Maintenance Manual

Publication Title Hand Portable Halon 1211 Fire Extinguisher Maintenance Manual Manufacturer Amerex Corp. P.O. Box 81 Trussville, AL 351 73-0081 CHAPTER 30 - ICE AND RAIN EQUIPMENT Publica- tion Part Number Publication Title 830415 McCauley Electrothermal De-Ice Systems Service, Parts and Installation Manual Manufacturer McCauley Propeller Systems 3535 McCauley Drive Vandalia, OH 45377 CHAPTER 32 - LANDING GEAR Publication Title Component Maintenance Manual Manufacturre Cleveland Wheels and Brakes! Parker Aerospace Parker Hannifin Corporation 1160 Center Road Avon, OH 44011 CHAPTER 34 - NAVIGATION Publication Title M881000D Altitude Encoder! Digitizer Owner! Installation Manual 006- 001 84- 0005 006- 10522- 0001 KAP 140 006- 00991- 0000 006- 10543- 0000 Installation Manual Installation Manual Installation Manual Installation Manual Manufacturer Trans-Cal Industries, Inc. 16141 Cohasset St. Van Nuys, CA 91406 Allied Signal Allied Signal Allied Signal Allied Signal LIST OF MANUFACTURERS TECHNICAL ©Cessna Aircraft Company PUBLICATIONS Page 4 Janl1/2007 Item Cessna Part Number Fire Extin- guisher Manufact- urers Part Numbre A352 GS Publica- tion Part N umber Item Cessna Part Number Manufact- urers Part N umber None Propeller De-ice System Item Cessna Part Number Manufact- urers Part Number Cleveland Wheels and Brakes Publica- tion Part Number None Item Cessna Part Number Blind Encoder Manufact- urers Part Number SSD1 20-20 Pu blica- tion Part Number Automatic Direction Finder Global Positioning System Autopilot KR87 KLN89/89B Nay Indicators K1209A CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL CHAPTER 34 - NAVIGATION Manufact- urers Part Number Publica- tion Part N urnber K1208/209 006-0 140- 0003 Publication Title Installation Manual G1000 Line Maintenance Manual G1000 Line Maintenance Manual G1000 Line Maintenance Manual G1000 Line Maintenance Manual G1000 Line Maintenance Manual G1000 Line Maintenance Manual G1000 Line Maintenance Manual Manufacturer Allied Signal Garmin USA 1200 East 151st Street Olathe, KS 66062 Garmin USA Garmin USA Garmin USA Garmin USA Garmin USA Garmin USA CHAPTER 71 - POWERPLANT Manufact- urers Part Number 10-540- AClA5 Publica- tion Part Number 10-540- ACi A5 Publication Title Operator's Manual Textron Lycoming Aircraft Engines Parts Catalog 10-540- Direct Drive Engine AClA5 Overhaul Manual T10-540- Operator's Manual AJ1A Textron Lycoming Aircraft Engines TIO-540- Parts Catalog AJ 1A TIO-540- Direct Drive Engine AJ11A Overhaul Manual LIST OF MANUFACTURERS TECHNICAL © Cessna Aircraft Company Manufacturer Textron Lycoming 652 Oliver Street Williamsport, PA 17701 Textron Lycoming Textron Lycoming Textron Lycoming Textron Lycoming Textron Lycoming PUBLICATIONS Page 5 Janl1/2007 Item Cessna Part N urnber Nay Indicators GDC 74 Air Data Unit GIA 63 Integrated Avionics Unit GMU 44 Magne- tometer GRS 77 AHRS GTX 33 Transpon- der GDU 1040 (PFD/MFD) GMA 1347 Audio Panel Item Cessna Part Number Engine (206) Engine (206) Engine (206) Engine (T206) Engine (T206) Engine (T206) CESSNA AIRCRAFT COMPANY MODEL 2061T206 MAINTENANCE MANUAL CHAPTER 73 - ENGINE FUEL AND CONTROL Publica- Publication Title tion Part Number 15-338D RSA-5 & RSA- 10 Fuel Injection Systems Operation & Service Manual 15-810B Troubleshooting Techniques for the Precision Airmotive RSA Fuel Metering System 15-895G Index of Manuals, Bulletins, and Service Information Letters for Precision Airmotive Fuel Controls Manufacturer Precision Airmotive 3220 100th St S.W.#E Everett, WA 98204 Precision Airmotive Precision Airmotive CHAPTER 74 - IGNITION Manufact- urers Part Number Publica- tion Part Number Publication Title 6351/6361 L-1 363C 4300/6300 Series Magneto Maintenance and Overhaul Manual Manufacturer Slick Aircraft Products 530 Blackhawk Park Ave. Rockford, IL 61104 LIST OF MANUFACTURERS TECHNICAL PUBLICATIONS Page 6 (DCessna Aircraft Company Janl1/2007 Item Cessna Part Number Manufact- urers Part Number Fuel Injection System RSA- 10ED1 Fuel Injection System 0 RSA- 10ED1 Fuel Injection System RSA- 10ED1 Item Cessna Part Number Magneto 0 CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL SERVICE BULLETIN LIST Service Bulletin Number SB99-71 -01 R2 SB99-21 -01 SB99-28-01 SB99-34-01 R1 SB99-71 -03 SB99-73-03 SB99-71 -04 SB99-25-01 R1 SB99-71 -05 SB99-71 -06 SBOO-24-01 SBOO-1 1-02 SBOO-22-01 SBOO-24-02 SBOO-25-01 SBOO-34-01 SBOO-53-02 SBOO-55-02 SBOO-61 -01 SBOO-73-01 R2 SBOO-79-01 R1 SB99-24-02 SB99-37-01 SBOO-27-02 R1 SBOO-32-01 Title Engine Piston Pin Plug Wear Inspection Fresh Air Vent Replacement Wing Fuel Tank Vent Check Valve Inspection KLN 89B GPS Navigation System Modification Engine Exhaust To Baffle Clearance Engine Fuel Pump Relief Valve Cover Screws Torque Inspection Alternate Air Door Hinge Assembly Inspection! Replacement Emergency Locator Transmitter (ELT) Operational Test Engine Valve Seat Inspection Engine Exhaust Tailpipe Lanyard Installation And Fuel Flow Transducer Relocation Main Power Junction Box Circuit Breaker Retrofit Kit Installation Pilot's Operating Handbook And Pilot's Checklist Revisions KAP-140 Autopilot Servo Inspection/Modification Electrical Panel Wiring Modifications Engine Winterization Kit Installation Pitot Tube Heater Assembly Insulation Installation Rivet Inspection/Installation Elevator Trim Tab Modification Propeller Governor Control Cable Routing Modification Engine Fuel Injection Lines And Support Clamps Inspection Engine Low Oil Pressure Swi tch Replacement Circuit Panel Assembly Cover Installation Vacuum Hose Modification Aileron Control Cable Quadrant Inspection! Modification Nose Landing Gear Strut Brace And Drag Link Clearance Inspection Service Bulletin Date 7/12/99 3/12/99 4/26/99 7/12/99 8/16/99 9/13/99 9/13/99 12/27/99 10/25/99 12/06/99 3/13/00 4/24/00 2/14/00 6/5/00 1/31/00 4/10/00 6/12/00 7/31/00 7/3/00 12/24/01 2/21/00 12/27/00 12/27/00 11/06/00 11/20/00 Manual Incorporation 9/02/99 9/02/99 9/02/99 9/02/99 9/20/99 9/02/99 9/02/99 3/31/00 3/31/00 3/31/00 3/31/00 9/15/00 9/15/00 9/15/00 9/15/00 9/15/00 9/15/00 9/15/00 9/15/00 No Effect 9/15/00 4/18/01 4/18/01 4/18/01 4/18/01 ©Cessna Aircrafl Company SERVICE BULLETIN LIST Page 1 Jul 1/2007 CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL Service Bulletin Number SBOO-37-01 SBOO-55-03 SBO01 -28-0 1 SBOl-11-01 SBO1 -73-01 R2 SBOl-11-03 SBOl-11-04 SBOl-74-01 SBO1 -25-01 SBO01 -28-05 SBOl -73-02 SBOl-71-04 SBO01 -53-02 SB02-1 1-03 SB02-11 -04 SB02-22-01 SB02-25-01 SB02-34-01 SB02-37-02 SB02-37-03 SB02-37-04 SB02-52-01 SB02-71 -01 SB02-71 -02 SB02-71 -02 R1 SB02-71 -03 Title Vacuum System Air Filter Element Inspection/ Replacement Horizontal Stabilizer Reinforcement Inspection/ Modification Fuel Selector Shaft Assembly Inspection/ Replacement Pilots Operating Handbook Revision Engine Driven Fuel Pump Inspection Airplane Weight, Balance And Installed Equipment Data Sheet Revision Pilot's Operating Handbook And Pilot's Checklist Revisions Ignition Switch Center Ground Terminal Inspection Glareshield Shroud Installation Fuel Line Inspection Engine Driven Fuel Pump Relief Valve Housing Replacement Engine Oil Filler Tube Replacement/Modification Battery Box Tray Liner Installation Pilot's Operating Handbook And Pilot's Checklist Revisions Pilot's Operating Handbook And Pilot's Checklist Revisions Honeywell KAP 140 Autopilot System Modification Pilot And Copilot Shoulder Harness Guide Removal Goodrich WX-500 Weather Mapping Sensor Modification Dry Vacuum Pump And Coupling Replacement Requirements Vacuum System Reducer Fitting Replacement Airborne Air And Fuel Products Check Valve Manifold Inspection Cabin Door Handle Replacement Engine Cylinder Drain Can Installation Engine Crankshaft Core Sample Inspection Engine Crankshaft Core Sample Inspection Engine Crankshaft Gear Retaining Bolt Replacement Service Bulletin Date 8/14/00 8/28/00 1/22/01 2/05/01 10/17/05 6/25/01 7/2 3/0 1 6/25/01 12/24/01 12/24/01 9/1 701 10/29/01 9/03/02 5/13/02 9/13/02 11/25/02 8/29/02 11/25/02 2/18/02 2/18/02 10/28/02 1/21/02 8/05/02 9/23/02 12/23/02 10/07/02 Manual Incorporation 4/18/01 4/18/01 10/15/01 10/15/01 10/15/01 10/15/01 No Eff ect 10/15/01 No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect 12/02/02 No Eff ect 4/05/04 No Eff ect SERVICE BULLETIN ©Cessna Aircraft Company LIST Page 2 Jul 1/2007 CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL Service Bulletin Number SB02-71 -03 R2 SB02-71 -05 SB02-71 -05 R1 Title Engine Crankshaft Gear Retaining Bolt Replacement Engine Oil Pump Plug Inspection Engine Oil Pump Plug Inspection Service Bulletin Date 5/10/04 Manual Incorporation No Effect 11/29/02 2/03/03 Honeywell KMA 26 Audio Panel Modification Alternator Replacement MC01-3A Main Electrical Power Junction Box Modification Flap Control Bracket Attach Bolts Replacement Fuel Cap Lanyard Removal Nose Landing Gear Wheel Fairing Modification Honeywell KS 270C, KS 271C and KS 272C Servo Friction Inspection Altimeter Inspection Vacuum Manifold Inspection/Replacement Bottom Cabin Door Post To Main Landing Gear Spring Inspection Bottom Cabin Door Post To Main Landing Gear Spring Inspection Throttle Arm Retention Inspection Cargo Door Placard Installation Inspection/ Mod ification Alternator Control Unit Inspection/Replacement Crew Seat Recline Modification Crew Seat Back Cylinder Lock Inspection And Crank Arm Modification Crew Seat Back Cylinder Lock Control Inspection/Adjustment Marker Beacon Placard Installation Security Lock Installation Bulkhead Rivet Inspection Firewall Sealant Application Engine Fuel Injection Lines And Support Clamps Inspection Engine Fuel Manifold Spring Replacement Cargo Door Decals And Center Passenger Seats Placard Inspection/Replacement C Cessna Aircraft Company SERVICE BULLETIN LIST Page 3 Janl1/2007 SB03-23-01 SB03-24-01 SB03-24-02 SB03-27-02 SB03-28-01 SB03-32-01 SB03-34-01 SB03-34-02 R1 SB03-37-01 SB03-53-02 SB03-53-02 R1 SB03-73-01 SB04-1 1-04 SB04-24-0 1 SB04-25-01 R1 SB04-25-02 R1 SB04-25-04 SB04-34-0 1 SB04-52-01 SB04-53-01 SB04-53-04 SB04-73-01 SB04-73-02 SB05-1 1-01 7/28/03 7/28/03 10/13/03 12/22/03 10/27/03 9/29/03 10/27/03 2/16/04 11/10/03 5/26/03 6/23/03 11/04/03 8/30/04 11/04/04 6/14/04 10/17/05 10/11/04 11/22/04 6/28/04 3/01/04 12/20/04 8/30/04 10/11/04 3/28/05 No Eff ect No Effect 1/02/06 No Effect No Eff ect No Eff ect No Eff ect No Effect No Effect No Effect No Eff ect No Eff ect No Eff ect No Effect No Eff ect No Effect No Effect No Eff ect 1/2/06 No Eff ect No Effect No Eff ect CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL Service Bulletin Number SB05-1 1-02 SB05-22-01 SB05-24-01 SB05-25-03 R1 SB05-28-01 SB05-33-01 SB05-34-01 SB05-34-02 SB05-34-03 SB05-34-04 SB05-34-05 SB05-34-06 SB05-34-07 SB05-34-08 SB05-34-09 SB05-34-1 1 SB05-34-l12 SB05-35-01 SB05-37-01 SB05-53-01 SB05-71 -01 SB05-71 -02 SB05-73-01 SB06-111-01 SB06-1 1-02 SB06-22-01 SB06-24-01 SB06-24-03 SB06-24-04 Title Pilot's Operating Handbook Revisions Trim Servo Cable Chain Inspection MC01 -3A Main Electrical Power Junction Box Circuit Breakers Inspection Inflatable Seat Restraints Installation Fuel Strainer Gasket Inspection High Intensity Discharge (Hid) Landing And Taxi Light Installation Garmin G1000 System Software Upgrade Garmin GMA 1347 Audio Panel Modifications Garmin GIA 63 Integrated Avionics Unit Modification Garmin GIA 63 Integrated Avionics Unit Modification Garmin G1000 System Software Upgrade Garmin G1000 GDL-69A Weather And Digital Audio Entertainment Interface Installation Garmin G1000 Obstacle And Terrain Avoidance System Database Update Garmin G1000 System Software Upgrade Garmin G1000 GDL-69A Weather And Digital Audio Entertainment Interface Installation Garmin GIA 63 Integrated Avionics Unit Outside Cover Replacement Garmin GIA 63 Integrated Avionics Unit Outside Cover Replacement Oxygen System Pressure Gage Replacement Vacuum Pump Inspection/Replacement Fuselage Rivet Inspection Engine Crankshaft Replacement Engine Cylinder Drain System Inspection Engine Driven Fuel Pump Inspection Pilot's Operating Handbook Revisions Pilot's Checklist Revisions Honeywell KS270C Pitch Servo And KS271 C Roll Servo Tach Generator Modification Electrical Ground Strap Inspection 60 Ampere Alternator Brush Replacement Circuit Breaker Inspection Service Bulletin Date 3/28/05 12/5/05 1/31/05 Dec 26/06 1/17/05 5/09/05 1/31/05 2/14/05 2/14/05 4/25/05 7/29/05 7/29/05 9/26/05 9/26/05 9/26/05 11/21/05 12/5/05 3/28/05 11/7/05 3/14/05 7/18/05 12/19/05 3/07/05 Mar 27/06 Nov 6/06 Apr 24/06 May 8/06 Dec 18/06 Dec 26/06 Manual Incorporation No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect 1/02/06 No Effect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect ©Cessna Aircraft Company SERVICE BULLETIN LIST Page 4 Jul 1/2007 CESSNA AIRCRAFT COMPANY MODEL 2061T206 MAINTENANCE MANUAL Service Bulletin Number SB06-24-05 SB06-25-01 SB06-27-01 SB06-32-01 SB06-34-01 SB06-34-02 R1 Title Circuit Breaker Panel Assembly Inspection Restraint System Child Buckle Inspection Flap Aft Roller Bearing Installation Modification Brake Master Cylinder Covers Inspection Honeywell KT 73 Mode S Transponder Installation Garmin G1000 System Software Upgrade Service Bulletin Date Dec 26/06 Dec 4/06 Apr 10/06 Sep 25/06 Feb 27/06 Mar 27/06 Manual Incorporation No Eff ect No Effect No Effect No Eff ect No Eff ect No Eff ect Enablement Of Garmin G1000 Terrain Awareness Warning System Class-B3 (Taws-B) Automatic Direction Finder (ADF) and Distance Measuring Equipment (DME) Installation Cabin Door Modification Main landing Gear Attach Fittings Fastners; Inspection Engine Crankshaft Retirement Engine Compartment Fuel Hoses Security Inspection © Cessna Aircraft Company SERVICE BULLETIN LIST Page 5 Jul 1/2007 SB06-34-03 SB06-34-04 SB06-52-01 SB06-53-02 SB06-71 -01 R1 SB06-71 -02 May 22/06 Oct 23/06 Mar 27/06 Nov 20/06 May 8/06 Jun 19/06 No Effect No Eff ect No Eff ect No Eff ect No Eff ect No Effect CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL INTRODUCTION 1. General WARNING: All the inspection intervals, replacement time limits, overhaul time limits, method of inspection, life limits, cycle limits, etc., recommended by Cessna are based on the use of new, remade, or overhauled Cessna-approved parts. If the parts are designed, made, remade, overhauled, and/or approved by someone other than Cessna, then the data in Cessna's maintenance/service manuals and parts catalogs are no longer applicable and the purchaser is warned not to rely on such data for non-Cessna parts. All inspection intervals, replacement time limits, overhaul time limits, the method of inspection, life limits, cycle limits, etc., for such non-Cessna parts must be received from the manufacturer and/or seller of such non-Cessna parts. A. The information in this publication is based on data available at the time of publication. This publication is updated, supplemented, and automatically changed by all information issued in Service Newsletters, Service Bulletins, Supplier Service Notices, Publication Changes, Revisions, Reissues and Temporary Revisions. All such changes become part of and are incorporated in this publication. Users must keep informed of the latest changes to this publication through information available at Cessna Authorized Service Stations or through the Cessna Product Support subscription services. The Cessna Service Stations have also been supplied with a group of supplier publications which gives disassembly, overhaul, and parts breakdowns for some of the different supplier equipment items. Supplier's publications are updated, supplemented, and changed by supplier issued revisions and service information. Cessna may reissue this publication, which will amend this publication; and is communicated to the field through the Cessna's Authorized Service Stations and/or through Cessna's subscription services. B. Inspection, maintenance and parts requirements for STC installations are not included in this manual. When an STC installation is incorporated on the airplane, you must have an inspection completed on those parts of the airplane affected by the installation. The inspection must be in accordance with the inspection program published by the owner of the STC. Since the STC installations may change systems interface, operating characteristics, component loads or stresses on adjacent structures, Cessna supplied inspection criteria may not be correct for airplanes with STC installations. C. Revisions, reissues and temporary revisions can be purchased from a Cessna Service Station or directly from Cessna Propeller Aircraft Product Support, Department 751, Cessna Aircraft Company, P.O. Box 7706, Wichita, Kansas 67277-7706. D. The information in this Maintenance Manual is applicable to all U.S. and Foreign Certified Model 206/ T206 airplanes beginning at Serial 206080001 and On for non-turbocharged airplanes and beginning at Serial T20608001 for turbocharged airplanes. Information unique to a particular country is identified in the chapter(s) affected. E. All the supplemental service information that is applicable to this manual is supplied to all applicable Cessna Service Stations so that they have the latest authoritative instructions to service these Cessna airplanes. It is recommended that Cessna owners use the knowledge and experience of the Cessna Service Organization. 2. Cross-Reference Listing of Popular Name Versus Model Numbers and Serials A. All the airplanes are certified under the model number designations. For market purposes, popular names are frequently used. To refer to these airplanes and give a consistent method, the model number will be used in this publication unless the popular name is necessary to identify the versions of the same basic model. The table that follows gives a list of popular names, model numbers and serial numbers. INTRODUCTION Page 1 © Cessna Aircraft Company Dec 2/2002 CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL NAME MODEL SERIALS BEGINNING Stationair 206H 20608001 Stationair TC T206H T20608001 3. Coverage and Format A. The Cessna Model 206/T206 1998 And On Maintenance Manual has been prepared to help the maintenance personnel to service and maintain the Model 206/T206 airplanes (beginning at Serial 20680001 and T20608001). This manual gives the necessary information required to let the mechanic service, troubleshoot, remove and replace components or repair systems and do an inspection. NOTE: This manual is not intended to cover Model 206/T206 airplanes made prior to 1997. For manuals related to these airplanes, refer to the applicable lists in the Propeller Aircraft Cessna Customer Care Supplies & Publications Catalog. B. This manual has been prepared with the Air Transport Association (ATA) Specification Number 100 for Manufacturer's Technical Data. C. For more information than this manual can supply, refer to the applicable Model 206/T206 Wiring Diagram Manual, Illustrated Parts Catalog and the Structural Repair Manual. D. Technical Publications are available for some of the different components and systems which are not supplied in this manual. These manuals must be used as required for maintenance of those components and systems, and may be purchased from the manufacturer. 4. Temporary Revisions A. Additional information which becomes available may be supplied by a temporary revision. This service is used to give, without delay, new information which will help to maintain safe flight/ground operations. Temporary revisions are numbered consecutively in the ATA chapter assignment. Page numbers use the three-element number which matches the maintenance manual. Temporary revisions are incorporated into the maintenance manual at the next regular revision schedule. 5. Serialization A. Each airplane is issued a serial number. This number is assigned as construction begins and will remain with the airplane during its service life. This serial number shows on the airplane ID plate. It is located below the horizontal stabilizer, and on a trim plate located on the pilot side doorpost. This serial number is used to identify changes in the text or within an illustration. The absence of a serial number in text or illustration shows the material is applicable to all airplanes. 6. Material Presentation A. This Maintenance Manual is available on paper, aerofiche or Compact Disc (CD/ROM). The CD/ROM contains the Maintenance Manual, Illustrated Parts Catalog Manual, Wiring Diagram Manual and Structural Repair Manual on a single disc. 7. Service Bulletins A. The Service Bulletins may require special inspections and authorize modifications to the airplane and/ or system. As service bulletins are issued, they will be incorporated in the next scheduled revision and noted in the Service Bulletin List, located before the Introduction. The list of service bulletins use four columns to summarize the information. (1) Service Bulletin Number - This service bulletin number column identifies the bulletin by number. Service bulletins are numbered consecutively within ATA chapter assignment. (2) Service Bulletin Date - The service bulletin date column shows the initial date the bulletin became active. (3) Title - The title column identifies the service bulletin by nomenclature. It is the same title that is displayed on page one of the service bulletin. INTRODUCTION Page 2 C Cessna Aircraft Company Dec 2/2002 CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL (4) Manual Incorporation - The manual incorporation column shows if the service bulletin has been incorporated in the maintenance manual (Incorp), if the service bulletin has no effect on the maintenance manual (No Effect), or if the service bulletin has not been worked (dashed lines). 8. Using the Maintenance Manual A. Division of Subject Matter. (1) The Maintenance Manual is divided into four major sections. The major sections are divided into chapters with each chapter with its own effectivity page and table of contents. The manual divisions are as follows: (a) Major Section 1 - Airplane General Chapter Title 5 Time Limits/Maintenance Checks 6 Dimensions and Areas 7 Lifting and Shoring 8 Leveling and Weighing 9 Towing and Taxiing 10 Parking, Mooring, Storage and Return to Service 11 Placards and Markings 12 Servicing (b) Major Section 2 - Airframe Systems Chapter Title 20 Standard Practices - Airframe 21 Air Conditioning 22 Auto Flight 23 Communications 24 Electrical Power 25 Equipment/Furnishings 26 Fire Protection 27 Flight Controls 28 Fuel 30 Ice and Rain Equipment 31 Indicating/Recording Systems 32 Landing Gear 33 Lights 34 Navigation 35 Oxygen 37 Vacuum (c) Major Section 3 - Structures INTRODUCTION Page 3 © Cessna Aircraft Company Dec 2/2002 CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL Title Standard Practices and Structures - General Doors Stabilizers Windows Wings (d) Major Section 4 - Power Plant Title Propeller Power Plant Engine Fuel and Control Ignition Engine Controls Engine Indicating Exhaust Oil Starting Turbines B. Page Numbering System. (1) The page number system used in the Maintenance Manual consists of three-element numbers divided by dashes. Refer to the example below for an illustration of a typical number layout as used in the ATA format. B1805 Chapter/System (Air Conditioning) 21-51-01 Subject/Unit (Compressor) Section/Subsystem (Freon Cooling) (2) When the chapter/system element number is followed with zeros in the section/subsystem and subject/unit element number (21-00-00), the information is applicable to the full system. (3) When the section/subsystem element number is followed with zeros in the subject/unit element number (21-51-00), the information is applicable to the subsystem in the system. (4) The subject/unit element number is used to identify information applicable to units in the subsystems. The subject/unit element number progresses sequentially from the number -01 in reference with the number of subsystem units requiring maintenance information. (5) All system/subsystem/unit (chapter/section/subject) maintenance data is divided into specific types of information: Description and Operation, Troubleshooting and Maintenance Practices. Blocks of sequential page numbers are used to identify the type of information: INTRODUCTION Page 4 © Cessna Aircraft Company Dec 2/2002 Chapter 51 52 55 56 57 Chapter 61 71 73 74 76 77 78 79 80 81 CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL * Page 1 through 99 - Description and Operation Page 101 through 199 - Troubleshooting * Page 201 through 299 - Maintenance Practices Page 301 through 399 - Servicing * Page 401 through 499 - Removal/Installation Page 501 through 599 - Adjustment/Test * Page 601 through 699 - Inspection/Check Page 701 through 799 - Cleaning/Painting * Page 801 through 899 - Approved Repairs NOTE: In most cases, the individual topics have been combined into a 200-series document (Maintenance Practices). When specific topics require a lot of information, they will use the page blocks shown. (6) A typical page number: B1806 21-51-01 Page 802 Second Page of Aug 1/95- Compressor LLmro| Approved Repairs Air Conditioning Compressor Date of Page Issue Cooling Subsystem (7) Illustrations are also supplied through the page block numbering system. For example, all illustrations in a Maintenance Practices section will begin with the number 2 (i.e. Figure 201, Figure 202, etc.). 9. Effectivity Pages A. A list of effective pages is supplied at the front of each maintenance manual chapter. All pages in the specific chapter are listed in numerical sequence on the Effectivity Page(s) with the date of issue for each page. 10. Revision Filing Instructions A. Regular Revision. (1) Pages to be removed or put in the maintenance manual will show on the effectivity page. Pages are listed in sequence by the three-element number (chapter/section/subject) and then by page number. When two pages display the same three-element number and page number, the page with the most recent Date of Page Issue must be put in the maintenance manual. The date column on the corresponding chapter effectivity page must show the active page. B. Temporary Revision. (1) Put the temporary revisions in the applicable chapter(s) in reference with the instructions shown on the first page of the temporary revision. (2) The rescission of a temporary revision is completed by incorporation into the maintenance manual or by a superseding temporary revision. A Record of Temporary Revisions is supplied in the Temporary Revision List located before the Introduction. A Manual Incorporation Date column on the Temporary Revision List page will show the date the Temporary Revision was incorporated which approves the rescission of the temporary revision. INTRODUCTION Page 5 © Cessna Aircraft Company Dec 2/2002 CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL 11. Identifying Revised Material A. Additions or revisions to text in a section will be identified by a revision bar in the left margin of the page and adjacent to the change. B. When technical changes cause unchanged text to appear on a different page, a revision bar will be placed in the left margin opposite to the chapter/section/subject, page number and date of all affected pages, as long as no other revision bar appears on the page. These pages will show the current revision date in the Date of Page Issue location. C. Revised text inside tables will not show revision bars; however, the affected page will display the current revision date in the Date of Page Issue location. D. When many technical changes are made to the text in an existing section, revision bars will show for the full length of text. E. When art in an illustration is revised, a hand indicator or revision bar will appear in the illustration. F. New art added to a section will be identified by a revision bar in the left margin. 12. Warnings, Cautions and Notes A. Warnings, cautions and notes are applicable to the procedures being described. These adjuncts to the text are used to inform important points. Warnings and cautions precede the text they are applicable to, and notes follow the text they apply to. (1) WARNING - Calls attention to the use of materials, processes, methods, procedures or limits which must be followed to prevent injury or death to persons. (2) CAUTION - Calls attention to methods and procedures which must be followed to prevent damage to the equipment or airplane. (3) NOTE - For information only. 13. Propeller Aircraft Customer Care Supplies and Publications Catalog A. A Cessna Propeller Aircraft Customer Care Supplies and Publications Catalog is available from a Cessna Service Station or directly from Cessna Propeller Aircraft Product Support, Dept. 751, Cessna Aircraft Company, P.O. Box 7706, Wichita, Kansas 67277-7706. The catalog lists all publications and Customer Care Supplies available from Cessna for prior year models as well as new products. To maintain this catalog in a current status, it is revised yearly and issued in paper and aerofiche form. 14. Customer Comments on Manual A. Cessna Aircraft Company has worked to give you an accurate, useful, up-to-date manual. This manual can be improved with your help. Please use the return card supplied with your manual to report any errors, discrepancies, and omissions in this manual as well as any general comments you want to make. INTRODUCTION Page 6 © Cessna Aircraft Company Dec 2/2002 CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL LIST OF REVISIONS 1. Revisions A. This Maintenance Manual includes the original issue and the revisions listed in Table 1. To make sure the information in this manual is current and the latest maintenance and inspections procedures are available, the revisions must be incorporated in the manual as they are issued. Table 1. Basic Manual - Original Issue - 3 November 1997 Date Writer 3 August 1998 31 March 2000 18 April 2001 2 December 2002 1 April 2005 3 July 2006 1 July 2007 km Revision Number Date Writer 2 2 September 1999 km 4 km jb dl bjo 6 8 10 12 15 September 2000 15 October 2001 5 April 2004 2 January 2006 1 January 2007 km km jb jb bjo j~cn jcn ©Cessna Aircraft Company LIST OF REVISIONS Page 1 Jul 1/2007 Revision Number 1 3 5 7 9 11 I 13 CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL LIST OF CHAPTERS CHAPTER Effective Date FICHE/FRAME 5 Time Limits/Maintenance Checks Jul 1/2007 1 B4 6 Dimensions and Areas Jul 1/2007 1 E16 7 Lifting and Shoring Apr 1/2005 1 F15 8 Leveling and Weighing Apr 1/2005 1 G2 9 Towing and Taxiing Apr 1/2005 1 G9 10 Parking and Mooring Jul 1/2007 1 G15 11 Placards and Markings Apr 1/2005 1 H2 12 Servicing Jan 1/2007 1 H8 20 Standard Practices - Airframe Jan 1/2007 2 A2 21 Air Conditioning Apr 1/2005 2 C12 22 Auto Flight Jul 1/2007 2 09 23 Communications Jan 1/2007 2 E2 24 Electrical Power Jul 3/2006 2 F2 25 Equipment/Furnishings Jan 1/2007 2 H9 26 Fire Protection Apr 1/2005 2 K8 27 Flight Controls Jul 1/2007 3 A2 28 Fuel Jul 1/2007 3 012 30 Ice and Rain Protection Jan 1/2007 3 F2 31 Indicating/Recording Systems Jan 2/2006 3 G2 32 Landing Gear Jan 1/2007 3 G18 33 Lights Jan 2/2006 3 J4 34 Navigation Jan 1/2007 4 A2 35 Oxygen Jan 2/2006 4 D11 37 Vacuum Jan 2/2006 4 E2 51 Standard Practices - Structures Apr 1/2005 4 F3 52 Doors Jul 3/2006 4 F12 55 Stabilizers Apr 1/2005 4 G10 56 Windows Jan 2/2006 4 H2 57 Wings Apr 1/2005 4 H18 61 Propellers Jul 1/2007 4 14 71 Powerplant Apr 1/2005 4 116 73 Engine Fuel and Control Jan 1/2007 4 K10 74 Ignition Jul 3/2006 4 L5 76 Engine Controls Jan 2/2006 5 A2 77 Engine Indicating Jul 1/2007 5 A13 78 Exhaust Apr 1/2005 5 B7 79 Oil Jul 3/2006 5 C2 80 Starting Jan 2/2006 5 C17 81 Turbines Apr 1/2005 5 02 NOTE 1: *Represents date of page one of each chapter's List of Effective Pages which is applicable to Manual revision date. LIST OF CHAPTERS Page 1 © Cessna Aircraft Company Jul 1/2007 CHAPTER TIME LIMITS/ MAINTENANCE CHECKS CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL LIST OF EFFECTIVE PAGES CHAPTER-SECTION-SUBJECT 05-Title 05-List of Effective Pages 05-Record of Temporary Revisions 05-Table of Contents 5-00-00 5-00-10 5-10-00 5-1 0-01 5-11-00 5-1 2-00 5-1 2-01 5-1 2-02 5-1 2-03 5-12-04 5-1 2-05 5-1 2-06 5-1 2-07 5-1 2-08 5-1 2-09 5-12-10 5-12-11 5-12-12 5-12-13 5-12-14 5-12-15 5-12-16 5-12-17 5-12-18 5-12-19 5-1 2-20 5-1 2-21 5-1 2-22 5-1 2-23 5-1 2-24 5-1 2-25 5-50-00 ©Cessna Aircraft Company 05 - LIST OF EFFECTIVE PAGES PAGE Pages 1-2 Page 1 Pages 1-2 Pages 1-16 Pages 1-3 Pages 1-2 Pages 1-7 Pages 1-6 Pages 1-7 Pages 1-6 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Pages 1-5 DATE Jul 1/2007 Dec 2/2002 Jul 3/2006 Jul 3/2006 Jul 1/2007 Jul 1/2007 Jul 3/2006 Jul 3/2006 Jul 3/2006 Jul 3/2006 Jul 3/2006 Dec 2/2002 Jul 3/2006 Dec 2/2002 Jul 3/2006 Jul 3/2006 Jul 3/2006 Jul 3/2006 Dec 2/2002 Jul 3/2006 Jul 3/2006 Jul 3/2006 Jul 3/2006 Jul 3/2006 Jul 3/2006 Jul 3/2006 Jul 3/2006 Jul 3/2006 Jul 3/2006 Jul 3/2006 Jul 3/2006 Jan 2/2006 Page 1 of 1 Jul 1/2007 Temporary Revision Number RECORD OF TEMPORARY REVISIONS Page Number Issue Date By Date Removed By CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL CONTENTS TIME LIMITS/MAINTENANCE CHECKS........ .............. S cope. .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Inspection Requirements........................... Inspection Program Selection ......................... Description ................................. General Inspection Terms and Guidelines ................... AIRWORTHINESS LIMITATIONS - FAA APPROVED DATA.............. Scope.................................... Airworthiness Limitations........................... INSPECTION TIME INTERVALS.......................... General................................... Procedure.................................. Inspection Terms and Guidelines ....................... Chart Legend ................................ INSPECTION TIME LIMITS ............................ Inspection Items............................... COMPONENT TIME LIMITS............................ General................................... Cessna-Supplied Replacement Time Limits .................. Supplier-Supplied Replacement Time Limits .................. PROGRESSIVE CARE PROGRAM ........................ General................................... Procedure.................................. Inspection Terms and Guidelines ....................... INSPECTION OPERATION 1........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 2 ........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 3 ........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 4 ........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 5 ........................... Description ................................. General Inspection Criteria .......................... PROGRESSIVE CARE .............................. Operation 6................................. INSPECTION OPERATION 7 ........................... Description ................................. General Inspection Criteria .......................... PROGRESSIVE CARE .............................. Operation 8................................. 5-00-00 Page 1 5-00-00 Page 1 5-00-00 Page 1 5-00-00 Page 1 5-00-00 Page 1 5-00-00 Page 2 5-00-1 0 Page 1 5-00-1 0 Page 1 5-00-10 Page 1 5-1 0-00 Page 1 5-1 0-00 Page 1 5-10-00 Page 1 5-10-00 Page 1 5-10-00 Page 1 5-1 0-01 Pagel1 5-1 0-01 Page 1 5-11 -00 Page 1 5-11 -00 Page 1 5-1 1-00 Page 1 5-1 1-00 Page 2 5-12-00 Page 1 5-12-00 Page 1 5-12-00 Page 2 5-12-00 Page 2 5-12-01 Page 1 5-12-01 Page 1 5-12-01 Page 1 5-12-02 Page 1 5-12-02 Page 1 5-12-02 Page 1 5-12-03 Page 1 5-12-03 Page 1 5-12-03 Page 1 5-12-04 Page 1 5-12-04 Page 1 5-12-04 Page 1 5-12-05 Page 1 5-12-05 Page 1 5-12-05 Page 1 5-12-06 Page 1 5-12-06 Page 1 5-12-07 Page 1 5-12-07 Page 1 S-1 2-07 Page 1 5-1 2-08 Page 1 5-1 2-08 Page 1 05 - CONTENTS Page 1 of 3 Jul 1/2007 © Cessna Aircraft Company CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL INSPECTION OPERATION 9 ........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 10........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 11........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 12........................... Description ................................. General Inspection Criteria .......................... PROGRESSIVE CARE .............................. Operation 13 ................................ INSPECTION OPERATION 14........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 15 ........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 16........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 17........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 18........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 19........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 20........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 21........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 22........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 23........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 24........................... Description ................................. General Inspection Criteria .......................... 5-12-09 Page 1 5-12-09 Page 1 5-12-09 Page 1 5-12-10 Page 1 5-12-10 Page 1 5-12-10 Page 1 5-12-11 Page 1 5-12-11 Page 1 5-12-11 Page 1 5-12-12 Page 1 5-12-12 Page 1 5-12-12 Page 1 5-12-13 Page 1 5-12-13 Page 1 5-12-14 Page 1 5-12-14 Page 1 5-12-14 Page 1 5-12-15 Page 1 5-12-15 Page 1 5-12-15 Page 1 5-12-16 Page 1 5-12-16 Page 1 5-12-16 Page 1 5-12-17 Page 1 5-12-17 Page 1 5-12-17 Page 1 5-12-18 Page 1 5-12-18 Page 1 5-12-18 Page 1 5-12-19 Page 1 5-12-19 Page 1 5-12-19 Page 1 5-12-20 Page 1 5-12-20 Page 1 5-12-20 Page 1 5-12-21 Page 1 5-12-21 Page 1 5-12-21 Page 1 5-12-22 Page 1 5-12-22 Page 1 5-12-22 Page 1 5-12-23 Page 1 5-12-23 Page 1 5-12-23 Page 1 5-12-24 Page 1 5-12-24 Page 1 5-12-24 Page 1 05 - CONTENTS Page 2of 3 Jul 1/2007 © Cessna Aircraft Company CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL INSPECTION OPERATION 25........................... Description ................................. General Inspection Criteria .......................... UNSCHEDULED MAINTENANCE CHECKS .................... General................................... Unscheduled Maintenance Checks Defined and Areas of Inspection ....... 5-12-25 Page 5-12-25 Page 5-12-25 Page 5-50-00 Page 5-50-00 Page 5-50-00 Page 05 - CONTENTS Page 3 of 3 Jul 1/2007 ©D Cessna Aircraft Company 1 1 1 1 1 1 CESSNA AIRCRAFT COMPANY MODEL 2061T206 MAINTENANCE MANUAL TIME LIMITS/MAINTENANCE CHECKS 1.Scope A. This chapter provides the time limits and maintenance checks for the Model 206 airplanes. It is divided into several sections, each with a specific purpose toward providing information necessary to establish inspection criteria. 2. Inspection Requirements A. As required by U.S. Federal Aviation Regulations, all civil aircraft of U.S. registry must undergo a complete inspection (annual) each twelve calendar months. In addition to the required annual inspection, aircraft operated commercially (for hire) must have a complete inspection every 100 hours of operation. B. Compliance with the regulations is accomplished using one of three methods: (1) Traditional (AnnuaV1OO Hour) inspection program which utilizes 14 CFR Part 43, Appendix D (scope and detail) to inspect the airplane. In addition, Cessna recommends certain components or items be inspected at 50 hour intervals. These inspection items are listed in Inspection Time Intervals, Section 5-10-01. (2) Progressive Care inspection program which allows the work load to be divided into smaller operations that can be accomplished in a shorter time period. This method is detailed in Progressive Care Program, Section 5-12-00. (3) PhaseCard inspection program which is geared toward high-utilization flight operations (approximately 600 flight hours per year). This system utilizes 50-hour intervals (Phase 1 and Phase 2) to inspect high-usage systems and components. At 12 months or 600 flight hours, whichever occurs first, the airplane undergoes a complete (Phase 3) inspection. PhaseCard Inspection programs can be ordered through Propeller Aircraft Product Support. P.O. Box 7706, Wichita, KS 67277, Phone (316) 941-7550, Fax (316) 942-9006. 3. Inspection Program Selection A. The selection of an inspection program (Annual, Progressive Care or PhaseCard) is primarily based on owner/operator preferences, whether an airplane is flown for hire, and numbers of hours flown during the year. 4. Description A. Listed below is a brief description and intended purpose of each section of this chapter. For detailed information related to each particular inspection program, refer to the specific section within this chapter. B. Section 5-00-00, Time Limits/Maintenance Checks - General. This section provides a general overview of inspection requirements. C. Section 5-1 0-01, Inspection Time Intervals. The primary purpose of this section is to provide a central location for inspection time intervals. This section may also be utilized in conjunction with 14 CFR Part 43 to provide greater detail on inspection criteria when performing Annual/i 00 Hour inspections. D. Section 5-11 -00, Component Time Limits. This section provides a list of components which are life- or time-limited. Although these components are not listed in any of Cessna's inspection programs, they must be considered and included in whatever inspection program is used. E. Section 5-12-00, Progressive Care Program. This section outlines the progressive inspection program. The program is divided into four primary operations which cover all inspection requirements up through the 200-hour interval inspection items. The remaining operations cover inspections which are at intervals other than what the four primary operations cover. Refer to the Progressive Care Program section for a more detailed description of the Progressive Care Program. 5-00-00 Page 1 © Cessna Aircraft Company Jul 1/2007 CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL 5. General Inspection Terms and Guidelines NOTE: When inspections criteria is required, this criteria is spelled out in the text. If more detailed instructions are required for an inspection, these instructions will be referenced out to appropriate locations (supplier publications and/or the maintenance manual). A. Definitions of terms used through the inspection programs are as follows: (1) ON CONDITION is defined as the necessary inspections and/or checks to determine that a malfunction or failure of the component will not occur prior to the next scheduled inspection. (2) CONDITION is defined as inspection for (but not limited to) cleanliness, cracks, deformation, corrosion, wear, and loose or missing fasteners. (3) SECURITY: Inspect for looseness of fasteners and fastener securing devices such as safety wire, cotter pins and self-locking nuts. B. During Inspections, use the following general guidelines: (1) MOVABLE PARTS: Inspect for lubrication, servicing, security of attachment, binding, excessive wear, safetying, proper operation, proper adjustment, correct travel, cracked fittings, security of hinges, defective bearings, cleanliness, corrosion, deformation, sealing, and tension. (2) FLUID LINES AND HOSES: Inspect for leaks, cracks, bulging, collapsed, twisted, dents, kinks, chafing, proper radius, security, discoloration, bleaching, deterioration, and proper routing; rubber hoses for hardness or flexibility and metal lines for corrosion. (3) METAL PARTS: Inspect for security of attachment, cracks, metal distortion, and heat deterioration. (4) WIRING: Inspect for security, chafing, burning, arcing, defective insulation, loose or broken terminals, heat deterioration, and corroded terminals. CAUTION: Torque values listed in this manual are not to be used for checking tightness of installed parts during service. (5) STRUCTURAL FASTENERS: Inspect for correct torque in accordance with applicable torque values. Refer to Chapter 20, Torque Data - Maintenance Practices, during installation or when visual inspection indicates the need for a torque check. (6) FILTERS, SCREENS, AND FLUIDS: Inspect for cleanliness and the need for replacement at specified intervals. (7) A system check (operation or function) that requires electrical power, must be performed using 28.5 Volts, +0.25 or -1 .00 Volts, bus voltage. This will make sure that all components are I ~ ~~~operating at their operational voltage. C. Airplane file. (1) Miscellaneous data, information, and licenses are a part of the airplane file. Check that the following documents are up-to-date and in accordance with current Federal Aviation Regulations. Most of the items listed are required by the Federal Aviation Regulations. Since the regulations of other nations may require other documents and data, owners of airplanes operated outside the United States should check with their own aviation officials to determine their individual requirements. (a) To be displayed in the airplane at all times: 1 Standard Airworthiness Certificate (FAA Form 81 00-2). 2 Aircraft Registration Certificate (FAA Form 8050-3). 3 Aircraft Radio Station License (Federal Communication Commission Form 556 if transmitter is installed). (b) To be carried in the airplane at all times: 1 Weight and Balance Data Sheets and associated papers (all copies of the Repair and Alteration Form, FAA Form 337, are applicable). 2 Equipment List. 3 Pilot's Operating Handbook and FAA Approved Airplane Flight Manual. (c) To be made available upon request: 1 Airplane, Engine and Propeller Logbooks. 5-00-00 Page 2 © Cessna Aircraft Company Jul 1/2007 CESSNA AIRCRAFT COMPANY MODEL 20611206 MAINTENANCE MANUAL AIRWORTHINESS LIMITATIONS - FAA APPROVED DATA 1.Scope A. The Airworthiness Limitations section is FAA approved and specifies maintenance required under Parts 43.16 and 91 .403 of the Federal Aviation Regulations unless an alternative program has been FAA approved. 2. Airworthiness Limitations A. There are no airworthiness limitations associated with this airplane. 5-00-10 Page 1 Dec 2/2002 © Cessna Aircraft Company CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL INSPECTION TIME INTERVALS 1. General A. The primary purpose of this section is to provide inspection time intervals. The section 5-10-01 may be utilized in conjunction with 14 CFR Part 43 inspection scope and detail, but is not intended to be utilized as the primary checklist for inspection of the airplane. NOTE: The inspection guidelines contained in this section are not intended to be all-inclusive, for no such charts can replace the good judgment of certified airframe and powerplant mechanics in performance of their duties. As the one primarily responsible for the airworthiness of the airplane, the owner or operator should select only qualified personnel to maintain the airplane. 2. Procedure A. A complete airplane inspection includes all inspection items as required by 14 CFR 43, Appendix D, Scope and Detail of annual/1 00-hour inspections. The chart provided in this section should be used to augment the inspection. B. The Component Time Limits section (5-11-00) should be checked in conjunction with this inspection to ensure proper overhaul and replacement requirements are accomplished at the specified times. C. The intervals shown are recommended intervals at which items are to be inspected based on normal usage under average environmental conditions. Airplanes operated in extremely humid areas (tropics), or in exceptionally cold, damp climates, etc., may need more frequent inspections for wear, corrosion, and lubrication. Under these adverse conditions, perform periodic inspections in compliance with this chart at more frequent intervals until the operator can set his own inspection periods based on field experience. (1) The 14 CFR Part 91 operator's inspection intervals shall not deviate from the inspection time limits shown in this manual except as provided below: (Refer to 14 CFR 91.409) (a) The airplane can only exceed its inspection point up to ten hours if the airplane is enroute to a facility to have the inspection completed. (b) Inthe event of late compliance of any operation scheduled, the next operation in sequence retains a due point from the time the late operation was originally scheduled (reschedule if late). (c) In the event of early compliance of any operation scheduled, that occurs 10 hours or less ahead of schedule, the next phase due point may remain where originally set. (d) In the event of early compliance on any operation scheduled, that occurs more than 10 hours ahead of schedule, the next phase due point must be rescheduled to establish a new due point from the time of early accomplishment. 3. Inspection Terms and Guidelines A. For inspection terms and guidelines, refer to Chapter 5, Time Limits/Maintenance Checks - General. 4. Chart Legend A. Each page of the inspection listed in Inspection Time Limits, section 5-10-01 contains the following five columns: (1) REVISION STATUS - This column provides the date that a given item was added, deleted or revised. A blank entry in this column indicates no change since the original issue of this manual. (2) INSPECTION ITEM CODE NUMBER - This column lists a six-digit number permanently assigned to a scheduled maintenance item. A given inspection item code number will never change and will not be reused in the event the scheduled maintenance item is deleted. (3) REQUIREMENTS - This column provides a short description of the inspection and/or servicing procedures. Where a more detailed description of the procedure is required, a reference will be made to either another selection located within the maintenance manual or a specific reference to a supplier publication. 5-1 0-00 Page 1 © Cessna Aircraft Company Jul 3/2006 CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL (4) INTERVAL - This column lists the frequency of inspection in alphabetic coded form. The legend for the alpha code is listed below. (5) OPERATION - The Progressive Care inspection program allows the work load to be divided into smaller operations that can be accomplished in a shorter time period. This program is detailed in section 5-12-00, which is the Progressive Care Program. (6) ZONE - This column locates the components within a specific zone. For a breakdown of how the airplane is zoned, refer to Chapter 6, Airplane Zoning - Description and Operation. INTERVAL OPERATION INTERVAL DETAILS A. 1, 2, 3, 4 Every 50 hours. B. 1, 2, 3, 4 Every 100 hours. C. 1, 2, 3, 4 Every 200 hours. D. 5 Every 400 hours or 1 year, whichever occurs first. E. (Not used) F. 7 Every 600 hours or 1 year, whichever occurs first. G. (Not used) H. 9 Every 500 hours. I. 10 Every 1000 hours. J. 11 Every 2 years. K. 12 Beginning five years from the date of the manufacture, you must make sure of the serviceability of the components every twelve months. Refer to Airborne Air and Fuel Products Service Letter Number 39A or latest revision. L. (Not used) M. 14 Every 2 years, or anytime components are added or removed which have the potential to affect the magnetic accuracy and/or variation of the compass calibration, or anytime the accuracy of the compass is in question. N. 15 Every 2000 hours. O. 16 Every 1000 hours or 1 year, whichever occurs first. P. 17 Every 12 calendar months. Q. 18 Every 6 years. R. 19 Every 12 years. S. 20 Every 3 years. T. 21 Every 1 year. U. 22 Every 100 hours or every one year, whichever occurs first. V. 23 Every 100 hours, every annual inspection, every overhaul, and any time fuel lines or clamps are serviced, removed or replaced. W. 24 First 600 hours and as defined by the manufacturer thereafter. X. 25 Every 1000 hours or 3 years, whichever occurs first. 5-10-00 Page 2 © Cessna Aircraft Company Jul 3/2006 CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL INSPECTION TIME LIMITS 1. Inspection Items REVISION ITEM CODE TASK INTERVAL OPERATION ZONE STATUS NUMBER Added 110000 Interior Placards, Exterior Placards, B 1,2,3,4 All Apr 1/05 Decals, Markings and Identification Plates - Inspect for security of installation and legibility. Refer to Chapter 11, Placards and Markings - Inspection/Check. Deleted 112101 Apr 5/04 Deleted 113101 Apr 5/04 212001 Ventilation System - Inspect clamps, D 5 211 hoses, and valves for condition and security. Revised 212002 Primary Flight Display (PFD) Fan and U 22 220, 225 Apr 1/05 Multi-Function Display (MFD) Fan, Deck Skin Fan, and Remote Avionics Cooling Fan - Operational Check. Refer to Chapter 21, Avionics Cooling - Maintenance Practices. 214001 Cold and Hot Air Hoses - Check B 2, 4 120 condition, routing, and security. Revised 214002 Heater Components, Inlets, and B 1,3 211 Aug 3/98 Outlets - Inspect all lines, ducts, clamps, seals, and gaskets for condition, restriction, and security. Revised 214003 Cabin Heat and Ventilation Controls - B 1, 3 211 Mar 31/00 Check freedom of movement through full travel. Check friction locks for proper operation. 221001 Autopilot Rigging - Refer to Autopilot - F 7 610 Maintenance Practices. Added 221002 Autopilot Servo Capstan Assemblies. O 16 610 Aug 3/98 Check slip-clutch torque settings. Refer to Autopilot - Maintenance Practices. Added 221003 Autopilot Servo Actuators. Inspect for O 16 610 Aug 3/98 evidence of corrosion and or buildup of dirt or other particulate matter which may interfere with servo operation. Refer to Autopilot - Maintenance Practices. 231001 Communication Antennas and Cables C 3 210 - Inspect for security of attachment, connection, and condition. 5-10-01 Page 1 © Cessna Aircraft Company Jul 3/2006 CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL REVISION ITEM CODE TASK INTERVAL OPERATION ZONE STATUS NUMBER 235001 Microphones, Headsets, and Jacks - C 1 211 Inspect for cleanliness, security, and evidence of damage. Added 235002 Microphone Push-To-Talk Switch B 1, 3 222, 223 Apr 5/04 - Clean the pilot's and copilot's microphone switches. Refer to Chapter 23, Communication Maintenance Practices. 242001 Alternator, Mounting Bracket, and A 1, 2, 3, 4 120 Electrical Connections - Check condition and security. Check alternator belts for condition and proper adjustment. Check belt tension. Revised 243001 Main Battery - Examine the general B 2, 4 120 Apr 1/05 condition and security. Complete a check of the level of electrolyte. Refer to Chapter 12-17-00. Revised 243002 Main Battery Box and Cables - Clean B 2, 4 120 Apr 1/05 and remove any corrosion. Examine the cables for routing, support, and security of the connections. 243003 General Airplane and System Wiring C 1 210 - Inspect for proper routing, chafing, broken or loose terminals, general condition, broken or inadequate clamps, and sharp bends in wiring. 243004 External Power Receptacle and Power C 2 120 Cables - Inspect for condition and security. Added 243005 Standby Battery - Complete the T 21 220 Apr 1/05 Standby Battery Capacity Test. Refer to Chapter 24, Standby Battery - Maintenance Practices. 246001 Switch and Circuit Breaker Panel, C 1 222 Terminal Blocks, and Junction Boxes - Inspect wiring and terminals for condition and security. Revised 246002 Power Junction Box - Check operation B 1, 3 222 Sep 15/00 and condition. Check availability and condition of spare fuse (if applicable). Added 246003 Alternator Control Unit - Complete the J 11 222 Jul 3/06 Over-voltage Protection Circuit Test. Refer to Chapter 24, Alternator Control Unit. 5-10-01 Page 2 © Cessna Aircraft Company Jul 3/2006 CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL REVISION ITEM CODE TASK INTERVAL OPERATION ZONE STATUS NUMBER Revised 246101 Essential and Crossfeed Bus Diodes - T 21 224 Apr 1/05 Check for proper operation. Complete the Essential and Crossfeed Bus Diode Inspection. Refer to Chapter 24, Essential and Crossfeed Bus Diodes - Maintenance Practices. Revised 251001 Seats - Examine the seats to make B 1, 3 211 Jul 3/06 sure they are serviceable and installed correctly. Make sure the seat stops and adjustment mechanism operate correctly. Examine the seat recline control and attaching hardware to make sure the hardware and lock are not damaged and are correctly installed. Lubricate the threads of the Seat Crank Handle Assembly with MIL-PRF-81322 general purpose grease. 251002 Seat Tracks and Stops - Inspect seat B 2, 4 230 tracks for condition and security of installation. Check seat track stops for damage and correct location. Inspect seat rails for cracks. 251101 Restraint System, front and rear - B 1, 3 211 Check belts for thinning, fraying, cutting, broken stitches, or ultra-violet deterioration. Check system hardware for security of installation. Added 251102 AMSAFE Aviation Inflatable Restraint T 21 211 Apr 1/05 (AAIR) - Examine the restraint for dirt, frayed edges, unserviceable stitching, loose connections, and other wear. 252201 Upholstery, Headliner, Trim, and D 5 211 Carpeting - Check condition and security. Revised 256001 Emergency Locator Transmitter - B 1, 3 310 Jan 2/06 Examine for security of attachment and check operation by verifying transmitter output. Check cumulative time and useful life of batteries in accordance with 14 CFR Part 91.207. 262001 Portable Hand Fire Extinguisher - B 1, 3 230 Inspect for proper operating pressure, condition, security of installation, and servicing date. Added 262002 Cockpit Mounted Halon Type Fire P 17 211 Aug 3/98 Extinguisher - Weigh bottle. Bottle must be reserviced by qualified individual if more than 2 ounces is lost. 5-10-01 Page 3 © Cessna Aircraft Company Jul 3/2006 CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL REVISION ITEM CODE TASK INTERVAL OPERATION ZONE STATUS NUMBER Added 262003 Cockpit Mounted Halon Type Fire R 19 211 Aug 3/98 Extinguishers - Perform hydrostatic test. The hydrostatic test shall be at twelve-year intervals based on initial servicing or date of last hydrostatic test. Added 262004 Cockpit Mounted Halon Type Fire Q 18 211 Aug 3/98 Extinguishers - Empty, inspect for damage, and recharge. Revised 271001 Aileron Controls - Check freedom B 1, 3 120, 520, Mar 31/00 of movement and proper operation 620 through full travel. 271002 Ailerons and Cables - Check operation C 3 120, 520, and security of stops. Check cables for 620 tension, routing, fraying, corrosion, and turnbuckle safety. Check travel if cable tension requires adjustment or if stops are damaged. Check fairleads and rub strips for condition. 271003 Aileron Structure, Control Rods, B 1, 3 520, 620 Hinges, Balance Weights, Bell Cranks, Linkage, Bolts, Pulleys, and Pulley Brackets - Check condition, operation, and security of attachment. 271004 Ailerons and Hinges - Check condition, B 1, 3 520, 620 security, and operation 271005 Control Wheel Lock - Check general C 1 222 condition and operation. Revised 271006 Control Linkage - Inspect pulleys, C 1 222, 223 Aug 3/98 cables, bearings, and turnbuckles for condition and security. 272001 Rudder - Check internal surfaces for C 3 340 corrosion, condition of fasteners, and balance weight attachment. Revised 272002 Rudder - Inspect the rudder skins for B 1, 3 340 Mar 31/00 cracks and loose rivets, rudder hinges for condition, cracks and security; hinge bolts, hinge bearings, hinge attach fittings, and bonding jumper for evidence of damage and wear, failed fasteners, and security. Inspect balance weight for looseness and the supporting structure for damage. Revised 272003 Rudder, Tips, Hinges, Stops, Clips and B 1, 3 340 Aug 3/98 Cable Attachment - Check condition, security, and operation. 5-10-01 Page 4 © Cessna Aircraft Company Jul 3/2006 CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL REVISION ITEM CODE TASK INTERVAL OPERATION ZONE STATUS NUMBER 272004 Rudder Pedals and Linkage - Check C 1 230 for general condition, proper rigging, and operation. Check for security of attachment. Added 272005 Rudder Control - Check freedom B 1, 3 340 Aug 3/98 of movement and proper operation through full travel. Check rudder stops for damage and security. Revised 273001 Elevator Control - Check freedom B 1, 3 222, 223 Aug 3/98 of movement and proper operation through full travel. Revised 273002 Elevator Control System - Inspect B 1, 3 222, 223 Mar 31/00 pulleys, cables, sprockets, bearings, chains, and turnbuckles for condition, security, and operation. Check cables for tension, routing, fraying, corrosion, and turnbuckle safety. Revised 273003 Elevator, Hinges, Stops, and Cable B 1, 3 320, 330 Aug 3/98 Attachment - Check condition, security, and operation. Added 273004 Elevator Downspring - Check structure, B 1, 3 310 Aug 3/98 bolts, linkage, bellcrank, and push-pull tube for condition, operation, and security. Check cables for tension, routing, fraying, corrosion, and turnbuckle safety. Check travels if cables require tension adjustment or if stops are damaged. 273101 Elevator Trim System - Check cables, B 1, 3 224, 240, push-pull rods, bell cranks, pulleys, 310 turnbuckles, fairleads, rub strips, etc. for proper routing, condition, and security. Revised 273102 Elevator Trim Control and Indicator C 1 224, 240, Mar 31/00 - Check freedom of movement and 310 proper operation through full travel. Check pulleys, cables, sprockets, bearings, chains, and turnbuckles for condition and security. Check electric trim controls for operation as applicable. Check cables for tension, routing, fraying, corrosion, and turnbuckle safety. 273103 Elevator Trim Tab and Hinges - Check B 1, 3 224 condition, security, and operation. 5-10-01 Page 5 © Cessna Aircrafl Company Jul 3/2006