Cessna 172 R Pilot Operating Handbook
  1. Manuals
  2. Brands
  3. Cessna Manuals
  4. Aircrafts
  5. 172R
  6. Pilot operating handbook

Cessna 172 R Pilot Operating Handbook

Hide thumbs Also See for 172 R:
Table of Contents

Advertisement

Quick Links

Supplemental Airplane Flight Manual
Pilot´s Operating Handbook
FAA Approved Airplane Flight Manual Supplement
TAE 125-01 and TAE 125-02-99
MODEL No.
SERIAL No.
REGISTER No.
This supplement must be attached to the Pilot's Operating Handbook
when the engine installation has been installed in accordance with STC
SA01303WI.
This manual constitutes a FAA approved AFM Supplement or
Supplemental AFM (as applicable) for US registered airplanes in
accordance with FAR 21.29.
The information contained in this supplement supersedes or adds to
the Pilot's Operating Handbook and FAA approved AFM (if required)
only as set forth herein.
For limitations, procedures, performance and loading information not
contained in this supplement, consult the basic Pilot's Operating
Handbook and FAA approved AFM (as applicable).
Continental Aerospace
Technologies GmbH
Platanenstraße 14
D - 09356 St. Egidien
or
and
(as applicable)
for the
Cessna 172 R & S
equipped with
Installation
Issue 3
Revision 3
Tel. +49 37204 696-0
Fax +49 37204 696-2912
www.continentaldiesel.com
support@continentaldiesel.com
Doc.-No.: 20-0310-22043*

Advertisement

Table of Contents
loading
Need help?

Need help?

Do you have a question about the 172 R and is the answer not in the manual?

Questions and answers

Subscribe to Our Youtube Channel

Related Manuals for Cessna 172 R

Summary of Contents for Cessna 172 R

  • Page 1 D - 09356 St. Egidien Supplemental Airplane Flight Manual Pilot´s Operating Handbook FAA Approved Airplane Flight Manual Supplement (as applicable) for the Cessna 172 R & S equipped with TAE 125-01 and TAE 125-02-99 Installation Issue 3 Revision 3 MODEL No.
  • Page 2 *The last digit of the document number describes the issue of the manual. All manuals with a lower last digit are previous issues of this version.

  • Page 3: Log Of Revisions

    Supplement POH Cessna 172 R&S (FAA-Version) APPROVAL The technical content of this document is approved under the authority of the DOA, ref. EASA.21J.010. LOG OF REVISIONS Revision Section Description Date Approved new Issue June 30, 2016 Change of Ownership Propeller MTV-6-A/190-69...

  • Page 5: List Of Effective Sections

    Supplement POH Cessna 172 R&S (FAA-Version) LIST OF EFFECTIVE SECTIONS Sections Issue/Revision Date Mar. 01, 2022 Mar. 01, 2022 Mar. 01, 2022 Jan. 22, 2018 June 30, 2016 June 30, 2016 June 30, 2016 June 30, 2016 June 30, 2016 Mar.
  • Page 6 Supplement POH Cessna 172 R&S (FAA-Version) This page intentionally left blank Page vi Issue 3 Revision 3, Mar. 2022...

  • Page 7: Table Of Contents

    Supplement POH Cessna 172 R&S (FAA-Version) TABLE OF CONTENTS COVER SHEET LOG OF REVISIONS............. page iii LIST OF EFFECTIVE SECTIONS ......... page v GENERAL REMARK ............. page v TABLE OF CONTENTS..........page vii CONVERSION TABLES ..........page viii ABBREVIATIONS ............page xii...

  • Page 8: Conversion Tables

    Supplement POH Cessna 172 R&S (FAA-Version) CONVERSION TABLES VOLUME Conversion factor Conversion factor Unit [Abbr.] SI to US / Imperial US / Imperial to Si Liter [l] [l] / 3.7854 = [US gal] [l] / 0.9464 = [US qt] [l] / 4.5459 = [[lmp gal] [l] x 61.024 = [in³]...
  • Page 9 Supplement POH Cessna 172 R&S (FAA-Version) PRESSURE Conversion factor Conversion factor Unit [Abbr.] SI to US / Imperial US / Imperial to Si Bar [bar] [bar] x 14.5038 = [psi] Hectopascal [hpa] [hpa] / 33.864= [inHg] =Millibar [mbar] [mbar] / 33.864 = [inHg] Pounds per square inch [psi] / 14.5038 = [bar]...
  • Page 10 Supplement POH Cessna 172 R&S (FAA-Version) °C °F Page x Issue 3 Revision -, June 2016...
  • Page 11 Supplement POH Cessna 172 R&S (FAA-Version) Page xi Issue 3 Revision -, June 2016...

  • Page 12: Abbreviations

    Supplement POH Cessna 172 R&S (FAA-Version) ABBREVIATIONS FADEC Full Authority Digital Engine Control CED 125 Compact Engine Display Multifunctional instrument for indication of engine data AED 125 Auxiliary Engine Display Multifunctional instrument for indication of engine and airplane data Page xii...

  • Page 13: General

    Supplement POH Cessna 172 R&S (FAA-Version) SECTION 1 GENERAL Safety Recommendations The following symbols and warnings are used in this manual. They must be heeded strictly to prevent personal injury and material damage, to avoid impairment of the operational safety of the aircraft and to rule out any damage to the aircraft as a consequence of improper handling.
  • Page 14 Supplement POH Cessna 172 R&S (FAA-Version) ENGINE  WARNING: The engine requires an electrical power source for operation. If the main battery and alternator fail, the engine will only operate for a maximum of 30 minutes on FADEC backup battery power.
  • Page 15 Supplement POH Cessna 172 R&S (FAA-Version) PROPELLER Manufacturer:......MT Propeller Entwicklung GmbH Model: ............MTV-6-A/187-129 ........MTV-6-A/190-69 (only TAE 125-02-99) Number of blades:..............3 Diameter: ........1.87 m (MTV-6-A/187-129) ............1.90 m (MTV-6-A/190-69) Type: ..............constant speed FUELS and LIQUIDS  WARNING: The engine must not be started under any circumstances if the level is too low.
  • Page 16 Supplement POH Cessna 172 R&S (FAA-Version)  Note: The additive Biobor JF can be used in jet and diesel fuel systems to prevent microbial contamination and ensure fuel quality. The recommended dosage is 1 gal per 9.5 gal fuel. Drain water bottoms prior application.
  • Page 17 Supplement POH Cessna 172 R&S (FAA-Version) Coolant:.... Use of Ready Mix ratio 50:50 is recommended  Note: If Ready Mix is not available please use concentrate and distilled water in a ratio of 50:50 to ensure an ice flocculation point at -38°C +/-2°C.
  • Page 18 Supplement POH Cessna 172 R&S (FAA-Version) This page intentionally left blank Page 1-6 Issue 3 Revision 2, Mar. 2022...
  • Page 19 Supplement POH Cessna 172 R&S (FAA-Version) SECTION 2 LIMITATIONS  WARNING: It is not allowed to start up the engine using external power. If starting the engine is not possible using battery power, the condition of the battery must be verified before flight.
  • Page 20 Supplement POH Cessna 172 R&S (FAA-Version) ENGINE OPERATING LIMITS FOR TAKE-OFF AND CONTINUOUS POWER  WARNING: It is not allowed to start the engine outside of these temperature limits.  Note: The operating limit temperature is a temperature limit below which the engine may be started, but not operated at the Take-off RPM.
  • Page 21 Supplement POH Cessna 172 R&S (FAA-Version) MIN. FUEL TEMPERATURE LIMITS IN THE FUEL TANK  WARNING: The fuel temperature of the fuel tank not used should be observed if its later use is intended.  WARNING: The following applies to Diesel and JET fuel...
  • Page 22 Supplement POH Cessna 172 R&S (FAA-Version) Oil pressure Minimum oil pressure: ........1.2 bar (17.4 psi) Minimum oil pressure (at Take-off power) ..2.3 bar (33.4 psi) Minimum oil pressure (in flight) ......2.3 bar (33.4 psi) Maximum oil pressure ..........6.0 bar (87 psi) Maximum oil pressure (cold start <...
  • Page 23 Supplement POH Cessna 172 R&S (FAA-Version) Figure 2-1a AED 125 Figure 2-1b CED 125  Note: The AED/CED caution lamp is switched on if an engine reading is in the amber or red range. The AED/CED caution lamp remains on...
  • Page 24 Maximum Ramp Weight: ....1112 kg (2452 lbs) Maximum Takeoff Weight: ....1111 kg (2450 lbs) Maximum Landing Weight ....1111 kg (2450 lbs) C172 S normal category (reduced); C172 R with Cessna Mod. KIT MK172-72-01 or LBA-EMZ SA1358 (FAA STC SA2196CE) normal category:  Note: MTOW for C172S is reduced to 1111kg if TAE 125-01 resp.TAE 125-02-99 and...
  • Page 25 Supplement POH Cessna 172 R&S (FAA-Version) MANEUVER LIMITS  CAUTION: Intentionally initiating negative G maneuvers is prohibited. Normal Category: No change Utility Category: Intentionally initiating spins is prohibited FLIGHT LOAD FACTORS No change  CAUTION: Avoid extended negative g-loads duration.
  • Page 26 Supplement POH Cessna 172 R&S (FAA-Version) MAXIMUM FUEL QUANTITIES Due to the higher specific density of Kerosene and Diesel in comparison to Aviation Gasoline (AVGAS) with the TAE 125 installation the permissible tank capacity has been reduced.  CAUTION: To prevent air from penetrating into the fuel system avoid running the tanks dry.
  • Page 27 Supplement POH Cessna 172 R&S (FAA-Version) PERMISSIBLE OIL TYPES  CAUTION: Use approved oil with exact designation only! Engine oil: .......... AeroShell Oil Diesel Ultra ........AeroShell Oil Diesel 10W-40 ..........Shell Helix Ultra 5W-30 ..........Shell Helix Ultra 5W-40 Gearbox oil: ....
  • Page 28 Supplement POH Cessna 172 R&S (FAA-Version) PLACARDS Near the fuel tank caps: for normal category aircraft: JET FUEL ONLY JET A-1 / DIESEL CAP. 84.4 LITERS (22.3 US GALLONS) USABLE TO BOTTOM OF FILLER INDICATOR TAB for utility category aircraft:...
  • Page 29 Supplement POH Cessna 172 R&S (FAA-Version) On the oil funnel or at the flap of the engine cowling: Figure 2-2 Drain Valve Fuel filter The decal is attached to the drain valve of the fuel filter. Figure 2-3 Expansion Tank Coolant: (only TAE 125-02-99) The decal is attached to the expansion tank.
  • Page 30 Supplement POH Cessna 172 R&S (FAA-Version) Figure 2.4 Next to the Alternator Warning Light: "Alternator" If installed, at the flap of the engine cowling to the External Power Receptacle: „ATTENTION 24 V DC OBSERVE CORRECT POLARITY“ All further placards contained in this section of the EASA- approved POH remain valid.
  • Page 31 Supplement POH Cessna 172 R&S (FAA-Version) SECTION 3 EMERGENCY PROCEDURES INDEX OF CHECKLISTS ENGINE MALFUNCTION ..............3-2 During Take-off (with sufficient Runway ahead)......3-2 Immediately after Take-off............3-3 During Flight ................3-3 Restart after Engine Failure ............3-4 FADEC Malfunction in Flight ............3-5 Abnormal Engine Behavior............
  • Page 32 Supplement POH Cessna 172 R&S (FAA-Version) GENERAL In addition to the original AFM/POH, the following applies:  WARNING: Due to an engine shut-down or failures indicated by the FADEC warning lights there might be a loss propeller valve currency which leads in a low pitch setting of the propeller.

  • Page 33: Engine Malfunction

    Supplement POH Cessna 172 R&S (FAA-Version) ENGINE MALFUNCTION DURING TAKE-OFF (WITH SUFFICENT RUNWAY AHEAD) (1) Thrust Lever – IDLE (2) Brakes – APPLY (3) Wing flaps (if extended) – RETRACT (4) Engine Master (“IGN“ resp.) – OFF (5) Alternator, Main Bus and Battery switch – OFF (6) Fuel Shut-off Valve –...

  • Page 34: During Flight

    Supplement POH Cessna 172 R&S (FAA-Version) DURING FLIGHT  Note: Running a tank dry activates both FADEC warning lights flashing. In case that one tank was flown empty, at the first signs of insufficient fuel feed proceed as follows: (1) Fuel Shut-off Valve – OPEN (push full in) (2) Immediately switch the Fuel Selector to BOTH position (3) Electric Fuel Pump –...

  • Page 35: Fadec Malfunction In Flight

    Supplement POH Cessna 172 R&S (FAA-Version)  Note: The propeller will normally continue to turn as long as the airspeed is above 65 KIAS. Should the propeller stop at an airspeed of more than 65 KIAS or more, the reason for this should be found out before attempting a restart.
  • Page 36 Supplement POH Cessna 172 R&S (FAA-Version) b) Both FADEC Lights are flashing  Note: CED load display should be considered unreliable with both FADEC lights illuminated. Use other indications to assess engine condition. 1. Press FADEC test knob at least 2 seconds 2.

  • Page 37: Abnormal Engine Behavior

    Supplement POH Cessna 172 R&S (FAA-Version) ABNORMAL ENGINE BEHAVIOR If the engine acts abnormal during flight and the system does not automatically switch to the B-FADEC, it is possible switch to the B-FADEC manually.  WARNING: It is only possible to switch from the...

  • Page 38: Fires

    Supplement POH Cessna 172 R&S (FAA-Version) FIRES ENGINE FIRE WHEN STARTING ENGINE ON GROUND (1) Engine Master (“IGN“ resp.) – OFF (2) Fuel Shut-off Valve / Fuel Selector - CLOSED (3) Electric Fuel Pump – OFF (4) Switch "Battery" – OFF (5) Extinguish the flames with a fire extinguisher, wool blankets or sand.

  • Page 39: Electrical Fire In Flight

    Supplement POH Cessna 172 R&S (FAA-Version) ELECTRICAL FIRE IN FLIGHT The first sign of an electrical fire is an unmistakable sharp, acrid smell. As the fire grows, electrical load might be higher than normal or circuit breakers start to trip. In this event proceed as follows: (1) STBY BATT Switch –...

  • Page 40: Engine Shut Down In Flight

    Supplement POH Cessna 172 R&S (FAA-Version) ENGINE SHUT DOWN IN FLIGHT If it is necessary to shut down the engine in flight (for instance, abnormal engine behavior does not allow continued flight or there is a fuel leak, etc.), proceed as follows:...

  • Page 41: Flight In Icing Conditions

    Supplement POH Cessna 172 R&S (FAA-Version) FLIGHT IN ICING CONDITIONS  WARNING: It is prohibited to fly in known icing conditions. In case of inadvertent icing encounter proceed as follows: (1) Pitot Heat switch – ON (if installed) (2) Turn back or change the altitude to obtain an outside air temperature that is less conducive to icing.

  • Page 42: Recovery From Spiral Dive

    Supplement POH Cessna 172 R&S (FAA-Version) RECOVERY FROM SPIRAL DIVE If a spiral is encountered in the clouds, proceed as follows: (1) Retard Thrust Lever to idle position (2) Stop the turn by using coordinated aileron and rudder control to align the symbolic airplane in the turn coordinator with the horizontal reference line.

  • Page 43: Electrical Power Supply System Malfunctions

    Supplement POH Cessna 172 R&S (FAA-Version) ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS  WARNING: If the power supply from both alternator and main battery is interrupted, continued engine operation is dependent on the remaining capacity of the FADEC backup battery. The...
  • Page 44 Supplement POH Cessna 172 R&S (FAA-Version) Equipment Time switched on in [min] in [%] NAV/COM 1 receiving NAV/COM 1 transmitting ON NAV/COM 2 receiving NAV/COM 2 transmitting OFF Annunciator Transponder Fuel Pump AED-125 Battery CED-125 Landing Light Flood Light Pitot Heat...

  • Page 45: Alternator Warning Light Illuminates During Normal Engine Operation

    Supplement POH Cessna 172 R&S (FAA-Version) ALTERNATOR WARNING LIGHT ILLUMINATES DURING NORMAL ENGINE OPERATION. (1) Ammeter – CHECK (2) Alternator switch CHECK – ON (3) Battery Switch CHECK – ON  CAUTION: If the FADEC was supplied by battery only until this point, the RPM can momentarily drop, when the alternator is switched on.

  • Page 46: Ammeter Shows Battery Discharge During Normal

    Supplement POH Cessna 172 R&S (FAA-Version) AMMETER SHOWS BATTERY DISCHARGE DURING NORMAL ENGINE OPERATION FOR MORE THAN 5 MINUTES  Note: When Ammeter indication decreases to the far left and the voltage indication is decreasing simultaneously, the battery is being discharged.

  • Page 47: Total Electrical Failure

    Supplement POH Cessna 172 R&S (FAA-Version) TOTAL ELECTRICAL FAILURE (all equipment inoperative, except engine)  WARNING: If both alternator and main battery fail, con- tinued engine operation is dependent on the remaining capacity of the FADEC backup battery. The engine has been...

  • Page 48: Rough Engine Operation Or Loss Of Power

    Supplement POH Cessna 172 R&S (FAA-Version) ROUGH ENGINE OPERATION OR LOSS OF POWER DECREASE IN POWER (1) Push Thrust Lever full forward (Take-off position) (2) Fuel Selector to BOTH Position. (3) Electric Fuel Pump – ON (4) Reduce airspeed to 65-85 KIAS (best glide recommended), (max.

  • Page 49: Oil Pressure Too Low

    Supplement POH Cessna 172 R&S (FAA-Version) OIL PRESSURE TOO LOW (< 2.3 BAR IN CRUISE (YELLOW RANGE) OR < 1.2 BAR AT IDLE (RED RANGE)): (1) Reduce power as quickly as possible (2) Check oil temperature: If the oil temperature is high or near...

  • Page 50: Coolant Temperature "Ct" Too High

    Supplement POH Cessna 172 R&S (FAA-Version) COOLANT TEMPERATURE "CT" TOO HIGH (RED RANGE): (1) Increase airspeed and reduce power as quickly as possible (2) Cabin Heat – COLD (3) If coolant temperature reduces rapidly to normal range, fly normally and monitor coolant temperature. Cabin heat as required.

  • Page 51: Fuel Temperature Too Low

    Supplement POH Cessna 172 R&S (FAA-Version) FUEL TEMPERATURE TOO LOW (AMBER RANGE for Diesel Operation, RED RANGE for Kerosine Operation): The fuel in the selected tank will be heated by the return flow, the temperature in the non-active tank must be monitored.

  • Page 52: Fluctuations In Propeller Rpm

    Supplement POH Cessna 172 R&S (FAA-Version) FLUCTUATIONS IN PROPELLER RPM: If the propeller RPM fluctuates by more than + / - 100 RPM with a constant Thrust Lever position: (1) Change the power setting and attempt to find a power set- ting where the propeller RPM no longer fluctuates.
  • Page 53 Supplement POH Cessna 172 R&S (FAA-Version) SECTION 4 NORMAL PROCEDURES PREFLIGHT INSPECTION Figure 4-1a Preflight Inspection  Note: Visually check airplane for general condition during walk around inspection. In cold weather, remove even small accumulations of frost, ice or snow from wing, tail and control surfaces.
  • Page 54 Supplement POH Cessna 172 R&S (FAA-Version) CABIN (1) Pitot Tube Cover – REMOVE. Check for pitot blockage (2) Pilot´s Operating Handbook – AVAILABLE IN THE AIRPLANE (3) Airplane Weight and Balance – CHECKED (4) Parking Brake – SET (5) Control Wheel Lock – REMOVE (6) "Engine Master"...
  • Page 55 Supplement POH Cessna 172 R&S (FAA-Version)  Note: When Battery is turned ON, some annunciators will flash for about 10 seconds before illuminating steadily. When panel TST switch is toggled up and held in position, all remaining lights will flash until the switch is released.
  • Page 56 Supplement POH Cessna 172 R&S (FAA-Version) RIGHT WING (1) Wing Tie-Down – DISCONNECT (2) Main Wheel Tire – CHECK for proper inflation and general condition (weather checks, tread depth and wear, etc.)  WARNING: If, after repeated sampling, evidence of contamination still exists, the airplane should not be flown.
  • Page 57 Supplement POH Cessna 172 R&S (FAA-Version) NOSE (1) Reservoir tank Quick Drain Valve – DRAIN at least a cupful of fuel (using sampler cup) from valve to check for water, sediment and proper fuel grade (Diesel or JET-A1) before each flight and after each refueling. If...
  • Page 58 Supplement POH Cessna 172 R&S (FAA-Version) (8) Nose Wheel Strut and Tire – CHECK for proper inflation of strut and general condition (weather checks, tread depth and wear, etc.) of tire. (9) Left Static Source Opening – CHECK for blockage LEFT WING (1) Fuel Quantity –...
  • Page 59 Supplement POH Cessna 172 R&S (FAA-Version) (2) Flap – Check for security and conditions BEFORE STARTING ENGINE (1) Preflight Inspection – COMPLETE (2) Passenger Briefing – COMPLETE (3) Seats and Seat Belts – ADJUST and LOCK. Ensure inertia reel locking.
  • Page 60 Supplement POH Cessna 172 R&S (FAA-Version) PROCEDURES UP TO 5500ft AIRFIELD ELEVATION STARTING ENGINE  WARNING: Do not use ground power unit for engine starts. It is not allowed to start up the engine using external power. If starting the...
  • Page 61 Supplement POH Cessna 172 R&S (FAA-Version) (11) FADEC Backup Battery test Alternator – OFF, engine must operate normally Battery – OFF, for min. 10 seconds; engine must operate normally, the red FADEC lamps must not be illuminated Battery – ON Alternator –...
  • Page 62 Supplement POH Cessna 172 R&S (FAA-Version) (10) FADEC and propeller adjustment function check: Thrust Lever – IDLE (both FADEC lights should be OFF) FADEC Test Button – PRESS and HOLD button for entire test. Both FADEC lights – ON, RPM increases ...
  • Page 63 Supplement POH Cessna 172 R&S (FAA-Version)  Note: If the test button is released before the self test is over, the FADEC immediately switches over to normal operation.  Note: While switching from one FADEC to another, it is normal to hear and feel a momentary surge in the engine.
  • Page 64 Supplement POH Cessna 172 R&S (FAA-Version) PROCEDURES OVER 5500ft AIRFIELD ELEVATION  Note: Procedures apply only to TAE 125-02-99. For TAE 125-01 refer to procedures for airfield elavations up to 5500ft.  Note: Due to the increase of the idle speed with...
  • Page 65 Supplement POH Cessna 172 R&S (FAA-Version)  CAUTION: Do not overheat the starter motor. Do not operate the starter motor for more than 10 seconds. After operating the starter motor, let it cool off for 20 seconds. After 6 attempts to start the engine, let the starter cool off for half an hour.
  • Page 66 Supplement POH Cessna 172 R&S (FAA-Version) (4) "Engine Master" ("IGN" resp.) - ON, wait until the Glow Control light extinguishes (5) Starter - ON, keep starter engaged until min. 500rpm Release when engine starts, leave Thrust Lever in idle (6) Ammeter - CHECK for positive charging current...
  • Page 67 Supplement POH Cessna 172 R&S (FAA-Version)  WARNING: The whole test procedure has to be performed without any failure. In case the engine shuts down or the FADEC lights are flashing, take off is prohibited. This applies even if the engine seems to run without failure after the test.
  • Page 68 Supplement POH Cessna 172 R&S (FAA-Version) (14) Annunciator Panel – Ensure no annunciators are illuminated (15) Wing Flaps – SET for Take-off (0° or 10°). (16) Electric Fuel Pump – ON (17) Strobe Lights – AS DESIRED (18) Radios and Avionics – ON and SET (19) Autopilot (if installed) –...
  • Page 69 Supplement POH Cessna 172 R&S (FAA-Version) CLIMB (1) Airspeed – 70 to 85 KIAS.  Note: If a maximum performance climb is necessary, use speeds shown in the "Maximum Rate Of Climb" chart in Section 5. In case that Oil Temperature and/or...
  • Page 70 Supplement POH Cessna 172 R&S (FAA-Version) CRUISE (1) Power – maximum load 100% (maximum continuous pow- er), 75% or less is recommended. For economic cruise set load 70% or less. (2) Elevator trim – ADJUST (3) Compliance with Limits for Oil Pressure, Oil Temperature, Coolant Temperature and Gearbox Temperature (CED 125 and Caution light) –...
  • Page 71 Supplement POH Cessna 172 R&S (FAA-Version) DESCENT (1) Fuel Selector Valve – SELECT BOTH position (2) Power – AS DESIRED BEFORE LANDING (1) Pilot and Passenger Seat Backs – MOST UPRIGHT POSI- TION (2) Seats and Seat Belts – SECURED and LOCKED (3) Fuel Selector Valve –...
  • Page 72 Supplement POH Cessna 172 R&S (FAA-Version) LANDING NORMAL LANDING (1) Airspeed – 69 to 80 KIAS (wing flaps UP) (2) Wing Flaps – AS REQUIRED (0°-10° below 110 KIAS; 10°– Full below 85 KIAS) (3) Airspeed – 60 to 70 KIAS (Flaps DOWN) (4) Touchdown –...
  • Page 73 Supplement POH Cessna 172 R&S (FAA-Version) AFTER LANDING (1) Wing Flaps – RETRACT (2) Electric Fuel Pump – OFF SECURING AIRPLANE (1) Parking Brake – SET (2) Thrust Lever – IDLE (3) Avionics Power Switch, Electric Equipment, Autopilot (if installed) – OFF (4) "Engine Master"...
  • Page 74 Supplement POH Cessna 172 R&S (FAA-Version) AMPLIFIED PROCEDURES STARTING ENGINE The TAE 125 is a direct Diesel injection engine with common- rail technology and a turbocharger. It is controlled automatically by the FADEC, which makes a proper performance of the FADEC test important for safe flight operation.
  • Page 75 Supplement POH Cessna 172 R&S (FAA-Version) TAXIING When taxiing, it is important that speed and use of brakes be held to a minimum and that all controls be utilized (Refer to Figure 4-2, Taxiing Diagram) to maintain directional control and balance.
  • Page 76 Supplement POH Cessna 172 R&S (FAA-Version) BATTERY CHECK If there is doubt regarding the battery conditions or functionality the battery has to be checked after warm-up as follows: Switch-off the alternator while the engine is running (battery remains "ON"). Perform a 10 sec. engine run. The voltmeter must remain in the green range.
  • Page 77 Supplement POH Cessna 172 R&S (FAA-Version) CLIMB Normal climbs are performed with flaps up and full load and at speeds 5 to 10 knots higher than best rate-of-climb speeds for the best combination of engine cooling, climb speed and visibility. The speed for best climb is about 70 KIAS/ . If an obstruction dictates the use of a steep climb angle, climb at 62 KIAS and flaps up.
  • Page 78 Supplement POH Cessna 172 R&S (FAA-Version) COLD WEATHER OPERATION Special attention should be paid to operation of the aircraft and the fuel system in winter or before any flight at low temperatures. Correct preflight draining of the fuel system is particularly important and will prevent the accumulation of water.
  • Page 79 Supplement POH Cessna 172 R&S (FAA-Version)  WARNING: The following applies to Diesel and JET fuel mixtures in the tank: As soon as the proportion of Diesel in the tank is more than 10% Diesel, the fuel temperature limits for Diesel operation must be observed.
  • Page 80 Supplement POH Cessna 172 R&S (FAA-Version) HOT WEATHER OPERATION Engine temperatures may rise into the yellow range and activate the "Caution" Light when operating in hot weather or longer climbouts at low speed. This indication gives the pilot the opportunity to keep the engine from possibly...
  • Page 81 Supplement POH Cessna 172 R&S SECTION 5 PERFORMANCE SAMPLE PROBLEM The following sample flight problem utilizes information from the various tables and diagrams of this section to determine the predicted performance data for a typical flight. Assume the following information has already been determined: AIRPLANE CONFIGURATION Takeoff Weight.......
  • Page 82 Supplement POH Cessna 172 R&S GROUND ROLL AND TAKE-OFF The ground roll and take-off distance chart, Figure 5-1c (Takeoff Distance), should be consulted, keeping in mind that distances shown are based on the short field technique. Conservative distances can be established by reading the chart at the next higher value of weight, temperature and altitude.
  • Page 83 Supplement POH Cessna 172 R&S CRUISE The cruising altitude should be selected based on a consideration of trip length, winds aloft and the airplanes performance. A typical cruising altitude and the expected wind enroute have been given for this sample problem. However, the power setting selection for cruise must be determined based on several considerations.
  • Page 84 Supplement POH Cessna 172 R&S FUEL REQUIRED The total fuel requirement for the flight may be estimated using the performance information in Figures 5-2 and 5-4. For this sample problem, Figure 5-2a shows that a climb from 1000 ft to 6,000 ft requires 4.6 l (1.2 US gal) of fuel.
  • Page 85 Supplement POH Cessna 172 R&S The resultant cruise distance is: Total Distance ............460.0 NM Climbout Distance............- 12.0 NM Cruise Distance............448.0 NM With an expected 10 Kt headwind, the ground speed for cruise is predicted to be: 101 Knot...
  • Page 86 Supplement POH Cessna 172 R&S Figure 5-1 Density Altitude Chart Page 5-6 Issue 3 Revision -, June 2016...
  • Page 87 Supplement POH Cessna 172 R&S Figure 5-2 Engine Power Over Altitude Page 5-7 Issue 3 Revision -, June 2016...
  • Page 88 Supplement POH Cessna 172 R&S This page intentionally left blank Page 5-8 Issue 3 Revision -, June 2016...
  • Page 89 Supplement POH Cessna 172 R&S (FAA-Version) SECTION 5a PERFORMANCE  Note: This chapter applies to aircraft with propellers MTV-6-A/187-129. The correct propeller designation can be found on the blades.  Note: The chapter not relevant to the respective propeller can be omitted.
  • Page 90 Supplement POH Cessna 172 R&S (FAA-Version) GROUND ROLL AND TAKE-OFF DISTANCE at 953 kg (2100 lbs) SHORT FIELD TAKEOFF Conditions: Take-off weight 953 kg (2100 lbs) Flaps 10° Full Power Prior to Brake Release Paved, level, dry runway Zero Wind Lift Off: .................44 KIAS...
  • Page 91 Supplement POH Cessna 172 R&S (FAA-Version) Ground Roll and Take-Off Distance [m] PRESS Outside Air Temperature [°C] [ft] -20°C 0°C 10°C 20°C 30°C 40°C 50°C Gnd Roll 15 m obst. Gnd Roll 1000 15 m obst. Gnd Roll 2000 15 m obst.
  • Page 92 Supplement POH Cessna 172 R&S (FAA-Version) Ground Roll and Take-Off Distance [ft] PRESS Outside Air Temperature [°C] [ft] -20°C 0°C 10°C 20°C 30°C 40°C 50°C Gnd Roll 50 ft obst. 1072 1147 1226 1321 1450 1623 Gnd Roll 1000 50 ft obst.
  • Page 93 Supplement POH Cessna 172 R&S (FAA-Version) GROUND ROLL AND TAKE-OFF DISTANCE at 1111 kg (2450 lbs) SHORT FIELD TAKEOFF Conditions: Take-off weight 1111 kg (2450 lbs) Flaps 10° Full Power Prior to Brake Release Paved, level, dry runway Zero Wind Lift Off: .................51 KIAS...
  • Page 94 Supplement POH Cessna 172 R&S (FAA-Version) Ground Roll and Take-Off Distance [m] PRESS Outside Air Temperature [°C] [ft] -20°C 0°C 10°C 20°C 30°C 40°C 50°C Gnd Roll 15 m obst. Gnd Roll 1000 15 m obst. Gnd Roll 2000 15 m obst.
  • Page 95 Supplement POH Cessna 172 R&S (FAA-Version) Ground Roll and Take-Off Distance [ft] PRESS Outside Air Temperature [°C] [ft] -20°C 0°C 10°C 20°C 30°C 40°C 50°C Gnd Roll 1020 1116 1244 50 ft obst. 1386 1601 1713 1830 1972 2164 2423...
  • Page 96 Supplement POH Cessna 172 R&S (FAA-Version) TIME, FUEL AND DISTANCE TO CLIMB AT 1111 kg (2450 lbs) Conditions: Takeoff weight 1111 kg (2450 lbs) Climb speed v = 70 KIAS Flaps Up Full Power Standard Temperature (ISA) Notes: 1. Add 4 l (1.1 US gal) of fuel for engine start, taxi and takeoff allowance.
  • Page 97 Supplement POH Cessna 172 R&S (FAA-Version) Press. Time Distance Fuel used Alt. [ft] [°C] [KIAS] [FPM] [MIN] [NM] Gal] 1000 2000 3000 4000 5000 11.5 6000 11.1 14.2 7000 13.2 17.0 8000 15.3 20.1 9000 17.6 23.5 10000 20.1 27.2 11000 22.8...
  • Page 98 Supplement POH Cessna 172 R&S (FAA-Version) MAXIMUM RATE-OF-CLIMB at 1111 kg (2450 lbs) Conditions: Take-off weight 1111 kg (2450 lbs) Climb speed v = 70 KIAS Flaps Up Full Power Notes: 1. For operation in air colder than this table provides, use cold- est data shown.
  • Page 99 Supplement POH Cessna 172 R&S (FAA-Version) CRUISE PERFORMANCE, RANGE AND ENDURANCE at 1111 kg (2450 lbs) Conditions: Take-off weight 1111kg (2450 lbs) Flaps Up Zero wind Notes: 1. Endurance information are based on 168.8 l (44.6 US gal) usable fuel.
  • Page 100 Supplement POH Cessna 172 R&S (FAA-Version) Endu- Press. Load Speed Fuel Flow Distance rance Alt. Time [ft] [KTAS] [mph] [l/h] [US Gal/h] [NM] [Hrs] 29.5 25.3 21.7 18.6 15.8 13.0 11.9 2000 29.5 2000 25.3 2000 21.7 2000 18.6 2000 15.8...
  • Page 101 Supplement POH Cessna 172 R&S (FAA-Version) Endu- Press. Load Speed Fuel Flow Distance rance Alt. Time [ft] [KTAS] [mph] [l/h] [US Gal/h] [NM] [Hrs] 10000 25.3 10000 21.7 10000 18.6 10000 15.8 10000 13.0 10.9 12000 21.7 12000 18.6 12000 15.8...
  • Page 102 Supplement POH Cessna 172 R&S (FAA-Version) This page intentionally left blank Page 5a-14 Issue 3 Revision -, June 2016...
  • Page 103 Supplement POH Cessna 172 R&S (FAA-Version) SECTION 5b PERFORMANCE  Note: This chapter applies to aircraft with propellers MTV-6-A/190-69 and TAE 125-02-99 installation. The correct propeller designation can be found on the blades.  Note: The chapter not relevant to the respective propeller can be omitted.
  • Page 104 Supplement POH Cessna 172 R&S (FAA-Version) GROUND ROLL AND TAKE-OFF DISTANCE at 953 kg (2100 lbs) SHORT FIELD TAKEOFF Conditions: Take-off weight 953 kg (2100 lbs) Flaps 10° Full Power Prior to Brake Release Paved, level, dry runway Zero Wind Lift Off: .................44 KIAS...
  • Page 105 Supplement POH Cessna 172 R&S (FAA-Version) Ground Roll and Take-Off Distance [m] PRESS Outside Air Temperature [°C] [ft] -20°C 0°C 10°C 20°C 30°C 40°C 50°C Gnd Roll 15 m obst. Gnd Roll 1000 15 m obst. Gnd Roll 2000 15 m obst.
  • Page 106 Supplement POH Cessna 172 R&S (FAA-Version) Ground Roll and Take-Off Distance [ft] PRESS Outside Air Temperature [°C] [ft] -20°C 0°C 10°C 20°C 30°C 40°C 50°C Gnd Roll 50 ft obst. 1047 1125 1200 1325 1499 Gnd Roll 1000 50 ft obst.
  • Page 107 Supplement POH Cessna 172 R&S (FAA-Version) GROUND ROLL AND TAKE-OFF DISTANCE at 1111 kg (2450 lbs) SHORT FIELD TAKEOFF Conditions: Take-off weight 1111 kg (2450 lbs) Flaps 10° Full Power Prior to Brake Release Paved, level, dry runway Zero Wind Lift Off: .................51 KIAS...
  • Page 108 Supplement POH Cessna 172 R&S (FAA-Version) Ground Roll and Take-Off Distance [m] PRESS Outside Air Temperature [°C] [ft] -20°C 0°C 10°C 20°C 30°C 40°C 50°C Gnd Roll 15 m obst. Gnd Roll 1000 15 m obst. Gnd Roll 2000 15 m obst.
  • Page 109 Supplement POH Cessna 172 R&S (FAA-Version) Ground Roll and Take-Off Distance [ft] PRESS Outside Air Temperature [°C] [ft] -20°C 0°C 10°C 20°C 30°C 40°C 50°C Gnd Roll 1062 1194 50 ft obst. 1263 1460 1563 1679 1792 1979 2238 Gnd Roll...
  • Page 110 Supplement POH Cessna 172 R&S (FAA-Version) GROUND ROLL AND TAKE-OFF DISTANCE at 1134 kg (2500 lbs) SHORT FIELD TAKEOFF Conditions: Take-off weight 1134 kg (2500 lbs) Flaps 10° Full Power Prior to Brake Release Paved, level, dry runway Zero Wind Lift Off: .................51 KIAS...
  • Page 111 Supplement POH Cessna 172 R&S (FAA-Version) Ground Roll and Take-Off Distance [m] PRESS Outside Air Temperature [°C] [ft] -20°C 0°C 10°C 20°C 30°C 40°C 50°C Gnd Roll 15 m obst. Gnd Roll 1000 15 m obst. Gnd Roll 2000 15 m obst.
  • Page 112 Supplement POH Cessna 172 R&S (FAA-Version) Ground Roll and Take-Off Distance [ft] PRESS Outside Air Temperature [°C] [ft] -20°C 0°C 10°C 20°C 30°C 40°C 50°C Gnd Roll 1017 1119 1259 50 ft obst. 1332 1539 1647 1769 1889 2085 2359...
  • Page 113 Supplement POH Cessna 172 R&S (FAA-Version) TIME, FUEL AND DISTANCE TO CLIMB AT 1111 kg (2450 lbs) Conditions: Takeoff weight 1111 kg (2450 lbs) Climb speed v = 70 KIAS Flaps Up Full Power Standard Temperature (ISA) Notes: 1. Add 4 l (1.1 US gal) of fuel for engine start, taxi and takeoff allowance.
  • Page 114 Supplement POH Cessna 172 R&S (FAA-Version) Press. Time Distance Fuel used Alt. [ft] [°C] [KIAS] [FPM] [MIN] [NM] Gal] 1000 2000 3000 4000 5000 6000 11.8 7000 10.9 14.1 8000 12.6 16.5 9000 14.4 19.2 10000 16.3 22.0 11000 18.3 25.1...
  • Page 115 Supplement POH Cessna 172 R&S (FAA-Version) TIME, FUEL AND DISTANCE TO CLIMB AT 1134 kg (2500 lbs) Conditions: Takeoff weight 1134 kg (2500 lbs) Climb speed v = 70 KIAS Flaps Up Full Power Standard Temperature (ISA) Notes: 1. Add 4 l (1.1 US gal) of fuel for engine start, taxi and takeoff allowance.
  • Page 116 Supplement POH Cessna 172 R&S (FAA-Version) Press. Time Distance Fuel used Alt. [ft] [°C] [KIAS] [FPM] [MIN] [NM] Gal] 1000 2000 3000 4000 5000 10.0 6000 12.3 7000 11.3 14.7 8000 13.1 17.2 9000 15.0 20.0 10000 17.0 23.0 11000 26.2...
  • Page 117 Supplement POH Cessna 172 R&S (FAA-Version) MAXIMUM RATE-OF-CLIMB at 1111 kg (2450 lbs) Conditions: Take-off weight 1111 kg (2450 lbs) Climb speed v = 70 KIAS Flaps Up Full Power Notes: 1. For operation in air colder than this table provides, use cold- est data shown.
  • Page 118 Supplement POH Cessna 172 R&S (FAA-Version) MAXIMUM RATE-OF-CLIMB at 1134 kg (2500 lbs) Conditions: Take-off weight 1134 kg (2500 lbs) Climb speed v = 70 KIAS Flaps Up Full Power Notes: 1. For operation in air colder than this table provides, use cold- est data shown.
  • Page 119 Supplement POH Cessna 172 R&S (FAA-Version) CRUISE PERFORMANCE, RANGE AND ENDURANCE at 1111 kg (2450 lbs) Conditions: Take-off weight 1111kg (2450 lbs) Flaps Up Zero wind Notes: 1. Endurance information are based on 168.8 l (44.6 US gal) usable fuel.
  • Page 120 Supplement POH Cessna 172 R&S (FAA-Version) Endu- Press. Load Speed Fuel Flow Distance rance Alt. Time [ft] [KTAS] [mph] [l/h] [US Gal/h] [NM] [Hrs] 29.5 25.3 21.7 18.6 15.8 13.0 1006 11.9 2000 29.5 2000 25.3 2000 21.7 2000 18.6 2000 15.8...
  • Page 121 Supplement POH Cessna 172 R&S (FAA-Version) Endu- Press. Load Speed Fuel Flow Distance rance Alt. Time [ft] [KTAS] [mph] [l/h] [US Gal/h] [NM] [Hrs] 10000 25.3 10000 21.7 10000 18.6 10000 15.8 12000 25.3 12000 21.7 12000 18.6 12000 15.8 14000 25.3...
  • Page 122 Supplement POH Cessna 172 R&S (FAA-Version) CRUISE PERFORMANCE, RANGE AND ENDURANCE at 1134 kg (2500 lbs) Conditions: Take-off weight 1134kg (2500 lbs) Flaps Up Zero wind Notes: 1. Endurance information are based on 168.8 l (44.6 US gal) usable fuel.
  • Page 123 Supplement POH Cessna 172 R&S (FAA-Version) Endu- Press. Load Speed Fuel Flow Distance rance Alt. Time [ft] [KTAS] [mph] [l/h] [US Gal/h] [NM] [Hrs] 29.5 25.3 21.7 18.6 15.8 13.0 1006 11.9 2000 29.5 2000 25.3 2000 21.7 2000 18.6 2000 15.8...
  • Page 124 Supplement POH Cessna 172 R&S (FAA-Version) Endu- Press. Load Speed Fuel Flow Distance rance Alt. Time [ft] [KTAS] [mph] [l/h] [US Gal/h] [NM] [Hrs] 8000 15.8 8000 13.0 11.2 10000 25.3 10000 21.7 10000 18.6 10000 15.8 12000 25.3 12000 21.7...
  • Page 125 Supplement POH Cessna 172 R&S (FAA-Version) SECTION 6 WEIGHT & BALANCE Item Weight x Arm = Moment (kg) (mkp) Empty Weight plus Engine Oil -0.31 (6 l to 0.9 kg/l) plus Gearbox Oil -0.69 (1 l to 0.9 kg/l) plus unusable fuel 1.17...
  • Page 126 Supplement POH Cessna 172 R&S (FAA-Version) Your aircraft Mass Moment 1. Basic Empty Weight: Use the values for your airplane with the present equipment. Unusable fuel, engine oil, gearbox oil and coolant are included. 2. Usable Fuel (at 0.84 kg/l), max.
  • Page 127 Supplement POH Cessna 172 R&S (FAA-Version) LOAD MOMENT 20 0 18 0 16 0 14 0 12 0 10 0 100 l 50 l 10 0 15 0 2 00 30 0 35 0 Lo a d M o m e n t ( m k p )
  • Page 128 Supplement POH Cessna 172 R&S (FAA-Version) This page has been intentionally left blank Page 6-4 Issue 3 Revision -, June 2016...
  • Page 129 Supplement POH Cessna 172 R&S (FAA-Version) SECTION 7 AIRPLANE AND SYSTEMS DESCRIPTION INSTRUMENT PANEL Components of the new installation can be seen as example in the following figure. Some installations are equipped with a key switch for the starter instead of the push button and the switch "Engine Master" is designated "IGN".
  • Page 130 Supplement POH Cessna 172 R&S (FAA-Version) Figure 7-2 Example of Instrument panel 51. "Starter" - Push Button (Switch resp.) for Starter 52. "ALT" - Switch for Alternator 53. "BAT"- Switch for Battery 54. "Engine Master" ("IGN" resp.) - Switch electrical supply FA- 55.
  • Page 131 (FAA-Version) FUEL SYSTEM The fuel system of both TAE 125 installations includes the original tanks of the Cessna 172. Additional sensors for fuel temperature are installed. The fuel flows out of the tanks to the Fuel Selector Valve with the positions LEFT, RIGHT and BOTH, through a reservoir tank to the fuel shut-off valve and then via the electrically driven Fuel Pump to the fuel filter.
  • Page 132 Supplement POH Cessna 172 R&S (FAA-Version) Total capacity:......180.2 litres (47.6 US gallons) Total capacity of usable fuel: ..168.8 litres (44.6 US gallons) Total capacity each tank: ....90.1 litres (23.8 US gallons) Total capacity of usable fuel each tank: ........84.4 litres (22.3 US gallons)
  • Page 133 Supplement POH Cessna 172 R&S (FAA-Version) ELECTRICAL SYSTEM The electrical system of both engine installations differs from the previous installation and is equipped with the following operating and display elements: 1. Switch "Alternator" Controls the alternator. Must be ON in normal operation.
  • Page 134 Supplement POH Cessna 172 R&S (FAA-Version) 8. Switch "Force B" If the FADEC does not automatically switch from A-FADEC to the B-FADEC in case of an emergency despite of obvious necessity, this switch allows to switch manually to the B- FADEC.
  • Page 135 Supplement POH Cessna 172 R&S (FAA-Version) Figure 7-4a Basic wiring of the electrical system with alternator circuit breaker and without FADEC backup battery Page 7-7 Issue 3 Revision -, June 2016...
  • Page 136 Supplement POH Cessna 172 R&S (FAA-Version) Figure 7-4b Basic wiring of the electrical system with alternator switch and FADEC backup battery Page 7-8 Issue 3 Revision -, June 2016...
  • Page 137 Supplement POH Cessna 172 R&S (FAA-Version) FADEC-RESET In case of a FADEC-warning, one or both FADEC warning lights are flashing. If then the "FADEC" Test Knob is pressed for at least 2 seconds, the active warning lights will extinguish if it was a LOW category warning.
  • Page 138 Supplement POH Cessna 172 R&S (FAA-Version) The supply of warm air into the cabin is controlled through the cabin heat control knob. In normal operation the cabin heat control knob must be in OPEN position. In case of certain emergencies (refer to section 3), the control knob "Shut-off Cabin Heat"...
  • Page 139 Supplement POH Cessna 172 R&S (FAA-Version) Coolant level warning Cooling system TAE 125 schematic Expansion Tank Flow direction Coolant radiator Water pump Heating radiator Small External circuit circuit Engine Gearbox oil cooler (oil/ water heat exchanger) Gearbox oil Temperature sensor...
  • Page 140 Supplement POH Cessna 172 R&S (FAA-Version) This page intentionally left blank Page 7-12 Issue 3 Revision -, June 2016...
  • Page 141 Supplement POH Cessna 172 R&S (FAA-Version) SECTION 8 AIRPLANE HANDLING, SERVICE AND MAINTENANCE  WARNING: Do not start the engine in any case when filling levels are below the corresponding minimum marking.  CAUTION: Normally, a refill of coolant or gearbox oil between service intervals is not necessary.
  • Page 142 Supplement POH Cessna 172 R&S (FAA-Version) GEARBOX OIL To ensure the necessary propeller speed, both engine variants are equipped with a reduction gearbox filled with gearbox oil. (refer to section 1 of this supplement for specification) The level can be checked through a viewing glass on the lower leading edge of the gearbox.
  • Page 143 Supplement POH Cessna 172 R&S (FAA-Version) FUEL Both engine variants can be operated with kerosene (JET A-1, Jet A, Fuel No.3, TS-1 [TAE 125-02-99 only]) or Diesel fuel. Due to the higher specific density of turbine engine fuel or Diesel in...
  • Page 144 Supplement POH Cessna 172 R&S (FAA-Version) This page has been intentionally left blank Page 8-4 Issue 3 Revision 1, Mar. 2022...
  • Page 145 Supplement POH Cessna 172 R&S (FAA-Version) SECTION 9 SUPPLEMENTS TABLE OF CONTENTS No supplement Page 9-1 Issue 3 Revision -, June 2016...
  • Page 146 Supplement POH Cessna 172 R&S (FAA-Version) This page intentionally left blank Page 9-2 Issue 3 Revision -, June 2016...

This manual is also suitable for:

172 s

Table of Contents

Save PDF