Specification and Description

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 EXTERIOR LIGHTS: Ground Recognition - Vertical Tail, Reduced Drag Navigation, LH/RH Wing Tip & Tail Navigation Light Detectors, LH/RH Wing Tip Strobe, LH/RH Landing and Taxi, LH Wing Underwing Courtesy, LH/RH Pg 4 of 14 FLIGHT CONTROLS: Hydraulic Brakes, Toe-Operated Parking Brake Stainless Steel Control Cables Leather Wrap Control Wheels, All Purpose Pilot/Copilot Electrical Preselect - Flaps Dual Flight Control - Aileron/Elevator/Rudder Steerable Nose Wheel Aileron and Elevator Lock Elevator Trim Rudder Trim FLIGHT INSTRUMENTS: Airspeed, w/True Airspeed Attitude Gyro Dual Mode Altimeter (In/Mb), Sensitive 35,000 ft Turn Coordinator, w/Slip Skid Directional Gyro w/Heading Bug Vertical Speed Magnetic Compass Digital Clock, w/OAT/Volts/Flight Hours Pitot System - Heated Static System Alternate Static Source Dual Vacuum Pump System, Engine Driven Audible Stall Warning System - Heated FUEL SYSTEM: Electric Auxiliary Fuel Pump Engine Driven Fuel Pump Integral 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 INTERIOR: Black Cloth/ Mink Vinyl Seats Seat Belts & Shoulder Harness, Inertia Reel, All Seats Pilot and Copilot Seats • Adjustable Fore and Aft • Reclining Backs • Vertical Adjustment Rear Seat Bench w/Individual Reclining Back Kydex Upholstery w/Cloth Insert Cup Holders - Passengers Jepp Map Storage Console w/Cup Holders Approach Plate Holder, Pilot Control Wheel Armrests - Pilot & Copilot Doors/Passenger Side Panels Oxygen System • Oxygen Indicator - Overhead Console • Oxygen Ports w/Masks - Pilot/Copilot/Passengers • Oxygen Bottle - 50 Cu. Ft. Wall-to-Wall Carpet Pilot's Check List Pilot's Operating Handbook Fire Extinguisher, Hand Held Glareshield w/Lighting Control Wheel Lock Clothes Hanger Bar Metal Instrument Panel, w/Removable Subpanels Map/Glove Compartment Baggage Net Radio Call Plate Map & Storage Pockets Cabin Door Scuff Plates Sun Visors, Pilot & Copilot Tow Bar INTERIOR LIGHTING: Avionics Instruments Internally Lighted Avionics Radios Internally Lighted Engine Instruments Internally Lighted Flight Instruments Internally Lighted Glareshield Lighting Cabin Overhead Lights w/Dimming Control, Pilot/Copilot Cabin Overhead Lights, Passenger Interior Lights Dimming Control Map Light, Pilot Control Wheel Radio Call Plate Internally Lighted Compass Internally Lighted Pedestal Lighting POWER PLANT AND ACCESSORIES: Lycoming TIO-540-AK1A Engine 235 HP @2400 RPM Certified for 100LL & 100 Fuel Turbocharging System, Fully Automatic • Turbocharger, Absolute Pressure Controller • Exhaust Wastegate Valve, Overboost Valve • Turbocharged Exhaust w/heater Muff • Turbine Access Door Fuel Injection System Tubular Steel Engine Mount Dynafocal Rear Mount Automatic Alternate Engine Air Oil Cooler Rigid - Shock 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 w/De-ice Boots Propeller Governor Propeller Spinner, Polished Electric Starter Pg 5 of 14 MD41-24P Remote Relay Unit KX 165A Nav/Comm with Glideslope KI-208 VOR/LOC/GS Indicator Exchanged w/ standard KI-209A VOR/LOC/GS NAV Antenna Coupler CI-2480 VHF/GPS Antenna w/Internal Notch Filter KMD-540 Multi-Function Display KMD-540 Data Card SSD 120-30A-RS232 Blind Encoder Exchanged w/standard Blind Encoder KI-525 Pictorial Navigation Indicator HSI Exchanged w/ Standard Directional Gyro KG-102 Directional Gyro KMT-112 Magnetic Azimuth Transmitter (Flux Valve) KA-51 Slaving Accessory WX-500 Stormscope NY-163 Stormscope Antenna KDR 510 FIS Wiring Provisions KMH 880 TAS/EGPWS Provisions GTX-33 Transponder - Mode S w/TIS CI-105 Transponder Antenna GIA-63 NAV/COM/GPS w/GS #1 GIA-63 NAV/COM/GPS w/GS #2 CI-2480 VHF/GPS Antenna w/Internal Notch Filter #1 CI-2480 VHF/GPS Antenna w/Internal Notch Filter #2 CI-120 NAV Antenna GEU-1040 Primary Flight Display (PFD) GDU-1040 Multi-Function Display (MFD) GEA-71 Engine/Airframe Computer GRS-77 AHRS GDC-74 Air Data Computer GMU-44 Magnetometer KAP-140 Dual Axis Autopilot w/ Altitude Preselect KCM-100 Configuration Module KS-270C Pitch Axis Servo Actuator KS-271C Roll Axis Servo Actuator KS-272C Pitch Trim Servo Actuator Pilot Control Wheel - Pitch Trim Switch/AP Disconnect 3000-11 Emergency Locator Transmitter Remote Mounted Switch WX-500 Stormscope NY-163 Stormscope Pg 6 of 14 Optional Equipment Avionics NAV I: Standard Avionics Plus: KLN 94 GPS-IFR KLN-94 Data Cable KLN-94 Data Card - CSE GPS-NAV Selector/Annunciator KX 155A Nav/Comm With Glideslope KI 209 VOR/LOC/GS Indicator NAV Antenna Coupler CI-2480 VHF/GPS Antenna w/Internal Notch Filter KMD-540 Multi-Function Display KMD-540 Data Card KDR 510 FIS Wiring Provisions KMH 880 TAS/EGPWS Provisions SDD 120-30A-RS232 Blind Encoder Exchange w/standard Blind Encoder NAV II: Standard Avionics Plus: KLN 94 GPS-IFR KLN-94 Data Cable KLN-94 Data Card CSE Avionics Selector/Annunciator HSI/NAV/GPS NAV III: Not Available until 2nd Quarter 2004 Standard Avionics Plus: GMA-1347 Digital Audio Panel w/Marker Beacon/Intercom CI-102 Marker Beacon Antenna NAV III: Continued Control Wheel Push-ToTalk Switch - Pilot/Copilot Mic & Pone Jacks - Pilot/Copilot/Passengers Auxiliary Stereo Input Jack Avionics Cooling Fan #1 - Instrument Panel Avionics Cooling Fan #2 - PFD Avionics Cooling Fan #3 - MFD Avionics Cooling Fan #4 - Avionics Equipment Lighted Switch/Circuit Breaker (Pullable) Panel Blind Turn Coordinator for KAP-140 Roll Rate Data Backup Single Pump Vacuum System - Dry Standby Battery, 24 volt 8 AH Backup Attitude Gyro, Airspeed & Altimeter Indicator Standard Avionics Removed Standard Flight Instruments Removed Standard Digital Clock Removed Standard Engine Instruments Removed Standard Annunciator Panel Removed Standard Test/Day/Night Switch Removed Prop Heat Annunciator Removed Standard Glareshield Lighting Removed Standard Dual Vacuum System - Dry Removed Pg 7 of 14 Exterior Striping Options Interior 516D: Vendetta Red and Gray Painted Stripes; Commercial Maroon Painted Tail and Cowling; White Vinyl Skylane TC Logo; Medium Gray Vinyl Cessna Logo and Registration Number 516E: Khaki and Black Painted Stripes; Royal Blue Painted Tail and Cowling; White Vinyl Skylane TC Logo; Black Vinyl Cessna Logo and Registration Number Leather Seat Surfaces, Mink Leather With Perforated Mink Leather Insert / Mink Vinyl Fabric Seat Surfaces, Black Cloth / Mink Vinyl KMH 880: with NAV II only Traffic Awareness System (TAS) and Terrain-Enhanced Ground Proximity Warning System (EGPWS) KMH-820 MHAS Processor KMH-820 America Database KCM-805 Configuration Module KA-815 Antenna L-Band Antenna KAC-502 EGPWS Module KAC-504 Traffic Module RS-232 Interface Adapter Annunciator Lens Modification KDR 510: with NAV II only KDR-510 VDL Receiver (FIS) CI-248 FIS Antenna KAC-503 FIS Module KR-87 ADF: KR 87 ADF KI-227 ADF Indicator KA-44B ADF Antenna Air Conditioning Keith Products (STC) Pedal Extensions Rudder Pedal Extension (Pilot or Copilot) Pg 8 of 14 Speed, CAS Maximum at 20,000 ft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 176 kts Cruise, 88% power at 12,500 ft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 159 kts Cruise (Recommended lean mixture with fuel allowance for engine start, taxi, takeoff, climb and 45-minute reserve) 88% power at 12,500 ft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . range 615 nm (1,139 km) 87 gallons usable fuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . time 4.0 hr 45% power at 10,000 ft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . range 971 nm (1,798 km) 87 gallons usable fuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . time 8.9 hr Rate of Climb at Sea Level . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1,039 fpm (317 mpm) Certificated Maximum Operating Altitude . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20,000 ft (6,096 m) Takeoff Performance Ground roll . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 775 ft (236 m) Total distance over 50-ft obstacle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1,385 ft (422 m) Landing Performance Ground roll . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 590 ft (180 m) Total distance over 50-ft obstacle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1,350 ft (411 m) Stall Speed, CAS Flaps up, power off . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 54 kts Flaps down, power off . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 49 kts Wing Loading . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17.8 lbs/sq ft (86.9 kg/sq m) Power Loading . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13.2 lbs/hp (6.0 kg/hp) Engine: Textron Lycoming . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TIO-540-AK1A 235 BHP at 2,400 rpm Propeller: 3-bladed Constant Speed, Diameter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 79 in (2.01 m) Specifications subject to change without notice. Performance Conditions All estimated performance data are based on airplane weights at 3,100 pounds; standard atmospheric conditions; level, hard-surface, 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. Pg 9 of 14 CESSNA'S LIMITED WARRANTY (SINGLE ENGINE PISTON AIRCRAFT) Cessna warrants the aircraft and all parts included therein are free from defects in material and workmanship under normal use and service for a period of twenty-four (24) months after delivery to the original retail purchaser or first user, except as hereafter noted. Cessna's limited warranty also applies to aircraft paint; however, the warranty period for aircraft paint is twelve months after delivery of the aircraft to the original retail purchaser or first user. Engines, engine parts accessories, avionics, batteries and propellers, are specifically excluded from this warranty. Replacement spare parts sold by Cessna, excluding engines, engine part accessories, avionics, batteries and propellers are warranted for 6 months after installation or first use, except as hereafter noted. Cessna's obligation under this warranty is limited to repairing or replacing with new, overhauled or exchange parts, at its option, any part or parts found defective by its examination which are returned by the owner within the applicable twenty-four (24) or six (6) month period to any Cessna appointed or Cessna Contracted Distributor appointed Service Station. 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 repair, except that the owner shall pay all import duties, sales and use taxes on replacements. 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 inspections, etc.); replacement of service items (light bulbs, brake linings, filters, hoses, tires, cowl mounts, etc.); or to normal deterioration of soft trim and appearance items (paint, upholstery, rubber-like items, etc.) due to wear and exposure. TO THE EXTENT ALLOWED BY APPLICABLE LAW, THIS LIMITED WARRANTY IS EXPRESSLY IN LIEU OF AND CESSNA SPECIFICALLY DISCLAIMS AND EXCLUDES ANY AND ALL OTHER WARRANTIES, EXPRESSED 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 ARE THE ONLY REMEDIES UNDER THIS WARRANTY. CESSNA DISCLAIMS AND EXCLUDES ALL OTHER OBLIGATIONS AND LIABILITIES WHETHER IN CONTRACT OR IN TORT, INCLUDING LOSS OF USE, LOSS OF TIME, LOSS OF VALUE, INCONVENIENCE, COMMERCIAL LOSS OR ANY OTHER DIRECT, CONSEQUENTIAL, SPECIAL OR INCIDENTAL DAMAGES. Pg 10 of 14 Textron Lycoming Warranty (Limited) New Reciprocating 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 engine model new reciprocating engine 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. 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 period. 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 obligations on the part of Textron Lycoming set forth above are your exclusive 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 nongenuine 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, express or implied or statutory, whether written or oral, including but not limited to any warranty 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, including 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 that 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 Lycoming 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 Williamsport, Pennsylvania Original Engine Installation Only Effective 1996 Pg 11 of 14 McCauley Limited Warranty McCauley Propeller Systems (McCauley), Wichita, KS, U.S.A. expressly warrants each new propeller and governor 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 first user. McCauley's obligation under this limited warranty is limited to repairing or replacing, at its option, any propeller, governor, or parts therefore that are properly returned by the owner, with a written statement providing a description of the alleged defect, to McCauley at 5800 E. Pawnee Wichita, KS 67218, or to any McCauley-appointed Service Station authorized by such appointment to service the individual McCauley new propeller and governor, within a thirty-six (36) month period after delivery to the original retail purchaser or first user, transportation charges prepaid, which upon examination shall be determined to McCauley's sole satisfaction to have been defective. A new warranty period is not established for warranty replacements. Replacements are warranted for the remainder of the applicable warranty period. The repair or replacement of defective parts under this warranty will be made by McCauley or its authorized Service Stations without charge to the owner for parts, cost of part repair, or labor for removal or installation, except that export/import duties, and sales and/or use taxes, if any, on replacements are solely the owner's or first user's responsibility. The provisions of this limited warranty do not apply to incidents including, but not limited to, any McCauley new propellers and governors, and the parts therefore, which have been subject to misuse, negligence, or accident; which shall have been repaired or altered outside of McCauley's factory in any way so as in the sole judgment of McCauley to adversely affect their performance, stability, or reliability; to normal maintenance services (such as cleaning, 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 parts that have been improperly installed by entities other than McCauley and/or McCauley-appointed Service Stations; or to propellers, governors, and the parts therefore, which are not maintained, stored, or utilized as directed in the aircraft's pilot's operating handbook. Without McCauley's prior written approval, the new propeller limited warranty is void on any new propeller and/or governor installed on a non-type certificated engine, or on any engine that has received an overhaul or modification which is not approved by the engine manufacturer and which 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 configuration, compression ratio, magneto timing, camshaft design, or any other overhaul or modification not expressly approved by the original engine manufacturer. To the extent allowed by applicable law, THIS WARRANTY 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 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 (AND WHETHER FOR NEGLIGENCE, STRICT LIABILITY, PRODUCT LIABILITY OR OTHERWISE), INCLUDING LOSS OF USE OF THE PRODUCT WARRANTED, LOSS OF TIME, INCONVENIENCE, LOSS OF PROFITS, COMMERCIAL LOSS, OR ANY OTHER DIRECT, CONSEQUENTIAL, SPECIAL, OR INCIDENTAL DAMAGES. THIS WARRANTY IS IN LIEU OF ANY OBLIGATION OR LIABILITY ON THE PART OF McCAULEY TO ANYONE OF ANY NATURE WHATSOEVER BY REASON OF THE MANUFACTURE, SALE, LEASE, OR USE OF THE WARRANTED PRODUCTS AND McCAULEY NEITHER ASSUMES NOR AUTHORIZES ANYONE TO ASSUME FOR IT ANY OTHER OBLIGATION OR LIABILITY IN CONNECTION WITH 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. Pg 12 of 14 Bendix/King Equipment Retail Warranty Statement For Cessna Aircraft Company Single Engine Program A. General Aviation Avionics products manufactured by Honeywell under the brand name Bendix/King (collectively referred to herein as "Honeywell") are warranted against defects in design, material, or workmanship caused by Honeywell or its authorized agent(s) for the warranty period as defined in Paragraph (B) of this statement, which occur under normal and intended use and service, subject to all of the qualifications and conditions hereinafter stated. B. The warranty term for new product(s) installed on new aircraft shall be twenty-four (24) months from delivery to the original retail purchaser or first user. Cessna to provide warranty start date information. C. Any product Honeywell finds to be in violation of the warranty as set out in Paragraph (A) hereof, at the option of Honeywell, shall be repaired, replaced, or exchanged in accordance with the following procedures: 1. Products shall be returned to any authorized Honeywell Service Center or Honeywell Regional Product Support Repair/Overhaul Facility, with transport charges prepaid. 2. After correction, the products shall be returned to the purchaser with surface transportation charges prepaid. 3. The risk of loss or damage to all products in transit shall be borne by the party initiating the transportation of such products unless the purchaser makes a request for specific mode of transportation. In such case, the risk of loss and the cost of shipment shall be borne by the purchaser. All items repaired or replaced hereunder shall be warranted for the unexpired portion of the original warranty period. D. This warranty specifically excludes defects that Honeywell determines to be the result of any or all of the following: 1. Abuse, accident, or misuse; 2. Contamination, negligence, tampering, or improper storage or maintenance; 3. Repair or attempted repair by unauthorized persons or use of non-Honeywell or unauthorized repair or replacement parts; 4. Products not installed by an authorized Honeywell Installation Facility in accordance with the appropriate installation manual. E. The warranty as set out in Paragraph (A) is the only warranty for Honeywell products and is in lieu of all other warranties expressed or implied, including the implied warranties of merchantability and fitness for a particular purpose that are herewith expressly excluded and disclaimed. F. The remedies as set out in Paragraph (C) hereof state the entire liability of Honeywell and constitute the sole and exclusive remedy of the purchaser. Honeywell shall not be liable for any other claim, loss, or damage, including, but not limited to, incidental, consequential, or other kinds of damages whether based on contract, tort, negligence, or other theory of product liability. G. Honeywell reserves the right to make design changes, additions to, and improvements in its products without the obligation to install same in products previously manufactured. THIS IS A LIMITED WARRANTY Honeywell 23500 W. 105th Street Olathe, Kansas 66061 Pg 13 of 14 Garmin Avionics Installed in Caravan and Single 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 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 customer 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 OTHER WARRANTIES EXPRESS OR IMPLIED OR STATUTORY, INCLUDING ANY LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE, STATUTORY 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 CONSEQUENTIAL 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 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 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 Romsey, SO51 9AQ, U.K. Phone: 44-1794-519944 FAX: 44-1794-519222 Visit our web site at: www.garmin.com Pg 14 of 14 SPA03-T182TSPEC 9/03 1M Litho in U.S.A.