Supplement Pilot´s Operating Handbook for the (Reims) Cessna (F) 172 F,G,H,I,K,L,M Equipped with TAE 125-01 and TAE 125-02-99 Installation
CESSNA F-172 H · Avionics Manual
Overview
This document is a supplement to the Pilot's Operating Handbook (POH) for the Reims Cessna 172 models F, G, H, I, K, L, and M equipped with the Thielert TAE 125-01 or TAE 125-02-99 engines. It provides critical information regarding the operation, limitations, and performance of these aircraft when fitted with the specified engines. The supplement is intended for pilots and maintenance personnel to ensure safe and efficient operation of the aircraft. It includes updated procedures, performance data, and safety warnings that supersede or add to the existing POH. The document is approved by EASA and must be used in conjunction with the approved POH.
- Maximum Ramp Weight: 1044 kg (2302 lbs)
- Maximum Takeoff Weight: 1043 kg (2300 lbs)
- Take-off Power: 99 kW (135 HP)
- Oil Temperature Limits: Min -32 °C, Max 140 °C
- Fuel Capacity for Standard Tanks: 125.7 l (33.2 US gal)
Document
Source
Originally published by www.tmg-service.de. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Avionics Manual
- Year
- 2013
- Pages
- 118
- File size
- 3.1 MB
- Publisher
- www.tmg-service.de
Common. Rarer than 1% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the CESSNA F-172 H.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the F172H to your watchlist and track it in one place.
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- SCHEDULE OF AIRWORTHINESS DIRECTIVESAirworthiness Directives
- PILOT AND COPILOT SECONDARY SEAT STOP INSTALLATIONService Bulletins
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In this document
General
This section outlines the conventions and warnings that must be followed to ensure safe operation of the aircraft. It emphasizes the importance of using the most current version of the POH supplement and provides guidelines for updates and revisions.
Limitations
This section details the weight limits for both Normal and Utility categories, including maximum ramp, takeoff, and landing weights. It also specifies maneuver limits and flight load factors, emphasizing the prohibition of intentional spins and negative G maneuvers.
Engine Operating Limits
The engine operating limits for the TAE 125-01 and TAE 125-02-99 engines are specified, including maximum power output of 99 kW (135 HP) and RPM limits. Temperature limits for oil and coolant are provided, along with fuel temperature limits.
Fuel System
The fuel system section describes the configuration of the fuel tanks, including total capacities and usable fuel amounts for different tank configurations. It also includes cautions regarding fuel selection during flight.
Electrical System
This section describes the electrical system components, including switches for the main bus, battery, and alternator, as well as the FADEC backup battery. It highlights the importance of maintaining electrical power for engine operation.
Safety notes
- Non-compliance with safety rules could lead to injury or death.
- Use of unapproved fuels may result in engine damage.
- The engine must not be started if coolant levels are low.
Full document text
Thielert Aircraft Engines GmbH Tel. +49-(0)37204/ 696-0 Platenenstr. 14 THIELERT D 09350 Lichtenstein AIRCRAFT ENGINES Fax +49-(0)37204/696-2912 www.centurion-engines.com info@centurion-engines.com Supplement Pilot's Operating Handbook for the (Reims) Cessna (F) 172 F.G.H.I.K.L.M Equipped with TAE 125-01 and TAE 125-02-99 MODEL No. SERIAL No. Installation REGISTER No. Issue 3 This supplement must be attached to the EASA approved Pilot's Operating Handbook when the TAE 125-01 or TAE 125-02-99 installation has been installed in accordance with EASA STC A.S.01527 or EASA STC 10014287. The information contained in this supplement supersede or add to the information published in the EASA approved Pilot's Operating Handbook only as set forth herein. For limitations, procedures, performance and loading information not contained in this supplement, consult the EASA approved Pilot's Operating Handbook. This supplement Pilot's Operating Handbook is approved with EASA AFM Approval 10031525. TAE-Nr.: 20-0310-21023 This page intentionally left blank Supplement POH Reims/Cessna (F) 172 F,G,H,I,K,L,M APPROVAL THIELERT AIRCRAFT ENGINES The content of approved chapters is approved by EASA. All other content is approved by TAE under the authority of EASA DOA No. EASA.21J.010 in accordance with Part 21. LOG OF REVISIONS Approved Revision Section Description Date Endorsed 3/0 all new Issue 23.08.2010 EASA AFM Approval 3/1 1 New oil, editorial changes April 14, 2011 2 New oil 3 Procedures updated 4 Procedures updated 5 Editorial changes 6 Editorial changes 7 New section 10031525 Revision No. 1 to AFM supplement ref. 20-0310-21023 is approved under the authority of DOA ref. EASA.21J.010. Date: April 14, 2011 Office of Airworthiness Page iii Issue 3 Revision 5, May 2013 THIELERT AIRCRAFT ENGINES Supplement POH Reims/Cessna (F)172 F,G,H,I,K,L,M Approved Revision Section Description Date Endorsed 3/2 1 New gearbox oil, editorial changes June 30, 2011 2 New gearbox oil 3/3 1 3/4 1 4 Procedures updated LO 5 Editorial changes New fuel, new gearbox oil March 16, 2 New fuel, new gearbox oil 4 New fuel, 9 Procedures updated New fuel 2012 New fuel, new gearbox oil March 11, 2 New fuel, new gearbox oil LO 5 Editorial changes Page iv Issue 3 Revision 5, May 2013 2013 Revision No.4 to AFM supplement ref. 20-0310-21023 is approved under the authority of DOA Date March 11 2013 ref. EASA.21J.010. Office of Airworthiness Revision No. 3 to AFM supplement ref. 20-0310-21023 is approved under the authority of DOA ref. EASA.21J.010 Date: March 16, 2012 Office of Airworthiness Revision No. 2 to AFM supplement ref. 20-0310-21023 is approved under the authority of DOA ref. EASA.21J.010. Date June 30, 2011 Office of Airworthiness Supplement POH Reims/Cessna (F)172 F,G,H,I,K,L,M Revision Section 3/5 Description THIELERT ARCAT DES Approved Date Endorsed EASA STC/AFM numbers May 27, 2013 corrected on the cover Revision No.5 to AFM supplement ref. 20-0310-21023 is approved under the authority of DOA ref. EASA.21J.010. Date May 27, 2013 Office of Airworthiness Remark: The parts of the text which changed are marked with a vertical line on the margin of the page. Page v Issue 3 Revision 5, May 2013 THIELERT AIRCRAFT ENGINES Supplement POH Reims/Cessna (F)172 F,G,H,I,K,L,M LIST OF APPLICABLE CHAPTERS Sections Issue/Revision Date 1 3/4 March 2013 2 3/4 March 2013 3 3/1 April 2011 4 3/3 March 2012 5 3/3 March 2013 00 6 7 3/2 March 2012 3/0 April 2011 General remark The content of this POH supplement is developed on basis of the EASA-approved POH. Page vi Issue 3 Revision 5, May 2013 THIELERT AIRCRAFT ENGINES Supplement POH Reims/Cessna (F)172 F,G,H,I,K,L,M TABLE OF CONTENTS COVER SHEET LOG OF REVISIONS... .page iii LIST OF APPLICABLE CHAPTERS..... ..page vi GENERAL REMARK page vi TABLE OF CONTENTS page vii CONVERSION TABLES ..... page viii ABBREVIATIONS........ .page xii SECTION 1 GENERAL SECTION 2 SECTION 3 SECTION 4 SECTION 5 SECTION 6 (a non-approved chapter) LIMITATIONS (an approved chapter) EMERGENCY PROCEDURES (a non-approved chapter) NORMAL PROCEDURES (a non-approved chapter) PERFORMANCE (a non-approved chapter) APPENDIX (a non-approved chapter) SECTION 7 SUPPLEMENTS Page vii Issue 3 Revision 3, March 2012 Supplement POH Reims/Cessna (F) 172 F,G,H,I,K,L,M CONVERSION TABLES Unit [Abbr.] Liter [1] US gallon [US gal] US quart [US qt] Imperial gallon [Imp gal] Cubic inch [in³] Unit [Abbr.] Kilopondmeter [kpm] Foot pound [ft.lb] Inch pound [in.lb] Unit [Abbr.] Degree Celsius [°C] Degree Fahrenheit [°F] Unit [Abbr.] Kilometers per hour [km/h] Meters per second [m/s] Miles per hour [mph] Knots [kts] Feet per minute [fpm] VOLUME Conversion factor SI to US/ Imperial [I]/3.7854 = [US gal] [1] / 0.9464 = [US qt] [1] 4.5459 = [[Imp gal] [1] x 61.024 = [in³] TORQUE Conversion factor SI to US/Imperial [kpm] x 7.2331 = [ft.lb] [kpm] x 86.7962 = [in.lb] TEMPERATURE Conversion factor SI to US/Imperial [°C] × 1.8 + 32 = [°F] SPEED Conversion factor SI to US/Imperial [km/h]/1.852 = [kts] [km/h] 1.609 = [mph] [m/s] x 196.85 = [fpm] THIELERT Conversion factor US / Imperial to Si AIRCRAFT ENGINES [US gal] x 3.7854 = [1] [[US qt] x 0.9464 = [1] [[Imp gal] x 4.5459 = [1] [in³] / 61.024 = [1] Conversion factor US / Imperial to Si [ft.lb] / 7.2331 = [kpm] [in.lb] / 86.7962 = [kpm] Conversion factor US / Imperial to Si ([F] - 32) / 1.8 = [°C] Conversion factor US / Imperial to Si [mph] x 1.609 = [km/h] [kts] x 1.852 = [km/h] [fpm] 196.85 = [m/s] Page viii Issue 3 Revision 3, March 2012 THIELERT AIRCRAFT ENGINES Supplement POH Reims/Cessna (F)172 F,G,H,I,K,L,M Unit [Abbr.] Bar [bar] Hectopascal [hpa] =Millibar [mbar] Pounds per square inch [psi] inches of mercury column [inHg] Unit [Abbr.] Kilogramm [kg] Pound [lb] Unit [Abbr.] Meter [m] Millimeter [mm] Kilometer [km] Inch [in] Foot [ft] Nautical mile [nm] Statute mile [sm] Unit [Abbr.] Newton [N] Decanewton [daN] Pound [lb] PRESSURE Conversion factor SI to US/ Imperial [bar] x 14.5038 = [psi]
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[hpa] / 33.864= [inHg] [mbar] / 33.864 = [inHg] MASS Conversion factor SI to US/ Imperial [kg] / 0.45359 = [lb] LENGTH Conversion factor SI to US/ Imperial [m]=0.3048 [ft] [mm] = 25.4 [in] [km] = 1.852 [nm] [km] / = 1.609 [sm] FORCE Conversion factor SI to US/Imperial [N] / 4.448 = [lb] [daN] / 0.4448 = [lb] Conversion factor US / Imperial to Si psi] 14.5038 = [bar] [inHg] x 33.864 = [hPa] [inHg] x 33.864 = [mbar] Conversion factor US / Imperial to Si [lb] x 0.45359 = [kg] Conversion factor US / Imperial to Si [in] x 25.4 = [mm] [ft] x 0.3048 = [m] [nm] x 1.852 = [km] [sm] x 1.609 = [km] Conversion factor US / Imperial to Si [lb] x 4.448 = [N] [lb] x 0.4448 = [daN] Page ix Issue 3 Revision 3, March 2012 Supplement POH Reims/Cessna (F) 172 F,G,H,I,K,L,M THIELERT AIRCRAFT ENGINES °C °F 150 302 140 282 130 262 120 242 110 Fuel Quantity 222 100 [US gal] ▲ [liter] 202 90 90 182 80 162 70 40 150 60 0 60 142 50 40 50 40 122 102 30 30 30 100 883 82 20 20 4 62 10 20 42 0 22 -10 50 2 -20 10 -18 -30 -40 -38 -50 -58 Page x Issue 3 Revision 3, March 2012 THIELERT AIRCRAFT ENGINES Supplement POH Reims/Cessna (F)172 F,G,H,I,K,L,M Load Mass [lb]▲ 500 225 Load Moment [kg] [kgm] A[in.lb] 50,000 200 400 175 300 150 125 100 200 75 50 100 25 Page xi Issue 3 Revision 3, March 2012 500 40,000 400 30,000 ||||||| |||| |||| |||| |||| |||| |||| |||| |||| |||| |||| 300 20,000 200 10,000 100 Supplement POH Reims/Cessna (F) 172 F,G,H,I,K,L,M TAE FADEC CED 125 AED 125 ABBREVIATIONS THIELERT AIRCRAFT ENGINES Thielert Aircraft Engines GmbH, developing and manufacturing company of the TAE 125 engine Full Authority Digital Engine Control Compact Engine Display Multifunctional instrument for indication of engine data of the TAE 125 Auxiliary Engine Display Multifunctional instrument for indication of engine and airplane data Page xii Issue 3 Revision 3, March 2012 Supplement POH Reims/Cessna (F) 172 F,G,H,I,K,L,M SECTION 1 GENERAL CONVENTIONS IN THIS HANDBOOK THIELERT AIRCRAFT ENGINES This manual contains following conventions and warnings. They should be strictly followed to rule out personal injury, property damage, impairment to the aircraft's operating safety. or damage to it as a result of improper functioning. ▲ WARNING: ■ CAUTION: Note: Non-compliance with these safety rules. could lead to injury or even death. Non-compliance with these special notes and safety measures could cause damage to the engine or to the other components. Information added for a better understanding of an instruction. UPDATE AND REVISION OF THE MANUAL ▲ WARNING: Note: A safe operation is only assured with an up to date POH supplement. Information about actual POH supplement issues and revisions are published in the TAE Service Bulletin TM TAE 000-0004. The TAE-No of this POH supplement is published on the cover sheet of this supplement. Page 1-1 Issue 3 Revision 4, March 2013 THIELERT AIRCRAFT ENGINES Supplement POH Reims/Cessna (F)172 F,G,H,I,K,L,M ENGINE Engine manufacturer:. Engine model:......... Thielert Aircraft Engines GmbH TAE 125-01 or TAE 125-02-99 The TAE 125-02-99 is the successor of the 125-01. Both engine variants have the same power output and the same propeller speeds but different displacement. While the TAE 125-01 has 1689 ccm, the TAE 125-02-99 has 1991 ccm. Both TAE 125 engine variants are liquid cooled in-line four-stroke 4-cylinder motors with DOHC (double overhead camshaft) and are direct Diesel injection engines with common-rail technology and turbocharging. Both engine variants are controlled by a FADEC system. The propeller is driven by a built-in-gearbox (i=1.69) with mechanical vibration damping and overload release. The engine variants have an electrical self starter and an alternator. WARNING: The engine requires an electrical power source for operation. If the main battery and alternator fail simultaneously, the engine will only operate for a maximum of 30 minutes on FADEC backup battery power. Therefore, it is important to pay attention to indications of alternator failure. Due to this specific characteristic, all of the information from the flight manual recognized by EASA are no longer valid with reference to: carburetor and carburetor pre-heating ignition magnetos and spark plugs, and mixture control and priming system PROPELLER Manufacturer: Model: ...... Number of blades:... Diameter: Type: ..... MT Propeller Entwicklung GmbH .... MTV-6-A/187-129 3 1.87 m .constant speed Page 1-2 Issue 3 Revision 4, March 2013 Supplement POH Reims/Cessna (F) 172 F,G,H,I,K,L,M THIELERT AIRCRAFT ENGINES FUELS and LIQUIDS ■ CAUTION: Fuel: Alternative: Use of unapproved fuels may result in damage to the engine and fuel system components, resulting in possible engine failure. .JET A-1/JET-A (ASTM 1655) Diesel (DIN EN 590) Fuel No.3 (GB 6537-2006) JP-8, JP-8+100 (MIL-DTL-83133E) Only TAE 125-02-99 (C2.0): Engine oil: TS-1 (GOST 10227-86) .TS-1 (GSTU 320.00149943.011-99) AeroShell Oil Diesel Ultra AeroShell Oil Diesel 10W-40 .Shell Helix Ultra 5W-30 .Shell Helix Ultra 5W-40 Gearbox oil: Shell Getriebeöl EP 75W-90 API GL-4 Shell Spirax EP 75W-90 .Shell Spirax GSX 75W-80 GL-4 Shell Spirax S4 G 75W-90 Shell Spirax S6 GXME 75W-80 Only TAE 125-02-99 (C2.0): CAUTION: Shell Spirax S6 ATF ZM Use approved oil with exact declaration only! Water/Radiator Protection at a ratio of 50:50 BASF Glysantin Protect Plus/G48 Coolant:....... Radiator Protection: WARNING: ■ CAUTION: Mobil Antifreeze Extra/G48 .ESSO Antifreeze Extra/G48 Comma Xstream Green - Concentrate/G48 Zerex Glysantin G 48 The engine must not be started under any circumstances if the level is too low. Normally it is not necessary to fill the cooling liquid or gearbox oil between maintenance intervals. If the level is too low, please notify the service department immediately. Page 1-3 Issue 3 Revision 4, March 2013
What's in the CESSNA F-172 H TCDS
A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.