CESSNA STATIONAIR TC SPECIFICATION AND DESCRIPTION

FIGURE I — CESSNA STATIONAIR EXTERIOR DIMENSIONS ................................................................................................ FIGURE II — CESSNA STATIONAIR INTERIOR DIMENSIONS ................................................................................................ FIGURE III — CESSNA STATIONAIR INSTRUMENT PANEL .................................................................................................... TABLE OF CONTENTS 3 3 6 7 8 8 9 10 11 11 11 12 12 12 12 13 13 14 14 14 14 15 15 17 18 4 5 10 December 2015, Revision B3 CESSNA STATIONAIR TC 1. GENERAL DESCRIPTION All information herein applies to the Turbo Stationair (Model T206H). The Stationair is an all-metal, six-place, high-wing, fixed gear, single-engine piston aircraft de- signed for general utility purposes. 1.1 CERTIFICATION The Model 206H is certified to the requirements of U.S. FAA Federal Aviation Regulation Part 23 through amend- ment 23-6, including day, night, VFR and IFR. 1. GENERAL DESCRIPTION December 2015, Revision B 4 CESSNA STATIONAIR TC 36 ft 0 in 28 ft 3 in 9 ft 3.5 in FIGURE I — CESSNA STATIONAIR EXTERIOR DIMENSIONS 1. GENERAL DESCRIPTION (CONTINUED) 13 ft 0 in 8 ft 1 in December 2015, Revision B5 CESSNA STATIONAIR TC FIGURE II — CESSNA STATIONAIR INTERIOR DIMENSIONS 1. GENERAL DESCRIPTION (CONTINUED) Face of Instrument Panel Firewall Baggage Shelf Code *Cabin **Lower Window Line *35.50 **42.50 Rear Wall of Cabin 24.00 36.00 42.00 44.00 49.50 Firewall 24.00 47.00 35.00 65.00 Forward Doorpost Bulkhead Tiedown Rings (10 Standard) *38.50 **44.00 45.50 21.00 *34.00 **42.00 *14.00 *14.00 *40.00 **43.50 *37.50 **42.00 *36.00 **40.00 *28.50 **36.00 *28.50 **34.50 *29.00 **30.00 December 2015, Revision B 6 CESSNA STATIONAIR TC 1. GENERAL DESCRIPTION (CONTINUED) 1.2 APPROXIMATE DIMENSIONS Overall Height ........................................................................................................................................................................ Overall Length .......................................................................................................................................................................... WING Span (overall) ................................................................................................................................................................................. Area ................................................................................................................................................................................................. CABIN INTERIOR Height (maximum) ....................................................................................................................................................................... Width (trim to trim) ............................................................................................................................................................................ Length (firewall to aft baggage bulkhead) ............................................................................................................................. CABIN DOOR Height (front) ..................................................................................................................................................................................... Height (rear) ..................................................................................................................................................................................... Width (top) .................................................................................................................................................................................... Width (bottom) ................................................................................................................................................................................ BAGGAGE DOOR Height (front) .............................................................................................................................................................................. Height (rear) ................................................................................................................................................................................. Width (top) ........................................................................................................................................................................................ Width (bottom) ................................................................................................................................................................................. 9 ft 3.5 in (2.83 m) 28 ft 3 in (8.61 m) 36 ft (10.97 m) 174 ft2 (16.2 m2) 49.5 in (1.26 m) 44 in (1.12 m) 145 in (3.68 m) 41 in (1.04 m) 39 in (1.00 m) 32.5 in (0.83 m) 37 in (0.94 m) 39.25 in (1.00 m) 37.5 in (0.95 m) 43 in (1.09 m) 40 in (1.02 m) December 2015, Revision B7 CESSNA STATIONAIR TC 1.3 DESIGN WEIGHTS AND CAPACITIES Maximum Ramp Weight ......................................................................................................................................................... Maximum Takeoff Weight .................................................................................................................................................... Maximum Landing Weight .................................................................................................................................................. Standard Empty Weight ....................................................................................................................................................... Maximum Useful Load ............................................................................................................................................................... Baggage Allowance ...................................................................................................................................................................... FUEL CAPACITY Total Capacity .............................................................................................................................................................................. Total Useable ............................................................................................................................................................................... Total Capacity (each tank) ........................................................................................................................................................... Total Useable Capacity (each tank) ..................................................................................................................................... OIL CAPACITY Sump ................................................................................................................................................................................................... Total Capacity ................................................................................................................................................................................... 1. GENERAL DESCRIPTION (CONTINUED) NOTES 1. Standard empty weight based upon: a) 0.6-mil primer on all details, 0.6-mil primer on all exterior surfaces and 2.0-mil paint on all exterior surfaces. 2. Total oil capacity is with 8 qts. in sump and 1 qt. in oil filter. 3,617 lb (1,641 kg) 3,600 lb (1,633 kg) 3,600 lb (1,633 kg) 2,336 lb (1059 kg) 1,281 lb (581 kg) 180 lb (82 kg) 92 gal (348.2 L) 87 gal (329.3 L) 46 gal (174.1 L) 43.5 gal (164.6 L) 11 gts (10.4 L) 12 qts (11.4 L) December 2015, Revision B 8 CESSNA STATIONAIR TC Service Ceiling ........................................................................................................................................................................................ Takeoff Distance S.L. (Ground Roll) ......………………...................................................…..............................................................………….. Takeoff Distance S.L. (To Clear 50 ft. Obstacle) .................................................................................................................................. Maximum Climb Rate S.L. .................................................................................................................................................................... Maximum Speed S.L. ............................................................................................................................................................. Maximum Range and Endurance .......................................................................................................................................... Cruise Speed (75% pwr at 6,200 ft) .................................................................................................................................... Cruise Range and Endurance (75% pwr at 6,200 ft) ....................................................................................................... Landing Distance (Ground Roll) ................................................................................................................................................................ Landing Distance (To Clear 50 ft. Obstacle) ....................................................................................................................................... 27,000 ft 910 ft 1,740 ft 1,050 fpm 178 kts / 205 mph 703 nm / 6.3 hrs 164 kts / 189 mph 559 nm / 3.6 hrs 735 ft 1,395 ft All estimated performance data are based on airplane weights at 3,600 pounds; standard atmospheric conditions; level, hardsurface, dry runways; and no wind. They are calculated values derived from flight tests conducted by Cessna Aircraft Company under carefully documented conditions and will vary with individual airplanes, pilots, and numerous other factors affecting flight performance. 2. PERFORMANCE 3. POWERPLANT & ACCESSORIES • Lycoming TIO-540-AJ1A Engine • 310 HP @2500 RPM • Certified for 100LL & 100 Fuel • Turbocharging System (Fully Automatic) • Fuel Injection System • Tubular Steel Engine Mount • Bed Dynafocal Engine Mounting System • Engine Driven Vacuum Pump • Automatic Alternate Engine Air • Oil Cooler • Rigid - Mounted Cowling • Manual Cowl Flaps • Induction Air Filter • Full Flow Oil Filter • Throttle Control • Vernier Mixture Control • Vernier Propeller Control • Dual Ignition System, Shielded Magneto • Engine Exhaust Muffler • McCauley Constant Speed, 3 Blade Metal Propeller with De-ice Boots • Propeller Governor • Propeller Spinner, Polished • Electric Starter December 2015, Revision B9 CESSNA STATIONAIR TC 4. STATIONAIR EQUIPMENT LIST Avionics • GMA-1347 Digital Audio Panel with Marker Beacon/ Intercom • GTX-33 Transponder-Mode S w-TIS • GIA-63W NAV/COM/GPS/WAAS with GS #1 • GIA-63W NAV/COM/GPS/WAAS with GS #2 • GDU-1044B Primary Flight Display (PFD) • GDU-1044B Multi-Function Display (MFD) • GEA-71 Engine/Airframe Computer • GRS-77 Attitude & Heading Reference System (AHRS) • GDC-74A Air Data Computer with OAT Probe • GMU-44 Magnetometer • Garmin SafeTaxi & FliteCharts • GFC-700 Autopilot • Go-Around Switch • Electric Trim • A/P Disconnect • Control Wheel Steering Button • Electronic Checklists • ME406 Two Frequency Emergency Locator Transmitter • Emergency Locator Transmitter Remote Mounted Switch • Backup Attitude Gyro, Altimeter and Airspeed Indicator • Control Wheel Push-To-Talk Switch-Pilot/Copilot • Mic & Phone Jacks-Pilot/Copilot/Passengers • Auxiliary Stereo Input Jack • Antennas: • Marker Beacon Antenna • Transponder Antenna • VHF/GPS Antenna (2) • NAV Antenna • Emergency Locator Transmitter External Antenna • Pitot System - Heated • Static System • Hand Held Microphone • Alternate Static Source • Compass The following list of equipment is included on the standard aircraft and does not reflect optional equipment. December 2015, Revision B 10 CESSNA STATIONAIR TC FIGURE III — CESSNA STATIONAIR INSTRUMENT PANEL 5. INSTRUMENTATION December 2015, Revision B11 CESSNA STATIONAIR TC 6. ELECTRICAL POWER • Alternator, 28 Volt, 95 Amp • Battery, 24 Volt, 10.0 AH (1 hr rate), Manifold Type • Standby Battery, 24 volt, 6.2 AH (1 hr rate), Sealed Type • Standby Battery Controller • Electrical Circuit Panel • Alternator/Battery Master Switch • Split Avionics Master Switch • Circuit Breakers, Electrical • Switches, Electrical • Electrical J-Box • Alternator Control Unit • Battery Current Sensor • Ground Service Receptacle • Starter Relay • Alternator Relay • Battery Relay • Ground Power Relay • Bus Circuit Protection • Cabin Power Jack -12 Volt (fore & aft) • Propeller De-Ice Timer • Propeller Heat 7. ENGINE INDICATING SYSTEM • Ammeters • Voltmeters • Vacuum • Manifold Pressure • Oil Pressure and Temperature • Tachometer - Hour Recorder • Fuel Flow (GPH) • LH/RH Fuel Quantity • CHT - Cylinder Head Temperature • EGT - Exhaust Gas Temperature • TIT - Turbine Inlet Temperature • Standby Vacuum System • Annunciation – Caution and Warning Alerts (PFDD) 8. ENVIRONMENTAL • Windshield Defroster, Pilot • Ventilator, Adjustable (6 places) • Heating System, Shrouded Muffler with Firewall Valve • Insulation / Soundproofing • Carbon Monoxide Detection System • Precise Flight Oxygen System - Consists of a micro- phone mask and A5 flowmeter and oxymizer cannula for the pilot, and standard mask, A5 flowmeter, and oxymizer cannulas for each passenger position. • 6 place oxygen equipment bag December 2015, Revision B 12 CESSNA STATIONAIR TC 9. EXTERIOR • Epoxy Corrosion Proofing, All Structure • LH Door, Pilot with Hinged Window, Lock and Key • RH Cargo Door • Openable Window – RH (Copilot) • Rear Window • All Windows Tinted • Fixed Landing Gear • Main and Nose Gear Fairings • White Polyurethane Exterior Paint • Refueling Steps and Handles, Wing Struts and Fuselage • Fixed Cabin Entrance Steps • Tie Down Rings, LH/RH Wing & Tail • Tube Type Tires • Nose – 5.00 X 5 • Mains - 6.00 X 6 • Conical Camber Wing Tip • Strut Braced, Camber Lift Wings • Static Wicks 10. EXTERIOR LIGHTS • LED Ground Recognition Beacon - Vertical Tail • LED Navigation, LH/RH Wing Tip & Tail • Navigation Light Detectors, LH/RH • Wing Tip Strobe, LH/RH • Dual Wing LED Landing and Taxi Lights with integrat- ed Pulse Recognition Technology • Underwing Courtesy, LH and RH 11. FLIGHT CONTROLS • Hydraulic Brakes, Toe-Operated • Parking Brake • Stainless Steel Control Cables • Dual Flight Controls - Aileron/Elevator/Rudder • Leather Wrap Control Wheels, All Purpose Pilot/ Copilot • Pilot Control Wheel Switches • Pitch Trim • AP Disconnect • Control Wheel Steering Button • Go-Around Switch • Elevator Trim - Manual/Electric • Rudder Trim - Manual • Electrical Preselect - Flaps • Steerable Nose Wheel • Aileron and Elevator Control Lock 12. FUEL SYSTEM • Electric Auxiliary Fuel Pump • Engine Driven Fuel Pump • Integral Wet Wing Fuel Tanks, 87 Gal. Usable • Fuel Selector Valve, Left/Both/Right/Off • Fuel Strainer, Incorporated with Fuselage Quick Drain • Fuel Tank Quick Drain, 5 per wing • Fuel Sampler Cup • Fuel Vapor Return System December 2015, Revision B13 CESSNA STATIONAIR TC 13. INTERIOR • Warm Beige Luxor II Leather Seating Surface • Door Panel, Upper Sidewall Accent - Beige Woven Vinyl • Door, Lower Sidewall, Kick Panel - Black Kydex • Vinyl Grip Flooring in Crew Area • Carpeting in Passenger Area • Approach Plate Holder, Pilot Control Wheel • Armrests - Pilot & Copilot Doors/Passenger Side Panels • Amsafe Inflatable Seat Belts & Shoulder Harness STC, Inertia Reel, Pilot, Copilot, Passenger 3 & 4 Seats • Pilot and Copilot Seats • Adjustable Fore and Aft • Reclining Backs • Vertical Adjustment • Rear, Passenger 3 & 4 Seats (Removable) • Adjustable Fore and Aft • Reclining Backs • Rear, Passenger 5 & 6 Bench Seat (Removable) • Flat Folding • Pilot’s Check List • Pilot’s Operating Handbook • Fire Extinguisher, Hand Held • Instrument Panel Glareshield • Clothes Hanger Bar • Metal Instrument Panel, with Removable Stby Instr. Subpanel • Map/Glove Compartment • Baggage Net • Radio Call Plate • Map & Storage Pockets • Cabin Door Scuff Plates • Rosen Sun Visors, Pilot & Copilot • Tow Bar 14. INTERIOR LIGHTING • LED Pilot/Copilot Cabin Overhead LED Lights • LED Passenger Overhead Lights • Interior Lights Dimming Controls • Map Light, Pilot Control Wheel • Sub-Panel Lighting (LED Backlighted) • Flaps • Throttle • Mixture • Propeller • Environmental Controls (Air and Heat) • Switch Panel Lighting (LED Backlighted) • Avionics and Master Switches • Dimming Rheostats • Landing, Taxi and Nav Switches • Beacon, Strobe, Fuel Pump, Pitot Heat • 12 Volt Cabin Power • Standby Battery Switch • Circuit Breakers • Ignition / Start Switch • LCD Lighted Glass Panel Displays: • Electronic Flight Instruments • Electronic Avionics Instruments • Electronic Engine Instruments • Audio Panel Bezel (Backlighted) • Radio Call Plate (Backlighted) • Compass Internally Lighted • Backup Attitude, Altimeter, Airspeed Internally Lighted December 2015, Revision B 14 CESSNA STATIONAIR TC 17.1 CESSNA’S LIMITED WARRANTY - SIN- GLE ENGINE PISTON AIRCRAFT Seller warrants the aircraft and all parts included therein to be free from defects in material and workmanship un- der normal use and service for a period of twenty-four (24) months after the Warranty Start Date, except as hereafter noted. Engines, engine part accessories, avionics, batter- ies, propellers and governors are specifically excluded from this warranty. Paint and graphics warranties are addressed separately. Spare parts sold by Seller, excluding engines, engine part accessories, avionics, batteries, propellers and governors are warranted for six (6) months after installation, except as hereafter noted. Seller’s obligation under this warranty is limited to repair- ing or replacing, at its option, with exchange, overhauled, or new parts, items found defective by Seller’s examination which are returned at the owner’s expense within the appli- cable twenty-four (24) or six (6) month period to any Cessna Service Station. A new warranty period is not established for replacement parts. Replacement parts are warranted only for the remain- der of the applicable twenty-four (24) or six (6) month origi- nal warranty period. The repair or replacement of defective parts under this war- ranty will be made without charge to the owner for parts and labor for removal, installation and/or actual repair, ex- cept that the owner shall pay all import duties and sales and use taxes on replacements and repairs. This limited warranty does not apply to parts subjected to misuse, negligence, improper installation, accident, altera- tion; repairs not authorized by Seller; normal maintenance services (cleaning, control rigging, brake and other me- chanical adjustments, maintenance inspections, etc.); re- placement of service items (light bulbs, brake linings, filters, hoses, tires, cowl mounts, etc.); or to normal deterioration of soft trim or appearance items (paint, upholstery, rubber-like items, etc.) due to corrosion, wear and exposure. WITH THE EXCEPTION OF THE WARRANTY OF TITLE, TO THE EXTENT ALLOWED BY APPLICABLE LAW, THIS WARRANTY IS EXPRESSLY IN LIEU OF ANY OTHER WAR- RANTIES, EXPRESSED OR IMPLIED IN FACT OR BY LAW, INCLUDING ANY IMPLIED WARRANTY OF MERCHANT- ABILITY OR FITNESS FOR A PARTICULAR PURPOSE. THE REMEDIES OF REPAIR OR REPLACEMENT AS ABOVE SET FORTH ARE THE ONLY REMEDIES UNDER THIS WARRANTY. SELLER DISCLAIMS ANY OBLIGATION OR LIABILITY WHETHER IN CONTRACT OR IN TORT (AND WHETHER FOR NEGLIGENCE, STRICT LIABILITY, PROD- UCT LIABILITY OR OTHERWISE), INCLUDING LOSS OF USE OF THE PRODUCT WARRANTED, LOSS OF TIME, 17. LIMITED WARRANTIES 16. TRAINING Cessna will offer one G1000 training course at no additional charge and one G1000 ground school course for a second person at no additional charge, with purchase of a new aircraft. This offer is valid for 12 months after aircraft delivery. Distinctive exterior styling in a variety of colors is provided. 15. EXTERIOR December 2015, Revision B15 CESSNA STATIONAIR TC 17. LIMITED WARRANTIES (CONTINUED) INCONVENIENCE, COMMERCIAL LOSS OR ANY OTHER DIRECT, CONSEQUENTIAL, SPECIAL OR INCIDENTAL DAMAGES. THIS WARRANTY IS IN LIEU OF ANY OTHER OBLIGATION OR LIABILITY OF SELLER OF ANY NATURE WHATSOEVER BY REASON OF THE MANUFACTURE, SALE OR LEASE OF SUCH AIRCRAFT PRODUCTS AND SELLER NEITHER ASSUMES NOR AUTHORIZES ANYONE TO ASSUME FOR IT ANY OTHER OBLIGATION OR LIABIL- ITY IN CONNECTION WITH SUCH AIRCRAFT PRODUCTS. COMPLIANCE WITH THIS LIMITED WARRANTY MAY BE AFFECTED IF EXPORT LICENSES ARE REQUIRED TO BE REQUESTED AND APPROVED BEFORE SPARE PARTS CAN BE SHIPPED TO CERTAIN FOREIGN COUNTRIES. 17.2 AIRCRAFT PAINT AND GRAPHICS– SINGLE ENGINE PISTON AIRCRAFT Seller endeavors to select and use high quality polyure- thane paints from the leading manufacturers. Polyurethane paints and graphics are used because of their high gloss characteristics and ability to withstand dramatic tempera- ture and pressure changes. The paint on your new aircraft will maintain its high gloss characteristics for an extended period of time provided it is cared for properly. The painted exterior surfaces require an initial curing period which may be as long as ninety (90) days after the finish is applied. During this curing period, some precautions should be taken to avoid damaging the finish or interfering with the curing process. The finish should be cleaned only by washing with clean water and mild soap, followed by a wa- ter rinse and drying with a cloth or chamois. Do not use pol- ish or wax, which would exclude air from the surface, during this ninety (90) day curing period. Once the finish has cured completely, it may be waxed with a good automotive wax, but power buffing should be avoided to prevent damage to the paint surface. Normal paint maintenance will include but is not limited to; touchup of abrasion and wear of the paint on screws heads, around access panels, wing leading edges, vertical and hor- izontal stabilizer leading edges, windshield retainers and other leading edge surfaces including parts on the landing gear subject to damage or erosion from airborne particles. Proper maintenance includes keeping surfaces clean, pol- ished, and touching up chipped or eroded areas to prevent further damage and corrosion. Paint and graphics warranty applies only to defects in mate- rial and workmanship for a period of one (1) year from the Warranty Start Date. Deterioration of paint and graphics due to normal wear, exposure, or improper care is not covered by the warranty. If proper paint maintenance procedures have been followed and paint peeling, blistering or cracking is evident in areas other than immediate leading edge sur- faces, warranty consideration may be requested thorough a Cessna Service Station. Generally speaking, warranty repair of paint is confined to a limited surface area. Workmanship or material defects can usually be identified to localized surface areas that were improperly prepared prior to paint application, or to areas where the paint or subsurface primer has been improperly applied. Complete strip and repaint of an entire airplane can ONLY be authorized if there is evidence of paint defects on sev- eral major surface areas of the aircraft. Contact your Cessna Field Service Engineer concerning paint defects on any ma- jor surface of an aircraft. 17.3 TEXTRON LYCOMING WARRANTY (LIMITED) NEW RECIPROCATING AIR- CRAFT ENGINE What Textron Lycoming Promises You Engine Model Aircraft Model IO-360-L2A Cessna-172R, 172S IO-540-AB1A5 Cessna-182T IO-540-AC1A5 Cessna-206H TIO-540-AK1A Cessna-T182T TIO-540-AJ1A Cessna-T206H Textron Lycoming warrants the above listed new recipro- cating engine models sold by it to be free from defects in December 2015, Revision B 16 CESSNA STATIONAIR TC material and workmanship for a period of twenty-four (24) months after aircraft delivery to the original retail purchaser or first user. The date of first operation must not exceed two (2) years from the date of shipment from Textron Lycoming. Textron Lycoming’s obligation under this warranty shall be limited to its choice of repair or replacement, on an ex- change basis, of the engine or any part of the engine, when Textron Lycoming has determined that the engine is defec- tive in material or workmanship. Such repair or replacement will be made by Textron Lycoming at no charge to you. Tex- tron Lycoming will also bear the cost for labor in connec- tion with the repair or replacement as provided in Textron Lycoming’s then current Removal and Installation Labor Al- lowance Guidebook. Any engine or part so repaired or replaced will be entitled to warranty for the remainder of the original warranty period. YOUR OBLIGATIONS The engine must have received normal use and service. You must apply for warranty with an authorized Textron Ly- coming distributor within 30 days of the appearance of the defect in material or workmanship. Textron Lycoming’s warranty does not cover normal main- tenance expenses or consumable items, the obligations on the part of Textron Lycoming set forth above are your exclu- sive remedy and the exclusive liability of Textron Lycoming. This warranty allocates the risk of product failure between you and Textron Lycoming, as permitted by applicable law. Textron Lycoming reserves the right to deny any warranty claim if it reasonably determines that the engine or part has been subject to accident or used, adjusted, altered, handled, maintained, or stored other than as directed in your operator’s manual, or if non-genuine Textron Lycoming parts are installed in or on the engine and are determined to be a possible cause of the incident for which the warranty application is filed. Textron Lycoming may change the construction of engines at any time without incurring any obligation to incorporate such alterations in engines or parts previously sold. THIS LIMITED WARRANTY IS EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES AND REPRESENTATIONS, EX- PRESS OR IMPLIED OR STATUTORY, WHETHER WRITTEN OR ORAL, INCLUDING BUT NOT LIMITED TO ANY WAR- RANTY OF MERCHANTABILITY OR FITNESS FOR ANY PARTICULAR PURPOSE, AND ANY IMPLIED WARRANTY ARISING FROM ANY COURSE OF PERFORMANCE OR DEALING OR TRADE USAGE. THIS WARRANTY IS ALSO IN LIEU OF ANY OTHER OBLIGATION, LIABILITY, RIGHT, OR CLAIM, WHETHER IN CONTRACT OR IN TORT, IN- CLUDING ANY RIGHT IN STRICT LIABILITY IN TORT OR ANY RIGHT ARISING FROM NEGLIGENCE ON THE PART OF TEXTRON LYCOMING, AND TEXTRON LYCOMING’S LIABILITY ON SUCH CLAIM SHALL IN NO CASE EXCEED THE PRICE ALLOCABLE TO THE ENGINE OR PART WHICH GIVES RISE TO THE CLAIM. LIMITATION OF LIABILITY IN NO EVENT, WHETHER AS A RESULT OF A BREACH OF WARRANTY, CONTRACT, OR ALLEGED NEGLIGENCE, SHALL TEXTRON LYCOM- ING BE LIABLE FOR SPECIAL OR CONSEQUENTIAL OR ANY OTHER DAMAGES, INCLUDING BUT NOT LIMITED TO LOSS OF PROFITS OR REVENUES, LOSS OF USE OF THE ENGINE, OR COST OF A REPLACEMENT. No agreement varying this warranty or Textron Lycoming’s obligations under it will be binding upon Textron Lycoming unless in writing signed by a duly authorized representative of Textron Lycoming. Cessna Model Aircraft Only Textron Lycoming Engines 652 Oliver Street Williamsport, Pennsylvania 17701 (570) 323-6181 www.lycoming.textron.com Original Engine Installation Only Effective 2000 17. LIMITED WARRANTIES (CONTINUED) December 2015, Revision B17 CESSNA STATIONAIR TC 17.4 MCCAULEY PROPELLER SYSTEMS STANDARD LIMITED WARRANTY McCauley Propeller Systems, a Division of Cessna Aircraft Company, Wichita, Kansas, U.S.A., expressly warrants new and remanufactured products produced and sold by Mc- Cauley to be free from defects in material and workmanship under normal use and service for a period of thirty-six (36) months after delivery to the original retail purchaser or un- til the expiration of the maximum hours of use or calendar limits for overhaul published by McCauley for the subject product, whichever occurs first. McCauley’s obligation under this limited warranty is limited to repairing or replacing, at its sole option, any propeller, propeller parts, governor or governor parts determined by McCauley to have been defective and which are properly re- turned by the owner, with a written statement describing the alleged defect, to any McCauley Authorized Service Center authorized to service the individual McCauley product. The repair or replacement of defective parts will be made with- out charge to the owner for parts, or labor for removal and installation, except export/import duties, and/or sales or use taxes, if any which are solely the owner’s responsibility. Mc- Cauley will warrant a part replaced pursuant to this limited warranty under the same terms as the original part for the remainder of he applicable warranty period of the original part. This limited warranty is not intended to and does not cover the costs of normal maintenance of overhaul. In addition, McCauley will repair or replace, at its option, any propeller, propeller parts, governor, or governor parts requiring replacement due to manufacturing defect if found at or before the first recommended overhaul interval as described in McCauley published service information. This first overhaul coverage does not include labor, standard overhaul replacement parts, parts repairable via published service information (re-plating, painting, etc.), other costs as- sociated with the propeller or governor overhaul, or export/ import duties, and/or sales or use taxes, nor does it apply to defects found after McCauley published overhaul hour or calendar limits. The provisions of this limited warranty do not apply to: any McCauley parts which have been subject to misuse, negligence or accident or which have been re- paired or altered in any way that, in the sole judgment of McCauley, adversely affects their performance, stability or reliability; to normal maintenance services (such as clean- ing, mechanical adjustments and maintenance inspections); to the replacement of service items made in connection with normal maintenance; to normal deterioration of soft trim and appearance items (such as paint and rubber-like items) due to wear and exposure; to propellers, governors or parts found defective beyond the McCauley recommend- ed overhaul period; or to parts which have been improperly installed by entities other than McCauley and/or McCauley Authorized Service Centers. The McCauley limited warranty is void on any new or re- manufactured product installed, without McCauley’s prior written approval, on a non-type certificated engine, or on any engine which has received an overhaul or modification which is not approved by the engine manufacturer and that results in a change to the vibratory environment of the en- gine such as, but not limited to, an alteration of horsepower, operating RPM, crankshaft damper configuration, compres- sion ratio, magneto timing, camshaft design, or any other overhaul or modification not expressly approved by the original engine manufacturer. The McCauley limited war- ranty is also void on any McCauley product shipped new from the factory or distributor in disassembled state, then later re-assembled by an unauthorized party. Parties autho- rized to re-assemble factory-new product must have spe- cific written permission from McCauley to do so, otherwise all McCauley warranty on the affected unit is void. No Mc- Cauley warranty coverage is offered for leakage on product assembled outside McCauley, regardless of the assembling party. To the extent allowed by applicable law, THIS WARRANTY IS EXPRESSLY IN LIEU OF ANY OTHER WARRANTIES, EX- PRESSED OR IMPLIED IN FACT OR BY LAW, INCLUDING ANY IMPLIED WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE. THE REMEDIES OF REPAIR OR REPLACEMENT SET FORTH HEREIN ARE THE ONLY REMEDIES UNDER THIS LIMITED WARRANTY. McCAULEY DISCLAIMS ANY OBLIGATION OR LIABILITY, WHETHER IN CONTRACT OR IN TORT , INCLUDING LOSS OF USE OF THE PRODUCT WARRANTED, LOSS OF TIME, 17. LIMITED WARRANTIES (CONTINUED) December 2015, Revision B 18 CESSNA STATIONAIR TC INCONVENIENCE, LOSS OF PROFITS, COMMERCIAL LOSS, OR ANY OTHER DIRECT, CONSEQUENTIAL, SPE- CIAL, OR INCIDENTAL DAMAGES. THIS WARRANTY IS IN LIEU OF ANY OBLIGATION OR LIABILITY ON THE PART OF McCAULEY TO ANYONE OF ANY NATURE WHATSO- EVER BY REASON OF THE MANUFACTURE, SALE, LEASE, OR USE OF THE WARRANTED PRODUCTS AND McCAU- LEY NEITHER ASSUMES NOR AUTHORIZES ANYONE TO ASSUME FOR IT ANY OTHER OBLIGATION OR LIABILITY IN CONNECTION WITH SUCH WARRANTED PRODUCTS. THE UNITED NATIONS CONVENTION ON CONTRACTS FOR THE INTERNATIONAL SALE OF GOODS, 1980, AND ANY SUCCESSOR THERETO, IS EXPRESSLY EXCLUDED FROM THIS WARRANTY. Issued 9/1/2003 17.5 GARMIN AVIONICS INSTALLED IN SIN- GLE ENGINE AIRCRAFT Aircraft OEM-Installed Avionics 2-Year Limited Warranty Policy This GARMIN Product is warranted to be free from defects in materials or workmanship for two years from the date of warranty activation. Within this period, GARMIN Internation- al, Inc. will at its sole option, repair or replace any compo- nents which fail in normal use. Such repairs or replacement will be made at no charge to the customer for parts or la- bor, provided that the customer shall be responsible for any transportation cost. This warranty does not cover failures due to abuse, misuse, accident or unauthorized alteration or repairs. THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRAN- TIES EXPRESS OR IMPLIED OR STATUTORY, INCLUDING ANY LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE, STATUTORY OR OTHERWISE. THIS WARRAN- TY GIVES YOU SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM STATE TO STATE. IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY IN- CIDENTAL, SPECIAL, INDIRECT OR CONSEQUENTIAL DAMAGES, WHETHER RESULTING FROM THE USE, MIS- USE OR INABILITY TO USE THIS PRODUCT OR FROM DEFECTS IN THE PRODUCT. Some states do not allow the exclusion of incidental or consequential damages, so the above limitations may not apply to you. GARMIN retains the exclusive right to repair or replace the product or offer a full refund of the purchase price at its sole discretion. SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY. To obtain warranty service, contact your local GARMIN au- thorized Service Center. For assistance in locating a Service Center near you, call GARMIN Customer Service at one of the numbers shown below. GARMIN International 1200 East 151st Street Olathe, Kansas 66062, U.S.A. Toll free: 1-800-800-1020 Phone: 1-913-397-8200 FAX: 1-913-397-0836 GARMIN (Europe) Ltd. Unit 5, The Quadrangle Abbey Park Industrial Estate Romsey, SO51 9AQ, U.K. Phone: 44-1794-519944 FAX: 44-1794-519222 Visit our web site at: www.garmin.com 17. LIMITED WARRANTIES (CONTINUED) U.S. + 1.844.44.TXTAV | INTERNATIONAL +1.316.517.8270 | TXTAV.COM © 2015 Textron Aviation Inc. The names of aircraft manufactured by Textron Aviation Inc. (“TAI”) (or formerly by its subsidiaries Cessna Aircraft Company (“Cessna”) and Beechcraft Corporation (“Beechcraft”) including Hawker aircraft); some names for products or services of TAI, Cessna, Beechcraft or their subsidiaries, and logos are registered trademarks or registered service marks or trademarks or service marks of Textron Innovation Inc., used by permission, or Beechcraft whether or not appearing in large print, with trade marking symbols or otherwise denoting rights to or ownership of the same. Third party products names, marks, etc., whether or not appearing in large print or with trade marking symbols or otherwise denoting right or ownership of the same, belong to their respective owners. December 2015 SD- PIST-T206H-1215B