CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL

Compliance with the regulations is accomplished using one of three methods: (1) Traditional (Annual/100 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. 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. 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. C. D. E. Section 5-00-00, Time Limits/Maintenance Checks - General. This section provides a general overview of inspection requirements. Section 5-10-01, 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/100 Hour inspections. 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. 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. O Cessna Aircraft Company 5-00-00 Page 1 Jul 1/2007 ம் 5. CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL 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. B. C. 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. CONDITION is defined as inspection for (but not limited to) cleanliness, cracks, deformation, corrosion, wear, and loose or missing fasteners. (2) (3) SECURITY: Inspect for looseness of fasteners and fastener securing devices such as safety wire, cotter pins and self-locking nuts. During Inspections, use the following general guidelines: (1) (2) (3) (4) (5) (6) 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. 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. METAL PARTS: Inspect for security of attachment, cracks, metal distortion, and heat deterioration. 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. 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. 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 operating at their operational voltage. 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: 123 Standard Airworthiness Certificate (FAA Form 8100-2). Aircraft Registration Certificate (FAA Form 8050-3). Aircraft Radio Station License (Federal Communication Commission Form 556 if transmitter is installed). (b) To be carried in the airplane at all times: 1 - 23- Weight and Balance Data Sheets and associated papers (all copies of the Repair and Alteration Form, FAA Form 337, are applicable). Pilot's Operating Handbook and FAA Approved Airplane Flight Manual. Equipment List. (c) To be made available upon request: 1 Airplane, Engine and Propeller Logbooks. O Cessna Aircraft Company 5-00-00 Page 2 Jul 1/2007 1. Scope 2. CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL AIRWORTHINESS LIMITATIONS - FAA APPROVED DATA 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. Airworthiness Limitations A. There are no airworthiness limitations associated with this airplane. 5-00-10 O Cessna Aircraft Company Page 1 Dec 2/2002 CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL INSPECTION TIME INTERVALS General 1. A. 2. 3. 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: Procedure A. B. C. 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. A complete airplane inspection includes all inspection items as required by 14 CFR 43, Appendix D, Scope and Detail of annual/100-hour inspections. The chart provided in this section should be used to augment the inspection. 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. 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) (၁) (d) In the 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). 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. 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. 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) TASK - This column gives a short description of the inspection and/or servicing procedures. Where a more detailed description of the procedure is necessary, a reference will be made to another selection found in the maintenance manual or a specific reference to a supplier publication. If a task does not refer to a specific model and/or system, then the inspection and/or servicing procedure applies to all equivalent models and/or systems in the airplane. O Cessna Aircraft Company 5-10-00 Page 1 Mar 1/2009 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. OPERATION INTERVAL DETAILS INTERVAL A. 1, 2, 3, 4 Every 50 hours. BCD B. 1, 2, 3, 4 Every 100 hours. C. 1, 2, 3, 4 Every 200 hours. D. 5 E. F. 7 σ X G. H. 9 I. 10 J. 11 K. 12 Зг L. M. 14 Every 400 hours or 1 year, whichever occurs first. (Not used) Every 600 hours or 1 year, whichever occurs first. (Not used) Every 500 hours. Every 1000 hours. Every 2 years. 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. (Not used) 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. Every 2000 hours. Every 1000 hours or 1 year, whichever occurs first. NO PƠs > N. O. P. Q. R. S. T. 21 U. V. 567% 22222 15 16 17 Every 12 calendar months. 18 Every 6 years. 19 Every 12 years. 20 Every 3 years. 23 W. 24 X. 25 Every 1000 hours or 3 years, whichever occurs first. Every 1 year. Every 100 hours or every one year, whichever occurs first. Every 100 hours, every annual inspection, every overhaul, and any time fuel lines or clamps are serviced, removed or replaced. First 600 hours and as defined by the manufacturer thereafter. 5-10-00 © Cessna Aircraft Company Page 2 Mar 1/2009 1. Inspection Items CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL INSPECTION TIME LIMITS INTERVAL OPERATION ZONE 1, 2, 3, 4 All REVISION ITEM CODE TASK STATUS Added Apr 1/05 NUMBER 110000 Interior Placards, Exterior Placards, B Decals, Markings and Identification Plates Inspect for security of installation and legibility. Refer to Chapter 11, Placards and Markings - Inspection/Check. Deleted Apr 5/04 112101 Deleted 113101 Apr 5/04 212001 Revised Apr 1/05 212002 Ventilation System - Inspect clamps, D hoses, and valves for condition and security. Primary Flight Display (PFD) Fan and U Multi-Function Display (MFD) Fan, Deck Skin Fan, and Remote Avionics Cooling Fan Operational Check. Refer to Chapter 21, Avionics Cooling Maintenance Practices. - - LO 5 211 222 22 220, 225 214001 Cold and Hot Air Hoses Check B condition, routing, and security. 2,4 120 Revised Aug 3/98 214002 Heater Outlets Components, Inlets, and B Inspect all lines, ducts, clamps, seals, and gaskets for condition, restriction, and security. 1,3 211 Revised Mar 31/00 214003 Cabin Heat and Ventilation Controls Check freedom of movement through full travel. Check friction locks for proper operation. B 1, 3 211 221001 Autopilot Rigging - Refer to Autopilot - F Maintenance Practices. 7 610 Added Aug 3/98 221002 Autopilot Servo Capstan Assemblies. Check slip-clutch torque settings. 16 610 Refer to Autopilot Practices. - Maintenance Added Aug 3/98 221003 231001 Autopilot Servo Actuators. Inspect for evidence of corrosion and or buildup of dirt or other particulate matter which may interfere with servo operation. Refer to Autopilot Maintenance Practices. - Communication Antennas and Cables 16 610 3 210 - Inspect for security of attachment, connection, and condition. O Cessna Aircraft Company 5-10-01 Page 1 Jul 1/2010 CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL INTERVAL OPERATION ZONE C 1 211 1, 3 222, 223 A 1, 2, 3, 4 120 A 1, 2, 3, 4 120 REVISION ITEM CODE TASK STATUS NUMBER 235001 Added Apr 5/04 235002 Revised Jul 1/10 242001 Added Jul 1/10 242002 Revised Apr 1/05 Revised Apr 1/05 243001 243002 243003 243004 Microphones, Headsets, and Jacks Inspect for cleanliness, security, and evidence of damage. Microphone Push-To-Talk Switch B Clean the pilot's and copilot's microphone switches. Refer to Chapter 23, Communication Maintenance Practices. Alternator and Mounting Bracket Check condition and security. Check alternator belts for condition and proper adjustment. Check belt tension. Alternator Electrical Connections Check condition and security. Check for cracks on the shank of terminals connecting to alternator BAT and GND connection posts. Make sure the terminals are not bent or under mechanical stress caused by the routing of the attached wire. Make sure the field wire connector on 95 alternators is secure and firmly latched. Main Battery - Examine the general B condition and security. Complete a check of the level of electrolyte. Refer to Chapter 12-17-00. Main Battery Box and Cables - Clean B and remove any corrosion. Examine the cables for routing, support, and security of the connections. General Airplane and System Wiring C - Inspect for proper routing, chafing, broken or loose terminals, general condition, broken or inadequate clamps, and sharp bends in wiring. 2,4 120 2,4 120 1 210 External Power Receptacle and Power C Cables Inspect for condition and 2 120 security. Added Apr 1/05 243005 Standby Battery Complete the T 21 220 Standby Battery Capacity Test. Refer to Chapter 24, Standby Battery Maintenance Practices. 246001 Switch and Circuit Breaker Panel, C Terminal Blocks, and Junction Boxes Inspect wiring and terminals for condition and security. 1 222 Revised Sep 15/00 246002 Power Junction Box - Check operation B and condition. Check availability and condition of spare fuse (if applicable). O Cessna Aircraft Company 1,3 222 5-10-01 Page 2 Jul 1/2010 CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL INTERVAL OPERATION ZONE 11 222 T 21 224 REVISION ITEM CODE TASK NUMBER STATUS Added Jul 3/06 246003 Revised Apr 1/05 246101 Revised Jul 3/06 251001 251002 251101 Alternator Control Unit - Complete the J Over-voltage Protection Circuit Test. Refer to Chapter 24, Alternator Control Unit. Essential and Crossfeed Bus Diodes Check for proper operation. Complete the Essential and Crossfeed Bus Diode Inspection. Refer to Chapter 24, Essential and Crossfeed Bus Diodes - Maintenance Practices. Seats Examine the seats to make B 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. Seat Tracks and Stops - Inspect seat B tracks for condition and security of installation. Check seat track stops for damage and correct location. Inspect seat rails for cracks. 1,3 211 2,4 230 Restraint System, front and rear B Check belts for thinning, fraying, cutting, broken stitches, or ultra-violet deterioration. Check system hardware for security of installation. - 1, 3 211 Revised Mar 1/09 251102 252201 AMSAFE Aviation Inflatable Restraint T (AAIR) - Examine the restraint for dirt, frayed edges, unserviceable stitching, loose connections, and other wear. Refer to Chapter 25, Inflatable Restraint System - Maintenance Practices, and do the Inflatable Restraint System Inspection and the Inflatable Restraint System Adjustment/Test. Upholstery, Headliner, Trim, and Carpeting Check condition security. - and 21 211 D 5 211 5-10-01 O Cessna Aircraft Company Page 3 Jul 1/2010 CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL INTERVAL OPERATION ZONE 1,3 310 B 1,3 230 REVISION ITEM CODE TASK STATUS Revised Jan 2/06 Added Aug 3/98 Added Aug 3/98 NUMBER 256001 262001 262002 262003 Added Aug 3/98 262004 Revised Mar 31/00 271001 271002 Emergency Locator Transmitter 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. Portable Hand Fire Extinguisher Inspect for proper operating pressure, condition, security of installation, and servicing date. B R Cockpit Mounted Halon Type Fire P Extinguisher Weigh bottle. Bottle must be reserviced by qualified individual if more than 2 ounces is lost. Cockpit Mounted Halon Type Fire Extinguishers Perform hydrostatic test. The hydrostatic test shall be at twelve-year intervals based on initial servicing or date of last hydrostatic test. Cockpit Mounted Halon Type Fire Q Extinguishers Empty, inspect for damage, and recharge. Aileron Controls Check freedom B of movement and proper operation through full travel. Ailerons and Cables - Check operation C and security of stops. Check cables for 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. 17 211 19 211 18 211 1,3 120, 520, 620 3 120, 520, 620 271003 Aileron Structure, Control Rods, B Hinges, Balance Weights, Bell Cranks, Linkage, Bolts, Pulleys, and Pulley 1, 3 520, 620 - Brackets Check condition, operation, and security of attachment. 271004 Ailerons and Hinges - Check condition, B security, and operation 1,3 520, 620 271005 Control Wheel Lock Check general C 1 222 condition and operation. Revised Aug 3/98 271006 Control Linkage Inspect pulleys, C 1 222, 223 cables, bearings, and turnbuckles for condition and security. 272001 Rudder Check internal surfaces for C corrosion, condition of fasteners, and balance weight attachment. 3 340 O Cessna Aircraft Company 5-10-01 Page 4 Jul 1/2010 CESSNA AIRCRAFT COMPANY MODEL 206/T206 MAINTENANCE MANUAL NUMBER REVISION ITEM CODE TASK STATUS Revised Mar 31/00 272002 Rudder Inspect the rudder skins for 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. INTERVAL OPERATION ZONE B 1,3 340 Revised Aug 3/98 272003 Rudder, Tips, Hinges, Stops, Clips and Cable Attachment Check condition, security, and operation. B 1,3 340 - 272004 - 1 230 Added Aug 3/98 272005 Rudder Pedals and Linkage Check C for general condition, proper rigging, and operation. Check for security of attachment. Rudder Control Check freedom B of movement and proper operation through full travel. Check rudder stops for damage and security. 1, 3 340 Revised Aug 3/98 273001 Elevator Control Check freedom B of movement and proper operation through full travel. 1,3 222, 223 Revised 273002 Mar 31/00 Elevator Control System Inspect B pulleys, cables, sprockets, bearings, chains, and turnbuckles for condition, security, and operation. Check cables for tension, routing, fraying, corrosion, and turnbuckle safety. 1, 3 222, 223 Revised Aug 3/98 273003 Elevator, Hinges, Stops, and Cable B Attachment Check condition, security, and operation. 1,3 320, 330 Added Aug 3/98 273004 1,3 310 273101 Elevator Downspring - Check structure, B 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. Elevator Trim System - Check cables, B push-pull rods, bell cranks, pulleys, turnbuckles, fairleads, rub strips, etc. for proper routing, condition, and security. 1, 3 224, 240, 310 5-10-01 O Cessna Aircraft Company Page 5 Jul 1/2010