Specification & Description

FAA Federal Aviation Regulation Part 23 through amend- ment 23-6, including day, night, VFR and IFR. 1 . G E N E R A L D E S C R I P T I O N 1.2 Approximate Dimensions Overall Height ....................................................................................................................................... Overall Length ....................................................................................................................................... Wing Span (overall) ................................................................................................................................ Area ...................................................................................................................................... Cabin Height (max) ................................................................................................................................ 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 sq ft (16.2 sq m) 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 2012 4 36’ -0” 13’ -0” 28’ -3” 1 . G E N E R A L D E S C R I P T I O N ( C o n t i n u e d ) FIGURE I — STATIONAIR EXTERIOR DIMENSIONS 8’ -1” Max 9’ -3.5” December 2012 5 1 . G E N E R A L D E S C R I P T I O N ( C o n t i n u e d ) FIGURE II — STATIONAIR INTERIOR DIMENSIONS Cabin Height Dimensions Cabin Width Dimensions Firewall 24.00 Tiedown Rings (10 Standard) Firewall Face of Instrument Panel Code *Cabin ** Lower Window Line *29.00 **30.00 Rear Wall of Cabin Baggage Shelf 35.00 49.50 45.50 44.00 36.00 65.00 47.00 24.00 Forward Doorpost Bulkhead *14.00 *40.00 **43.50 42.00 21.00 *38.50 **44.00 *14.00 *34.00 **42.00 *35.50 **42.50 *37.50 **42.00 *36.00 **40.00 *28.50 **36.00 *28.50 **34.50 Cabin Floorplan Layout December 2012 6 1 . G E N E R A L D E S C R I P T I O N ( C o n t i n u e d ) 1.3 Design Weight 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 .................................................................................................................................... 3,617 lbs (1,641 kg) 3,600 lbs (1,633 kg) 3,600 lbs (1,633 kg) 2,336 lbs (1059 kg) 1,281 lbs (581 kg) 180 lbs (82 kg) 92 gal (348.2 L) 87 gal (329.3 L) 46 gal (174.1 L) 43.5 gal (164.6 L) 11qts (10.4 L) 12 qts (11.4 L) December 2012 7 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) ......................................................................................................... 2 . P E R F O R M A N C E All estimated performance data are based on airplane weights at 3,600 pounds; standard atmospheric conditions; lev- el, 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. 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 3 . P O W E R P L A N T & A C C E S S O R I E S • 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 2012 8 4 . S T A T I O N A I R E Q U I P M E N T L I S T 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 Trans- mitter • Emergency Locator Transmitter Remote Mounted Switch • Backup Attitude Gyro, Altimeter and Airspeed Indica- tor • 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 An tenna • 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 2012 9 5 . I N S T R U M E N T A T I O N FIGURE III — STATIONAIR INSTRUMENT 1. MASTER Switch (ALT and BAT) 2. STBY BATT Switch 3. STBY BATT Test Annunciator 4. AVIONICS Switch (BUS 1 and BUS 2) 5. Electrical Switches 6. GDU-1044B Primary Flight Display 7. Backup Attitude Gyro, Airspeed & Altimeter Indicator 8. GMA-1347 Audio Panel 9. Compass 10. GDU-1044B Multi-Function Display 11. ELT Remote Switch/Annunciator 12. Flight Hour Recorder (Hobbs Meter) 13. Cabin Air Control 14. Wing Flap Switch Lever And Position Indicator 15. Mixture Control 16. Propeller Control Knob 17. Throttle (With Friction Lock) 18. Go-Around Switch 19. ALT Static Air Valve Control 20. Electrical and Avionics Circuit Breakers 21. Magnetos/Start Switch, Key Operated 22. Dimming Panel 22 21 20 17 16 11 15 14 13 12 9 8 6 4 5 7 3 2 10 1 19 18 December 2012 10 6 . E L E C T R I C A L P O W E R • 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 . E N G I N E I N D I C A T I N G S Y S T E M ( E L E C T R O N I C ) • 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 . E N V I R O N M E N T A L • 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 can- nula for the pilot, and standard mask, A5 flowmeter, and oxymizer cannulas for each passenger position. • 6 place oxygen equipment bag 9 . E X T E R I O R • 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 1 0 . E X T E R I O R L I G H T S • 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 inte- grated Pulse Recognition Technology • Underwing Courtesy, LH and RH December 2012 11 1 1 . F L I G H T C O N T R O L S • 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 1 2 . F U E L S Y S T E M • 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 1 3 . I N T E R I O R • High Contrast Sport Interior Theme - Light Taupe and Black • Light Taupe Leather Seating Surface with Black Perforated (Embossed) Leather Inserts on Seat Cushion and Seat Back • Door Panel, Upper Sidewall Accent - Black Perfo- rated (Embossed) Leather • Door, Lower Sidewall, Kick Panel - Black Kydex • Vinyl Grip Flooring in Crew Area • Carpeting in Passenger Area • Passenger Cup Holders • Jepp Map Storage Console with Cup Holders • 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 December 2012 12 1 4 . I N T E R I O R L I G H T I N G • 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 1 5 . E X T E R I O R S T R I P I N G O P T I O N S • Distinctive exterior styling in a variety of colors is provided. 1 6 . T R A I N I N G • 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. December 2012 13 17.1 CESSNA’S LIMITED WARRANTY - SINGLE EN- GINE PISTON AIRCRAFT Cessna warrants the aircraft and all parts included there- in to be free from defects in material and workmanship under 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, avi- onics, batteries, propellers and governors are specifically excluded from this warranty. Paint and graphics warran- ties are addressed separately. Spare parts sold by Cessna, excluding engines, engine part accessories, avionics, batteries, propellers and gov- ernors are warranted for six (6) months after installation, except as hereafter noted. Cessna’s obligation under this warranty is limited to re- pairing or replacing, at its option, with exchange, over- hauled, or new parts, items found defective by Cessna’s examination which are returned at the owner’s expense within the applicable twenty-four (24) or six (6) month pe- riod to any Cessna Service Station. A new warranty period is not established for replace- ment parts. Replacement parts are warranted only for the remainder of the applicable twenty-four (24) or six (6) month original warranty period. The repair or replacement of defective parts under this warranty will be made without charge to the owner for parts and labor for removal, installation and/or actual re- pair, except 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, alteration; repairs not authorized by Cessna; normal maintenance services (cleaning, control rigging, brake and other mechanical adjustments, maintenance inspec- tions, etc.); replacement 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 corro- sion, wear and exposure. WITH THE EXCEPTION OF THE WARRANTY OF TI- TLE, TO THE EXTENT ALLOWED BY APPLICABLE LAW, THIS WARRANTY IS EXPRESSLY IN LIEU OF ANY OTHER WARRANTIES, EXPRESSED OR IM- PLIED IN FACT OR BY LAW, INCLUDING ANY IM- PLIED WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE. THE REM- EDIES OF REPAIR OR REPLACEMENT AS ABOVE SET FORTH ARE THE ONLY REMEDIES UNDER THIS WARRANTY. CESSNA DISCLAIMS ANY OBLIGATION OR LIABILITY WHETHER IN CONTRACT OR IN TORT (AND WHETHER FOR NEGLIGENCE, STRICT LIABIL- ITY, PRODUCT LIABILITY OR OTHERWISE), INCLUD- ING LOSS OF USE OF THE PRODUCT WARRANTED, LOSS OF TIME, INCONVENIENCE, COMMERCIAL LOSS OR ANY OTHER DIRECT, CONSEQUENTIAL, SPECIAL OR INCIDENTAL DAMAGES. THIS WAR- RANTY IS IN LIEU OF ANY OTHER OBLIGATION OR LIABILITY OF CESSNA OF ANY NATURE WHATSO- EVER BY REASON OF THE MANUFACTURE, SALE OR LEASE OF SUCH AIRCRAFT PRODUCTS AND CESSNA NEITHER ASSUMES NOR AUTHORIZES ANYONE TO ASSUME FOR IT ANY OTHER OBLIGA- TION OR LIABILITY IN CONNECTION WITH SUCH AIRCRAFT PRODUCTS. COMPLIANCE WITH THIS LIMITED WARRANTY MAY BE AFFECTED IF EX- PORT LICENSES ARE REQUIRED TO BE REQUEST- ED AND APPROVED BEFORE SPARE PARTS CAN BE SHIPPED TO CERTAIN FOREIGN COUNTRIES. 17.2 AIRCRAFT PAINT AND GRAPHICS– SINGLE EN- GINE PISTON AIRCRAFT Cessna endeavors to select and use high quality poly- urethane paints from the leading manufacturers. Poly- urethane paints and graphics are used because of their high gloss characteristics and ability to withstand dra- matic temperature and pressure changes. The paint on your new aircraft will maintain its high gloss characteris- tics 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 pre- cautions 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 water rinse and drying with a cloth or chamois. Do not use polish 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 1 7 . L I M I T E D W A R R A N T I E S December 2012 14 should be avoided to prevent damage to the paint sur- face. 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, ver- tical and horizontal 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 keep- ing surfaces clean, polished, and touching up chipped or eroded areas to prevent further damage and corrosion. Paint and graphics warranty applies only to defects in material 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 mainte- nance procedures have been followed and paint peeling, blistering or cracking is evident in areas other than im- mediate leading edge surfaces, 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 de- fects 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 several major surface areas of the aircraft. Contact your Cessna Field Service Engineer concerning paint defects on any major surface of an aircraft. 17.3 Textron Lycoming Warranty (Limited) New Re- ciprocating Aircraft 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 recip- rocating engine models sold by it to be free from defects in 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 exchange basis, of the engine or any part of the engine, when Textron Lycoming has determined that the engine is defective in material or workmanship. Such repair or replacement will be made by Textron Lycoming at no charge to you. Textron Lycoming will also bear the cost for labor in connection with the repair or replacement as provided in Textron Lycoming’s then current Removal and Installation Labor Allowance Guidebook. Any engine or part so repaired or replaced will be entitled to warranty for the remainder of the original warranty pe- riod. YOUR OBLIGATIONS The engine must have received normal use and service. You must apply for warranty with an authorized Textron Lycoming distributor within 30 days of the appearance of the defect in material or workmanship. Textron Lycoming’s warranty does not cover normal maintenance expenses or consumable items, the obliga- tions on the part of Textron Lycoming set forth above are your exclusive remedy and the exclusive liability of Tex- tron 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 war- ranty 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 di- rected in your operator’s manual, or if non-genuine Tex- tron 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 en- gines at any time without incurring any obligation to in- corporate such alterations in engines or parts previously sold. 1 7 . L I M I T E D W A R R A N T I E S ( C o n t i n u e d ) December 2012 15 THIS LIMITED WARRANTY IS EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES AND REPRE- SENTATIONS, EXPRESS OR IMPLIED OR STATU- TORY, WHETHER WRITTEN OR ORAL, INCLUDING BUT NOT LIMITED TO ANY WARRANTY OF MER- CHANTABILITY OR FITNESS FOR ANY PARTICULAR PURPOSE, AND ANY IMPLIED WARRANTY ARISING FROM ANY COURSE OF PERFORMANCE OR DEAL- ING OR TRADE USAGE. THIS WARRANTY IS ALSO IN LIEU OF ANY OTHER OBLIGATION, LIABILITY, RIGHT, OR CLAIM, WHETHER IN CONTRACT OR IN TORT, INCLUDING ANY RIGHT IN STRICT LIABIL- ITY IN TORT OR ANY RIGHT ARISING FROM NEG- LIGENCE ON THE PART OF TEXTRON LYCOMING, AND TEXTRON LYCOMING’S LIABILITY ON SUCH CLAIM SHALL IN NO CASE EXCEED THE PRICE AL- LOCABLE 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, CON- TRACT, OR ALLEGED NEGLIGENCE, SHALL TEX- TRON LYCOMING BE LIABLE FOR SPECIAL OR CONSEQUENTIAL OR ANY OTHER DAMAGES, IN- CLUDING 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 Lycom- ing’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 17.4 McCauley Propeller Systems Standard Limited Warranty McCauley Propeller Systems, a Division of Cessna Air- craft Company, Wichita, Kansas, U.S.A., expressly war- rants new and remanufactured products produced and sold by McCauley 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 until the expiration of the maximum hours of use or calendar limits for overhaul published by McCau- ley for the subject product, whichever occurs first. McCauley’s obligation under this limited warranty is lim- ited to repairing or replacing, at its sole option, any pro- peller, propeller parts, governor or governor parts deter- mined by McCauley to have been defective and which are properly returned by the owner, with a written state- ment describing the alleged defect, to any McCauley Au- thorized Service Center authorized to service the indi- vidual McCauley product. The repair or replacement of defective parts will be made without charge to the owner for parts, or labor for removal and installation, except ex- port/import duties, and/or sales or use taxes, if any which are solely the owner’s responsibility. McCauley will war- rant a part replaced pursuant to this limited warranty un- der 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 op- tion, any propeller, propeller parts, governor, or governor parts requiring replacement due to manufacturing defect if found at or before the first recommended overhaul in- terval as described in McCauley published service in- formation. This first overhaul coverage does not include labor, standard overhaul replacement parts, parts repair- able via published service information (re-plating, paint- ing, etc.), other costs associated with the propeller or governor overhaul, or export/import duties, and/or sales or use taxes, nor does it apply to defects found after Mc- Cauley 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, neg- ligence or accident or which have been repaired or al- tered in any way that, in the sole judgment of McCauley, adversely affects their performance, stability or reliabil- ity; to normal maintenance services (such as cleaning, 1 7 . L I M I T E D W A R R A N T I E S ( C o n t i n u e d ) December 2012 16 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, gover- nors or parts found defective beyond the McCauley rec- ommended 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 modifica- tion which is not approved by the engine manufacturer and that results in a change to the vibratory environment of the engine such as, but not limited to, an alteration of horsepower, operating RPM, crankshaft damper configu- ration, compression ratio, magneto timing, camshaft de- sign, or any other overhaul or modification not expressly approved by the original engine manufacturer. The Mc- Cauley limited warranty is also void on any McCauley product shipped new from the factory or distributor in dis- assembled state, then later re-assembled by an unau- thorized party. Parties authorized to re-assemble factory- new product must have specific written permission from McCauley to do so, otherwise all McCauley warranty on the affected unit is void. No McCauley warranty coverage is offered for leakage on product assembled outside Mc- Cauley, regardless of the assembling party. To the extent allowed by applicable law, THIS WAR- RANTY IS EXPRESSLY IN LIEU OF ANY OTHER WARRANTIES, EXPRESSED OR IMPLIED IN FACT OR BY LAW, INCLUDING ANY IMPLIED WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PAR- TICULAR PURPOSE. THE REMEDIES OF REPAIR OR REPLACEMENT SET FORTH HEREIN ARE THE ONLY REMEDIES UNDER THIS LIMITED WARRAN- TY. McCAULEY DISCLAIMS ANY OBLIGATION OR LIABILITY, WHETHER IN CONTRACT OR IN TORT , INCLUDING LOSS OF USE OF THE PRODUCT WAR- RANTED, LOSS OF TIME, INCONVENIENCE, LOSS OF PROFITS, COMMERCIAL LOSS, OR ANY OTHER DIRECT, CONSEQUENTIAL, SPECIAL, OR INCIDEN- TAL 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 McCAULEY NEITHER ASSUMES NOR AUTHO- RIZES ANYONE TO ASSUME FOR IT ANY OTHER OBLIGATION OR LIABILITY IN CONNECTION WITH SUCH WARRANTED PRODUCTS. THE UNITED NA- TIONS 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 Single Engine Air- craft Aircraft OEM-Installed Avionics 2-Year Limited War- ranty Policy This GARMIN Product is warranted to be free from de- fects in materials or workmanship for two years from the date of warranty activation. Within this period, GARMIN International, Inc. will at its sole option, repair or replace any components which fail in normal use. Such repairs or replacement will be made at no charge to the cus- tomer for parts or labor, 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 OTH- ER WARRANTIES EXPRESS OR IMPLIED OR STATU- TORY, INCLUDING ANY LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FIT- NESS FOR A PARTICULAR PURPOSE, STATUTO- RY OR OTHERWISE. THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM STATE TO STATE. IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR CONSEQUEN- TIAL DAMAGES, WHETHER RESULTING FROM THE USE, MISUSE 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 1 7 . L I M I T E D W A R R A N T I E S ( C o n t i n u e d ) December 2012 17 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 authorized Service Center. For assistance in locating a Service Center near you, call GARMIN Customer Ser- vice 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 1 7 . L I M I T E D W A R R A N T I E S ( C o n t i n u e d ) Cessna Single Engine Piston Aircraft, 2625 S. Hoover Rd, Wichita, Kansas 67215, Telefax 316-517-2772