la brújula magnética en incrementos de 30º. (Continued Next Page) 54 KG MÁXIMO EQUIPAJE ADELANTE DE LA TRABA DE LA PUERTA DE EQUIPAJE 22 KG MÁXIMO EQUIPAJE POSTERIOR A LA TRABA DE LA PUERTA DE EQUIPAJE MÁXIMO: 54 KG COMBINADOS PARA INSTRUCCIONES ADICIONALES DE CARGA VER DATOS DE PESO Y BALANCEO 172SPHUS-S14-00 S14-8 For Training Purposes Only CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 14 U.S. FAA APPROVED PLACARDS (Continued) 7. On oil filler cap: OIL 8 QTS ACEITE 8 QTS 8. On control lock: CAUTION! CONTROL LOCK REMOVE BEFORE STARTING ENGINE ¡ADVERTENCIA! TRABA DE CONTROL QUITAR ANTES DE ENCENDER EL MOTOR 9. Near airspeed indicator: (Continued Next Page) VELOCIDAD DE MANIOBRA -105 KIAS 172SPHUS-S14-00 S14-9 For Training Purposes Only SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 14 MODEL 172S U.S. FAA APPROVED PLACARDS (Continued) 10. On the upper right side of the aft cabin partition: 11. On forward face of firewall adjacent to the battery: (Continued Next Page) TRANSMISOR LOCALIZADOR DE EMERGENCIA INSTALADO EN LA PARTE POSTERIOR DE ESTE TABIQUE SERVICE EN CONFORMIDAD CON RAAC 91.207 ADVERTENCIA 24 VOLTIOS C.C. ESTA AERONAVE ESTÁ EQUIPADA CON ALTERNADOR Y UN SISTEMA DE CONEXIÓN A MASA NEGATIVO RESPETAR LA POLARIDAD APROPIADA LA POLARIDAD INVERSA DAÑARÁ LOS COMPONENTES ELÉCTRICOS 172SPHUS-S14-00 S14-10 For Training Purposes Only CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 14 U.S. FAA APPROVED PLACARDS (Continued) 12. On the upper right instrument panel: PROHIBIDO FUMAR 172SPHUS-S14-00 S14-11 For Training Purposes Only SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 14 MODEL 172S U.S. FAA APPROVED EMERGENCY PROCEDURES There is no change to the airplane emergency procedures when used for Argentine Certified Airplanes. NORMAL PROCEDURES There is no change to the airplane normal procedures when used for Argentine Certified Airplanes. PERFORMANCE There is no change to the airplane performance when used for Argentine Certified Airplanes. 172SPHUS-S14-00 S14-12 For Training Purposes Only CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 14 U.S. FAA APPROVED LOG OF D.N.A. ACCEPTED SUPPLEMENTS The following list contains D.N.A. accepted supplements. Refer to Log of Approved Supplements in the basic Pilot's Operating Handbook and FAA Approved Airplane Flight Manual for revision status. (Continued Next Page) Supplement Number Name Equipment Installed 1 Bendix/King KX 155A VHF NAV/COMM with KI 208 or KI 209A Indicator Head _____________ 2 Bendix/King KT 76C Transponder with Blind Encoder _____________ 3 Bendix/King KMA 26 Audio Selector Panel _____________ 4 Pointer Model 3000-11 or Model 4000-11 Emergency Locator Transmitter (ELT) _____________ 5 Bendix/King KLN 89B Global Positioning System (GPS) _____________ 6 Bendix/King KR 87 Automatic Direction Finder (ADF) _____________ 7 Bendix/King KAP 140 Single Axis Autopilot _____________ 8 Winterization Kit _____________ 9 Davtron Model 803 Clock/OAT _____________ 10 Bendix/King KLN 89 Global Positioning System (GPS) _____________ 11 Reserved 12 Reserved 13 Bendix/King KCS-55A Slaved Compass System with KI-525A Horizontal Situation Indicator (HSI) _____________ 14 Argentine Certified Airplanes _____________ 15 Bendix/King KAP 140 2 Axis Autopilot _____________ 16 Bendix/King KT 73 Mode S Transponder _____________ 17 Reserved 172SPHUS-S14-00 S14-13 For Training Purposes Only SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 14 MODEL 172S U.S. FAA APPROVED LOG OF D.N.A. ACCEPTED SUPPLEMENTS Supplement Number Name Equipment Installed 18 Reserved 19 Bendix/King KLN 94 Global Positioning System _____________ 20 Bendix/King KMA 28 Audio Selector Panel _____________ 21 Bendix/King KMD 550 Multi-Function Display _____________ 22 12 Volt Cabin Power System _____________ 23 Reserved 24 Astrotech Model TC-2 Clock/OAT/Volt Indicator _____________ 25 Bendix/King KX 165A VHF NAV/COM _____________ 26 Bendix/King KDR 510 Flight Information Services (FIS) _____________ 172SPHUS-S14-00 S14-14 For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only U.S. CESSNA MODEL 172S NAV I/NAV II AVIONICS OPTION Serials 172S8001 thru 172S10431 SUPPLEMENT 18 UKRAINIAN CERTIFIED AIRPLANES This supplement must be inserted into Section 9 of the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual for Ukrainian Certified Airplanes. This supplement is approved by the U.S. Federal Aviation Administration (FAA) on behalf of the State Aviation Administration of Ukraine (SAA). SERIAL NO. REGISTRATION NO. 172SPHUS-S18-00 COPYRIGHT © 2012 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA S18-1 8 MAY 2012 For Training Purposes Only SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 18 MODEL 172S NAV I/NAV II U.S. FAA APPROVED SUPPLEMENT 18 UKRAINIAN CERTIFIED AIRPLANES Use the Log of Effective Pages to determine the current status of this supplement. Pages affected by the current revision are indicated by an asterisk (*) preceding the page number. LOG OF EFFECTIVE PAGES Supplement Status Date Original Issue 8 May 2012 Page Number Page Status Revision Number S18-1 thru S18-16 Original 0 172SPHUS-S18-00 S18-2 For Training Purposes Only CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 18 NAV I/NAV II U.S. FAA APPROVED SERVICE BULLETIN CONFIGURATION LIST The following is a list of Service Bulletins that are applicable to the operation of the airplane, and have been incorporated into this supplement. This list contains only those Service Bulletins that are currently active. Number Title Airplane Serial Effectivity Revision Incorporated Incorporated in Airplane 172SPHUS-S18-00 S18-3 For Training Purposes Only SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 18 MODEL 172S NAV I/NAV II U.S. FAA APPROVED UKRAINIAN CERTIFIED AIRPLANES GENERAL This supplement must be placed in Section 9 of the basic Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual for Ukrainian Certified Airplanes. The information contained herein supplements the information of the basic Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual. Limitations, procedures, and performance found in this supplement supersedes those found in the basic Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual. For limitations, procedures, and performance information not contained in this supplement, consult the basic Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual. NOTE In Ukraine, FAA operating rules (i.e., 14 CFR Part 91 and 14 CFR Part 135) are not applicable. The airplane must be equipped and operated in accordance with applicable Ukraine operational requirements. 172SPHUS-S18-00 S18-4 For Training Purposes Only CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 18 NAV I/NAV II U.S. FAA APPROVED OPERATING LIMITATIONS The following Limitations supersede and/or are in addition to the Limitations set forth in the basic Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual: Minimum Flight Crew: . . . . . . . . . . . One (1) Pilot (flying from left seat) Maximum Number Of Seats: . . . . . . . . . . . . . . . . . . . . . . . . . . Four (4) Maximum Number Of Passengers: . . . . . . . . . . Three (3) Passengers The Nav I/Nav II Avionics Option equipped with the KAP 140 Single or 2 Axis Autopilot is approved for Category I ILS approach operations only. The Global Positioning Satellite (GPS) system is not approved for approach. Operation over water beyond the Maximum Glide distance from shore is prohibited (Refer to the POH/AFM, Section 3, Figure 3-1). A Flight Data Recorder (FDR) must be installed and operational for all commercial transportation operations. A portable COSPAS-SARSAT (406MHz) Emergency Radio Beacon must be carried and operational for all operations over areas that are difficult to access, certain regions that are rarely populated and when flying over large bodies of water. A HF radio must be installed and operational if airplane operates in areas where communication through VHF radio stations cannot be performed. 172SPHUS-S18-00 S18-5 For Training Purposes Only SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 18 MODEL 172S NAV I/NAV II U.S. FAA APPROVED OPERATING LIMITATIONS (Continued) FUEL LIMITATIONS Approved Fuels: 100LL (ASTM-D910) 100 (Formerly 100/130) (ASTM-D910) B91/115 (GOST 1012-72) * NOTE * If Russian B91/115 fuel is used, the airplane must be equipped with either float type or Gen 3.0 fuel level senders. See the latest revision of Lycoming Service Instruction No.1070 for approved fuel grades. Fuels must contain an anti-icing fuel additive (Isopropyl Alcohol or DiEGME) in concentrations mixed as noted in Section 8 of the POH/ AFM. MAXIMUM APPROVED OPERATING ALTITUDE The maximum operating barometric altitude is limited to the following: With Passengers . . . . . . . . . . . . . . . . . . . . . . . . . . . 3000 m (9800 feet) Flight Crew Only (30 Minutes Maximum) . . . . . . . 3600 m (11,800 feet) OUTSIDE AIR TEMPERATURE LIMITS Ground operations limits for a cold day:. . . . . . . . . . . . . . . . Minus 40°C Ground operations limits for a hot day: . . . . . . . . . . . . . . . . . . . . +40°C (Continued Next Page) S18-6 172SPHUS-S18-00 For Training Purposes Only CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 18 NAV I/NAV II U.S. FAA APPROVED OPERATING LIMITATIONS (Continued) TAXI OPERATIONAL LIMITS Uncontaminated paved taxiway: • Maximum wind velocity while taxiing: . . . . . . . . . . . 14 m/s (27 Knots) Paved taxiway contaminated with precipitation: • Maximum wind velocity while taxiing: . . . . . . . . . . . . . 3 m/s (5 Knots) Refer to Section 4 of the POH/AFM for additional information on taxiing. TAKEOFF AND LANDING OPERATIONAL LIMITS Maximum Takeoff and Landing Altitude: . . . . . . . . . 2438 m (8000 feet) Maximum Headwind Velocity: . . . . . . . . . . . . . . . . . . 14 m/s (27 Knots) Maximum Tailwind Velocity: . . . . . . . . . . . . . . . . . . . . . 5 m/s (10 Knots) Maximum crosswind velocity on uncontaminated paved runway: . . . . . . . . . . . . . . . .7m/s (15 Knots) ALLOWABLE RUNWAY SURFACE CONDITIONS 1. Uncontaminated runway with paved surface. 2. Paved runway contaminated with precipitation (average depth and types): a. Water, less that 10.0 mm. b. Slush, less than 10.0 mm. c. Loose snow less than 30.0 mm. 3. Unpaved runway a. Surface hardness not less than 7 kg/cm2 with wheel fairings installed. b. Surface hardness not less than 5 kg/cm2 with wheel fairings removed. c. Landing on contaminated unpaved runways is prohibited. Operating with the landing gear fairings removed is recommended on wet or unpaved runways when temperatures are near or below freezing. (Continued Next Page) 172SPHUS-S18-00 S18-7 For Training Purposes Only SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 18 MODEL 172S NAV I/NAV II U.S. FAA APPROVED OPERATING LIMITATIONS (Continued) TAKEOFF AND LANDING OPERATIONAL LIMITS (Continued) MAXIMUM CROSSWIND ON CONTAMINATED RUNWAYS Contaminated paved runways with: Water, less than 10.0 mm . . . . . . . . . . . . . . . . . . . . . 3 m/s (5 Knots) Slush, less than 10.0 mm . . . . . . . . . . . . . . . . . . . . . 3 m/s (5 Knots) Loose snow, less than 30.0 mm . . . . . . . . . . . . . . . . 3 m/s (5 Knots) Paved runway with less than 3 mm of water, snow or slush and braking coefficient of friction(μ) of: μ=0.3 (poor braking) . . . . . . . . . . . . . . . . . . . . . . . . . 3 m/s (5 Knots) μ=0.4 (average braking) . . . . . . . . . . . . . . . . . . . . . . 5 m/s (9 Knots) μ=0.5 (good braking, dry or equivalent to dry runway) . . . . . . . . . . . . . . . 7 m/s (15 Knots) NOTE • For intermediate values of coefficient of friction (ȝ), crosswind is to be estimated by interpolation. • Operation is prohibited on a runway covered with ice at a coefficient of friction ȝ < 0.3. 172SPHUS-S18-00 S18-8 For Training Purposes Only CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 18 NAV I/NAV II U.S. FAA APPROVED OPERATING LIMITATIONS (Continued) REQUIRED PLACARDS AND MARKINGS Located adjacent to the left and right exterior door handles. Placard is approximately 11.33 inches (28.78 cm) by 4.66 inches (11.84 cm) with 1.00 inch (2.54 cm) red letters on a white background: 172SPHUS-S18-00 S18-9 For Training Purposes Only SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 18 MODEL 172S NAV I/NAV II U.S. FAA APPROVED EMERGENCY PROCEDURES FORCED LANDINGS If all attempts to restart the engine fail and a forced landing is imminent, select a suitable field and prepare for the landing as discussed under the Emergency Landing Without Engine Power checklist. Transmit Mayday message on 121.5 MHz giving location, intentions and squawk 7700. Before attempting an off airport landing with engine power available, one should fly over the landing area at a safe, but low altitude, to inspect the terrain for obstructions and surface conditions, proceeding as discussed in the Precautionary Landing With Engine Power checklist. Prepare for ditching by securing or jettisoning heavy objects located in the baggage area and collect folded coats for protection of occupants' face at touchdown. Transmit Mayday messages on 121.5 MHz giving location, intentions and squawk 7700. Avoid a landing flare because of the difficulty in judging height over a water surface. The checklist assumes the availability of power to make a precautionary water landing. If power is not available, use of the airspeeds noted with minimum flap extension will provide a more favorable attitude for a power off ditching. In a forced landing situation, do not turn off the MASTER switch or AVIONICS switch until a landing is assured. Premature deactivation of the switches will disable all airplane electrical systems. 172SPHUS-S18-00 S18-10 For Training Purposes Only CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 18 NAV I/NAV II U.S. FAA APPROVED NORMAL PROCEDURES BEFORE STARTING ENGINE NOTE • When flight over water surface is intended, the airplane must be equipped with emergency ditching flotation equipment as required by Operation Regulations. • Life vests must be put on before boarding the airplane. COLD SOAK If extended exposure to cold weather is expected, refer to Maintenance Manual, Model 172 Series 1996 and On, Chapter 12 Servicing, Section 12-30-00 Unscheduled Servicing-Description and Operation, paragraph 3 Cold Soak, for procedures to prepare the airplane for cold soak. After extended exposure, for more than two hours, at temperatures colder than Minus -10°C (14°F), refer to Maintenance Manual, Model 172 Series 1996 and On, Chapter 12 Servicing, Section 12-30-00 Unscheduled Servicing-Description and Operation, paragraph 3 Cold Soak, for procedures of an airplane for preparing the airplane for flight. Cold temperatures will affect control cable tension. See Chapter 27 of the Maintenance Manual for flight control cable tensions. See Chapter 12 of the Maintenance Manual for information on lubrication and greasing of moving parts. See Section 8 of the POH/AFM for correct engine oil viscosity. See paragraphs on Cold Weather Operation in Section 4 of the POH/AFM for additional information on procedures for operating the airplane in cold temperatures. When the outside temperature is less than Minus 34ºC, the airplane batteries should be removed and stored in the warm conditions. (Continued Next Page) 172SPHUS-S18-00 S18-11 For Training Purposes Only SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 18 MODEL 172S NAV I/NAV II U.S. FAA APPROVED NORMAL PROCEDURES (Continued) COLD SOAK (Continued) Engine must be preheated before starting if engine temperature is less than Minus 6°C. Refer to Lycoming Service Instruction No. 1505 for recommendation of an engine preheating procedures. When the outside temperature is less than 0°C, moisture from combustion can freeze on the engine spark plugs if the engine does not continue to operate after it is started. This will prevent the engine from starting again. Preheat the engine to more than 0°C before starting the engine again. Preheat the engine by directing warm air into the engine cowling inlets behind the propeller. The temperature of the preheating air should not be more than 120°C to prevent damage to the exterior paint. Open flames are prohibited near the airplane. Before takeoff, preheat the airplane cabin to more than Minus 30°C for correct operation of the standby altimeter. If there is no warning that an instrument is operating incorrectly, all other instruments will operate down to the minimum temperature of the airplane. Before operating the airplane, it is recommended to heat the cabin to a comfortable temperature for the cabin occupants. 172SPHUS-S18-00 S18-12 For Training Purposes Only CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 18 NAV I/NAV II U.S. FAA APPROVED PERFORMANCE TAKEOFF DISTANCE The takeoff distance on a paved runway with no more than 3 mm of precipitation is equal to dry runway takeoff distance. The takeoff distance on a paved runway with precipitation greater than 3 mm is 20% greater than the dry runway takeoff distance. LANDING DISTANCE DRY RUNWAY - BASIC AIRFIELD To determine the required landing distance for Ukrainian Certified Airplanes on a dry paved runway, the dry runway landing distance listed in Section 5, Performance, Short Field Landing Distance, Figure 5-11, of the U.S. POH must be multiplied by 1.67. DRY RUNWAY - DIVERSION OR ALTERNATE AIRFIELD To determine the required landing distance for Ukrainian Certified Airplanes on a dry paved runway, the dry runway landing distance listed in Section 5, Performance, Short Field Landing Distance, Figure 5-11, of the U.S. POH must be multiplied by 1.43. CONTAMINATED RUNWAY To determine the required landing distance for Ukrainian Certified Airplanes on a contaminated paved runway, the Ukrainian-Factored dry runway landing distance must be multiplied by 1.43. WET RUNWAY To determine the required landing distance for Ukrainian Certified Airplanes on a wet paved runway, the Ukrainian-Factored dry runway landing distance must be multiplied by 1.15. For unpaved runway landing distance, refer to Section 5, Performance, Short Field Landing Distance, Figure 5-11, of the U.S. POH for the correction applied to grass runway landing distance. 172SPHUS-S18-00 S18-13/S18-14 For Training Purposes Only For Training Purposes Only CESSNA SECTION 9 - SUPPLEMENTS MODEL 172S SUPPLEMENT 18 NAV I/NAV II U.S. FAA APPROVED LOG OF UKRAINE APPROVED SUPPLEMENTS The following list contains Ukrainian SAA accepted supplements. Refer to Log of Approved Supplements in the basic Pilot's Operating Handbook and FAA Approved Airplane Flight Manual for revision status. (Continued Next Page) Supplement Number Name Equipment Installed 1 Bendix/King KX 155A VHF NAV/COMM with KI 208 or KI 209A Indicator Head _____________ 2 Bendix/King KT 76C Transponder with Blind Encoder _____________ 3 Bendix/King KMA 26 Audio Selector Panel _____________ 4 Pointer Model 3000-11 or Model 4000-11 Emergency Locator Transmitter (ELT) _____________ 5 Bendix/King KLN 89B Global Positioning System (GPS) _____________ 6 Bendix/King KR 87 Automatic Direction Finder (ADF) _____________ 7 Bendix/King KAP 140 Single Axis Autopilot _____________ 8 Winterization Kit _____________ 9 Davtron Model 803 Clock/OAT _____________ 10 Bendix/King KLN 89 Global Positioning System (GPS) _____________ 11 Reserved 12 Reserved 13 Bendix/King KCS-55A Slaved Compass System with KI-525A Horizontal Situation Indicator (HSI) _____________ 14 Reserved 15 Bendix/King KAP 140 2 Axis Autopilot _____________ 16 Bendix/King KT 73 Mode S Transponder _____________ 172SPHUS-S18-00 S18-15 For Training Purposes Only SECTION 9 - SUPPLEMENTS CESSNA SUPPLEMENT 18 MODEL 172S NAV I/NAV II U.S. FAA APPROVED LOG OF UKRAINE APPROVED SUPPLEMENTS Supplement Number Name Equipment Installed 17 Reserved 18 Ukrainian Certified Airplanes _____________ 19 Bendix/King KLN 94 Global Positioning System _____________ 20 Bendix/King KMA 28 Audio Selector Panel _____________ 21 Bendix/King KMD 550 Multi-Function Display _____________ 22 12 Volt Cabin Power System _____________ 23 Reserved 24 Astrotech Model TC-2 Clock/OAT/Volt Indicator _____________ 25 Bendix/King KX 165A VHF NAV/COM _____________ 26 Bendix/King KDR 510 Flight Information Services (FIS) _____________ 172SPHUS-S18-00 S18-16 For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only For Training Purposes Only